| HONEYWELL INTERNATIONAL INC. Patent applications |
| Patent application number | Title | Published |
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| 20120035866 | FLOW SENSOR WITH PRESSURE OUTPUT SIGNAL - This disclosure relates generally to flow sensors, and more particularly, to flow sensors that include a pressure related output signal. In one example, a flow sensor assembly may include a housing with an inlet flow port, an outlet flow port and a fluid channel extending therebetween, with a flow sensing element positioned in the housing and exposed to the fluid channel. A filter insert may be situated in the fluid channel, sometimes upstream of the flow sensor. When so configured, the flow sensor assembly may output a pressure or differential pressure based, at least in part, on a value of the flow rate through the fluid channel as sensed by the flow sensor. | 02-09-2012 |
| 20120035841 | AIRBORNE SEPARATION ASSURANCE SYSTEM AND REQUIRED TIME OF ARRIVAL FUNCTION COOPERATION - Methods and systems are provided for enhancing the functionality of an airborne separation assurance system (ASAS) by modifying it to cooperate with a required time of arrival (RTA) functionality. The system comprises an autopilot configured to execute a trajectory of an aircraft and a flight management system (FMS) in operable communication with the autopilot. The FMS includes a required time of arrival (RTA) system that is configured to determine an RTA aircraft trajectory of the aircraft based on a required time of arrival of the aircraft at a waypoint along the flight plan. The system also includes an airborne separation assurance system (ASAS) in operable communication with the RTA and is configured to determine a spacing trajectory based on a spacing interval from a first reference aircraft. | 02-09-2012 |
| 20120035789 | ENHANCED FLIGHT VISION SYSTEM FOR ENHANCING APPROACH RUNWAY SIGNATURES - Methods and apparatus are provided for visually enhancing approach runway signatures on en Enhanced Flight Vision System (EFVS). The EFVS may retrieve a location and an approach course for a runway, display, on the EFVS, a representation of the runway and the approach course for the runway relative to a position of the aircraft, define an area, along the approach course and before a first end of the runway, where the approach runway signature should be located, and visually enhance, on the EFVS, the defined area. | 02-09-2012 |
| 20120034882 | RECONFIGURABLE WIRELESS MODEM ADAPTER - A reconfigurable wireless modem adapter is provided. The reconfigurable wireless modem adapter includes a control board and a radio frequency switch. The control board has at least two interfaces for a respective at least two modems and is configured to communicatively couple to at least one onboard system in a vehicle. The control board activates a selected modem interfaced to one of the at least two interfaces. The radio frequency switch is communicatively coupled to the control board via the selected one of the at least one modem. The radio frequency switch communicatively couples an antenna to the selected modem. When the control board is communicatively coupled to the at least one onboard system and activates the selected modem, and when the radio frequency switch is communicatively coupled to the antenna, the antenna is communicatively coupled to the at least one onboard system via the selected modem. | 02-09-2012 |
| 20120034568 | COMBUSTION AIR CONTROL - Embodiments of the present disclosure include devices and methods for controlling combustion air. For example, in one embodiment, a method for controlling combustion air includes determining an amount of leaking air in a boiler, determining a constant that depends on a heating value of a fuel in the boiler, and adjusting an amount of controlled air supplied to the boiler. | 02-09-2012 |
| 20120034471 | THERMAL BARRIER SYSTEMS INCLUDING YTTRIUM GRADIENT LAYERS AND METHODS FOR THE FORMATION THEREOF - Embodiments of a thermal barrier system are provided, as are embodiments of a method for forming such a thermal barrier system over a gas turbine engine component. In one embodiment, the thermal barrier system includes a bond coat formed over a surface of a gas turbine engine component, and an yttrium-stabilized zirconia thermal barrier coating formed over the bond coat. The yttrium-stabilized zirconia thermal barrier coating includes an yttrium gradient layer having an yttrium content that increases with increasing distance from the bond coat. | 02-09-2012 |
| 20120033904 | HYDRODYNAMIC GAS FILM BEARING COOLING FLOW CONTROL SYSTEM - A hydrodynamic gas film bearing cooling gas control system includes a hydrodynamic gas film bearing, a supply conduit, and a flow control device. The supply conduit is in fluid communication with the hydrodynamic gas film bearing, is coupled to receive a flow of cooling gas from a cooling gas supply source, and is configured to supply the flow of cooling gas to the hydrodynamic gas film bearing. The flow control device is coupled to the supply conduit and is responsive to a physical characteristic of the cooling gas or ambient environment to move between at least two positions to thereby vary the flow of cooling gas, through the supply conduit, to the hydrodynamic gas film bearing. | 02-09-2012 |
| 20120033718 | RECONFIGURABLE WIRELESS MODEM ADAPTER INCLUDING DIVERSITY/MIMO MODEMS - A reconfigurable wireless modem adapter is provided. The reconfigurable wireless modem adapter includes a control board and a radio frequency switch. The control board includes at least two user-data interfaces for respective at least two modems, the modems including at least one diversity/multiple-input-multiple-output (MIMO) modem. The control board is configured to communicatively couple to at least one onboard system in a vehicle and to activate one of the at least one diversity/MIMO modem interfaced to one of the at least two user-data interfaces. The radio frequency switch is communicatively coupled to the control board via a modem-select interface and the selected one of the at least one diversity/MIMO modem. The radio frequency switch communicatively couples one of at least one diversity/MIMO antenna on the vehicle to the selected one of the at least one diversity/MIMO modem based on a control signal. | 02-09-2012 |
| 20120033225 | NEON OR IODINE ABSORPTION ENHANCED HENE RING LASER GYROSCOPE - One embodiment of a ring laser gyroscope discussed herein includes a cavity containing a gain medium having a first linewidth, a first plurality of reflective surfaces coupled to the cavity, and at least one medium exciter operable to excite the gain medium. The first plurality of reflective surfaces includes at least first, second, and third reflective surfaces. The first, second, and third reflective surfaces are positioned to reflect light along a path defined in the cavity between the plurality of reflective surfaces. The excited gain medium induces first and second laser fields within the cavity. A portion of the cavity contains an absorption medium having a second linewidth that is narrower than the first linewidth of the gain medium. The absorption medium reduces the gain of the first and second laser fields at a first range of frequencies. | 02-09-2012 |
| 20120033224 | INCREASING THE SCALE FACTOR OF GAS LASER BASED GYROSCOPES WITH AN EXTERNAL GAIN SATURATION BEAM - A ring laser gyroscope that includes a cavity containing a gain medium, a first plurality of reflective surfaces coupled to the cavity, a medium exciter operable to excite the gain medium, and a saturation beam source operable to emit a saturation beam. The first plurality of reflective surfaces includes a first reflective surface, a second reflective surface, and a third reflective surface. The first, second, and third reflective surfaces are positioned to reflect light along a path defined in the cavity between the plurality of reflective surfaces. The excited gain medium induces first and second laser fields within the cavity. The emitted saturation beam intersects with the first and second laser fields at a first interaction region of the cavity. The saturation beam interacts with the gain medium to reduce the gain of the first and second laser fields at a first range of frequencies. | 02-09-2012 |
| 20120033096 | MOTION BLUR MODELING FOR IMAGE FORMATION - The present disclosure includes motion blur modeling methods and systems for image formation. One motion blur modeling method for image formation includes obtaining image data utilized to form a particular image taken by a camera of a subject, obtaining velocity vector data for the subject at the time the image was taken, defining a convolution kernel for use formation of the particular image and based upon the velocity vector data, and applying the convolution kernel to the image data to produce a de-blurred set of image data utilized to form the particular image. | 02-09-2012 |
| 20120032818 | AVIONICS DISPLAY INTERFACE AND METHOD OF OPERATION - A method for operating a display unit such as an avionics display interface is provided. The method comprises displaying a plurality of logical categories of options available, with each of the logical categories including a plurality of items of information, selecting a first item of information in a first logical category when a first input key is pressed, and selecting a next item of information in the first logical category when the first input key is pressed again. The method further includes selecting a first item of information in a second logical category when a second input key is pressed, and selecting a next item of information in the second logical category when the second input key is pressed again. | 02-09-2012 |
| 20120032768 | LINEAR VARIABLE DIFFERENTIAL TRANSFORMERS - Linear variable differential transformers include a core comprising a non-ferromagnetic material and a ferromagnetic material, and a coil assembly including an axial bore within which the core is disposed and through which the core axially translates. | 02-09-2012 |
| 20120032674 | Current Sensor - This disclosure is directed to current sensing techniques for use within a magnetic current sensor. According to one aspect of the disclosure, a current sensing device includes a magnetic core, and a magnetic field sensor positioned substantially within a cavity formed by an air gap interface of the magnetic core and configured to sense a magnetic field induced by an electrical current that is conducted through a conductor passing through a central opening of the magnetic core. | 02-09-2012 |
| 20120032106 | REFRIGERANT COMPOSITIONS HAVING A SILOXANE SOLUBILIZING AGENT - Provided are refrigerant compositions which are blends of one or more hydrofluorocarbons, siloxanes, hydrocarbons and lubricants, as well as methods for using these compositions in applications such as the recharging of refrigeration systems and for replacing a chlorofluorocarbon or hydrochlorofluorocarbon in a refrigeration system. | 02-09-2012 |
| 20120032097 | Flame Detector Personality Module - A flame detector includes a sensor module, which carries a plurality of pyroelectric sensors, and a filter module which carries a plurality of replaceable filters with one filter being associated with each sensor. The modules are coupled together and carried in an exterior housing. A cover can overlay the filters to retain them in predetermined positions relative to the respective sensors. | 02-09-2012 |
| 20120032048 | ADJUSTABLE AND LOCKABLE BUSHING ASSEMBLY AND COMPONENT MOUNTING ASSEMBLY USING THE SAME - An adjustable and lockable bushing assembly includes a locking plate and a bushing. The locking plate has a bushing engagement opening that is defined by a plurality of first serrations, and a boss that extends axially therefrom. The bushing engages the locking plate and includes a concentric section, an eccentric section, a lock interface section, and an opening. The opening has a fixed diameter and extends along a longitudinal axis through the bushing. The concentric section has an outer surface that has a circumference that is concentric with the longitudinal axis. The eccentric section extends from the concentric section has an outer surface that has a circumference that is eccentric with the longitudinal axis. The lock interface section extends from the concentric section and includes an outer surface defined by a plurality of second serrations that engage the first serrations. | 02-09-2012 |
| 20120031520 | INSULATION ASSEMBLY FOR USE WITH AN AUXILIARY POWER UNIT HAVING AN EXHAUST MUFFLER - An insulation assembly for use with an APU having an exhaust muffler is disclosed herein. The insulation assembly includes, but is not limited to, a first insulating member that is configured for placement on a top portion of the exhaust muffler and a second insulating member attached to the first insulating member and configured for placement on a bottom portion of the exhaust muffler. The second insulating member is less resistant to heat transfer than the first insulating member. | 02-09-2012 |
| 20120031490 | QUANTUM DOT SOLAR CELLS AND METHODS FOR MANUFACTURING SUCH SOLAR CELLS - Solar cells, methods for manufacturing a quantum dot layer for a solar cell, and methods for manufacturing solar cells are disclosed. An illustrative method for manufacturing a solar cell may include dissolving a cadmium-containing compound in a first non-aqueous solvent to form a cadmium precursor solution, dissolving a selenium-containing compound in a second non-aqueous solvent to form a selenium precursor solution, combining the cadmium precursor solution with the selenium precursor solution to form a mixed solution, and exposing an electron conductor film to the mixed solution. Exposing the electron conductor film to the mixed solution may cause a cadmium and selenium quantum dot layer to be provided on the electron conductor film. This is just one example method. | 02-09-2012 |
| 20120030901 | AIR BURST TO CLEAR DETECTION WINDOW - An apparatus including a housing having at least one window, an air burst nozzle positioned atop the housing and aimed at the window, a compressed air source, an air control solenoid connected to the air burst nozzle, the compressed air source, and a support box. The compressed air source provides compressed air to the air control solenoid. A timer module directs a magnetic valve of the support box to supply power to the coil of the air control solenoid in order to engage the solenoid. When the air control solenoid is engaged, compressed air is provided to the air burst nozzle. The air burst nozzle directs a burst of air at the window of the housing to clear it of any particulates. In accordance with user programming of the timer module, the process is then repeated at regular intervals. | 02-09-2012 |
| 20120030519 | INTEGRATED DISSIMILAR HIGH INTEGRITY PROCESSING - A self-checking network is provided, comprising a first command processor configured to execute a performance function and a second command processor configured to execute the performance function, coupled to the first command processor. The self-checking network also comprises a first monitor processor configured to execute a monitor function that is coupled to the first command processor and a second monitor processor configured to execute the monitor function that is coupled to the second command processor. The first and second command processors compare outputs, the first and second monitor processors compare outputs, and the first monitor processor determines whether an output of the first command processor exceeds a first selected limit. | 02-02-2012 |
| 20120030501 | AUTOMATIC DETERMINATION OF SUCCESS OF USING A COMPUTERIZED DECISION SUPPORT SYSTEM - Methods and systems are provided for improving the repair efficacy of a repair action using inferred feedback. The method comprises downloading a repair procedure, which has a probability of success for correcting the fault code. Repair action data is input into to the computing device and is tracked and correlated with the downloaded procedure. The method then adjusts a probability of success of the repair procedure in clearing the fault code generated by the complex system based at least on the correlation. The system comprises a means for receiving repair data, a means for tracking repair action data taken, a means for correlating the tracked repair action and the repair data, and a means for updating a probability of success of the repair action based at least in part on the correlation of the repair data, the repair action data and the operating status of the complex system. | 02-02-2012 |
| 20120028587 | DUAL-FEED ANTENNA ARRAY WITH INTEGRAL COMPARISON CIRCUIT FOR PHASE AND AMPLITUDE CALIBRATION - A two-element array antenna system includes a first antenna element and a second antenna element. A transmitting, receiving, and processing (TRP) system is coupled to the first and second antenna elements via, respectively, a single first transmission element and a single second transmission element. The first and second transmission elements have respective transmit-path and receive-path functionality. The TRP system is configured to determine an amplitude offset and phase offset associated with the transmit-path functionality of the first and second transmission elements, and, based on data obtained during the determination of amplitude offset and phase offset associated with the transmit-path functionality of the first and second transmission elements, determine an amplitude offset and phase offset associated with the receive-path functionality of the first and second transmission elements. | 02-02-2012 |
| 20120027310 | SYSTEMS AND METHODS FOR PROCESSING EXTRACTED PLANE FEATURES - Systems and methods for processing extracted plane features are provided. In one embodiment, a method for processing extracted plane features includes: estimating an area of each plane of a plurality of planes extracted from data collected by an imaging sensor; generating a list of detected planes including the area of each plane; filtering the list of detected planes to produce a list of candidates for merger, filtering the list of detected planes discarding any plane not satisfying an actual points received criteria; applying a primary merge algorithm to the list of candidates for merger that iteratively produces a list of merged planes by testing hypothetical merged planes against a merging criteria, the hypothetical merged planes each comprising a plane from the list of merged planes and a plane from the list of candidates for merger; and outputting a final list of planes. | 02-02-2012 |
| 20120027022 | MULTIPLE SOURCE VIRTUAL LINK REVERSION IN SAFETY CRITICAL SWITCHED NETWORKS - In a system that uses a switched network and virtual links (for example, an AFDX, TT-ETHERNET, or TT-Gigabit ETHERNET switched ETHERNET network), the system is configured so that, for at least one virtual link, the end system that sources frames for that virtual link can change (for example, when an end system that was previously sourcing frames for that virtual link fails). The switches used in such a system are configured to be able to accept frames if there is such a change. | 02-02-2012 |
| 20120026872 | METHOD FOR MAINTAINING DATALINK NETWORK THROUGHPUT BY DELAYING LOWER PRIORITY MESSAGES - A method of maintaining datalink network throughput in a communications channel by delaying lower priority messages is provided. The method comprises receiving periodic channel occupancy data from a radio, and updating channel occupancy status from the channel occupancy data. A determination is then made whether the channel occupancy has reached a first predetermined occupancy threshold. If the first predetermined occupancy threshold has been reached, high priority messages are transmitted, and medium and low priority messages are stored. If the first predetermined occupancy threshold has not been reached, a determination is made whether the channel occupancy has reached a second predetermined occupancy threshold that is less than the first predetermined occupancy threshold. If the second predetermined occupancy threshold has been reached, high and medium priority messages are transmitted, and low priority messages are stored. If the second predetermined occupancy threshold has not been reached, messages of all priorities are transmitted. | 02-02-2012 |
| 20120026502 | VARIABLE PATH LENGTH CONTROL MODULATION FREQUENCY - A gyroscope system comprises a gyroscope block having a plurality of cavities and a plurality of passages that define a path; a plurality of mirrors each located in one of the plurality of cavities; at least one mirror drive coupled to one of the plurality of mirrors and configured to change a position of the respective mirror, wherein the path's length is changed by the change in the position of the respective mirror; a dither system coupled to the gyroscope block and configured to induce an angular rotation of the gyroscope block; and a controller configured to provide a dither signal indicative of a dither frequency to the dither system and a path length control (PLC) signal indicative of a PLC frequency to the at least one mirror drive. The controller is configured to calculate the PLC frequency as a function of the dither frequency. | 02-02-2012 |
| 20120026340 | SYSTEMS AND METHODS FOR PRESENTING VIDEO DATA - Described herein are systems and methods for presenting video data to a user. In overview, video data originates from a source, such as a capture device in the form of a camera. This video data is defined by a plurality of sequential frames, having a common geometric size. This size is referred to as the “geometric bounds of captured video data”. Analytics software is used to track objects in the captured video data, and provide position data indicative of the location of a tracked object relative to the geometric bounds of captured video data. Video data is presented to a user via a “view port”. By default, this view port is configured to display video data corresponding to geometric bounds of captured video data. That is, the view port displays the full scope of video data, as captured. Embodiments of the present invention use the position data to selectively adjust the view port to display a geometrically reduced portion of the geometric bounds of captured video data, thereby to assist the user in following a tracked object. | 02-02-2012 |
| 20120026190 | METHODS AND SYSTEMS FOR ATTITUDE DIFFERENTIATION IN ENHANCED VISION IMAGES - Methods and systems are provided for displaying information on a flight deck display onboard an aircraft. An exemplary method comprises obtaining image data for an imaging region and displaying, on the display device, a graphical representation of a first portion of the image data using a first visually distinguishable characteristic and a graphical representation of a second portion of the image data using a second visually distinguishable characteristic. The first portion corresponds to a portion of the image data above an attitude reference and the second portion corresponds to a portion of the image data below the attitude reference, and the first visually distinguishable characteristic and the second visually distinguishable characteristic are different. | 02-02-2012 |
| 20120025971 | METHOD AND APPARATUS FOR GENERATING LOCALIZED FIRE INCIDENT AND FIRE EXIT ROUTE MAP - A method and apparatus are provided for finding fires. The method includes providing a plurality of reference locations within a facility where each of the reference locations is associated with a readily identifiable feature of the facility, detecting a fire within the facility, receiving a fire location request from a monitoring location within the facility and dynamically generating a routing map from the monitoring location to a location of the fire and from the fire to a fire exit of the facility using at least some of the plurality of reference locations based upon the request. | 02-02-2012 |
| 20120025332 | SYSTEMS AND METHODS FOR MOUNTING INERTIAL SENSORS - Systems and methods for mounting inertial sensors on a board. On a wafer containing one or more sensor packages having a substrate layer, a sensor layer and an insulator layer located between the sensor layer and the substrate layer, a V-groove is anisotropically etched into one of the substrate layer. The substrate layer is in the 100 crystal plane orientation. The sensor package is then separated from the wafer. Then, a surface of the substrate layer formed by the etching is attached to a board. In one example, three sensor packages are mounted to the board so that their sense axis are perpendicular to each other. | 02-02-2012 |
| 20120025118 | BUTTERFLY VALVE PLATE SEALING ASSEMBLIES - A sealing assembly for use in a valve plate assembly includes a sealing ring and a retention spacer. The sealing ring has a radial ring section and an axial ring section, the axial ring section extends axially from the radial section and includes an outer diameter surface and a contact face, the contact face includes a contact surface and an annular slot, and the contact surface is located radially outward relative to the annular slot. The retention spacer is configured to be positioned adjacent the sealing ring | 02-02-2012 |
| 20120024043 | THERMAL CONDUCTIVITY DETECTORS - Thermal conductivity detectors and methods of operating thermal conductivity detectors are described herein. One or more device embodiments include a single fluidic channel, wherein the single fluidic channel includes a single inlet and a single outlet, and multiple sensors configured to determine one or more properties associated with a thermal conductivity of a fluid in the single fluidic channel. | 02-02-2012 |
| 20120023870 | METHODS OF FORMING INSULATED WIRES AND HERMETICALLY-SEALED PACKAGES FOR USE IN ELECTROMAGNETIC DEVICES - A method includes coating a conductive wire with a paste comprising a first inorganic dielectric material, an organic binder, and a solvent to form a coated wire, drying the coated wire at a first drying temperature to remove at least a portion of the solvent and form a green wire, winding the green wire around a core to form a green assembly, heat treating the green assembly at a decomposing temperature above the first temperature and below a melting point of the first inorganic dielectric material to decompose the organic binder to form an intermediate assembly, and exposing the intermediate assembly to a densifying temperature that is above the decomposing temperature and substantially equal to or above the melting point of the first inorganic dielectric material to densify the dielectric material on the conductive wire. | 02-02-2012 |
| 20120023428 | ENVIRONMENTAL SENSOR TOUCHSCREEN INTERFACE FOR PUBLIC AREAS - A HVAC device is provided. The device includes at least one environmental sensor, a control processor that compares data from the at least one environmental sensor with a reference value, the processor providing an output indicating the environmental data exceeds the reference value a communication interface coupled to the processor, the communication interface transfers the output of the control processor to a remotely located control panel and an interactive display coupled to the processor, the display depicting environmental data from the at least one environmental sensor for a predetermined time period after activation of the interactive display by a user and a blank screen thereafter. | 01-26-2012 |
| 20120022778 | SYSTEMS AND METHODS FOR SEARCHING AND DISPLAYING FLIGHT PLANS - An aircraft system is provided for an aircraft having a flight plan with a plurality of flight plan elements. The system includes a user interface configured to receive an input from a user corresponding to a selected flight plan element within the flight plan; a processor coupled to the user interface, the processor configured to receive the input from the user interface and generate first display signals and second display signals based on the input; a first display coupled to the processor and configured to display the selected flight plan element within a textual list based on the first display signals; and a second display coupled to the processor and configured to display the selected flight plan element within a navigation map based on the second display signals. | 01-26-2012 |
| 20120022701 | CONTROLLER INTERFACE WITH SEPARATE SCHEDULE REVIEW MODE - A controller equipped with a user interface having a separate schedule review mode, including methods of accessing and/or programming such devices, are disclosed. The controller may include a user interface that can be utilized to initiate a scheduling routine having a separate schedule review mode for displaying one or more schedule parameters of the controller without initiating the editing mode. An illustrative method of accessing a schedule on a controller coupled to a user interface may include the steps of initializing a scheduling routine within the controller, initiating a schedule review mode within the controller, displaying one or more schedule parameters for at least one period on the user interface, and exiting the scheduling routine. One or more of the schedule parameters can be modified, if desired, by initiating a separate editing mode within the controller. | 01-26-2012 |
| 20120022302 | INTEGRATED PROCESS FOR THE MANUFACTURE OF FLUORINATED OLEFINS - The instant invention relates, at least in part, to a method increasing the cost efficiency for dehydrohalogenation production of a fluorinated olefin by recovering and recycling spent dehydrohalogenation agent. In one aspect, the present invention relates to dehydrohalogenating a fluorinated alkane (e.g. pentafluoropropane and/or hexafluoropropane) in the presence of a dehydrohalogenating agent to produce a fluorinated olefin (e.g. tetrafluoropropenes and/or pentafluoropropenes). Removal of spent dehydrohalogenating agent from the reactor allows for facile separation of organic and dehydrohalogenating agent, the latter of which is recycled. | 01-26-2012 |
| 20120022300 | Methods for Making 3-Chloro-1,1,1,6,6,6-Hexafluoro-2,4-Hexadiene - Disclosed are compositions and systems having utility in numerous situations, including in particular solvent cleaning systems, as well as refrigerant lubricants and/or compatibilizing agents, and to methods which utilize such compositions and systems. More particularly, the present invention in preferred aspects is directed to solvents, blowing agents, heat transfer fluids and compatibilizing agents comprising the compound | 01-26-2012 |
| 20120020534 | EXPEDIENT ENCODING SYSTEM - An encoding system for an iris recognition system. In particular, it presents a robust encoding method of the iris textures to compress the iris pixel information into few bits that constitute the iris barcode to be stored or matched against database templates of same form. The iris encoding system is relied on to extract key bits of information under various conditions of capture, such as illumination, obscuration or eye illuminations variations. | 01-26-2012 |
| 20120017759 | ULTRASOUND-ASSISTED ELECTROSPRAY IONIC LIQUID FOR CARBON DIOXIDE CAPTURE - A system includes an ultrasound wave generator, a fluid cavity coupled to the ultrasound wave generator, an array of micro-machined ultrasonic-assisted electrospray nozzles coupled to the fluid cavity, an electrode configured to impart a charge onto the fluid output of the electrospray nozzles, and a carbon dioxide release unit configured to receive the ionic liquid after absorption of carbon dioxide by the ionic liquid and to remove carbon dioxide from the ionic liquid such that the regenerated ionic liquid can be recycled for additional carbon dioxide capture. | 01-26-2012 |
| 20120017596 | COMBUSTORS WITH QUENCH INSERTS - A combustor for a turbine engine is provided. The combustor includes a first liner having a first hot side and a first cold side; a second liner having a second hot side and a second cold side, the second hot side and the first hot side forming a combustion chamber therebetween, the combustion chamber configured to receive an air-fuel mixture for combustion therein; and an insert including a body portion extending through the first liner, a shoulder circumscribing the body portion and abutting the first hot side, and an inlet portion coupled to the body portion and abutting the first cold side such that the inlet portion and the shoulder capture the second liner therebetween to retain the insert. | 01-26-2012 |
| 20120017115 | APPARATUS AND METHOD FOR OPERATING A COMPUTING PLATFORM WITHOUT A BATTERY PACK - An application control engine computing platform having a shut-down mechanism that permits the platform to adequately start up and operate upon return of power after a power interruption, without a need of a battery pack. The mechanism may target the saving of control object runtime values and operational settings of those objects, rather than the saving of the complete set of objects, and all unsaved alarm and history records upon a power interruption. | 01-19-2012 |
| 20120016647 | SYSTEM AND METHOD FOR CONFIGURING A SIMULATION MODEL UTILIZING A TOOL FOR AUTOMATIC INPUT/OUTPUT ASSIGNMENT - A method and system for configuring a model of a process. A model of a process is provided, which follows a particular sequence. Such a model includes a plurality of component sub-models, wherein each component sub-model among the component sub-models includes one or more input variables and one or more output variables. Such a method and system also generally includes automatically assigning one or more output variables to one or more input variables based on information associated with the particular sequence of the process. | 01-19-2012 |
| 20120016539 | SYSTEMS AND METHODS OF ALTITUDE DETERMINATION - A system includes a memory device, and a processor coupled to the memory device. The processor is configured to receive, in a first time interval, from a first component a signal indicating an altitude of the aircraft, from a second component a signal indicating a first heading of the aircraft, and from a third component a signal indicating a first position of the aircraft. The processor is further configured to receive, in a second time interval later than the first time interval, and from the second and third components, signals respectively indicating a second heading and second position of the aircraft. The processor does not receive a signal from the first component in the second time interval. The processor is further configured to determine an estimated altitude of the aircraft and a geometric altitude of the aircraft. | 01-19-2012 |
| 20120016531 | METHOD AND SYSTEM FOR POWER QUALITY PROTECTION - A method for power quality protection includes measurement of electrical and nonelectrical parameters, calculation of additional electrical and nonelectrical parameters, comparison of the value of the calculated parameters with maximum allowed values from a power quality perspective, activation of protection mechanisms for transitioning to a safe mode or for isolation from the bus. The systems and methods may prevent equipment failures when out of the spec power quality is present in the distribution bus and may protect the distribution bus from imposing power quality problems due to equipment failures. Because most of the sensors in the systems of the present invention are already used for other control and protection purposes, there may be no reliability degradation. Most of the calculations and the control logic may be performed digitally for improved reliability and flexibility to modify algorithms. | 01-19-2012 |
| 20120015863 | CLEANING COMPOSITIONS AND METHODS - The invention provides solvent and cleaning compositions comprising an ionic surfactant, which preferably has a fluorinated portion thereof, and a solvent selected from hydrofluoro- and/or hydrochlorofluoro-olefins. Additionally, the invention provides drying, dry cleaning, and soil repellency compositions containing a hydrofluoro- or hydrochlorofluoro-olefin and said surfactant. Additionally, the invention provides drying compositions containing a hydrofluoro-olefin or hydrochlorofluoro-olefin and an alcohol such as methanol, ethanol or isopropanol. | 01-19-2012 |
| 20120014490 | REAL TIME DISTRIBUTED EMBEDDED OSCILLATOR OPERATING FREQUENCY MONITORING - A method for clock monitoring in a network is provided. The method comprises receiving a first network clock signal at a network device and comparing the first network clock signal to a local clock signal from a primary oscillator coupled to the network device. | 01-19-2012 |
| 20120013744 | METHOD AND APPARATUS FOR ACTIVATING AND DEACTIVATING VIDEO CAMERAS IN A SECURITY SYSTEM - A method used a security system monitoring a secure area. The method includes a first processor of the security system providing a status of the security system including an active status output and a disarmed status output signal, a video system monitoring the secured area by capturing and locally saving images, a second processor of the video monitoring system activating one or more video cameras of the video monitoring system monitoring an interior space of the secured area upon receipt of the active status output signal and deactivating the video cameras upon receipt of a disarmed status output signal. | 01-19-2012 |
| 20120013653 | SMART DISPLAY PIXEL - Construction of a pixel-based display using a set of pixel assemblies poured or placed into a display area or volume. Each pixel assembly has a means to produce a visible display output at its position and identify its own position within a 2-D or 3-D display space continuously or when needed. One or more image signals are distributed to the pixel assemblies collectively. Each pixel assembly uses its own self-detected position and other criteria to autonomously decide to which part of the signal(s) it will respond and what value to display as an output. Optionally each pixel assembly may also be able to: decode pixel identity encoded in the input signal(s) to implement a stroke/random access display; communicate with adjacent display elements in order to engage in collective action in local regions of the display; detect faults and remove itself from the display; and reprogram itself using an external signal. | 01-19-2012 |
| 20120013278 | RESISTORLESS DYNAMIC MOTOR BRAKING SYSTEM AND METHOD - Systems and methods are provided for regenerative motor braking. The regenerative braking systems and methods allow the braking torque of a multi-phase motor to be controlled while keeping currents to acceptable levels and without supplying electrical energy back to the voltage source. The regenerative braking systems and methods dissipate energy in the motor windings instead of sending this energy to the voltage source by intelligently switching the low-side switches in the inverter between the ON and OFF states at the commutation frequency while maintaining the high-side switches in the inverter in the OFF state. | 01-19-2012 |
| 20120012957 | NEUTRON DETECTOR WITH WAFER-TO-WAFER BONDING - A method of manufacturing a neutron detector comprises forming a first wafer by at least forming an oxide layer on a substrate, forming an active semiconductor layer on the oxide layer, and forming an interconnect layer on the active semiconductor layer, forming at least one electrically conductive pathway extending from the interconnect layer through the active semiconductor layer and the oxide layer, forming a circuit transfer bond between the interconnect layer and a second wafer, removing the substrate of the first wafer after forming the circuit transfer bond, depositing a bond pad on the oxide layer after removing the substrate of the first wafer, wherein the bond pad is electrically connected to the electrically conductive pathway, depositing a barrier layer on the oxide layer after removing the substrate of the first wafer, and depositing a neutron conversion layer on the barrier layer after depositing the barrier layer. | 01-19-2012 |
| 20120012662 | BUILDING CONTROLLERS WITH LOCAL AND GLOBAL PARAMETERS - A building controller is configured to designate one or more stored parameters as local or global. Parameters that are designated as global may be selectively communicated to remote devices and, parameters that are designated as local, may remain local to the building controller. In some instances, the remote devices may be selectable by a user, include all the other devices on the network, and/or include devices that share a common wireless accessory (e.g. an outdoor temperature sensor). | 01-19-2012 |
| 20120012591 | Systems For Efficient Heating And/Or Cooling And Having Low Climate Change Impact - A heat transfer system and method for controlling heat transfer to and from a container having thermal insulation disposed with respect to said container or compartment so as to inhibit the flow of heat into and/or out of the compartment, said insulation comprising a polymeric material having closed cells therein wherein said cells are formed from and/or contain a haloalkene according to Formula IA: | 01-19-2012 |
| 20120011863 | METHODS OF SERVICING MOBILE AIR CONDITIONING SYSTEMS - The present invention relates to methods and systems for introducing one or more hydrohalocarbon refrigerants into a heat transfer system from a vessel by recovering the one or more hydrohalocarbon refrigerants from the heat transfer system; monitoring the vapor pressure in the vessel and if the vapor pressure in the vessel becomes greater than 3 psi over the expected saturation pressure for the one or more hydrohalocarbon refrigerants then releasing vapor from the vessel; and returning said one or more hydrohalocarbon refrigerants to the heat transfer system by drawing liquid refrigerant from the vessel. | 01-19-2012 |
| 20120011636 | WATER RESISTANT AND CHEMICAL RESISTANT GLOVE - A flexible, form-fitting glove having improved water and chemical permeation resistance and a method of manufacture. The glove is multi-layered and formed utilizing a standard dip line. | 01-19-2012 |
| 20120011403 | METHODS SYSTEMS AND APPARATUS FOR DETERMINING WHETHER BUILT-IN-TEST FAULT CODES ARE INDICATIVE OF AN ACTUAL FAULT CONDITION OR A FALSE ALARM - Methods and apparatus are provided for determining whether a built-in-test fault code (BITFC) data sequence generated by a built-in-test (BIT) of a particular module of a complex system is indicative of an actual fault condition. A regression function is generated for the particular module based on stored BITFC data sequences generated by the BIT and stored repair data for that module from a fault history database. Later, during operation of the particular module, the BIT generates a new BITFC data sequence. A processor can then load the new BITFC data sequence and execute the regression function with respect to the new BITFC data sequence to determine whether the new BITFC data sequence is indicative of an actual fault condition at the particular module or is indicative of a false fault condition at the particular module. | 01-12-2012 |
| 20120010887 | SPEECH RECOGNITION AND VOICE TRAINING DATA STORAGE AND ACCESS METHODS AND APPARATUS - Embodiments include a speech recognition system and a personal speech profile data (PSPD) storage device that is physically distinct from the speech recognition system. In the speech recognition system, a PSPD interface receives voice training data, which is associated with an individual, from the PSPD storage device. A speech input module produces a digital speech signal derived from an utterance made by a system user. A speech processing module accesses voice training data stored on the PSPD storage device through the PSPD interface, and executes a speech processing algorithm that analyzes the digital speech signal using the voice training data, in order to identify one or more recognized terms from the digital speech signal. A command processing module initiates execution of various applications based on the recognized terms. Embodiments may be implemented in various types of host systems, including an aircraft cockpit-based system. | 01-12-2012 |
| 20120010841 | SYSTEM AND METHOD FOR ADJUSTING AN ON-LINE APPEARANCE SENSOR SYSTEM - A system, apparatus and method are provided for adjusting an on-line appearance sensor system (OnLASS) for color and other appearance characteristic(s) of a web product produced during a production run of a web production system. The OnLASS is calibrated and its setting(s) are sent to a color error minimizer (CEM). The OnLASS measures a first appearance characteristic of the web product during the production run and the on-line measurement is sent to the CEM. After the production run, a second appearance characteristic of the web product is measured with an off-line appearance sensor system (OffLASS) and the off-line measurement is sent to the CEM. The CEM compares the on-line and off-line appearance measurements and adjusts at least one setting based on the comparison. The adjusted setting(s) are sent to the OnLASS. | 01-12-2012 |
| 20120010765 | SYSTEM FOR DISPLAYING A PROCEDURE TO AN AIRCRAFT OPERATOR DURING A FLIGHT OF AN AIRCRAFT - A system is disclosed for displaying a procedure to an aircraft operator during a flight of an aircraft. The system includes, but is not limited to, a display unit, a data storage unit that is configured to store the procedure, an input unit, and a processor that is communicatively connected to the display unit, to the data storage unit and to the input unit. The processor is configured to obtain the procedure from the data storage unit, to receive an input from the input unit, and to control the display unit to display the procedure as a vertical profile having a compressed portion and an expanded portion, the expanded portion corresponding to the input. | 01-12-2012 |
| 20120010732 | CONFIGURABLE AUTOMOTIVE CONTROLLER - An engine control unit having a one-time integration of a model predictive control template via a potentially long software process. Changes to the control structure may subsequently be made via a calibration dataset connected to the engine control unit without incurring the potentially long and laborious software process of implementing the template of other approaches in the related art. | 01-12-2012 |
| 20120009490 | POWER GENERATOR SHUT-OFF VALVE - A power generator comprises a hydrogen producing fuel, multiple fuel cells arranged in a ring, and a rotatable ring valve. Each fuel cell has a proton exchange membrane and an opening separating the hydrogen producing fuel from ambient. The rotatable ring valve has multiple openings corresponding to the openings of the fuels cells such that ambient water is controllably prevented from entering the fuel cell by rotation of the ring valve. | 01-12-2012 |
| 20120008041 | CCTV CAMERA HOUSING - A camera housing incorporates a glass window, as an optical port, to improve image quality. The window can be curved or flat. The housing can be dome shaped and can also include metal or plastic along with the glass window. A camera installed in the housing has a field of view that intersects the window. The clear glass window enhances image quality when tilting or zooming the camera. A panning mechanism rotates the camera and housing together | 01-12-2012 |
| 20120007736 | System and Method of Determining Gas Detector Information and Status via RFID Tags - In large systems of ambient condition detectors the respective detectors can each include an RFID-type tag or integrated circuit. The tag can transmit detector identification information and status information wirelessly to a displaced receiver. Receivers can be installed in docking/test stations as well as in portable units which can be carried by an individual entering, or, moving through a region being monitored by the detectors | 01-12-2012 |
| 20120007590 | SYSTEMS AND METHODS FOR PERFORMING VIBRATION ANALYSIS USING A VARIABLE-RELUCTANCE SENSOR - A balanced bridge variable-reluctance sensor with no internal circuit components, springs, or dielectric for performing vibration analysis in high-vibration, high-temperature, and other extreme environments. The present invention includes a variable-reluctance sensor in a vibration-sensing capacity. The present invention has inherently high reliability due to its simplicity. The sensor is solidly mounted to a structure that is being monitored and allows a vibration wave to pass through a floating sensor bridge. The sensor vibrates at the same frequency as the application being measured. | 01-12-2012 |
| 20120007584 | FIBER CURRENT SENSOR WITH REDUCED TEMPERATURE SENSITIVITY - A sensor head assembly is provided, comprising a quarter wave device having shape-induced-birefringence and a sensing coil coupled to the quarter wave device and operable to wind around a current conductor. The quarter wave device converts linearly polarized light from a polarization maintaining fiber to circularly polarized light. | 01-12-2012 |
| 20120007360 | STARTING METHOD FOR BRUSHLESS WOUND FIELD STARTER-GENERATOR WITHOUT ROTATING DIODE RECTIFIER - A starting system may comprise a wound-field electric machine with a main generator and an exciter generator. The main generator and the exciter generator may each have stator windings and rotor windings. A shorting switch may be provided for interconnecting the stator windings of the exciter generator together when power is applied to stator windings of the main generator. This may result in starting torque being produced by the exciter generator, which starting torque may be additive to starting torque produced by the main generator. | 01-12-2012 |
| 20120006593 | ELECTROMAGNETIC INTERFERENCE (EMI) DIVERTER - An external EMI diverting structure to electrically shield an electronic device from EMI is presented. The electronic device is physically isolated from the case ground which interrupts the EMI or lightning fault path. This shield provides a return path to ground for the EMI away from the electronic device and replaces conventional EMI filter capacitors, which are not connected to case ground. The external EMI diverter comprises a first conducting enclosure enclosing the electrical circuit and is electrically coupled to the electric circuit and a second conducting enclosure enclosing the first conducting enclosure and being electrically isolated from the first conducting enclosure and the electric circuit. The diverter is physically and electrically connected to the case ground at an attachment point. | 01-12-2012 |
| 20120006524 | OPTIMIZED TUBE BUNDLE CONFIGURATION FOR CONTROLLING A HEAT EXCHANGER WALL TEMPERATURE - A heat exchanger comprises: a first medium inlet operable to receive a first medium into the heat exchanger; a first medium outlet operable to expel the first medium from the heat exchanger; a second medium inlet operable to receive a second medium into the heat exchanger; a second medium outlet operable to expel the second medium from the heat exchanger; and a plurality of parallel tubes running from the second medium inlet to the second medium outlet operable to carry the second medium from the second medium inlet to the second medium outlet, the plurality of tubes including: a first section of a first plurality of tubes, at least one of the first plurality of tubes having a first diameter, situated so that the first medium first flows from the first medium inlet over exterior walls of the first plurality of tubes and through gaps between the first plurality of tubes; and a second section of a second plurality of tubes, at least one of the second plurality of tubes having a second diameter that is different than the first diameter, situated so that after the first medium flows past the first section of the first plurality of tubes the first medium then flows over exterior walls of the second plurality of tubes and through gaps between the second plurality of tubes to the first medium outlet. | 01-12-2012 |
| 20120005208 | SYSTEM FOR INFORMATION DISCOVERY IN VIDEO-BASED DATA - A system for information discovery of items, such as individuals or objects, from video-based tracks. The system may compute similarities of characteristics of the items and present the results in a matrix form. A similarity portrayal may have nodes representing the items with edges between the nodes. The edges may have weights in the form of vectors indicating similarities of the characteristics between the nodes situated at the ends of the edges. The edges may be augmented with temporal and spatial properties from the tracks which cover the items. These properties may play a part in a multi-objective presentation of information about the items in terms of a negative or supportive basis. The presentation may be partitioned into clusters which may lead to a merger of items or tracks. The system may pave a way for higher-level information discovery such as video-based social networks. | 01-05-2012 |
| 20120004743 | APPARATUS AND METHOD FOR OPTIMIZING MAINTENANCE AND OTHER OPERATIONS OF FIELD DEVICES IN A PROCESS CONTROL SYSTEM USING USER-DEFINED DEVICE CONFIGURATIONS - A method includes receiving a request to access a field device and identifying a first device configuration associated with the field device. The first device configuration identifies (i) a subset of device parameters associated with the field device, (ii) a subset of device methods associated with the field device, and/or (iii) an interface arrangement of device parameters or methods associated with the field device. The method also includes retrieving a value for each device parameter identified by the first device configuration and generating a graphical user interface using the first device configuration and the retrieved values. The method could also include determining whether a user has requested use of the first device configuration. If not, the method can include identifying a second device configuration associated with the field device, retrieving the value for each device parameter identified by the second device configuration, and generating a second graphical user interface. | 01-05-2012 |
| 20120004299 | AZEOTROPE-LIKE COMPOSITIONS OF CIS-1,1,1,4,4,4-HEXAFLUORO-2-BUTENE - This invention relates to azeotrope-like compositions, methods and systems having utility in numerous applications, and in particular, uses for azeotrope-like compositions comprising effective amounts of the compound cis-1,1,1,4,4,4-hexafluoro-2-butene (Z-HFO-1336mzzm), which has the following structure: | 01-05-2012 |
| 20120003730 | PORTABLE SAMPLE ANALYZER CARTRIDGE - A sample analyzer cartridge for use at a point of care of a patient such as in a doctor's office, in the home, or elsewhere in the field. By providing a removable and/or disposable cartridge with all of the needed reagents and/or fluids, the sample analyzer can be reliably used outside of the laboratory environment, with little or no specialized training. | 01-05-2012 |
| 20120003595 | HIGH TURN DOWN LOW NOX BURNER - An air-fuel burner includes a heat-transfer tube, an air-fuel mixing chamber, and an air-fuel nozzle. The air-fuel nozzle is coupled to the air-fuel chamber to communicate a combustible air-fuel mixture into a combustion chamber defined between the air-fuel nozzle and the heat-transfer tube. The combustible air-fuel mixture, when ignited, establishes a flame in the combustion chamber to produce heat which is transferred through heat-transfer tube to an adjacent medium external to the heat-transfer tube. | 01-05-2012 |
| 20120003138 | AZEOTROPE-LIKE COMPOSITION OF PF5 AND HF - Provided are azeotropic and azeotrope-like compositions of PF | 01-05-2012 |
| 20120003137 | EXTRACTIVE DISTILLATION OF AsF5 AND PF5 USING HF - Arsenic can be an impurity in phosphorous pentafluoride production processes. It is desirable to remove arsenic from phosphorous pentafluoride prior to using of the phosphorous pentafluoride in the production of lithium hexafluorophosphate. The present technology provides methods of removing arsenic from phosphorous pentafluoride by extractive distillation. | 01-05-2012 |
| 20120003086 | TURBINE NOZZLES AND METHODS OF MANUFACTURING THE SAME - A turbine nozzle is provided and includes a first ring having a first microstructure, a vane extending from the first ring, a first porous zone between the first ring and the vane that is more porous than the first microstructure to attenuate thermo-mechanical fatigue cracking between the vane and the first ring. Methods of manufacturing the turbine nozzle are also provided. | 01-05-2012 |
| 20120003084 | FLOW DISCOURAGING SYSTEMS AND GAS TURBINE ENGINES - A flow discouraging system includes a stator assembly, a rotor assembly, and a plurality of fingers. The stator assembly includes one or more stationary components forming a side wall, the side wall including an annular groove defined by an outer axially-extending surface, an inner axially-extending surface, and a radial surface extending between the outer and inner axially-extending surfaces. The rotor assembly is disposed adjacent to and spaced apart from the stator assembly to form a portion of a cavity and includes an annular rim extending at least partially into the annular groove. The plurality of fingers is disposed in the annular groove and extends from the one or more stationary components the annular rim. | 01-05-2012 |
| 20120001355 | VARIABLE-ORIFICE PRILL PLATE - Prill heads having prilling assemblies that include adjustable openings. Prilling methods using the prilling assemblies can allow for the size of the openings to be varied during processing to alter the size of the prills as desired, or for clogged openings to be cleared, while maintaining operation of the prilling process. The prilling assemblies and prilling methods can be used to produce fertilizer products, including fertilizers comprising ammonium sulfate nitrate. | 01-05-2012 |
| 20120000271 | ENHANCED CAVITY FOR A PHOTOACOUSTIC GAS SENSOR - Photoacoustic cells for gas sensors are described. In some instances, the photoacoustic cell may be configured to provide an increased internal path length of the light beam in the photoacoustic cell relative to, for example, a conventional cylindrical photoacoustic cell. The photoacoustic cell may be shaped to provide increased internal reflection of the light within the photoacoustic cell, thereby increasing the absorption of the light by a gas to be detected in the photoacoustic cell. One example photoacoustic cell that can provide such increased internal reflection may be a generally conical-shaped. | 01-05-2012 |
| 20110320086 | METHODS AND APPARATUS FOR GENERATING AND ACCESSING INFORMATION IN BINARY FILES - An embodiment of a method for generating a binary file includes receiving information defining an entity that forms a portion of loadable diagnostics information, generating metadata defining a location within a binary file where the entity is to be located, and generating the binary file to include the metadata and the entity stored at the location. Additional embodiments include an aircraft diagnostic system and a method for the diagnostics system to access information within a binary file. The diagnostics system includes data storage and an accessor module. The data storage is configured to store the binary file, which includes metadata and an entity stored at a location within the binary file, where the metadata defines the location of the entity. The accessor module is configured to evaluate the metadata to make a determination of the location, and to access the entity within the binary file based on the determination. | 12-29-2011 |
| 20110320070 | SYSTEMS AND METHODS FOR ADJUSTING TARGET APPROACH SPEED - Systems and methods for adjusting target approach speed for use in a “Too Fast” approach to landing condition. An exemplary system stores predefined maximum wind setting and a predefined reference speed and a pilot set bug speed value. A processing device sets a target speed equal to the bug speed, if the bug speed is less than the reference speed plus a value associated with a predefined maximum wind setting, and sets the target speed equal to the reference speed plus the max wind added value, if the manual bug speed is not less than the reference speed plus the max wind added value. An output device outputs an alert if the received aircraft speed is greater than the set target speed plus a predefined error value when the received aircraft location is within a threshold value of a touchdown point. | 12-29-2011 |
| 20110319674 | PROCESS FOR THE MANUFACTURE OF FLUORINATED OLEFINS - Provided are methods for producing fluorinated organic compounds, which preferably comprises converting at least one compound of formula (I) CH | 12-29-2011 |
| 20110318162 | GAS TURBINE ENGINE ROTOR TIP CLEARANCE AND SHAFT DYNAMICS SYSTEM AND METHOD - A gas turbine engine rotor tip clearance and shaft dynamics system and method are provided. The system includes a gas turbine engine that is disposed within an engine case and includes a rotor. A rotor bearing assembly disposed within the engine case rotationally mounts the gas turbine engine rotor. Vibration isolators mounted on the engine case are coupled to the rotor bearing assembly, and are configured to provide linear and independently tunable stiffness and damping. A method includes determining the location of a gas turbine engine rotor rotational axis, disposing the gas turbine engine rotor in an engine case at the rotational axis location, mounting a plurality of vibration isolators that include a plurality of adjustment devices on the engine case, coupling each vibration isolator to the gas turbine engine rotor, and locking the gas turbine engine rotor at the rotational axis location using the plurality of adjustment devices. | 12-29-2011 |
| 20110317739 | SENSOR TEMPERATURE SENSING DEVICE - The present disclosure includes sensing device embodiments. One sensing device includes a heater layer, a resistance detector layer, constructed and arranged to indicate a temperature value based upon a correlation to a detected resistance value, an electrode layer, and a sensing layer. | 12-29-2011 |
| 20110317165 | BEAM INTENSITY DETECTION IN A CAVITY RING DOWN SENSOR - A cavity ring down gas sensor is disclosed. In one illustrative embodiment, the cavity ring down gas sensor includes an electromagnetic radiation source (e.g. laser) configured to emit an input beam of light having a wavelength corresponding to an absorption line of a gas to be detected. The input beam of light may be coupled into an optical cavity to amplify an internal beam of light that is reflected about the optical cavity. An optical element may be disposed in the optical cavity at an angled close to, but not at, the Brewster's angle to reflect a relatively small portion of the internal beam of light in the optical cavity to a detector for determining the intensity of the internal beam of light in the optical cavity. When a specified light intensity is reached in the optical cavity, the input beam of light may be shut off or otherwise prevented from entering the optical cavity, and a cavity ring down time decay may be measured. The cavity ring down time decay may be related to the gas concentration of a gas to be detected in the optical cavity. | 12-29-2011 |
| 20110317164 | MULTIPLE WAVELENGTH CAVITY RING DOWN GAS SENSOR - An illustrative cavity ring down gas sensor includes an optical cavity for receiving a gas to be detected and at least two electromagnetic radiation sources. The first electromagnetic radiation source may emit a first beam of light having a wavelength corresponding to an absorption wavelength of the gas to be detected, and the second electromagnetic radiation source may emit a second beam of light having a second wavelength that is off of an absorption wavelength of the gas to be detected. The first beam of light may detect a cavity ring down time decay, which is related to the concentration of the gas to be detected. The second beam of light may be used to detect a baseline cavity ring down time decay, which may be used to help increase the accuracy of the sensor by, for example, helping to compensate the concentration of the gas detected by the first beam of light for sensor variations caused by, for example, sensor age, temperature or pressure changes, and/or other conditions. | 12-29-2011 |
| 20110316857 | CROSSING TRAFFIC DEPICTION IN AN ITP DISPLAY - Provided are methods and systems for the disambiguation of an in trail procedure (ITP) vertical display by calculating and rendering symbology on a plan view traffic collision avoidance system (TCAS) display. The symbology represents an intersection point between the ground track of an ITP aircraft and the ground track of a blocking aircraft and further represents an association between the intersection point and the respective ITP blocking aircraft. | 12-29-2011 |
| 20110316688 | ALARM MANAGEMENT SYSTEM HAVING AN ESCALATION STRATEGY - An alarm management system having an escalation strategy which may be applied to each state of an alarm and increase a level of escalation if a required action has not been taken in response to an alarm. This approach is for avoiding an overlooking of any alarms and for assuring closure of alarms as soon as possible. An alarm may be in one of several intermediate states. Each state may have a threshold which if exceeded escalates an alarm's urgency. Alarm notifications may be provided to recipients according to their preferences. | 12-29-2011 |
| 20110316129 | MULTILAYER STRUCTURES FOR MAGNETIC SHIELDING - A magnetic shield is presented. The shield may be used to protect a microelectronic device from stray magnetic fields. The shield includes at least two layers. A first layer includes a magnetic material that may be used to block DC magnetic fields. A second layer includes a conductive material that may be used to block AC magnetic fields. Depending on the type of material that the first and second layers include, a third layer may be inserted in between the first and second layers. The third layer may include a non-conductive material that may be used to ensure that separate eddy current regions form in the first and second layers. | 12-29-2011 |
| 20110315223 | COATING HAVING IMPROVED HYDROLYTIC RESISTANCE - Coatings utilized in multilayer sheets such as laminated films used for photovoltaic backsheets can be prepared by adding epoxy and carbodiimide to a polyurethane mixture to be utilized as the adhesive, prior to application of the coating to a substrate. Such coatings can exhibit improved resistance to hydrolysis, and can maintain bond strength under prolonged conditions of high heat and humidity. | 12-29-2011 |
| 20110314958 | TUNABLE MASS DAMPER FOR USE WITH A REACTION WHEEL ASSEMBLY - A tunable mass damper (TMD) is provided that can be coupled to a rotating inertia apparatus such as a reaction wheel assembly (RWA). The TMD includes a housing that contains a flexure, a mass, and damping fluid within the housing. The housing is coupled to the flexure, and the flexure is coupled to the mass. The mass is free to sway in the damping fluid. The damping fluid envelops the mass and provides damping between the mass and the housing. At least one of the mass, flexure and the damping fluid can be adjusted to tune the TMD to produce a resonance at or near a mode that is to be mitigated by the TMD such that it operates at a desired or optimal operating frequency. | 12-29-2011 |
| 20110313726 | CONDITION-BASED MAINTENANCE SYSTEM FOR WIND TURBINES - A condition-based maintenance system having instrumentation for collecting data from one or more wind turbines and having a performance monitor for analyzing the data. Also, the system may have a wind turbine anomaly detector. Information from the performance monitor and the anomaly detector may be used for indicating conditions of the one or more wind turbines. These conditions may be a basis for determining maintenance recommended for any of the wind turbines. | 12-22-2011 |
| 20110313658 | SYSTEM AND METHOD FOR ENHANCING COMPUTER-GENERATED IMAGES OF TERRAIN ON AIRCRAFT DISPLAYS - A system and method are disclosed for enhancing the visibility and ensuring the correctness of terrain and navigation information on aircraft displays, such as, for example, continuous, three-dimensional perspective view aircraft displays conformal to the visual environment. More specifically, an aircraft display system is disclosed that includes a processing unit, a navigation system, a database for storing high resolution terrain data, a graphics display generator, and a visual display. One or more independent, higher precision databases with localized position data, such as navigation data or position data is onboard. Also, one or more onboard vision sensor systems associated with the navigation system provides real-time spatial position data for display, and one or more data links is available to receive precision spatial position data from ground-based stations. Essentially, before terrain and navigational objects (e.g., runways) are displayed, a real-time correction and augmentation of the terrain data is performed for those regions that are relevant and/or critical to flight operations, in order to ensure that the correct terrain data is displayed with the highest possible integrity. These corrections and augmentations performed are based upon higher precision, but localized onboard data, such as navigational object data, sensor data, or up-linked data from ground stations. Whenever discrepancies exist, terrain data having a lower integrity can be corrected in real-time using data from a source having higher integrity data. A predictive data loading approach is used, which substantially reduces computational workload and thus enables the processing unit to perform such augmentation and correction operations in real-time. | 12-22-2011 |
| 20110313597 | METHODS AND SYSTEMS FOR DISPLAYING ANNOTATIONS ON AN AIRCRAFT DISPLAY - Methods and systems are provided for presenting content on a display device onboard an aircraft. A method comprises displaying, on the display device, information corresponding to a first procedure and displaying an annotation associated with the first procedure on the display device. The first procedure is associated with an airport and prescribes operation of the aircraft in a vicinity of the airport, and the annotation comprises user-defined information pertaining to the first procedure. | 12-22-2011 |
| 20110311389 | METHODS FOR MANUFACTURING TURBINE COMPONENTS - A method is provided for manufacturing a turbine component. The method includes forming a first intermediate turbine article with an additive manufacturing process; encapsulating the first intermediate turbine article with an encapsulation layer to form a second intermediate turbine article; and consolidating the second intermediate turbine article to produce the turbine component. | 12-22-2011 |
| 20110311369 | GAS TURBINE ENGINE COMPONENTS WITH COOLING HOLE TRENCHES - An engine component includes a body having an interior surface and an exterior surface; a cooling hole formed in the body and extending from the interior surface to the exterior surface; and a concave trench extending from the cooling hole at the exterior surface of the body in a downstream direction. | 12-22-2011 |
| 20110311354 | COMPRESSORS WITH CASING TREATMENTS IN GAS TURBINE ENGINES - A compressor section includes a rotor platform; a rotor blade extending radially outwardly from the rotor platform, the rotor blade including a pressure sidewall and a circumferentially opposing suction sidewall extending in a radial direction between a root and a tip and in an axial direction between a leading edge and a trailing edge; a casing having an inner surface surrounding the tip and spaced radially outwardly thereform to define a gap therebetween; a plurality of grooves disposed in the inner surface of the casing and extending in a generally circumferential direction, the plurality of grooves including a first groove and a second groove; and a channel system comprising at least a first channel positioned within the casing and configured to provide fluid communication between the first groove and the second groove. | 12-22-2011 |
| 20110311332 | CHASSIS MOUNTING SYSTEM - An assembly includes a chassis coupled to a mounting surface via a mounting system. The mounting system includes a bolt, a dashpot, and a spring. The dashpot and the spring are configured to reduce vibration forces transferred from the mounting surface to the chassis. Techniques for forming the assembly are also described. | 12-22-2011 |
| 20110310234 | METHODS AND SYSTEMS FOR PRESENTING SEQUENTIAL VIDEO FRAMES - Methods and systems are provided for presenting content comprising a plurality of frames using display panel comprising an array of display elements. A method comprises transferring image data for a first frame of the plurality of frames to a display element at the beginning of a first frame interval and activating an illumination assembly after transferring image data for the first frame to the display element to present the first frame. The method further comprises transferring image data for a second frame to an energy storage element corresponding to the display element during the first frame interval, and deactivating the illumination assembly prior to transferring the image data for the second frame from the energy storage element to the display element. | 12-22-2011 |
| 20110309809 | HIGH POWER DC SSPC WITH CAPABILITY OF SOFT TURN-ON TO LARGE CAPACITIVE LOADS - Pre-charge circuitry allows capacitive loads connected to a solid state power controller to be gradually charged up by a PWM, generated with a cycle by cycle current limit, switching a single MOSFET in series with an inductor, before the SSPC is turned on. The pre-charge circuitry may require only three additional components, e.g., a MOSFET, an inductor and a diode, along with a designated MOSFET gate driver. | 12-22-2011 |
| 20110309770 | LED LAMP HEAD WITH VARIABLE BRIGHTNESS - A lamp head is configured to be electrically coupled solely to a power-supply element and a return element. A power voltage carried by the power-supply element is regulated by a control element. The lamp includes at least one LED configured to emit light, and a first circuit coupled to the at least one LED and configured to adjust the brightness of the light emitted by the at least one LED solely in response to adjustments made to the power voltage by the control element. | 12-22-2011 |
| 20110308782 | THERMAL INTERFACE MATERIAL AND METHOD OF MAKING AND USING THE SAME - A thermal interface material comprises a polymeric elastomer material, a thermally conductive filler, and a coupling agent, along with other optional components. In one exemplary heat transfer material, a coupling agent having the formula: | 12-22-2011 |
| 20110307218 | SYSTEM AND METHOD FOR CONFLICT RESOLUTION TO SUPPORT SIMULTANEOUS MONITORING OF MULTIPLE SUBSYSTEMS - A system includes a plurality of sensors configured to measure one or more characteristics of a gearbox. The system also includes a subsystem interaction module device, which includes at least one interface configured to receive input signals associated with multiple components of a system. The subsystem interaction module device also includes at least one processing unit configured to identify a potential fault in one or more of the components using the input signals and to provide an indicator identifying the potential fault. The at least one processing unit is configured to identify the potential fault by: identifying conflicting frequencies that are associated with different faults in the components of the system; and determining a confidence level associated with the potential fault based on the conflicting frequencies. | 12-15-2011 |
| 20110305921 | PROTECTIVE COATING SYSTEMS FOR GAS TURBINE ENGINE APPLICATIONS AND METHODS FOR FABRICATING THE SAME - Protective coating systems for gas turbine engine applications and methods for fabricating such protective coating systems are provided. An exemplary protective coating system comprises an aluminide-comprising bond coating disposed on a substrate, a thermal barrier coating overlying the aluminide-comprising bond coating, and a silicate layer interposed between the thermal barrier coating and the aluminide-comprising bond coating. | 12-15-2011 |
| 20110305554 | LIGHT WEIGHT VANELESS COMPRESSOR CONTAINMENT DESIGN - A vaneless compressor containment design has an inner bolt circle with more than three fasteners situated in the vaneless space to cut up tri-hub pieces to smaller pieces prior to reaching an outer bolt circle and its associated flange. This containment design may allow a thinner radial wall thickness for the outermost flange as compared to the conventional design. The thinner radial wall thickness may reduce the weight of the compressor. This weight reduction may be achieved with little or no increase in the compressor space envelope. | 12-15-2011 |
| 20110304852 | SYSTEM TO REDUCE GYROSCOPIC ERRORS WITH LIMITED POWER SUPPLY QUALITY IN A FIBER OPTIC GYROSCOPE - One embodiment is directed to a power supply for a fiber optic gyroscope that comprises at least one main power supply, at least one demodulator local power supply to operatively couple the main power supply to a demodulator included in the fiber optic gyroscope, and at least one modulator local power supply to operatively couple the main power supply to a bias modulator included in the fiber optic gyroscope. The demodulator local power supply comprises a first current source to source current to the demodulator and a first shunt regulator coupled across a load associated with the demodulator. The modulator local power supply comprises a second current source to source current to the bias modulator and a second shunt regulator coupled across a load associated with the bias modulator. | 12-15-2011 |
| 20110304721 | METHOD AND SYSTEM FOR IRIS IMAGE CAPTURE - According to one example embodiment, a process and system include a camera used to capture a sequence of illuminated images of an subject, wherein the images are stored in frames. The focus point is changed for each image captured so that the focus point sweeps from a far to a near end of a sweep range, in discrete steps or continuous motion, so that successive images have slightly overlapping depths of field. The sweep range and overlapping depths of field provide that at least one image is well focused on the iris of the eye of the subject. In one other example embodiment, one or more of the images are illumined with a illumination fired for a respective captured image. In another embodiment, the sweep range is determined at least in part using a range finder or is otherwise controlled to determine a position of the subject so that the sweep range starts and stops a desired distance in front of and behind the subject, respectively. | 12-15-2011 |
| 20110304224 | COMPACT STARTER-GENERATOR WITH COMMON CORE FOR MAIN AND EXCITER WINDING - A power system for a vehicle may comprise an electric machine attached to an engine of the vehicle. The electric machine may comprise only one stator core; a stator main winding wound on the one stator core; a stator exciter winding wound on the one stator core. The stator main winding and the stator exciter winding may be magnetically independent from one another even though magnetic-field-isolation material is not interposed between the stator main winding and the stator exciter winding. | 12-15-2011 |
| 20110303867 | Foams And Articles Made From Foams Containing 1-Chloro-3,3,3-Trifluoropropene (HFCO-1233zd) - The present invention relates to poured-in place polyurethane foams and polyol premixes comprising 1-chloro-3,3,3-trifluoropropene (HFCO-1233zd) and one or more additional co-blowing agents. | 12-15-2011 |
| 20110303802 | ARMREST ASSEMBLY - An armrest assembly for use with a first control device and a second control device arranged generally in a tandem configuration is disclosed herein. The armrest assembly includes, but is not limited to, a base member configured for mounting to the horizontal surface proximate the first control device in a position aligned with the first and the second control devices. The armrest assembly also includes an arm support member movably mounted to the base member. The arm support member is configured to move between a first position and a second position. The arm support member is configured to steady a user's arm when accessing the first control device when the arm support member is in the first position. The arm support member is further configured to steady the user's arm when accessing the second control device when the arm support member is in the second position. | 12-15-2011 |
| 20110303485 | Anti-slip Quick-connect Hardware - An anti-slip harness buckle element has a planar body portion with a plurality of slots formed therein. A biased, U-shaped, friction generating member is carried in one of the slots and slidably engages same. A portion of a support strap, or webbing extends through at least two of the slots of the buckle element and is in part forced toward an edge of one of the slots by the U-shaped, friction generating member thereby crating locking friction relative two the webbing to prevent slippage thereof. | 12-15-2011 |
| 20110303003 | ACCUMULATOR WITH BOTH DIRECT AND REMOTE QUANTITY LEVEL INDICATION - An apparatus for determining the fluid level of a container, such as an accumulator, may include both a remote quantity indicator and a direct quantity indicator. The remote quantity indicator may include a remote dial at the end of a flexible cable or an electrical signal receiver receiving an electrical signal from a rotary variable differential transformer (RVDT), such as a potentiometer. The RVDT type of indicator may include an electrical connector on the accumulator to attach an electrical cable to carry the quantity level signal. The direct quantity indicator may include a dial directly mounted on the accumulator. The remote/direct quantity indicators may include, for example, one of the following three combinations: 1) a dial directly on the accumulator and a remote dial at the end of a flexible cable; 2) an RVDT output and a dial directly on the accumulator; and 3) an RVDT output on an accumulator, a remote dial at the end of a flexible cable and a dial directly on the accumulator. | 12-15-2011 |
| 20110302125 | SYSTEMS AND METHODS FOR VIRTUAL SUB-METERING - The present inventors devised, among other things, systems and methods for estimating the energy usage of individual appliances based on cumulative household energy usage data and energy consumption profiles of the appliances. One exemplary system receives cumulative or aggregate energy usage for a building or other structure including a set of two or more appliances having different load ratings. Based on the aggregate energy usage and predefined usage profiles for the appliances, the exemplary system estimates individual energy usage of the appliances. In one embodiment, the system estimates individual energy usage of the appliances using a Bayesian estimator and displays the usage estimates, referred to as virtual submeter readings, on a graphical user interface. | 12-08-2011 |
| 20110301898 | AUTOMATIC DATA COLLECTION ALGORITHM FOR 3D MAGNETIC FIELD CALIBRATION WITH REDUCED MEMORY REQUIREMENTS - A magnetic compass comprising a magnetometer for taking readings of a magnetic field and a processing unit that calibrates the magnetic compass is provided. The processing unit is configured to validate a predetermined number of magnetic field samples and calculate calibration coefficients from the validated magnetic field samples. Each validated magnetic field sample is at least a minimum separation angle apart from every other validated magnetic field sample. | 12-08-2011 |
| 20110301842 | DISPLAY OF NAVIGATION LIMITS ON AN ONBOARD DISPLAY ELEMENT OF A VEHICLE - A method of displaying navigation limits for a planned travel route of a vehicle is presented here. The method calculates estimated navigation limits for the vehicle using an onboard subsystem of the vehicle, where the estimated navigation limits represent self-assessed navigation accuracy of the vehicle relative to the planned travel route. Contracted navigation limits are acquired for the vehicle, where the contracted navigation limits represent specified navigation accuracy of the vehicle, relative to the planned travel route, as mandated by a third party navigation controller. A navigation display is rendered on an onboard display element such that it includes graphical representations of the planned travel route, at least one of the estimated navigation limits, and at least one of the contracted navigation limits. | 12-08-2011 |
| 20110301783 | SYSTEMS AND METHODS FOR INERTIALLY CONTROLLING A HOVERING UNMANNED AERIAL VEHICLES - Systems and methods for inertially controlling a hovering unmanned aerial vehicle (HUAV) are provided. One inertial controller includes a frame and a sensor for detecting a change in an orientation and/or motion of the frame with respect to a predetermined neutral position. The inertial controller also includes a processor for generating commands to the HUAV to modify its current orientation and/or motion in accordance with the change. A system includes the above inertial controller and a sensor for determining a second change for an orientation and/or motion for the HUAV based on the change, and a processor for generating a signal commanding an HUAV control system to orient and/or move the HUAV in accordance with the second change. One method includes detecting a change in an orientation and/or motion of an inertial controller frame and commanding the HUAV to modify its current orientation and/or motion in accordance with the change. | 12-08-2011 |
| 20110301774 | SYSTEM FOR USING ATTRIBUTES TO DEPLOY DEMAND RESPONSE RESOURCES - A system for using attributes to deploy demand response resources. A service provider may provide energy to customers. The provider may via interactions modify consumption of the energy by the customers. Customers that participate in these interactions may be regarded as demand response resources. Interactions may incorporate demand response signals sent to the resources at their respective facilities. Each resource may have a demand response client which has an association with a customer account in a demand response management system of the provider. The association may be regarded as a binding of the demand response client. The binding may involve inputting an attribute of the demand response client, which can be correlated to the customer account. The attribute may be, for example, a location of the demand response client. Such attribute may be used for the association of the demand response client with a proper customer account. | 12-08-2011 |
| 20110301723 | USING MODEL PREDICTIVE CONTROL TO OPTIMIZE VARIABLE TRAJECTORIES AND SYSTEM CONTROL - A method and system of predictive model control of a controlled system with one or more physical components using a model predictive control (MPC) model, determining an iterative, finite horizon optimization of a system model of the controlled system, in order to generate a manipulated value trajectory as part of a control process. At time t sampling a current state of the controlled system a cost function minimizing manipulated variables trajectories is computed with the MPC model for a relatively short time horizon in the future, wherein the MPC uses a quadratic programming (QP) algorithm to find the optimal solution, and wherein the QP algorithm is solved using an Active Sets solver (AS) class algorithm with simple constraints based on gradient projection and using Newton step projection. A move of the manipulated value trajectory is implemented and the control process is moved forward by continuing to shift the prediction horizon forward. | 12-08-2011 |
| 20110300658 | METHODS OF CREATING A MICRO ELECTRO-MECHANICAL SYSTEMS ACCELEROMETER USING A SINGLE DOUBLE SILICON-ON-INSULATOR WAFER - Methods for creating a microelectromechanical systems (MEMS) device using a single double, silicon-on-insulator (SOI) wafer. The double SOI wafer includes at least a base layer of silicon, a first layer of silicon, and a second layer of silicon, the layers of silicon are separated by an oxide layer. A stationary electrode with rigid support beams is formed into the second layer of silicon. A proof mass and at least one spring are formed into the first layer of silicon. The proof mass is separated from the stationary electrode by a first gap and the proof mass is separated from the base silicon layer by a second gap. | 12-08-2011 |
| 20110299972 | IMPELLER BACKFACE SHROUD FOR USE WITH A GAS TURBINE ENGINE - An impeller or axial stage compressor disk backface shroud for use with a gas turbine engine is disclosed. The backface shroud includes, but is not limited to, a substantially funnel shaped body having a surface. The substantially funnel shaped body is configured to be statically mounted to the gas turbine engine substantially coaxially with the impeller or axial stage compressor disk. The surface and a backface of the impeller or axial stage compressor disk form a cavity that guides an airflow portion to a turbine when the substantially funnel shaped body is mounted coaxially with the impeller or axial stage compressor disk and axially spaced apart therefrom. The airflow portion has a tangential velocity and a recessed groove in the surface of the backface shroud is oriented generally transversely to the tangential velocity to at least partially interfere with the airflow portion, thus affecting static pressure in the cavity. | 12-08-2011 |
| 20110299293 | AIRCRAFT POSITION LIGHT ASSEMBLY - An aircraft position light assembly having one or more light emitting diode (LED) modules. The LED module can be installed in a variety of aircraft wing-tip cavities. An example LED module includes a support device that mounts within an aircraft wingtip, a bracket device that attaches to the support device, at least one circuit board that mounts to the bracket, and two pairs of LEDs. Each pair of LEDs is mounted on opposing major surfaces at a first end of the circuit board. A first pair of reflectors is attached to the circuit board adjacent to two of the LEDs on the opposing major surfaces. A second pair of reflectors is attached to the circuit board adjacent to the other two LEDs on the opposing major surfaces. | 12-08-2011 |
| 20110298912 | WAVEFRONT SENSING FOR BIOMETRIC IMAGING - Devices and approaches for addressing wavefront corruption in biometric applications. A biometric imaging system may have a laser, a wavefront sensor, and an optical system. The laser may be configured to project a laser spot onto a skin portion of a human face, and the optical system may be configured to collect scattered light from the laser spot and relay the light to the wavefront sensor. The biometric imaging system may also have an adaptive optical element and a controller configured to provide actuation commands to the adaptive optical element based at least in part upon a wavefront distortion measurement output from the wavefront sensor. The optical system may further be configured to relay image light to an image camera of the optical system. The image camera may be an iris camera configured for obtaining iris images suitable for biometric identification. | 12-08-2011 |
| 20110298661 | SYSTEM AND METHOD OF COMPENSATING FOR MICRO-JUMP EVENTS - A system comprises a Global Navigation Satellite System (GNSS) receiver configured to acquire and track a unique radio frequency (RF) signal for each of a plurality of channels, wherein the GNSS receiver is configured to provide one or more system state measurements based on the unique RF signals; processing functionality configured to calculate a respective code delay error for each of the plurality of channels based on the respective unique RF signal; and micro jump detection functionality configured to calculate an average code delay error across all of the plurality of channels based on the plurality of calculated code delay errors, wherein the micro jump detection functionality is further configured to compare the calculated average code delay error to an error threshold to detect a micro jump event when the calculated average code delay error exceeds the error threshold. | 12-08-2011 |
| 20110298608 | SITE AND ALARM PRIORITIZATION SYSTEM - An approach for site prioritization and then a review and prioritization of the alarms at the site. A feature may to first find the site most in need of attention and then check the alarms of that site. A rule algorithm may determine a prioritization of site according to primitive rules which can be customized and modified nearly at any time making site priority a dynamic determination. At the site, the alarms may be ordered by criticality. | 12-08-2011 |
| 20110298527 | REAL TIME DYNAMIC OPTIMIZATION OF DEADTIME - A deadtime optimization apparatus and method may determine when it is safe to turn a switch ON, eliminating the need to have a switch controller purposely insert a deadtime period in the algorithm (i.e., it can go back to producing ideal PWM). Since the decision of when it is safe to turn ON the switch may be achieved through measurement, it is expected that the length of time may change for each pulse as the operating conditions change. Therefore, the apparatus and methods of the present invention may take on a dynamic characteristic because the safe to turn ON (STTO) time may vary for each pulse. | 12-08-2011 |
| 20110298434 | HIGH VOLTAGE SYNCHRONOUS RECTIFIER CONTROLLER - A power supply may comprise a pulse-width-modulation (PWM) controller; a synchronous rectifier having a forward metal oxide field effect transistor (MOSFET) and a catch MOSFET; a forward gate driver; a catch gate driver; and the PWM controller connected so that a low output of the PWM controller facilitates operation of the catch MOSFET and so that the low output precludes operation of the forward MOSFET. The power supply may include a self powered synchronous rectifier that may be constructed with delay times that are independent of lot-to-lot and temperature-related timing variations of MOSFETS. | 12-08-2011 |
| 20110297516 | LIMIT SWITCH ASSEMBLY - A limit switch assembly includes a housing having a first end, a second end, an inner surface that defines an inner volume and a spring engagement surface, and an outer surface. A limit switch disposed within the inner volume includes a threaded bushing section at least partially extending from the first end. A spring within the inner volume surrounds the bushing section, and engages the limit switch and the spring engagement surface. A calibration nut threaded onto the bushing section engages the first end of the housing. A seal divides the inner volume of the housing into a first volume and a second volume. A drain hole formed in the housing fluidly communicates the first volume to a surrounding environment. A terminal assembly connected to the second end of the housing seals the second volume from the surrounding environment. | 12-08-2011 |
| 20110297354 | SYSTEM AND METHOD THAT DISSIPATE HEAT FROM AN ELECTRONIC DEVICE - The electronic system includes an electronic device and a liquid holding section that is thermally coupled to the electronic device. The electronic system further includes an impermeable section that engages the liquid holding section. The impermeable section includes a channel and a plurality of passages that provide fluid communication between the liquid holding section and the channel. The electronic system further includes (i) a first fluid that flows through the channel in the impermeable section to facilitate heat transfer from the electronic device to the first fluid; and (ii) a second fluid that flows from the liquid holding section through the plurality of passages into the channel when the second fluid boils within the liquid holding section due to heat transfer from the electronic device to the second fluid. In some embodiments, the first and second fluids are different types of substances. | 12-08-2011 |
| 20110296900 | Integrated IR Source and Acoustic Detector for Photoacoustic Gas Sensor - A photoacoustic gas detector includes an integrated source, infrared filter and an acoustic sensor. The source, filter and acoustic sensor can be integrated onto one or more semiconductor substrates, such as silicon. Processing circuitry can also be integrated onto the substrate. Further, the source, filter and acoustic sensor can be integrated into a single component package, such as a metal can transistor package. | 12-08-2011 |
| 20110296812 | THRUST REVERSER ACTUATION SYSTEM ARCHITECTURE - A thrust reverser actuation system includes a plurality of actuators, a power drive unit, and a gear set. Each actuator is coupled to receive an actuator input torque and is configured, upon receipt of the actuator input torque, to move between a stowed position and a deployed position. The power drive unit has only one output shaft, and is configured to supply a drive torque via the output shaft. The gear set is connected to the output shaft and is coupled to each of the actuators. The gear set is configured to receive the drive torque via the output shaft and to supply the actuator input torque to each of the actuators. | 12-08-2011 |
| 20110296379 | AUTOMATED METHOD FOR DECOUPLING AVIONICS APPLICATION SOFTWARE IN AN IMA SYSTEM - A method to decouple software in an integrated modular system that employs message-based data exchange is provided. The method includes generating at least one configuration table for use by core software in at least one module in the integrated modular system. The at least one module hosts at least one of a consuming application. The method also includes gathering parameter data from producer messages at the core software in the at least one module based on the generated configuration table, and creating target messages at the core software based on the gathered parameter data. The target messages have a format specific to the consuming application. | 12-01-2011 |
| 20110295569 | WIND ESTIMATION FOR AN UNMANNED AERIAL VEHICLE - The speed of the wind during operation of a UAV is estimated. In one example the speed of the wind is estimated by modeling an acceleration of an unmanned aerial vehicle (UAV) based on a measured ground speed of the UAV, determining an actual acceleration of the UAV with one or more sensors, and estimating the speed of the wind as an integral of a difference between the modeled acceleration and the actual acceleration. | 12-01-2011 |
| 20110295540 | Non-Contacting Temperature Profile Measurement of Rotating Rolls - A high-resolution, non-contact sensor that measures the temperature of an elongated roll comprises an array of low-mass air temperature elements positioned adjacent the cylindrical surface. As the roll rotates a boundary layer of air is formed along the contour of the roll. Each air temperature element can be housed in a chamber into which a portion of the boundary layer air directed. The temperature of the air temperature element eventually stabilizes and is a function of the roll surface temperature. Associated air compensator elements detect ambient air temperatures and the actual surface temperature profile is extracted from calibration curves based on measurements from both the air temperature and compensator elements. | 12-01-2011 |
| 20110295511 | APPARATUS AND METHOD FOR DETECTING THE PRESENCE OF AN AGENT - An apparatus and method for detecting an agent utilizes a substrate, a waveguide on the substrate, a light source, a photo-detector, an optical coupler on the substrate, and a processor. The light source is configured to emit light into the waveguide. The photo-detector is configured to detect light. The optical coupler is configured to direct a first portion of light propagating from the waveguide towards the photo-detector and to direct a second portion of the light propagating from the waveguide back into the waveguide. The waveguide and the optical coupler at least partially form a resonator. A substance is at least one of embedded within the waveguide and adjacent to the waveguide. The substance is reactive to the agent. The processor detects a change in a resonance lineshape of the resonator caused by the reaction of the substance to the agent. | 12-01-2011 |
| 20110295449 | METHODS AND SYSTEMS FOR REDUCING ANGULAR VELOCITY USING A GYROSCOPE ARRAY - Methods and systems are provided for reducing angular velocity of a vehicle using a gyroscope array. A method comprises dithering a gyroscope of the gyroscope array, obtaining current through a gimbal motor of the gyroscope while dithering the gyroscope, determining a gimbal rate command to reduce angular velocity of the vehicle based on the current through the gimbal motor obtained while dithering the gyroscope, and operating the gimbal motor of the gyroscope based on the gimbal rate command. | 12-01-2011 |
| 20110295045 | Azeotrope-Like Composition of Hexafluoropropane, Hexafluoropropene and Hydrogen Fluoride - The present invention relates to an azeotropic or azeotrope-like mixture consisting essentially of 1,1,1,2,3,3-hexafluoropropane, hexafluoropropene and hydrogen fluoride. | 12-01-2011 |
| 20110293963 | COATINGS, TURBINE ENGINE COMPONENTS, AND METHODS FOR COATING TURBINE ENGINE COMPONENTS - A coating is disclosed that consists essentially of, by weight, about 27.5% to about 31.5% aluminum, about 0.20% to about 0.60% hafnium, about 0.08% to about 0.30% zirconium, about 0.005% to about 0.100% of two or more reactive elements selected from a group consisting of yttrium, lanthanum, and cerium, and a balance of nickel. Turbine engine components including the coating and methods of applying the coating on such components are also disclosed. | 12-01-2011 |
| 20110293845 | METHODS OF BONDING PURE RHENIUM TO A SUBSTRATE - Methods are provided for bonding pure rhenium to a substrate comprising a material. Non-lubricated components configured to have friction contact with another component are also provided. In an embodiment, by way of example only, a method includes disposing a eutectic alloy over the substrate to form an inter layer, the eutectic alloy comprised essentially of a base alloy and one or more melting point depressants and having a melting temperature that is lower than a melting temperature of the substrate material and a melting temperature of rhenium, placing pure rhenium over the inter layer, and heating the inter layer to a temperature that is substantially equal to or greater than the melting temperature of the eutectic alloy, but that is below the melting temperature of the substrate material and the melting temperature of the pure rhenium to bond the pure rhenium to the substrate. | 12-01-2011 |
| 20110293246 | SYSTEMS AND METHODS OF MANAGING NETWORK VIDEO RECORDING SYSTEMS - A system and method for managing a network video recording system are provided. The method includes interfacing a network video recording system with an end user operating system, and managing the network video recording system via the end user operating system. | 12-01-2011 |
| 20110292967 | HIGH RESOLUTION MEASUREMENT OF THERMISTOR THERMOMETRY SIGNALS WITH WIDE DYNAMIC RANGE - A thermistor amplifier device comprising a first amplifier and a second amplifier is provided. The first amplifier generates an analog temperature signal output based on a voltage across at least one thermistor. The second amplifier generates an offset voltage input to the first amplifier, wherein the offset voltage is based on maintaining the analog temperature signal within a predefined voltage range. The second amplifier selects the offset voltage corresponding to one of a plurality of range levels, wherein each of the plurality of range levels is associated with a temperature range of the at least one thermistor. | 12-01-2011 |
| 20110292951 | FIBER LIGHT SOURCE WITH HIGH MEAN WAVELENGTH STABILITY AND RELIABILITY - A broadband light source configured to emit a stable broadband optical beam is provided. The broadband light source includes at least one optical pump source, an optical system including a polarization beam combiner, and a solid state laser medium. The optical system is configured to receive at least one optical pump beam from a respective one of the at least one optical pump source. The solid state laser medium receives a substantially unpolarized pump beam from a first output of the optical system. Stable broadband amplified spontaneous emission is output from a second output of the optical system. | 12-01-2011 |
| 20110292907 | METHOD AND SYSTEM FOR GROUND STATION SIGNAL HANDOVER FOR AIRCRAFT - A method and system for ground station signal handoff for an aircraft. The method comprises receiving signal quality data and position data from each of a plurality of ground stations as a signal from each of the ground stations becomes detectable onboard the aircraft, while the aircraft is in communication with an active ground station. A position of the aircraft is determined each time a signal quality from one of the ground stations reaches a predetermined threshold indicating that the signal quality is suitable for handoff. A set of ground stations potentially suitable for handoff is identified based on their signal quality data when an insufficient signal quality of the active ground station is detected. The set of potentially suitable ground stations is evaluated based on their position and signal quality, and a trajectory or speed vector of the aircraft, to determine an optimal ground station for handoff. A handoff request is then transmitted to the optimal ground station. | 12-01-2011 |
| 20110292396 | SYSTEM AND METHOD FOR ENHANCING SIGNAL-TO-NOISE RATIO OF A RESONATOR FIBER OPTIC GYROSCOPE - A resonator fiber optic gyroscope includes a sensing resonator having a first resonance frequency for a first laser beam propagation direction and a second resonance frequency for a second laser beam propagation direction; an intensity modulator coupled to an output of the sensing resonator and configured to modulate the intensity of a signal output from the sensing resonator, wherein the intensity modulator modulates the output signal at an intensity modulation frequency; and resonance tracking electronics coupled to an output of the intensity modulator and configured to demodulate the intensity modulated signal output from the intensity modulator at a resonance tracking modulation frequency to produce a first demodulated signal; the resonance tracking electronics further configured to demodulate the first demodulated signal at the intensity modulation frequency, wherein the intensity modulation frequency is different from the resonance tracking modulation frequency. | 12-01-2011 |
| 20110291831 | TIME BASED VISUAL REVIEW OF MULTI-POLAR INCIDENTS - A system and method for time based review of multi-polar incidents is provided. The method includes selecting at least one past alarm incident, and populating a floor plan map with representations of the past alarm incident and a set of alarms that were active during the past alarm incident. | 12-01-2011 |
| 20110291778 | QUADRUPOLE MAGNETIC CODED SWITCH - A quadrupole magnetic coded switch includes a switch housing, an actuator, one or more switch dipole magnets, and a plurality of magnetically operated switch circuits. The actuator housing is movable relative to the switch housing. The plurality of actuator dipole magnets are coupled to the actuator housing and are movable therewith. The one or more switch dipole magnets are coupled to the switch housing. The one or more switch dipole magnets and the plurality of actuator dipole magnets are arranged to generate a quadrupole magnetic field. Each magnetically operated switch circuit is disposed within the switch housing and is configured to transition between a plurality of switch positions in response to relative movement of the actuator housing and the switch housing. | 12-01-2011 |
| 20110290108 | SLUG MITIGATION BY INCREASING AVAILABLE SURGE CAPACITY - A system includes a controller and an apparatus that includes a housing having a volume and an inlet. The inlet can receive a fluid that includes a gas and a liquid. The apparatus also includes a baffle that partitions the volume into a first portion and a second portion. The baffle extends from a base of the housing. The first portion can receive the liquid and separate the liquid into a first part and a second part. The second portion can receive the second part of the liquid from the first portion. The controller regulates an amount of the second part of the liquid in the second portion such that a level of the second part of the liquid is higher than a height that the baffle extends from the base of the housing, thus enabling the use of the extra surge capacity in the vessel. | 12-01-2011 |
| 20110290021 | HEMITOROIDAL RESONATOR GYROSCOPE - One exemplary embodiment is directed to a vibratory structure gyroscope having a substrate having a top surface. The vibratory structure gyroscope can also include a resonator having a hemitoroidal shape, the resonator including a stem and an outer lip that surrounds the stem, the stem attached to the top surface of the substrate and the outer lip located apart from the top surface to allow the resonator to vibrate. | 12-01-2011 |
| 20110289748 | COMPOSITIONS CONTAINING TETRAFLUOROPROPENE AND CARBON DIOXIDE - Disclosed are compositions useful in a wide variety of applications, including heat transfer fluids which possess a highly desirable and unexpectedly superior combination of properties, and heat transfer systems and methods based on these fluids. The preferred heat transfer fluid comprises from about 1 to about 40 percent, on a weight basis, of carbon dioxide (CO | 12-01-2011 |
| 20110288846 | TECHNIQUE AND TOOL FOR EFFICIENT TESTING OF CONTROLLERS IN DEVELOPMENT (H-ACT PROJECT) - An improved tool and technique for performance quality testing of a synthesized controller or a controller-in-development is disclosed. A controller's performance in a test run within a simulation testing environment is quantitatively compared to an optimal performance parameter as defined in a controller performance model. Deviation between these compared results is recorded as an indicator of poor controller performance. Only deviating test results are recorded for review to guide further fine tuning or modifications of controller settings, and to save mass storage space. The controller performance test runs autonomously and may be automatically restarted should any failure within the simulation environment occur. | 11-24-2011 |
| 20110288828 | DISTRIBUTED MODEL IDENTIFICATION - A method and system for identifying a distributed model for a nonlinear system represented by a block diagram. The distributed model identification can be achieved by first replacing all signal links across the block diagram with elastic links by augmenting each input port of a plurality of blocks with a signal generator that produces a replacement signal value (s | 11-24-2011 |
| 20110288796 | CONDITION BASED MONITORING SYSTEM BASED ON RADAR SENSOR - A sensing system comprising a radar-based vibration sensor and processing unit used to collect and process vibration information from a machine of interest. The radar-based vibration sensor obtains vibration data from mechanical operation of a component or series of components in the machine, and may be steered toward specific regions of interest of the machine. The processing unit analyzes the data, and may fuse data from a plurality of vibration sensors, such as radar-based vibration sensors and multiple machine-mounted sensors such as accelerometers. From this analysis, indications related to a status of the mechanical operation of the components in the machine of interest may be provided to relevant users. | 11-24-2011 |
| 20110288350 | PROCESS FOR THE PREPARATION OF FLUORINATED CIS-ALKENE - Disclosed is a process for the preparation of fluorine-containing olefins comprising contacting a chlorofluoroalkane with hydrogen in the presence of a catalyst at a temperature sufficient to cause replacement of the chlorine substituents of the chlorofluoroalkane with hydrogen to produce a fluorine-containing olefin. Also disclosed are catalyst compositions for the hydrodechlorination of chlorofluoroalkanes comprising copper metal deposited on a support, and comprising palladium deposited on calcium fluoride, poisoned with lead and reducing the in the presence or absence of a dehydrochlorination catalyst under conditions effective to form a product stream comprising cis-1,1,1,4,4,4-hexafluoro-2-butene (HFO-1336). | 11-24-2011 |
| 20110288349 | PROCESS FOR THE PRODUCTION OF FLUORINATED ALKENES - The present invention provides a method for the preparation of suitable chlorofluorocarbon and hydrochlorofluorocarbon materials or chlorofluorocarbon and hydrochlorofluorocarbon alkene and alkyne intermediates which serve as useful feedstock for fluorination and reduction to cis-1,1,1,4,4,4-hexafluoro-2-butene. Also presented is a continuous process for the production of cis-1,1,1,4,4,4-hexafluoro-2-butene from the alkene and alkyne intermediates. | 11-24-2011 |
| 20110288348 | PROCESS FOR THE PREPARATION OF HEXAFLUORO-2-BUTYNE - Disclosed is a process for making hexafluoro-2-butyne comprising the steps of: (a) providing a composition comprising CF | 11-24-2011 |
| 20110288347 | PROCESS FOR THE MANUFACTURE OF FLUORINATED OLEFINS - A method for producing 1,1,1,2-tetrafluoropropene and/or 1,1,1,2,3-pentafluoropropene using a single set of four unit operations, the unit operations being (1) hydrogenation of a starting material comprising hexafluoropropene and optionally recycled 1,1,1,2,3-pentafluoropropene; (2) separation of the desired intermediate hydrofluoroalkane, such as 1,1,1,2,3,3-hexafluoropropane and/or 1,1,1,2,3-pentafluoropropane; (3) dehydrofluorination of the intermediate hydrofluoroalkane to produce the desired 1,1,1,2-tetrafluoropropene and/or 1,1,1,2,3-pentafluoropropene, followed by another separation to isolate the desired product and, optionally, recycle of the 1,1,1,2,3-pentafluoropropene. | 11-24-2011 |
| 20110288346 | PROCESS FOR CIS 1,1,1,4,4,4-HEXAFLUORO-2-BUTENE - Disclosed is a process for preparing cis-1,1,1,4,4,4-hexafluoropropene comprising the steps of (a) reacting CCl | 11-24-2011 |
| 20110287996 | Azeotrope-Like Compositions of 1,1,2,3-Tetrachloropropene And Hydrogen Fluoride - An azeotrope-like composition consisting essentially of 1,1,2,3-tetrachloropropene and hydrogen fluoride is provided, as well as methods that involve such an azeotrope-like composition. | 11-24-2011 |
| 20110286884 | HYDROGEN AND ELECTRICAL POWER GENERATOR - A device using needed hydrogen gas flow and electricity for operation obtained from a fuel cell power supply. Also, water generated by the fuel cell may be recycled for hydrogen generation which may be used by the device and in turn expanded by the fuel cell for further electrical power generation. The device may be a gas chromatograph, a fluid calibration mechanism, a flame ionization detector, or the like. | 11-24-2011 |
| 20110285851 | INTRUDER SITUATION AWARENESS SYSTEM - An approach for detecting, tracking and capturing images of an intruder in a building. The intruder's bearing and speed, and structural information about the building may provide at least a partial basis for calculating potential paths of the intruder. Cameras along the anticipated paths may be selected. These cameras may be optimized to cover nearly any area where the intruder may appear. Location, one or more images, and possibly other information may provide an intruder situation awareness for display. | 11-24-2011 |
| 20110285845 | DISTANT FACE RECOGNITION SYSTEM - A method and system for automatic face recognition. A primary and a plurality of secondary video cameras can be provided to monitor a detection area. The primary video camera can detect people present in the detection zone. Data can be then transmitted to a prioritizor module that produces a prioritized list of detected people. The plurality of secondary video cameras then captures a high-resolution image of the faces of the people present in the detection area according to the prioritized list provided by the prioritizor module. The high-resolution images can be then provided to a face recognition module, which is used to identify the people present in the detection area. | 11-24-2011 |
| 20110285578 | RF BASED TRACKER FOR ROTATING OBJECTS - An RF beam is used to probe the presence or absence of a rotating blade in a known field of view. Timing of appearance or disappearance or “zero-crossing” of a reflected signal is correlated with timing of the blade movement. Blades which are leading or lagging versus other blades will produce different timing signatures representative of alignment of the blades | 11-24-2011 |
| 20110285404 | PROXIMITY SENSOR WITH HEALTH MONITORING - A proximity sensor includes a relatively simple health monitoring circuit. The proximity sensor includes a variable gain oscillator, a feedback circuit, and a proximity determination circuit. The variable gain oscillator has a gain that varies with the proximity of a target to a sensor coil, generates an oscillating electrical signal having a substantially constant amplitude magnitude, and generates an energy signal representative of the electrical energy needed to sustain oscillations. The feedback circuit supplies feedback to the oscillator, and the proximity determination circuit, based on the energy signal, supplies a proximity signal representative of target proximity to the sensor coil. The health monitor circuit also receives the oscillating electrical signal and supplies a health status signal representative of proximity sensor health. | 11-24-2011 |
| 20110284784 | SEALS, BALL VALVE ASSEMBLIES, AND METHODS OF OPERATING BALL VALVE ASSEMBLIES - Seals, ball valve assemblies, and methods of operating ball valves assemblies are provided. The seal includes an annular jacket, a restrictor, and a spring energizer. The annular jacket includes a first annular pocket and a second annular pocket. The restrictor is disposed in the first annular pocket and is capable of restricting shrinkage of the first annular pocket to a predetermined diameter range, if the seal is exposed to a temperature within a predetermined temperature range. The spring energizer is disposed in the second annular pocket and is configured to supply a force against the annular jacket to maintain the seal against a contact surface. | 11-24-2011 |
| 20110284178 | APPARATUS AND METHOD FOR CONTROLLING CURLING POTENTIAL OF PAPER, PAPERBOARD, OR OTHER PRODUCT DURING MANUFACTURE - A method includes receiving a measurement associated with an anisotropy of a first surface and a measurement associated with an anisotropy of a second surface of a sheet of material. The method also includes adjusting an operating parameter associated with a headbox based on the measurements. The headbox is associated with manufacture of the sheet. The operating parameter could include a jet speed, a jet impingement angle, a jet thickness, a slice opening, and/or a slice apron projection. Adjusting the operating parameter could be based on a difference between a measured anisotropy of the first surface and a measured anisotropy of the second surface. For example, the operating parameter could be adjusted to achieve a desired difference between the measured anisotropy of the first surface and the measured anisotropy of the second surface. Multiple headboxes could be controlled, such as when different headboxes are used to produce different layers of a multi-layer sheet. | 11-24-2011 |
| 20110284106 | PARTIAL STROKE TESTING - Partial Stroke Testing (PST) equipment and methodologies provide PST data for an electromechanical valve, wherein power is withheld from the valve to trigger the vale to move away from a fully open position and power is subsequently applied to reinstate the fully open position immediately following detecting that the test valve has moved away from the fully open position. These operations are performed and monitored to determine whether they are completed within a prescribed period of time and associated data is generated that indicates a health of the valve subjected to the PST. | 11-24-2011 |
| 20110283826 | CONTROL MOMENT GYROSCOPE ASSEMBLY AND METHOD FOR MAKING THE SAME - A control moment gyroscope assembly including, but not limited to, a rotor that includes a shaft, a primary rim and a web that connects the shaft to the primary rim. The rotor is made from a metal material and is adapted to spin about the shaft. The control moment gyroscope assembly further includes a secondary rim that is made of the metal material and that is disposed around the rotor. The secondary rim is configured to compress the rotor in the direction of the shaft. | 11-24-2011 |
| 20110283802 | MODULAR PRESSURE SENSOR - A pressure sensor device for a modular pressure sensor package is provided, comprising a substrate having a pressure port that extends through the substrate from a first side of the substrate to a second side of the substrate. A pressure sensor die is attached to the first side of the substrate, forming a seal over the pressure port on the first side of the substrate. A cover is attached to the first side of the substrate over the pressure sensor die, forming a sealed cavity wherein the pressure sensor die is located within the cavity. The device also comprises a plurality of electrical connectors mounted to the substrate external to the cavity, the plurality of electrical connectors electrically coupled to the pressure sensor die. Further, the substrate includes at least one mounting element configured to secure a pressure port interface to the second side of the substrate in a position around the pressure port. | 11-24-2011 |
| 20110283768 | SELF-CALIBRATING VIBRATION SENSOR - An antenna in a radar sensor is vibrated at a known frequency and velocity in a direction generally normal to the antenna surface. A response received by the antenna is used to scale or calibrate sensor responses at frequencies of interest. | 11-24-2011 |
| 20110283698 | Variable-Nozzle Assembly for a Turbocharger - A variable-nozzle turbocharger includes a turbine housing and a center housing, and a generally annular nozzle ring and an array of vanes rotatably mounted to the nozzle ring such that the vanes are rotatably adjustable for regulating exhaust gas flow to the turbine wheel. An elastically deformable member is disposed between a radially inwardly facing surface of the nozzle ring and a radially outwardly facing surface of the center housing, the elastically deformable member having a radially inner surface contacting the radially outwardly facing surface of the center housing and having a radially outer surface contacting the radially inwardly facing surface of the nozzle ring so as to radially center the nozzle ring relative to the center housing. | 11-24-2011 |
| 20110282580 | METHOD OF IMAGE BASED NAVIGATION FOR PRECISION GUIDANCE AND LANDING - A method to improve landing capability for an aircraft is provided. The method includes storing calibrated-offline-reference images of at least one runway in the aircraft and capturing real-time images of a destination runway during an approach to the destination runway. The destination runway is one of the at least one runway. The method further includes comparing the real-time images of the destination runway with the calibrated-offline-reference images of the destination runway to select respective closest calibrated-offline-reference images from the calibrated-offline-reference images for the associated real-time images; evaluating translational differences and rotational differences between associated real-time images and selected closest calibrated-offline-reference images; and determining errors in translational coordinates and rotational coordinates provided by a navigation system in the aircraft during the approach based on the evaluated translational differences and rotational differences. | 11-17-2011 |
| 20110282568 | METHODS AND SYSTEMS FOR AN IMPROVED IN-TRAIL PROCEDURES DISPLAY - Systems and methods for improving situational awareness on an in-trail procedures display. The present invention provides a display with visual identification and indication for aircraft that do not meet the ITP criteria. In the in-trail procedures display, feedback is provided when a pilot selects an invalid ITP flight level, unambiguous feedback is provided to the pilot upon selection of a valid flight level, and valid inter-target aircraft located in intervening flight levels after selection of a valid flight level are positively identified and invalid target aircraft for selection are uniquely identified. | 11-17-2011 |
| 20110282111 | Method For Making Catalyst Compositions Of Alkali Metal Halide-Doped Bivalent Metal Fluorides And A Process For Making Fluorinated Olefins - There is provided methods for making a catalyst composition represented by the formula MX/M′F | 11-17-2011 |
| 20110279680 | PASSIVE INFRARED IMAGER - An infrared camera includes a lens to receive infrared radiation from an image to be viewed. A thermal detector is positioned to receive the infrared radiation from the lens and vary the amount of light transmitted through the thermal detector responsive to the infrared radiation. | 11-17-2011 |
| 20110279678 | Surveillance System with Direct Database Server Storage - A video surveillance system includes at least one of a camera or a streamer. A data base server is coupled to the camera and can store metadata for a video clip from the camera or streamer. A media storage server is coupled to both the camera or, the streamer, and to the data base server to store the clip in the absence of any network video recorders. | 11-17-2011 |
| 20110277822 | COMPOSITE ELECTRON CONDUCTOR FOR USE IN PHOTOVOLTAIC DEVICES - A photovoltaic device such as solar cell includes a substrate, a composite electron conductor layer adjacent to the substrate, an active layer coupled relative to the composite electron conductor layer, and an electrode electrically coupled to the active layer. In some embodiments, the composite electron conductor layer includes a mixture of different sized particles, such as a mixture of smaller nanoparticles along with larger ground up or otherwise processed nanopillar, nanowire, nanorod, nanotubes, inverse opal and/or any other suitable structured nanocomponents as desired. Methods for making such photovoltaic device are also disclosed. | 11-17-2011 |
| 20110277522 | PASTILLATION OF AMMONIUM SULFATE NITRATE - Processes are presented for the production of ammonium sulfate nitrate. The processes provide for producing a highly uniform product and having a substantially uniform size. The processes include reacting ammonium sulfate and ammonium nitrate to form an FASN slurry melt. The slurry melt is continuously stirred and heated to keep the slurry melt under a shear thinned condition and at a uniform temperature until the slurry melt is extruded, cooled and solidified. | 11-17-2011 |
| 20110276264 | SYSTEM FOR GUIDANCE AND NAVIGATION IN A BUILDING - A system for guidance and navigation in a building. For example, the system may determine a route for egress or rescue of one or more people from a building with a hazardous condition. The system may process the route into waypoints and segments developed within a set of constraint rules. Semantic information about the building may be associated with the waypoints and/or segments. The waypoints and segments may be processed into navigation commands. The navigation commands may be formed in natural language from sentence templates. The system may additionally have 3D beacon audio to assist in guidance and navigation of the one or more people in the building. | 11-10-2011 |
| 20110276200 | SYSTEMS AND METHODS FOR PERFORMING EXCESSIVE NEGATIVE PITCH ALERT AND BIASING SINK RATE ALERT - Systems and methods that alert the pilot of the unusual negative pitch attitude. Additionally, the system can bias a “sink rate” envelope toward a more sensitive direction, such that the pilot can be alerted while (or before) a large sink rate is built up during an unusual negative pitch attitude condition. | 11-10-2011 |
| 20110276198 | VERTICAL PROFILE DISPLAY WITH VARIABLE DISPLAY BOUNDARIES - A display system includes instrumentation configured to obtain aircraft data comprising current flight status data of the host aircraft and current flight status data of neighboring aircraft located near the host aircraft. The system also includes a processor coupled to the instrumentation. The processor analyzes and filters the aircraft data, using lateral boundary criteria for the host aircraft, to identify a proper subset of the neighboring aircraft, and the processor generates image rendering display commands based upon the current flight status data of the host aircraft and based upon the current flight status data of neighboring aircraft included in the proper subset. A display element receives the image rendering display commands and, in response thereto, renders a vertical situation display that includes graphical representations of the host aircraft and each neighboring aircraft included the proper subset. | 11-10-2011 |
| 20110276160 | REFERENCE MODEL FOR PRODUCTION PLANTS AND RELATED SYSTEM AND METHOD - Systems and methods that include selecting a physical model and a procedural model associated with an industrial plant, projecting a cross-product of the physical model and the procedural model into a unit-operation association set using a projection matrix, the unit-operation association set associating units representing equipment in the industrial plant and operations representing processes performed in the industrial plant, and establishing internal and external adjacency sets within structures, the internal adjacency set identifying connections between inputs and outputs of individual units and operations, the external adjacency set identifying connections between outputs of some units and operation and inputs of other units and operations. These systems and methods may also include generating a hyperstructure representing the industrial plant using the association and adjacency sets. | 11-10-2011 |
| 20110275724 | Azeotrope-Like Compositions Of Pentafluoropropene And Water - Provided are azeotropic and azeotrope-like compositions of 1,2,3,3,3-pentafluoropropene (HFO-1225ye) and water. Such azeotropic and azeotrope-like compositions are useful in isolating 1,2,3,3,3-pentafluoropropene from impurities during production. Azeotropes of the instant invention are similarly useful in final compositions or manufacturing final compositions, such as blowing agent, propellants, refrigerants, diluents for gaseous sterilization and the like. | 11-10-2011 |
| 20110275723 | Azeotrope-Like Compositions Of Tetrafluoropropene And Water - Provided are azeotropic and azeotrope-like compositions of trans-1,3,3,3-tetrafluoropropene (HFO-1234ze(E)) and water. Such azeotropic and azeotrope-like compositions are useful in isolating trans-1,3,3,3-tetrafluoropropene from impurities during production. Azeotropes of the instant invention are similarly useful in final compositions or for the manufacture of final compositions, such as blowing agent, propellants, refrigerants, diluents for gaseous sterilization and the like. | 11-10-2011 |
| 20110274535 | TURBOCHARGER ASSEMBLY HAVING HEAT SHIELD-CENTERING ARRANGEMENTS - A turbocharger for internal combustion engines, having a heat shield disposed between a turbine housing and center housing of the turbocharger for shielding the center housing from exhaust gases passing through the turbine. The heat shield in one embodiment is centered on a generally conical surface of the center housing, by engagement between the conical surface and a centering portion of the heat shield. In another embodiment, the heat shield has a generally conical portion that is non-axisymmetric, having a plurality of radially enlarged lobes that engage a radially inwardly facing surface of the turbine housing for centering the heat shield. | 11-10-2011 |
| 20110274343 | SYSTEM AND METHOD FOR EXTRACTION OF FEATURES FROM A 3-D POINT CLOUD - A method of extracting a feature from a point cloud comprises receiving a three-dimensional (3-D) point cloud representing objects in a scene, the 3-D point cloud containing a plurality of data points; generating a plurality of hypothetical features based on data points in the 3-D point cloud, wherein the data points corresponding to each hypothetical feature are inlier data points for the respective hypothetical feature; and selecting the hypothetical feature having the most inlier data points as representative of an object in the scene. | 11-10-2011 |
| 20110274133 | SYSTEMS AND METHODS FOR IMPROVED RING LASER GYROSCOPE DEVICES THROUGH MIX RATIO OPTIMIZATION - Systems and methods for improved ring laser gyroscope devices through mix ratio optimization are provided. In one embodiment, a ring laser gyroscope device comprises: a laser block assembly having a cavity therein that defines a ring shaped laser beam path around the laser block assembly, the cavity containing a fill gas mixture comprising Helium and Neon, wherein the laser block assembly is characterized as having a Neon depletion life limiter; and a readout assembly optically coupled to the laser block assembly. The readout assembly outputs a laser intensity monitor (LIM) voltage that represents optical energy within the cavity. The fill gas mixture has a Helium to Neon ratio richer in Neon than a ratio that would produce a peak LIM voltage from the readout assembly. | 11-10-2011 |
| 20110273315 | SYSTEMS AND METHODS FOR ADJUSTING LANDING GEAR ALERT ENVELOPE FOR OFFSHORE PLATFORMS AND BUILDING-TOP LANDINGS - Systems and methods for improving landing gear alerting on a rotary wing aircraft. An example system includes a user interface device that allows a user to set a bug altitude value and a radio altimeter that produces an altitude value, both of which are in communication with a processor. The processor receives a bug altitude setting, generates a landing gear alert altitude value based on the received bug altitude setting and a predefined additive, receives a radio altitude value for the rotary-wing aircraft, and generates a landing gear alert if the radio altitude value is less than the landing gear alert altitude value and the landing gear is not in a landing position. An output device in signal communication with the processor, outputs the generated landing gear alert. | 11-10-2011 |
| 20110271144 | APPROACH FOR DATA INTEGRITY IN AN EMBEDDED DEVICE ENVIRONMENT - A system for providing data integrity in an embedded device environment. One approach is operating an embedded control engine with non-battery backup power and providing data backup with inexpensive memory. Just data having changes may be provided to a volatile memory such as an SRAM module. After an accumulation of a certain amount of data, the data may be moved onto a relatively larger non-volatile memory, such as an NVRAM module or other type of flash memory. Non-battery backup power may maintain the SRAM module for a period after a power loss, so as to retain data. After restoration of power, data from NVRAM and SRAM modules may be read by the backup service to recreate the last known state of the control engine before the power loss. | 11-03-2011 |
| 20110270992 | ENHANCED FLIGHT CREW DISPLAY FOR SUPPORTING MULTIPLE CONTROLLER/PILOT DATA LINK COMMUNICATIONS (CPDLC) VERSIONS - An avionics system comprising a human machine interface configured to display a user interface and a control device is provided. The control device coupled to the human machine interface, wherein the control device is configured to send and receive controller/pilot data link communications (CPDLC) messages and adjust the user interface based on a first CPDLC version of an established first CPDLC session. | 11-03-2011 |
| 20110270584 | BUILDING STRUCTURE DISCOVERY AND DISPLAY FROM VARIOUS DATA ARTIFACTS AT SCENE - An approach for developing information about a building of which little or no information is known at a time when firefighters need to enter the building. The approach may incorporate obtaining an image of the building from a publicly available resource. An outside boundary of the building may be determined from the image. The number of floors may be determined. A 3D floor plan may be generated from the boundary and the number of floors. Structural components may be added to the 3D floor plan, which are deduced from movements of firefighters, and the movements may be deduced from their locations. The locations may be transmitted by devices on the firefighters. Structural components of the building indicated by persons in the vicinity of the building may also be added to the 3D floor plan. | 11-03-2011 |
| 20110270544 | STORAGE DEVICE ENERGIZED ACTUATOR HAVING DIAGNOSTICS - A system having unified diagnostics where an electrical energy storage device may supply an actuator. Various techniques may be used to determine energy storage capacity and actuator current usage. Measured storage capacity and actuator current may indicate the health of the energy storage device and the actuator, respectively. Also, operation of a service switch for the actuator may be checked relative to its state. | 11-03-2011 |
| 20110270470 | AIRCRAFT SYSTEMS AND METHODS WITH ACTIVE DECELERATION CONTROL - A system is provided for controlling the speed of an aircraft during a deceleration segment between a first state associated with a first speed and a first time and a second state associated with a second speed and a second time. The system includes a navigation system configured to determine the first state; a guidance system configured to determine the second state; and an active deceleration system coupled to the navigation system and the guidance system and configured to construct the deceleration segment between the first state and the second state with at least one intermediate speed between the first speed and the second speed. | 11-03-2011 |
| 20110270000 | METHOD FOR PRODUCING TETRAFLUOROPROPENES - The current invention relates to a process for making a tetrafluoropropene using a tetrafluorochloropropane and/or a pentafluoropropane as starting or intermediate reagents. More specifically, though not exclusively, the present invention relates to a novel method for preparing a tetrafluoropropene by dehydrohalogenating a starting or intermediate tetrafluorochloropropane and/or pentafluoropropane material in the presence of a caustic solution at a temperature range greater than 40° C. and less than or equal to 80° C. | 11-03-2011 |
| 20110269999 | PROCESS FOR DEHYDROHALOGENATION OF HALOGENATED ALKANES - A process for the manufacture of halogenated olefins in semi-batch mode by dehydrohalogenation of halogenated alkanes in the presence of an aqueous base such as KOH which simultaneously neutralizes the resulting hydrogen halide. During the process, aqueous base is continuously added to the haloalkane which results in better yields, lower by-product formation and safer/more controllable operation. | 11-03-2011 |
| 20110269861 | SOLVENT COMPOSITIONS CONTAINING CHLOROFLUOROOLEFINS OR FLUOROOLEFINS - Compositions and methods based on the use of fluoroalkene containing from 3 to 4 carbon atoms and at least one carbon-carbon double bond, such as HFO-1214, HFO-HFO-1233, or HFO-1354, having properties highly beneficial in foaming and blowing agent applications, articles and methods. | 11-03-2011 |
| 20110269359 | ULTRA-HIGH STRENGTH UHMW PE FIBERS AND PRODUCTS - Multi-filament UHMW PE fibers can be produced according to processes that result in improved properties. The UHMW PE can have an intrinsic viscosity in decalin at 135° C. of at least about 30 dl/g, and can be processed under optimal conditions to achieve a gel spun fiber having a tenacity of greater than about 45 g/denier (40.5 g/dtex). | 11-03-2011 |
| 20110269082 | GAS PRESSURE CONTROL FOR WARM AIR FURNACES - Systems, methods, and controllers for controlling gas-fired appliances such as warm air furnaces are disclosed. An illustrative furnace system can include a burner unit in communication with a combustion air flow conduit and heat exchanger, a variable speed inducer fan or blower adapted to provide a flow of combustion air to the burner unit, a furnace controller and motor speed control unit adapted to regulate the speed of the inducer fan or blower, and a pneumatically modulated gas valve adapted to variably output gas pressure to the burner unit based at least in part on the combustion air flow. | 11-03-2011 |
| 20110268967 | PROCESS AND PRODUCT OF HIGH STRENGTH UHMW PE FIBERS - An improved process for solution spinning of ultra-high molecular weight polyethylene (UHMW PE) filaments, wherein the 10 wt % solution of the UHMW PE in mineral oil at 250° C. has a Cogswell extensional viscosity and a shear viscosity within select ranges. | 11-03-2011 |
| 20110268896 | ORGANIC FLUORESCENT COMPOSITIONS - A composition comprising an organic fluorophore having a structure of: | 11-03-2011 |
| 20110268584 | BLADES, TURBINE BLADE ASSEMBLIES, AND METHODS OF FORMING BLADES - Blades, turbine blade assemblies, and methods of forming blades are provided. The blade includes an airfoil including a convex suction side wall, a concave pressure side wall, a leading edge, a trailing edge, a root, and a tip, the convex suction side wall, the concave pressure side wall, and the tip each including interior surfaces that together define an internal cooling circuit, the airfoil including a single crystal superalloy, and a cladding layer disposed over the tip, the cladding layer including a zirconia grain stabilized platinum alloy. | 11-03-2011 |
