DE60105815D1 - Flugsteuereinheit mit integrierter spoilerantriebsteuerelektronik - Google Patents

Flugsteuereinheit mit integrierter spoilerantriebsteuerelektronik

Info

Publication number
DE60105815D1
DE60105815D1 DE60105815T DE60105815T DE60105815D1 DE 60105815 D1 DE60105815 D1 DE 60105815D1 DE 60105815 T DE60105815 T DE 60105815T DE 60105815 T DE60105815 T DE 60105815T DE 60105815 D1 DE60105815 D1 DE 60105815D1
Authority
DE
Germany
Prior art keywords
spoiler
ace
fcm
flight control
control
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
DE60105815T
Other languages
English (en)
Other versions
DE60105815T2 (de
Inventor
Larry Yount
John Todd
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Honeywell International Inc
Original Assignee
Honeywell International Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Honeywell International Inc filed Critical Honeywell International Inc
Publication of DE60105815D1 publication Critical patent/DE60105815D1/de
Application granted granted Critical
Publication of DE60105815T2 publication Critical patent/DE60105815T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/12—Adjustable control surfaces or members, e.g. rudders surfaces of different type or function being simultaneously adjusted
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B64C9/323—Air braking surfaces associated with wings
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
DE60105815T 2000-07-14 2001-07-13 Flugsteuereinheit mit integrierter spoilerantriebsteuerelektronik Expired - Fee Related DE60105815T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US616195 2000-07-14
US09/616,195 US6561463B1 (en) 2000-07-14 2000-07-14 Flight control module with integrated spoiler actuator control electronics
PCT/US2001/022210 WO2002006909A2 (en) 2000-07-14 2001-07-13 Flight control module with integrated spoiler actuator control electronics

Publications (2)

Publication Number Publication Date
DE60105815D1 true DE60105815D1 (de) 2004-10-28
DE60105815T2 DE60105815T2 (de) 2005-10-13

Family

ID=24468408

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60105815T Expired - Fee Related DE60105815T2 (de) 2000-07-14 2001-07-13 Flugsteuereinheit mit integrierter spoilerantriebsteuerelektronik

Country Status (6)

Country Link
US (1) US6561463B1 (de)
EP (1) EP1301835B1 (de)
JP (1) JP2004504209A (de)
AT (1) ATE277376T1 (de)
DE (1) DE60105815T2 (de)
WO (1) WO2002006909A2 (de)

Families Citing this family (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0127254D0 (en) * 2001-11-13 2002-01-02 Lucas Industries Ltd Aircraft flight surface control system
WO2003071228A2 (en) * 2002-02-19 2003-08-28 Jeppesen Sanderson, Inc. Airport taxway navigation system
US20040059474A1 (en) 2002-09-20 2004-03-25 Boorman Daniel J. Apparatuses and methods for displaying autoflight information
US6892982B2 (en) * 2003-01-29 2005-05-17 Northrop Grumman Corporation Aircraft with forward opening inlay spoilers for yaw control
WO2004074094A2 (en) 2003-02-15 2004-09-02 Gulfstream Aerospace Corporation System and method for aircraft cabin atmospheric composition control
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
FR2866627B1 (fr) * 2004-02-24 2006-05-05 Airbus France Procede et dispositif pour l'optimisation du braquage des volets deporteurs d'un aeronef en vol
US7357358B2 (en) * 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
US7494094B2 (en) 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7789345B2 (en) * 2005-03-03 2010-09-07 Nabtesco Corporation Actuator control apparatus
US20100318245A1 (en) * 2005-03-03 2010-12-16 Nabtesco Corporation Flight control system
US7300021B2 (en) * 2005-05-20 2007-11-27 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7367530B2 (en) * 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
US7709210B2 (en) * 2005-10-05 2010-05-04 Children's Hospital Medical Center Diagnosis and prevention of fetal heart disease
US7475854B2 (en) 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
BRPI0706613A2 (pt) * 2006-01-17 2011-04-05 Gulfstream Aerospace Corp aparelho e método para controle de backup em um sistema de controle de vÈo distribuìdo
EP1977292A2 (de) * 2006-01-17 2008-10-08 Gulfstream Aerospace Corporation System und verfahren für ein integriertes backup-steuerungssystem
GB2435246A (en) * 2006-02-17 2007-08-22 Decoma U K Ltd Spoiler
CA2683132C (en) 2007-04-05 2013-10-29 Bombardier Inc. Multi-axis serially redundant, single channel, multi-path fly-by-wire flight control system
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US7840316B2 (en) * 2007-12-17 2010-11-23 Honeywell International Inc. Limited authority and full authority mode fly-by-wire flight control surface actuation control system
US7822493B2 (en) * 2008-01-03 2010-10-26 The Boeing Company Control system actuation fault monitoring
US8180562B2 (en) * 2008-06-04 2012-05-15 The Boeing Company System and method for taxi route entry parsing
US8386167B2 (en) 2008-11-14 2013-02-26 The Boeing Company Display of taxi route control point information
FR2942612B1 (fr) * 2009-03-02 2012-09-28 Airbus France Procede et dispositif d'optimisation automatique au sol de la configuration aerodynamique d'un avion
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
EP2296064B1 (de) * 2009-09-10 2019-04-24 Sikorsky Aircraft Corporation Leben verbesserndes Flugsteuerungssystem
US8935015B2 (en) 2011-05-09 2015-01-13 Parker-Hannifin Corporation Flight control system with alternate control path
US8712606B2 (en) * 2012-04-27 2014-04-29 The Boeing Company System and method for configuring a direct lift control system of a vehicle
JP6097596B2 (ja) * 2013-02-28 2017-03-15 三菱航空機株式会社 グランドスポイラの駆動システム、及び、航空機
US10183738B2 (en) * 2014-04-08 2019-01-22 Marc Arnold Flight control augmentation system and method for high aspect ratio aircraft including motorglider aircraft, optionally piloted vehicles (OPVs) and unpiloted air vehicles (UAVs)
US10759520B2 (en) 2017-09-29 2020-09-01 The Boeing Company Flight control system and method of use
US10940939B2 (en) 2017-12-11 2021-03-09 Textron Innovations, Inc. Ground spoiler control architecture for aircraft
EP3650336A1 (de) * 2018-11-12 2020-05-13 Goodrich Actuation Systems SAS Trimsteuerungssystem
CN109582033B (zh) * 2018-11-28 2022-02-08 中国航空工业集团公司西安飞行自动控制研究所 一种民机电传飞控计算机控制模式转换方法
US11260959B2 (en) * 2019-07-16 2022-03-01 Gulfstream Aerospace Corporation Integrated thrust and drag control of an aircraft

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3945593A (en) * 1972-10-10 1976-03-23 Bodenseewerk Geratetechnik Gmbh Flight control apparatus
US4087065A (en) 1977-02-04 1978-05-02 The Boeing Company Electrical control system for actuating inboard spoilers on aircraft
US4272046A (en) 1979-08-17 1981-06-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Hydraulic actuator mechanism to control aircraft spoiler movements through dual input commands
US4363098A (en) * 1980-06-24 1982-12-07 The Boeing Company Electric command spoiler system
US4472780A (en) * 1981-09-28 1984-09-18 The Boeing Company Fly-by-wire lateral control system
US4567813A (en) 1982-05-06 1986-02-04 Moog Inc. Pressure equalization of multiple valves
FR2557854B1 (fr) * 1984-01-09 1987-01-23 Aerospatiale Systeme de commandes de vol pour aeronef
US4807516A (en) * 1987-04-23 1989-02-28 The Boeing Company Flight control system employing three controllers operating a dual actuator
US4887214A (en) 1987-10-27 1989-12-12 The Boeing Company Flight control system employing two dual controllers operating a dual actuator
US5036469A (en) 1989-03-02 1991-07-30 The Boeing Company Pitch attitude command flight control system for landing flare
FR2686310B1 (fr) 1992-01-20 1994-04-08 Aerospatiale Ste Nationale Indle Systeme pour la commande d'une surface aerodynamique d'un aeronef.
US5493497A (en) * 1992-06-03 1996-02-20 The Boeing Company Multiaxis redundant fly-by-wire primary flight control system
US5714948A (en) * 1993-05-14 1998-02-03 Worldwide Notifications Systems, Inc. Satellite based aircraft traffic control system
JP3168448B2 (ja) * 1994-07-08 2001-05-21 川崎重工業株式会社 ディジタル飛行制御システム
US5670856A (en) 1994-11-07 1997-09-23 Alliedsignal Inc. Fault tolerant controller arrangement for electric motor driven apparatus
US5806805A (en) 1996-08-07 1998-09-15 The Boeing Company Fault tolerant actuation system for flight control actuators
FR2756252B1 (fr) 1996-11-22 1999-01-22 Eurocopter France Systeme de commande de vol pour aeronef a voilure tournante, notamment pour un helicoptere

Also Published As

Publication number Publication date
EP1301835B1 (de) 2004-09-22
DE60105815T2 (de) 2005-10-13
EP1301835A2 (de) 2003-04-16
JP2004504209A (ja) 2004-02-12
WO2002006909A3 (en) 2002-10-03
WO2002006909A2 (en) 2002-01-24
US6561463B1 (en) 2003-05-13
ATE277376T1 (de) 2004-10-15

Similar Documents

Publication Publication Date Title
DE60105815D1 (de) Flugsteuereinheit mit integrierter spoilerantriebsteuerelektronik
DE60108637D1 (de) Flugsteuerungsmodule, eingebaut in die integrierte modulare avionik
WO2007011408A3 (en) High-lift distributed active flow control system and method
BR0106936A (pt) Dispositivo, utilização do dispositivo, e processo de comando de órgãos de manobra de uma aeronave
KR960043310A (ko) 배터리 지속 장치 및 이를 위한 방법
ES2175133T3 (es) Maquina de juegos y sistema que la utiliza.
WO1999044116A3 (en) Energy-conserving power-supply system
HK1043584A1 (zh) 化學用的輸送系統及輸送方法
BRPI0403104A (pt) Sistema de flaps na asa de sustentação de um avião com asas rìgidas
GB2396706A (en) Airplane emergency navigational system
GB2357872A (en) A power failure safe computer architecture
DE50200846D1 (de) Vorrichtung zum Überschalltransport
DE50115848D1 (de) Flugkontrollsystem
BR9808274A (pt) Circuito de interface de potência para um amplificador de potência, transmissor de acesso múltiplo por divisão no tempo, e, processo para fornecer seletivamente uma tensão de alimentação a um amplificador de potência
DK1074467T3 (da) Flybarnesæde
AU2003249514A1 (en) Transponder with a controllable power-on-reset circuit
CA2551918A1 (en) Device and method for temperature control in an aircraft cabin
HK1055583A1 (en) Propeller-driven aircraft with improved stability about its yaw axis.
ATE279746T1 (de) Verfahren zur verbesserung der steuerung bei einer steuerverbindung in einem luftfahrzeug
US6170525B1 (en) Opto-electric/hydraulic servoactuation
ATE376686T1 (de) Peripheriechipsatz
CN207819080U (zh) 微数据中心的抽屉式配电模组
CN207557766U (zh) 一种固定翼无人机强制返航系统
McBryan et al. Rotorcraft pilot's associate hierarchical planning
CN205924746U (zh) 一种脉冲调节供氧装置的应急供氧模块

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee