Patent application number | Description | Published |
20100083745 | Method of Dynamically Measuring Stiffness of a Wheel and Tire Assembly - A test machine and method for dynamically testing a tire/wheel assembly. A first laser measurement gage is directed to an inboard rim flange of the wheel to measure radial deflection of the tire/wheel assembly. A second laser measurement gage is directed to the inboard rim flange to measure axial deflection of the tire/wheel assembly. Displacement data and loading data are correlated to provide values for lateral stiffness, radial stiffness and ride stiffness. | 04-08-2010 |
20110081229 | METHOD FOR ATTACHING A CONNECTOR TO DEPOSITED MATERIAL - A method for attaching a connector to deposited material includes the steps of depositing material on a substrate using a thin- or thick-film deposition process and attaching at least one connector to the deposited material using a high energy beam welding process. | 04-07-2011 |
20120096933 | SENSOR WITH G-LOAD ABSORBING SHOULDER - A sensor is provided and includes a body disposed at a point of measurement interest on a rotor at a radial distance from a centerline thereof and having a substantially cylindrical shape and first and second opposing ends and a sensing end coupled to one of the first and second opposing ends, the other of the first and second opposing ends being coupled to a communication system, the sensing end including a sensing device configured to generate a signal reflective of a detected condition at the point of measurement interest, and at least one of the first and the second opposing ends being formed to define a shoulder portion for absorbing gravitational loading. | 04-26-2012 |
20120096934 | COMMUNICATION SYSTEM FOR TURBINE ENGINE - A communication system is provided and includes a sensor to measure a condition at a point of measurement interest defined on a rotor of a turbine at a radial distance from a centerline about which the rotor is rotatable, wiring disposed on the rotor at a radial distance from the centerline, the wiring including a first wiring section coupled to the sensor, a second wiring section and a first connection by which the first and second wiring sections are connectable, a second connection by which the second wiring section transmits a signal reflective of the detected condition to a non-rotating recording element and a temperature compensation module disposed on the second wiring section to adjust the signal. | 04-26-2012 |
20120096946 | SENSOR PACKAGING FOR TURBINE ENGINE - A turbine is provided and includes a rotor, which is rotatable about a centerline thereof, a sensor to measure a condition at a point of measurement interest defined on the rotor at a radial distance from the centerline, a communication system by which condition measurements are transmittable from the sensor to a non-rotating recording system and a probe holder to secure the sensor and a portion of the communication system on the rotor proximate to the point of measurement interest. | 04-26-2012 |
20120096961 | PROBE HOLDER FOR TURBINE ENGINE SENSOR - A turbine is provided and includes a component having a body, which is rotatable about a rotor centerline and which is formed to define a cavity radially proximate to a point of measurement interest defined at a radial distance from the centerline, a sensor to measure a condition at the point of measurement interest, a communication system by which condition measurements are transmittable from the sensor to a non-rotating recording system and a probe holder insertible into the cavity to secure the sensor proximate to the point of measurement interest. | 04-26-2012 |
20120128468 | SENSOR ASSEMBLY FOR USE WITH A TURBOMACHINE AND METHODS OF ASSEMBLING SAME - A method for assembling a sensor assembly for use with a turbomachine is provided. The method includes providing a cover that includes a first portion and a second portion that extends from the first portion. A cavity is defined within the first portion. Moreover, a sensing device that is configured to measure at least one variable of a component of the turbomachine is inserted into the cavity. The second portion is removably coupled to a surface of the turbomachine component such that the cover securely couples the sensing device to the turbomachine component. | 05-24-2012 |
20120171037 | PROBE ASSEMBLY FOR USE IN TURBINE ENGINES AND METHOD OF ASSEMBLING SAME - A method of assembling a probe assembly is provided. At least one probe is coupled to an annular tube, wherein the tube includes an interior surface and an exterior surface. The tube also includes at least one first opening that extends between the interior and exterior surfaces and at least one second opening that extends between the interior and exterior surfaces. Moreover, at least one annular flange is coupled to the tube. The flange has a substantially elliptical shape that facilitates substantially preventing the relative rotation of the tube. | 07-05-2012 |
20120285237 | INSTRUMENTATION RAKE ASSEMBLY - An instrumentation rake assembly comprises a rake tower capped at an immersed end and mated to a lead carrier at a base end. The rake tower comprises a curved wall oriented along a longitudinal axis and supporting a plurality of probe holders. The curved wall has an inner surface defining an internal passage for carrying instrumentation from the probe holders to the lead carrier. In another aspect, an instrumentation rake assembly comprises a plurality of rake towers, each having a base end and an immersed end, and each rake tower being coupled at its immersed end to one or more other rake towers. | 11-15-2012 |
20160061638 | FITTING FOR POSITIONING A PROBE IN A HOT GAS PATH OF A GAS TURBINE ENGINE - A fitting for positioning a probe in a hot gas path within a casing of a gas turbine engine is disclosed herein. The fitting may include a main body attachable to the casing opposite the hot gas path. The main body may include an internal bore and one or more cooling holes in communication with the internal bore. A compliant seal may be positionable within the internal bore. In addition, a follower may be positionable within the internal bore adjacent to the compliant seal. Moreover, the fitting may include a fastener configured to mate with the main body. In this manner, the follower may deform the compliant seal about the probe within the main body to secure and seal the probe within the main body. | 03-03-2016 |
20160064835 | SYSTEMS AND METHODS FOR SPLICING WIRES - A splicer device is disclosed herein. The splicer device includes a main body having an internal passage formed between a first end of the main body and a second end of the main body. The first end of the main body is configured to receive at least one first wire, and the second end of the main body is configured to receive at least one second wire. A window is disposed within the main body and in communication with the internal passage between the first end of the main body and the second end of the main body for accessing and splicing the at least one first wire and the at least one second wire. | 03-03-2016 |
20160084736 | SYSTEMS AND METHODS FOR ATTACHING A PROBE TO A CASING OF A GAS TURBINE ENGINE - A system for attaching a probe to a casing of a gas turbine engine is disclosed. The system may include a probe receptacle attachable to the casing. The probe receptacle may include an internal bore, a bayonet slot, a spring disposed within the internal bore adjacent to the bayonet slot, and a sealing surface within the internal bore. The system also may include a probe attachment assembly disposed about the probe and configured to engage the probe receptacle. The probe attachment assembly may include at least one bayonet positionable within the bayonet slot and a seal positionable adjacent to the sealing surface within the internal bore. | 03-24-2016 |
20160090860 | DAMPING SYSTEM FOR A TURBOMACHINE SLIP RING - A damping system for a turbomachine slip ring includes a slip ring assembly. The slip ring assembly includes a rotating component which is coupled at one end to a rotor shaft of the turbomachine and a stator component which circumferentially surrounds a rotatable center core portion of the rotating component. The system further includes a static structure which defines a carrier sleeve where the carrier sleeve circumferentially surrounds a portion of the stator component. The system also includes a damping material which extends radially between an inner surface of the carrier sleeve and an outer surface of the stator component so as to dissipate vibrational energy of the slip ring assembly during rotation of the rotor shaft. | 03-31-2016 |
20160100503 | SYSTEMS AND METHODS FOR COOLING A PROBE DISPOSED ABOUT A HOT GAS PATH - A system for cooling a probe disposed about a hot gas path is disclosed herein. The system may include a probe holder having a main body including an inner passage, an intermediate passage, and an outer passage. The intermediate passage and the outer passage may be in fluid communication. The probe may be disposed within the inner passage of the probe holder. The probe may include an internal passage. The system also may include a first cooling circuit in fluid communication with internal passage of the probe. Moreover, the system may include a second cooling circuit having an inlet in fluid communication with the intermediate passage and an outlet in fluid communication with the outer passage. | 04-07-2016 |
Patent application number | Description | Published |
20090162733 | FLOW FIELD PLATE FOR A FUEL CELL WITH FEATURES TO ENHANCE REACTANT GAS DISTRIBUTION - A flow field plate for a fuel cell includes features in the gas input area that enhance gas distribution to the flow field channels. The input area of the flow field plate directs gases from an input manifold to the flow field channels. The input area includes one or more input channels which are defined by input channel walls. One or more features are included within the input area to enhance the distribution of the gas to the flow field channels. The gas distribution enhancement features may provide support for a sealing element to reduce blockage of the channels and/or may provide a path for fluid communication between adjacent input channels. | 06-25-2009 |
20120123387 | HOLLOW MICRONEEDLE ARRAYS - The present disclosure relates to apparatus, assemblies, combinations, and methods for infusing fluids by hollow microneedles. | 05-17-2012 |
20130257278 | ELECTRICAL CONNECTORS FOR SOLID STATE LIGHT - A light having integrated light and thermal guides and separable electrical connectors. The light has a base for connection to a power supply, a light circuit electrically connected with solid state light sources such as LEDs, and a driver circuit for receiving power from the power supply and providing power to drive the light sources. A light guide is coupled to the light sources for receiving and distributing light from the light sources, and a thermal guide is integrated with the light guide for providing thermal conduction from the light source for cooling the light. The separable connectors include a first connector for providing an electrical connection between the driver circuit and light circuit, a second connector for providing an electrical connection between the power supply and driver circuit, and a third connector for providing a ground connection to the driver circuit. | 10-03-2013 |
20140243786 | DELIVERY SYSTEM FOR HOLLOW MICRONEEDLE ARRAYS - The present disclosure relates to systems and methods for delivering microneedles to a patient's skin. In one aspect, the present disclosure provides a system for delivering a microneedle array to a patient's skin surface, the system comprising: a delivery apparatus including a housing; and an infusion device detachably received in the housing. | 08-28-2014 |
20150202650 | DEVICES FOR COATING CONTOURED SURFACES - Provided are devices for coating ( | 07-23-2015 |