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특허 상세정보

Avionic control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G06F-015/50   
미국특허분류(USC) 364/424 ; 364/187 ; 364/434 ; 318/564
출원번호 US-0754330 (1985-07-12)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 38  인용 특허 : 6
초록

An all-electric powered flight control system for an aircraft incorporating fault-tolerant avionics combined with a redundant power actuation control system utilizing electro-mechanical devices for actuating aerodynamic control surfaces; and wherein, the redundancy is implemented through the division of the total aerodynamic surface area to be actuated into multi-segments, with each control segment having its own channel in the avionic control system. The avionic control system is effective in minimizing the effects of power actuated control loads reacti...

대표
청구항

An avionic control system for an aerodynamic vehicle, comprising: a flight control surface divided into a plurality of flight control surface segments, each control surface segment being independently mounted for angular movement about a hinge axis; a power actuator for each said control surface segment, connected adjacent to each said control surface segment for independent angular movement thereof; a manually operable controller for generating a first signal related to direction and magnitude of displacement of said controller; air data sensing means i...

이 특허를 인용한 특허 피인용횟수: 38

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  24. Bernard, Guy. Hydrostatic sidestick coupling. USP2003066572055.
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  26. Goupil, Philippe; Dayre, Rémy; Le Berre, Hervé; Gheorghe, Anca; Zolghadri, Ali; Cieslak, Jérôme; Henry, David. Method and device for detecting the jamming of an aircraft control surface. USP2014068755956.
  27. Peyrucain, Eric; Rouquette, Patrice; Jourdan, Christophe. Method and device to assist in the piloting of an aircraft in a non-precision approach during a landing phase. USP2010047690603.
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  29. Vos, David W.. Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation. USP2005026859689.
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  31. Fervel, Marc; Gentilhomme, Alexandre. More electric flight control system onboard an aircraft. USP2014068740155.
  32. Lin, Shu; Smith, Timothy; De Serres, Pierre. Multi-axis serially redundant single channel, multi-path fly-by wire flight control system. USP2017019533751.
  33. Shehu, Edvin. Multiphase buck converter controller without PID compensator or compensated error amplifier in the control loop. USP2016039293993.
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  35. Noll, Christopher; Avritch, Steven A.. Redundant two stage electro-hydraulic servo actuator control. USP2013098534599.
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  37. Ausman, Marc; DeVries, Kevin; Dostal, Jake. Variable speed flap retraction and notification. USP2013018346409.
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