|
JPH03186601A
(ja)
*
|
1989-12-14 |
1991-08-14 |
Teijin Seiki Co Ltd |
電気油圧サーボ機構
|
|
US5274554A
(en)
*
|
1991-02-01 |
1993-12-28 |
The Boeing Company |
Multiple-voting fault detection system for flight critical actuation control systems
|
|
US5206810A
(en)
*
|
1991-02-07 |
1993-04-27 |
General Electric Company |
Redundant actuator control
|
|
US5087866A
(en)
*
|
1991-05-22 |
1992-02-11 |
Lucas Industries |
Temperature compensating circuit for LVDT and control system
|
|
US5493497A
(en)
*
|
1992-06-03 |
1996-02-20 |
The Boeing Company |
Multiaxis redundant fly-by-wire primary flight control system
|
|
JPH07245811A
(ja)
*
|
1994-03-04 |
1995-09-19 |
Honda Motor Co Ltd |
電動車両における制御装置
|
|
US5875818A
(en)
*
|
1994-09-23 |
1999-03-02 |
The Boeing Company |
Opto-electric/hydraulic servocactuation
|
|
US5719566A
(en)
*
|
1996-06-28 |
1998-02-17 |
Sundstrand Corporation |
Method and apparatus for detecting dormant actuator failure
|
|
DE19628395C2
(de)
*
|
1996-07-13 |
1998-06-04 |
Daimler Benz Aerospace Airbus |
System zur Regelung der Abluftmengenströme eines Flugzeuges
|
|
US5806805A
(en)
*
|
1996-08-07 |
1998-09-15 |
The Boeing Company |
Fault tolerant actuation system for flight control actuators
|
|
US5844390A
(en)
*
|
1997-01-27 |
1998-12-01 |
Cameron; Robert |
Method and apparatus for regulating a fluid operated machine
|
|
US6003811A
(en)
*
|
1997-03-24 |
1999-12-21 |
The Boeing Company |
Aircraft servovalve current rate limiter
|
|
FR2787759B1
(fr)
*
|
1998-12-28 |
2001-03-16 |
Aerospatiale |
Procede et systeme de commande d'une gouverne d'un aeronef a actionnement par verins hydrauliques multiples et a puissance modulable
|
|
US6513885B1
(en)
*
|
1999-05-14 |
2003-02-04 |
Hydro-Aire, Inc. |
Dual redundant active/active brake-by-wire architecture
|
|
DE19927372C2
(de)
*
|
1999-06-16 |
2003-06-18 |
Eads Deutschland Gmbh |
Verfahren und Vorrichtung zum Erkennen einer Fehlfunktion von Stellantrieben
|
|
DE10012405A1
(de)
*
|
2000-03-15 |
2001-09-20 |
Mannesmann Rexroth Ag |
Einrichtung zur Steuerung eines hydraulischen Aktuators
|
|
US6366837B1
(en)
|
2000-07-14 |
2002-04-02 |
Honeywell International Inc. |
Method for providing command augmentation to a command lane within a vehicle
|
|
US6561463B1
(en)
*
|
2000-07-14 |
2003-05-13 |
Honeywell International Inc. |
Flight control module with integrated spoiler actuator control electronics
|
|
US6446911B1
(en)
*
|
2000-07-14 |
2002-09-10 |
Honeywell International Inc. |
Method for controlling actuators on a vehicle
|
|
US6443399B1
(en)
|
2000-07-14 |
2002-09-03 |
Honeywell International Inc. |
Flight control module merged into the integrated modular avionics
|
|
US6618628B1
(en)
*
|
2000-10-05 |
2003-09-09 |
Karl A. Davlin |
Distributed input/output control systems and methods
|
|
DE10204553A1
(de)
*
|
2002-02-05 |
2003-08-14 |
Wabco Gmbh & Co Ohg |
Elektromagnetisch betätigbare Ventileinrichtung sowie Anordnung zur Ansteuerung einer solchen Ventileinrichtung
|
|
DE03734034T1
(de)
*
|
2002-05-16 |
2005-07-14 |
Bell Helicopter Textron, Inc., Fort Worth |
Integrierte dreifunktions-hydraulikventilbaugruppe
|
|
FR2850084B1
(fr)
*
|
2003-01-21 |
2005-12-30 |
Airbus France |
Procede et systeme de commande d'une gouverne d'aeronef.
