Patent application number | Description | Published |
20100128555 | SYSTEMS AND METHODS FOR MATERIAL BLENDING AND DISTRIBUTION - Systems and methods for mixing pure feed materials utilizes a first and a second compressible volume, such as defined in first and second liner-based containers adapted for pressure dispensation, wherein such materials are supplied to a mixing apparatus (e.g., reversible-flow or circulatable flow apparatus) adapted to form and maintain a mixture or suspension. Multiple redundant groups of containers may be used to enable mixing of contents of one group while contents of another group are being dispensed, to provide uninterrupted delivery of feed material to a process. Sensors adapted to generate signals indicative of flow, weight/mass, particle size distribution, concentration, and other material properties may be provided. | 05-27-2010 |
20110008964 | SYSTEMS AND METHODS FOR DELIVERY OF FLUID-CONTAINING PROCESS MATERIAL COMBINATIONS - Common sources of different (e.g., concentrated) process materials are controllably supplied to multiple blending manifolds associated with multiple process tools, processing stations, or other points of use, to create an independently controllable process material blend for each tool, station, or point of use. Multi-constituent process materials may be circulated from a supply container through a blending manifold to a return container to ensure homogeneity until immediately prior to blending and use. Such containers may include liner-based containers adapted for pressure dispensation. | 01-13-2011 |
20120138631 | FLUID PROCESSING SYSTEMS AND METHODS - Systems and methods for delivering fluid-containing feed materials to process equipment are disclosed. A liner-based pressure dispensing vessel is subjected to filling by application of vacuum between the liner and overpack. Multiple feed material flow controllers of different calibrated flow ranges may be selectively operated in parallel for a single feed material. Feed material blending and testing for scale-up may be performed with feed materials supplied by multiple liner-based pressure dispensing containers. A gravimetric system may be used to determine concentration of at least one component of a multi-component solution or mixture. | 06-07-2012 |
Patent application number | Description | Published |
20120310524 | METHODS AND SYSTEMS FOR DISPLAYING PROCEDURE INFORMATION ON AN AIRCRAFT DISPLAY - Methods and systems are provided for presenting information on a display device associated with an aircraft. An exemplary method involves displaying a navigational map on the display device, obtaining status information for the aircraft, determining an amount of procedure information to be displayed based at least in part on the status information, and displaying the determined amount of aircraft procedure information on the display device overlying the navigational map. The procedure information prescribes operation of the aircraft during execution of an aircraft procedure. | 12-06-2012 |
20130035848 | SYSTEM AND METHOD FOR DISPLAYING A PROCEDURE TO AN AIRCREW MEMBER - A system and method is disclosed for displaying a procedure to an aircrew member of an aircraft. The system includes, but is not limited to, a moving map display, a position detecting unit, a flight management system, an electronic storage unit for storing navigation procedures associated with geographic locations, and a processor coupled with the moving map display, the position detecting unit, the flight management system, and the electronic storage unit. The processor is configured to receive a current location of the aircraft from the position determining unit and a flight path from the flight management system, to retrieve a navigation procedure from the electronic storage unit corresponding to the current location and the flight path of the aircraft, and to command the moving map display to display a graphic depiction of the flight path. | 02-07-2013 |
20130057414 | ELECTRIC TAXI SYSTEM GUIDANCE - A taxi guidance system is provided for an aircraft having a primary thrust engine and an onboard electric taxi system. The taxi guidance system includes or cooperates with a source of aircraft status data for the aircraft, and a source of airport feature data associated with synthetic graphical representations of an airport field. The taxi guidance system includes a processor operatively coupled to the source of aircraft status data and to the source of airport feature data to generate, in response to at least the aircraft status data and the airport feature data, taxi path guidance information for the aircraft, start/stop guidance information associated with operation of the primary thrust engine, and speed guidance information for the onboard electric taxi system. The processor generates image rendering display commands that can be received by a display system to render a dynamic synthetic representation of the airport field that includes graphical indicia of the taxi path guidance information, the start/stop guidance information, and the speed guidance information. | 03-07-2013 |
20130131888 | SYSTEM AND METHOD FOR GENERATING AND DISPLAYING AN ELECTRIC TAXI INDEX - A taxi method for an aircraft having a primary thrust engine taxi system and an electric taxi system is provided. The method involves obtaining aircraft and airport status data and generating therefrom taxi drive information indicative of the relative cost of taxiing the aircraft along a predetermined route using the electric taxi system versus the aircraft engine taxi system. The taxi drive index information is presented to a user. | 05-23-2013 |
20130297102 | ELECTRIC TAXI AUTO-GUIDANCE AND CONTROL SYSTEM - An auto-guidance and control method and system is provided for use in conjunction with an aircraft electric taxi system. Aircraft status data is obtained, and airport feature data accessed. A processor generates taxi path guidance and control information including at least taxi speed guidance information, and sends commands derived from the taxi speed guidance information by the processor directly to an electric taxi controller to regulate the taxi speed of the aircraft. | 11-07-2013 |
20140067169 | ELECTRIC TAXI AUTO-GUIDANCE AND CONTROL SYSTEM - An auto-guidance and control method and system are provided for use in conjunction with an aircraft electric taxi system, wherein electric taxi guidance may be performed in a manual mode by a crew or in an auto-mode by an auto-guidance and control system. First, aircraft status data and airport feature data are accessed. A processor, in response to at least the aircraft status data and the airport feature data, generates taxi guidance information and renders the taxi guidance information on a display. A guidance route is manually navigated utilizing guidance information on the display in the manual mode. In the auto mode, taxi-path commands, generated by the processor, are applied to taxi path guidance controllers in the auto-mode. | 03-06-2014 |
20140114557 | HIGH INTEGRITY, SURFACE GUIDANCE SYSTEM FOR AIRCRAFT ELECTRIC TAXI - A high-integrity auto-guidance and control method for use in conjunction with an aircraft electric taxi drive system comprises obtaining taxi path data generating in a plurality of processors taxi path guidance and control information from the taxi path guidance data, and sending commands derived from the taxi path guidance and control information from one of the plurality of processors based on a predetermined priority scheme to at least one electric taxi controller. | 04-24-2014 |
20140337796 | METHODS AND SYSTEMS FOR SELECTING A DISPLAYED AIRCRAFT APPROACH OR DEPARTURE - A system and method are provided for highlighting and selecting one of a plurality of graphical IFR procedure depiction on an aircraft display. A displayed legend includes a plurality of textual procedure identifications, one each for each of the graphical IFR procedure depictions. Movement of a cursor over either a graphical IFR procedure depiction or a textual procedure identification highlights both, and selection thereof removes all other graphical IFR procedure depictions and textual procedure identifications from being displayed. | 11-13-2014 |
20150134149 | PILOT INTERFACE FOR AIRCRAFT ELECTRIC TAXI SYSTEM - A pilot interface panel may comprise at least one input mechanism configured to receive at least one user input, generate at least one input signal corresponding to the at least one user input, and send the at least one input signal to a controller. The controller may be configured to control movement of an electric taxi system of an aircraft in a manner according to the at least one input signal, wherein the electric taxi system may be configured to rotate at least one wheel of the aircraft by force from a purely electromotive source. The pilot interface panel may further comprise at least one safety mechanism, which may be configured to prevent at least one of the at least one input mechanisms from receiving an inadvertent user input resulting from an unintended action by the user. | 05-14-2015 |
20150183511 | CONTROL PANEL INTEGRATION INTO AIRCRAFT THROTTLE CONTROL - A lever control system integrates taxi operation using an electric motor in an aircraft with speed control of a jet engine in the same aircraft. The lever control system provides a smooth transition between the electric motor system used for aircraft taxi operation, and a jet engine system used to fly the aircraft. The lever control system may include a reverse lockout mechanism to prevent unintended reverse taxi movement of the aircraft. | 07-02-2015 |
20150210383 | ELECTRIC TAXI SYSTEM WITH SPEED CONTROL (ETSSC) - An electric taxi system (ETS) for an aircraft may include a ground speed sensor, a speed selection unit and a speed computer coupled to the ground speed sensor and to the speed selection unit. The speed computer may produce a speed error signal. A motor controller coupled to a wheel motor may control speed of the wheel motor responsively to the speed error signal. | 07-30-2015 |