[특허]Flight control module merged into the integrated modular avionics

[미국특허] Flight control module merged into the integrated modular avionics 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64C-013/00
출원번호	US-0616196 (2000-07-14)
발명자 / 주소	Larry Yount John Todd
출원인 / 주소	Honeywell International Inc.
인용정보	피인용 횟수 : 47 인용 특허 : 12

초록 ▼

In an aircraft using fly-by-wire technology, the flight control functions have been integrated into the integrated modular avionics ("IMA"). The new flight control module ("FCM") resides on the same data bus as the other modules in the IMA and receives power from the same power supply. In addition, the FCM is also connected to a separate power supply to add redundancy to the system. Several benefits arise from this configuration of an FCM. There is no longer a separate chassis needed for the flight control functions, thus resulting in a reduction in weight. In addition, the FCM now has access to all of the data on the IMA bus, instead of a limited amount of data over an ARINC 629 bus. The FCM provides augmentation signals to the actuator control electronics ("ACE") to aid in the flying of the aircraft. In the event of a failure of the FCM, the ACE still provides enough control to fly the airplane.

대표청구항 ▼

1. An fly-by-wire control system comprising,an integrated modular avionics unit; an actuator control electronics system; a hydraulic actuator; wherein said integrated modular avionics comprises a power supply; a processor; a plurality of inputs accepting sensor data from various sensors located throughout an aircraft; and a flight control module configured to process incoming flight control data and output various flight control data, wherein said flight control module is coupled to an actuator control electronics system which is external to said flight control module; and said actuator control electronics system is configured to operate a hydraulic actuator coupled to one primary flight control surface.

이 특허에 인용된 특허 (12) 인용/피인용 타임라인 분석

El Sherif Fouad (Valencia CA) Svoboda Harry J. (Granada Hills CA), Electrohydraulic control module.
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Elbert Ralph P. ; Hafner Michael A., Fault tolerant actuation system for flight control actuators.
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Le Dong Tuan (Lakewood CA) Huggett Colin E. (Torrance CA), Fault tolerant controller arrangement for electric motor driven apparatus.
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Takats Imre J. (Bellevue WA), Flight control system employing three controllers operating a dual actuator.
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Takats Imre J. (Bellevue WA) Aziz George W. (Seattle WA), Flight control system employing two dual controllers operating a dual actuator.
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Chenoweth Charles C. (Renton WA) Takats Imre J. (Bellevue WA), Fly-by-wire lateral control system.
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Bothe Hans-Jurgen,CAX, Hybrid aircraft.
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Morgan Earl ; Ligon Robert ; Seger Mark, Integrated electric power system.
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Pelton, Scott L., Pitch attitude command flight control system for landing flare.
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Garnjost Kenneth D. (Orchard Park NY), Pressure equalization of multiple valves.
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Avis William D. (Costa Mesa CA), Redundant servo with fail-safe electric system.
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Traverse Pascal (Tournefeuille FRX) Le Tron Xavier (Toulouse FRX), System for control of an aerodynamic surface of an aircraft.
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이 특허를 인용한 특허 (47) 인용/피인용 타임라인 분석