|
|
BRPI0407491A
(pt)
|
2003-02-15 |
2006-02-14 |
Gulfstream Aerospace Corp |
métodos para redução da probabilidade de formação de trombose da veia profunda, para elevação de concentração de oxigênio atmosférico, e de concentração de nitrogênio, para monitoração de pressão parcial de oxigênio, para controle do grau de deslocamento de oxigênio/nitrogênio de ar de chegada em resposta à pressão parcial de oxigênio, para remisturar a atmosfera nas áreas ocupadas e não ocupadas da aeronave, para abaixamento da pressão parcial de oxigênio para abaixo do nìvel natural, e para ajuste de concentrações de nitrogênio e oxigênio no interior de regiões de uma aeronave
|
|
US7689383B2
(en)
*
|
2003-11-20 |
2010-03-30 |
The Boeing Company |
Component health assessment for reconfigurable control
|
|
FR2864024B1
(fr)
*
|
2003-12-22 |
2006-04-07 |
Messier Bugatti |
Procede de gestion d'une architecture de systeme de freinage d'aeronef, et architecture de systeme de freinage faisant application
|
|
US20100318245A1
(en)
*
|
2005-03-03 |
2010-12-16 |
Nabtesco Corporation |
Flight control system
|
|
US7789345B2
(en)
*
|
2005-03-03 |
2010-09-07 |
Nabtesco Corporation |
Actuator control apparatus
|
|
DE102005042511A1
(de)
*
|
2005-09-07 |
2007-04-05 |
Airbus Deutschland Gmbh |
Trimmaktuator-Betätigungssystem für einen hydraulisch betätigbaren Trimmable Horizontal Stabilizer Actuator
|
|
WO2007084529A2
(en)
*
|
2006-01-17 |
2007-07-26 |
Gulfstream Aerospace Corporation |
System and method for an integrated backup control system
|
|
JP2009523658A
(ja)
*
|
2006-01-17 |
2009-06-25 |
ガルフストリーム・エアロスペース・コーポレイション |
分散型飛行制御システムのバックアップ制御のための装置及び方法
|
|
US7424642B2
(en)
*
|
2006-04-24 |
2008-09-09 |
Gm Global Technology Operations, Inc. |
Method for synchronization of a controller
|
|
GB0616730D0
(en)
*
|
2006-08-23 |
2006-10-04 |
Airbus Uk Ltd |
Jam-tolerant actuator
|
|
WO2008079038A1
(en)
*
|
2006-12-25 |
2008-07-03 |
Otkrytoe Aktsionernoe Obschestvo 'opytno-Konstruktorskoe Byuro Im. A.S. Yakovleva' |
Light multipurpose aircraft provided with a control integrated system
|
|
EP2156256A2
(de)
|
2007-04-05 |
2010-02-24 |
Bombardier Inc. |
Seriell redundantes einkanaliges mehrwege-fly-by-wire-flugsteuersystem mit mehreren achsen
|
|
FR2927308B1
(fr)
*
|
2008-02-08 |
2010-10-22 |
Airbus France |
Systeme distribue de commande de vol.
|
|
US8955365B2
(en)
*
|
2008-12-23 |
2015-02-17 |
Embraer S.A. |
Performance monitoring and prognostics for aircraft pneumatic control valves
|
|
FR2941551B1
(fr)
|
2009-01-28 |
2011-06-03 |
Airbus France |
Circuit electronique de determination d'une donnee representative d'un parametre de l'air et systeme comprenant un tel circuit
|
|
US8594852B2
(en)
*
|
2010-02-22 |
2013-11-26 |
Eaton Corporation |
Device and method for controlling a fluid actuator
|
|
JP5590955B2
(ja)
*
|
2010-04-26 |
2014-09-17 |
ナブテスコ株式会社 |
アクチュエータ制御システム
|
|
US8534599B2
(en)
|
2011-03-31 |
2013-09-17 |
Hamilton Sundstrand Corporation |
Redundant two stage electro-hydraulic servo actuator control
|
|
US8620522B2
(en)
|
2011-05-25 |
2013-12-31 |
The Boeing Company |
Suppressing electrical failure effects in servo control systems
|
|
US9625894B2
(en)
*
|
2011-09-22 |
2017-04-18 |
Hamilton Sundstrand Corporation |
Multi-channel control switchover logic
|
|
CN103303466B
(zh)
*
|
2012-03-09 |
2016-03-30 |
陕西飞机工业(集团)有限公司 |
一种飞机舵面锁防差错电气控制方法及其系统
|
|
CN102662383B
(zh)
*
|
2012-05-29 |
2014-11-19 |
张二浩 |
用于控制链条系统的控制链条实现方法
|
|
JP6178587B2
(ja)
*
|
2013-02-28 |
2017-08-09 |
三菱航空機株式会社 |
航空機のアクチュエータ装置、及び、航空機
|
|
FR3009581B1
(fr)
*
|
2013-08-09 |
2015-09-25 |
Snecma |
Procede de surveillance d'une vanne d'un moteur d'aeronef
|
|
WO2015051294A1
(en)
*
|
2013-10-03 |
2015-04-09 |
Transocean Innovation Labs, Ltd. |
Hydraulic devices and methods of actuating same
|
|
KR101530181B1
(ko)
*
|
2014-12-09 |
2015-06-22 |
국방과학연구소 |
가상 제어 구조를 갖는 다중화 구동 제어시스템
|
|
US9563523B2
(en)
*
|
2015-04-16 |
2017-02-07 |
GM Global Technology Operations LLC |
Architecture for scalable fault tolerance in integrated fail-silent and fail-operational systems
|
|
EP3424821B1
(de)
|
2016-02-29 |
2021-01-27 |
SZ DJI Technology Co., Ltd. |
Drosselsteuersignalverarbeitungsverfahren, elektronischer drehzahlregler, steuergerät und mobile plattform
|
|
CN106774367B
(zh)
*
|
2016-12-27 |
2020-05-15 |
歌尔股份有限公司 |
一种飞行器的冗余控制方法
|
|
US10759520B2
(en)
*
|
2017-09-29 |
2020-09-01 |
The Boeing Company |
Flight control system and method of use
|
|
CN109407631B
(zh)
*
|
2018-09-29 |
2020-09-22 |
珠海格力电器股份有限公司 |
输入负载信息的处理方法、装置、机组和存储介质
|
|
CN109991841B
(zh)
*
|
2019-03-27 |
2022-04-05 |
西安联飞智能装备研究院有限责任公司 |
飞行控制计算系统及控制信号输出方法、装置和存储介质
|
|
JP6772341B2
(ja)
*
|
2019-07-01 |
2020-10-21 |
トランスオーシャン イノベーション ラブス リミテッド |
液圧デバイスおよびそれを作動する方法
|
|
US11572901B2
(en)
*
|
2020-03-16 |
2023-02-07 |
Woodward, Inc. |
Redundant electrohydraulic positioning control system
|
|
KR20260103120A
(ko)
*
|
2023-10-30 |
2026-07-02 |
위스크 에어로 엘엘씨 |
명령 모니터 백업 제어 아키텍처
|