DE602006005069D1 - Betätigungssystem für Flugzeugsteuerflächen mit redundantkonfigurierten Schliessbetätigungsvorrichtungen - Google Patents

Betätigungssystem für Flugzeugsteuerflächen mit redundantkonfigurierten Schliessbetätigungsvorrichtungen

Info

Publication number
DE602006005069D1
DE602006005069D1 DE602006005069T DE602006005069T DE602006005069D1 DE 602006005069 D1 DE602006005069 D1 DE 602006005069D1 DE 602006005069 T DE602006005069 T DE 602006005069T DE 602006005069 T DE602006005069 T DE 602006005069T DE 602006005069 D1 DE602006005069 D1 DE 602006005069D1
Authority
DE
Germany
Prior art keywords
actuation system
control surfaces
aircraft control
redundantly configured
closing actuators
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.)
Active
Application number
DE602006005069T
Other languages
English (en)
Inventor
Paul T Wingett
Calvin C Potter
Casey Hanlon
Dwayne M Benson
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 DE602006005069D1 publication Critical patent/DE602006005069D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/40—Transmitting means with power amplification using fluid pressure
    • B64C13/42—Transmitting means with power amplification using fluid pressure having duplication or stand-by provisions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/504—Transmitting means with power amplification using electrical energy using electro-hydrostatic actuators [EHA's]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Transmission Devices (AREA)
DE602006005069T 2005-05-11 2006-05-05 Betätigungssystem für Flugzeugsteuerflächen mit redundantkonfigurierten Schliessbetätigungsvorrichtungen Active DE602006005069D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US68007305P 2005-05-11 2005-05-11
US11/192,625 US7607611B2 (en) 2005-05-11 2005-07-28 Flight control surface actuation system with redundantly configured and lockable actuator assemblies

Publications (1)

Publication Number Publication Date
DE602006005069D1 true DE602006005069D1 (de) 2009-03-19

Family

ID=36750951

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006005069T Active DE602006005069D1 (de) 2005-05-11 2006-05-05 Betätigungssystem für Flugzeugsteuerflächen mit redundantkonfigurierten Schliessbetätigungsvorrichtungen

Country Status (3)

Country Link
US (1) US7607611B2 (de)
EP (1) EP1721825B1 (de)
DE (1) DE602006005069D1 (de)

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006030315A1 (de) * 2006-06-30 2008-01-17 Airbus Deutschland Gmbh Hochauftriebssystem am Tragflügel eines Flugzeugs
FR2912374B1 (fr) * 2007-02-08 2009-05-08 Goodrich Actuation Systems Sas Detection de la reprise d'effort par une voie secondaire d'un actionneur de commande de vol
US8033509B2 (en) 2007-02-27 2011-10-11 Honeywell International Inc. Load optimized redundant flight control surface actuation system and method
FR2913949B1 (fr) * 2007-03-23 2009-10-02 Goodrich Actuation Systems Sas Perfectionnements a la detection de la reprise d'effort de la voie secondaire d'un actionneur de commande de vol.
US8104710B2 (en) * 2007-04-25 2012-01-31 Goodrich Actuation Systems Limited Actuator arrangement
DE102008023628B4 (de) * 2008-05-15 2015-10-08 Airbus Operations Gmbh Stellsystem für eine hydraulisch betätigbare Höhenflosse und Testverfahren zur Überprüfung der Integrität eines Stellsystems
US8172174B2 (en) * 2008-11-13 2012-05-08 Honeywell International Inc. Hybrid electromechanical/hydromechanical actuator and actuation control system
DE102009017653A1 (de) * 2009-04-16 2010-10-21 Airbus Deutschland Gmbh Hochauftriebssystem eines Flugzeugs, Flugzeugsystem und Propeller-Flugzeug mit einem Hochauftriebssystem
GB0917693D0 (en) * 2009-10-09 2009-11-25 Goodrich Actuation Systems Ltd Actuator arrangement
FR2953494B1 (fr) * 2009-12-08 2012-02-17 Goodrich Actuation Systems Sas Dispositif de test de la detection de la reprise effort par une voie secondaire d'un actionneur de commande de vol, et procede de test associe
US9032739B2 (en) 2011-04-11 2015-05-19 Hamilton Sundstrand Corporation Load limited actuator
GB201108450D0 (en) * 2011-05-20 2011-07-06 Airbus Operations Ltd Aircraft wing assembly
EP2812242B1 (de) 2012-02-09 2017-11-15 Moog Inc. Aktuatorsystem und methode
JP5905294B2 (ja) * 2012-02-27 2016-04-20 ナブテスコ株式会社 航空機アクチュエータの油圧システム
JP6178571B2 (ja) * 2012-12-26 2017-08-09 三菱航空機株式会社 動翼のアクチュエータ装置、航空機の動翼、及び、航空機
US9086125B2 (en) * 2013-03-15 2015-07-21 Moog Inc. Rotary actuator
US9284996B2 (en) 2013-10-23 2016-03-15 Sikorsky Aircraft Corporation Selective electrical control of electromechanical clutch assembly
JP6230873B2 (ja) * 2013-10-24 2017-11-15 ナブテスコ株式会社 電動アクチュエータ及びアクチュエータユニット
FR3016607B1 (fr) * 2014-01-20 2016-01-22 Sagem Defense Securite Actionneur de commande d'un plan horizontal de stabilisation d'un aeronef
US9586675B2 (en) 2014-06-09 2017-03-07 The Boeing Company Apparatus and method for arrestment of a flight control surface
EP3072808B1 (de) * 2015-03-26 2017-10-25 Goodrich Actuation Systems SAS Obere befestigung für einen trimmbaren horizontalen stabilisatoraktuator
CA2919342C (en) 2015-04-15 2023-08-15 Goodrich Actuation Systems Sas Check device for flight actuator primary load path failure detection device
KR20180100673A (ko) 2016-01-13 2018-09-11 무그 인코포레이티드 합산 및 결함 허용성 로터리 액추에이터 어셈블리
GB2557273A (en) * 2016-12-02 2018-06-20 Airbus Operations Ltd Actuator testing
US10882604B2 (en) 2018-01-18 2021-01-05 The Boeing Company Distributed trailing edge wing flap systems
US10843792B2 (en) * 2018-02-01 2020-11-24 Hamilton Sundstrand Corporation Autonomous reconfiguration of a multi-redundant actuator control system
EP3533707B1 (de) * 2018-03-01 2020-06-24 Goodrich Actuation Systems SAS Thermische ema-verwaltungsoptimierung
US10882603B2 (en) 2018-03-20 2021-01-05 The Boeing Company Distributed trailing edge wing flap systems
US10829203B2 (en) 2018-04-06 2020-11-10 The Boeing Company Distributed trailing edge wing flap systems
US11001371B2 (en) * 2018-08-07 2021-05-11 The Boeing Company Hydraulic droop control for aircraft wing
US11027824B2 (en) 2018-09-05 2021-06-08 The Boeing Company Distributed trailing edge wing flap systems
US10926867B2 (en) 2018-09-10 2021-02-23 The Boeing Company Distributed trailing edge wing flap systems
US11926408B2 (en) 2019-01-28 2024-03-12 Moog Inc. Failsafe valve for geared rotary actuator
US11247767B2 (en) * 2020-03-05 2022-02-15 Ruben Leon Wireless autopilot system
US11661175B2 (en) 2020-03-05 2023-05-30 Ruben Leon Wireless autopilot system
US11787528B2 (en) * 2020-12-23 2023-10-17 Whippany Actuation Systems Llc Jam free dual-redundant actuator lane changer system and process
US11407496B1 (en) 2021-08-17 2022-08-09 Beta Air, Llc Systems and methods for redundant flight control in an aircraft
US20240124130A1 (en) * 2022-10-14 2024-04-18 Honeywell International Inc. Control surface actuator assembly with gust lock

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1861318A (en) * 1931-01-23 1932-05-31 Handley Page Ltd Means for controlling aeroplanes
US2665084A (en) 1949-11-14 1954-01-05 Northrop Aircraft Inc Flap actuator and control system
US3426650A (en) * 1965-12-23 1969-02-11 Bell Aerospace Corp Triple channel redundant hydraeric control system
US3401600A (en) * 1965-12-23 1968-09-17 Bell Aerospace Corp Control system having a plurality of control chains each of which may be disabled in event of failure thereof
US3949958A (en) 1973-12-07 1976-04-13 Lockheed Aircraft Corporation Pitch control system
US4470569A (en) 1981-12-28 1984-09-11 Mcdonnell Douglas Corporation Locking, redundant slat drive mechanism
US4498647A (en) 1982-03-15 1985-02-12 Mcdonnel Douglas Corporation Surface hold-down mechanism
US4688744A (en) 1982-09-03 1987-08-25 Sundstrand Corporation Jam tolerant rotary actuation system
US4800798A (en) 1984-12-11 1989-01-31 The United States Of America As Represented By The Secretary Of The Air Force Control surface dual redundant servomechanism
FR2591557B1 (fr) * 1985-12-13 1988-03-25 Aerospatiale Systeme de couplage de deux volets d'une aile d'aeronef, et aile d'aeronef equipee d'un tel systeme
DE3669475D1 (de) 1986-03-14 1990-04-19 Boeing Co Flugregelsystem.
DE3638820A1 (de) 1986-09-12 1988-03-24 Messerschmitt Boelkow Blohm Seitenruder-steuerungsanordnung fuer luftfahrzeuge
FR2617120B1 (fr) * 1987-06-24 1989-12-08 Aerospatiale Systeme pour la commande d'un aeronef en roulis et en lacet
JPS6441498A (en) 1987-08-07 1989-02-13 Teijin Seiki Co Ltd Controller for rudder surface
US5493497A (en) * 1992-06-03 1996-02-20 The Boeing Company Multiaxis redundant fly-by-wire primary flight control system
US6062262A (en) * 1995-10-10 2000-05-16 Tash; George Water drain pipe test plug device
US6116065A (en) * 1998-08-13 2000-09-12 Winner Aviation Corporation Anti-theft device for aircraft
GB0127254D0 (en) * 2001-11-13 2002-01-02 Lucas Industries Ltd Aircraft flight surface control system
US6776376B2 (en) 2002-10-18 2004-08-17 Hamilton Sunstrand Flight control surface actuation system
US6755375B2 (en) * 2002-10-22 2004-06-29 The Boeing Company Method and apparatus for controlling aircraft devices with multiple actuators
US6929222B2 (en) 2003-09-08 2005-08-16 Mihailo P. Djuric Non-jamming, fail safe flight control system with non-symmetric load alleviation capability
US6923405B2 (en) 2003-11-17 2005-08-02 The Boeing Company Enhanced rudder control system

Also Published As

Publication number Publication date
EP1721825A1 (de) 2006-11-15
US20070018040A1 (en) 2007-01-25
US7607611B2 (en) 2009-10-27
EP1721825B1 (de) 2009-02-04

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