Turung, Brian E., Airplane emergency navigational system.
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Hirvonen, Jukka Matti, Apparatus and method for backup control in a distributed flight control system.
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Hirvonen, Jukka Matti, Apparatus and method for backup control in a distributed flight control system.
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Boorman, Daniel J.; Griffin, III, John C.; Gunn, Peter D.; Mumaw, Randall J., Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information.
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Boorman, Daniel J.; Griffin, III, John C.; Gunn, Peter D.; Mumaw, Randall J., Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information.
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Boorman, Daniel J.; Griffin, III, John C.; Gunn, Peter D.; Mumaw, Randall J., Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information.
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Boorman, Daniel J.; Griffin, III, John C.; Gunn, Peter D.; Mumaw, Randall J., Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information.
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Boorman, Daniel J.; Griffin, III, John C.; Gunn, Peter D.; Mumaw, Randall J., Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information.
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Boorman,Daniel J.; Griffin, III,John C.; Gunn,Peter D.; Mumaw,Randall J., Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information.
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Boorman, Daniel J.; Gunn, Peter D.; Griffin, III, John C., Apparatuses and methods for displaying autoflight information.
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Boorman, Daniel J.; Gunn, Peter D.; Griffin, III, John C., Apparatuses and systems for controlling autoflight systems.
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Knotts, Louis H.; Ohmit, Eric E., Autonomous outer loop control of man-rated fly-by-wire aircraft.
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Belkadi, Jean-Francois; Ambroise, Richard, Device for determining the position of a throttle lever in an aircraft.
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Clark, Samuel T.; Johnson, Keith L.; Neff, Andrew D.; Bowe, Roglenda R., Display of taxi route control point information.
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Fervel, Marc; Lecanu, Arnaud; Maussion, Antoine; Aubert, Jean-Jacques, Distributed flight control system implemented according to an integrated modular avionics architecture.
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Saint-Marc, Laurent; Brunel, Luc; Zaccaria, Patrick; Alexandre, Matthieu; Feau, Julien; Leborgne, Frédéric; Immordino, Thierry; Belkadi, Jean-François; Durand, Nathalie, FADEC and avionic component distributed architecture.
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Mottura, Alain, Flight control system for aircraft and test for testing such a flight control system.
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Yeh, Ying Chin, High integrity and availability multi-channel systems.
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Mitani, Yoichi; Tamaru, Masahiro; Ikarashi, Reiichi; Isobe, Taisei, Integrated electronic system mounted on aircraft.
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Sahasrabudhe, Vineet; Wulff, Ole, Life improving flight control system.
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Yount, Larry J.; Kelley, Gerald B.; Stange, Kent A.; Pond, Welsh C., Limited authority and full authority mode fly-by-wire flight control surface actuation control system.
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Sikora,Joseph A., Method and apparatus for displaying aircraft engine characteristics.
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Yeh,Ying Chin, Method and apparatus for obtaining high integrity and availability in multi-channel systems.
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Johansson, Rikard, Method, an electrical system, a digital control module, and an actuator control module in a vehicle.
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Griffin, III,John C.; Sandell,Gordon R. A.; Gunn,Peter D.; Pullen,Charles A.; Wiedemann,John, Methods and systems for automatically displaying information, including air traffic control instructions.
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Tafs, William D.; Griffin, III, John C., Methods and systems for automatically tracking information during flight.
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Crane,Jean M.; Green,David A.; Wiedemann,John, Methods and systems for controlling the display of information at an aircraft flight deck.
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Sikora,Joseph A.; Wiedemann,John, Methods and systems for displaying aircraft engine characteristics.
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Gunn, Peter D.; Griffin, III, John C., Methods and systems for displaying assistance messages to aircraft operators.
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Gunn,Peter D.; Wiedemann,John; Griffin, III,John C.; Hammack,Jason L., Methods and systems for displaying the source of aircraft control instructions.
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Mumaw,Randall J.; Boorman,Daniel J.; Bresley,William M.; Griffin, III,John C.; Gunn,Peter D., Methods and systems for graphically displaying sources for and natures of aircraft flight control instructions.
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Seve,Philippe, Process and device for the optimization of the deflection of the spoiler flaps of an aircraft in flight.
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Geary, Robert; Stevenson, Jason Marc, System and method for aircraft cabin atmospheric composition control.
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Hirvonen, Jukka Matti; Palfreyman, Gary, System and method for an integrated backup control system.
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Hirvonen, Jukka Matti; Palfreyman, Gary, System and method for an integrated backup control system.
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Clark, Samuel T.; Bowe, Roglenda R.; Jones, Wayne R., System and method for taxi route entry parsing.
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Moody, Larry A., System, autopilot supplement assembly and method for increasing autopilot control authority.
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Sandell,Gordon R. A.; Griffin, III,John C.; Gunn,Peter D.; Pullen,Charles A., Systems and methods for handling aircraft information received from an off-board source.
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Chen, Sherwin S.; Gunn, Peter D.; Wiedemann, John, Systems and methods for handling the display and receipt of aircraft control information.
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Chen, Sherwin S.; Gunn, Peter D.; Wiedemann, John, Systems and methods for handling the display and receipt of aircraft control information.
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Chen, Sherwin S.; Gunn, Peter D.; Wiedemann, John, Systems and methods for handling the display and receipt of aircraft control information.
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Chen,Sherwin S.; Gunn,Peter D.; Wiedemann,John, Systems and methods for handling the display and receipt of aircraft control information.
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Hamasaki, George H.; Sikora, Joseph A.; Kesterson, Bryan P.; Owens, Gregory P.; Hale, Justin E.; Kirby, Norman F.; Herter, Thanh Ha N.; McAvoy, Michael B.; Nguyen, Phuoc D.; Crane, Robert J., Systems and methods for monitoring and controlling circuit breakers.
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Boorman, Daniel J.; Bresley, William M.; Griffin, III, John C.; Gunn, Peter D.; Mumaw, Randall J., Systems and methods for presenting and obtaining flight control information.
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Boorman,Daniel J.; Bresley,William M.; Griffin, III,John C.; Gunn,Peter D.; Mumaw,Randall J., Systems and methods for presenting and obtaining flight control information.
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Curtis, Sydney Robert, Universal multi-role aircraft protocol.
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Curtis, Sydney Robert, Universal multi-role aircraft protocol.
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A	생활필수품
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A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

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[미국특허] Flight control module merged into the integrated modular avionics 원문보기