ATE277376T1 - Flugsteuereinheit mit integrierter spoilerantriebsteuerelektronik - Google Patents

Flugsteuereinheit mit integrierter spoilerantriebsteuerelektronik

Info

Publication number
ATE277376T1
ATE277376T1 AT01952738T AT01952738T ATE277376T1 AT E277376 T1 ATE277376 T1 AT E277376T1 AT 01952738 T AT01952738 T AT 01952738T AT 01952738 T AT01952738 T AT 01952738T AT E277376 T1 ATE277376 T1 AT E277376T1
Authority
AT
Austria
Prior art keywords
spoiler
ace
fcm
flight control
control
Prior art date
Application number
AT01952738T
Other languages
English (en)
Inventor
Larry Yount
John Todd
Original Assignee
Honeywell Int 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 Int Inc filed Critical Honeywell Int Inc
Application granted granted Critical
Publication of ATE277376T1 publication Critical patent/ATE277376T1/de

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Automatic Cycles, And Cycles In General (AREA)
AT01952738T 2000-07-14 2001-07-13 Flugsteuereinheit mit integrierter spoilerantriebsteuerelektronik ATE277376T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
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 (1)

Publication Number Publication Date
ATE277376T1 true ATE277376T1 (de) 2004-10-15

Family

ID=24468408

Family Applications (1)

Application Number Title Priority Date Filing Date
AT01952738T ATE277376T1 (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 (50)

* 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
ATE487925T1 (de) 2002-02-19 2010-11-15 Boeing Co Flughafenrollweg-navigationssystem
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
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
US7243881B2 (en) 2003-06-03 2007-07-17 The Boeing Company Multi-function trailing edge devices and associated methods
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7424350B2 (en) 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing 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
US7270305B2 (en) 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding 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
US7322547B2 (en) 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding 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
US7309043B2 (en) 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
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
US7500641B2 (en) 2005-08-10 2009-03-10 The Boeing Company Aerospace vehicle flow body 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
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
GB2435246A (en) * 2006-02-17 2007-08-22 Decoma U K Ltd Spoiler
US7463360B2 (en) 2006-04-18 2008-12-09 Honeywell International Inc. Optical resonator gyro with integrated external cavity beam generator
US7535576B2 (en) 2006-05-15 2009-05-19 Honeywell International, Inc. Integrated optical rotation sensor and method for sensing rotation rate
DE102006039671B4 (de) 2006-08-24 2026-03-12 Liebherr-Aerospace Lindenberg Gmbh Modulares elektronisches Flugsteuerungssystem
EP2156256A2 (de) 2007-04-05 2010-02-24 Bombardier Inc. Seriell redundantes einkanaliges mehrwege-fly-by-wire-flugsteuersystem mit mehreren achsen
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
EP4660076A1 (de) * 2024-06-04 2025-12-10 Goodrich Actuation Systems SAS Aktuatoranordnungsarchitektur

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
WO2002006909A2 (en) 2002-01-24
JP2004504209A (ja) 2004-02-12
DE60105815D1 (de) 2004-10-28
US6561463B1 (en) 2003-05-13
DE60105815T2 (de) 2005-10-13
EP1301835A2 (de) 2003-04-16
WO2002006909A3 (en) 2002-10-03
EP1301835B1 (de) 2004-09-22

Similar Documents

Publication Publication Date Title
DE60105815D1 (de) Flugsteuereinheit mit integrierter spoilerantriebsteuerelektronik
ATE287822T1 (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
ES2175133T3 (es) Maquina de juegos y sistema que la utiliza.
ATE270999T1 (de) Flugverriegelungsstellantrieb mit zwei energiequellen
DE50200846D1 (de) Vorrichtung zum Überschalltransport
AU3189893A (en) Extruded panel unit for constructional purposes
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
BR9001775A (pt) Veiculo provido de um sistema de alimentacao eletrica auxiliar que utiliza celulas solares,em particular para acionamento,com o veiculo parado,de um equipamento de climatizacao do dito veiculo
DK1074467T3 (da) Flybarnesæde
CA2383553A1 (en) Adhesive tape
WO2003015186A3 (de) Thermisch antreibbare spannungsversorgung
AU2003249514A1 (en) Transponder with a controllable power-on-reset circuit
CA2551918A1 (en) Device and method for temperature control in an aircraft cabin
US6170525B1 (en) Opto-electric/hydraulic servoactuation
ATE376686T1 (de) Peripheriechipsatz
EP0369782A3 (de) Schaltung zum Betrieb eines Gerätes, wie ein Drucker
IT1261689B (it) Circuito di pilotaggio adattativo per carichi induttivi e relativo procedimento.
BR0203311A (pt) Sistema detector de sub-tensão em um aparelho elétrico
CN206537521U (zh) 一种飞行照明器的控制系统
Yuan Design of propulsion only emergency flight control system using H-infinity model matching
McBryan et al. Rotorcraft pilot's associate hierarchical planning
McConnell Helicopter avionics bay is a cost reduction success
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
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties