CN100548796C - 着陆襟翼驱动系统 - Google Patents

着陆襟翼驱动系统 Download PDF

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Publication number
CN100548796C
CN100548796C CNB2006800120488A CN200680012048A CN100548796C CN 100548796 C CN100548796 C CN 100548796C CN B2006800120488 A CNB2006800120488 A CN B2006800120488A CN 200680012048 A CN200680012048 A CN 200680012048A CN 100548796 C CN100548796 C CN 100548796C
Authority
CN
China
Prior art keywords
landing flap
drive system
landing
drive
flap
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 - Lifetime
Application number
CNB2006800120488A
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English (en)
Chinese (zh)
Other versions
CN101184664A (zh
Inventor
马丁·雷克西克
克里斯托夫·吉贝勒
伊纳·布鲁克纳
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.)
Airbus Operations GmbH
Deutsches Zentrum fuer Luft und Raumfahrt eV
Original Assignee
Airbus Operations GmbH
Deutsches Zentrum fuer Luft und Raumfahrt eV
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 Airbus Operations GmbH, Deutsches Zentrum fuer Luft und Raumfahrt eV filed Critical Airbus Operations GmbH
Publication of CN101184664A publication Critical patent/CN101184664A/zh
Application granted granted Critical
Publication of CN100548796C publication Critical patent/CN100548796C/zh
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • B64D2045/001—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear for indicating symmetry of flaps deflection

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Transmission Devices (AREA)
  • Retarders (AREA)
  • Tires In General (AREA)
CNB2006800120488A 2005-04-14 2006-04-12 着陆襟翼驱动系统 Expired - Lifetime CN100548796C (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102005017307.1 2005-04-14
DE102005017307A DE102005017307A1 (de) 2005-04-14 2005-04-14 Landeklappenantriebssystem
US60/671,386 2005-04-14

Publications (2)

Publication Number Publication Date
CN101184664A CN101184664A (zh) 2008-05-21
CN100548796C true CN100548796C (zh) 2009-10-14

Family

ID=37067742

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2006800120488A Expired - Lifetime CN100548796C (zh) 2005-04-14 2006-04-12 着陆襟翼驱动系统

Country Status (9)

Country Link
US (1) US8157208B2 (https=)
EP (1) EP1868888B1 (https=)
JP (1) JP4954195B2 (https=)
CN (1) CN100548796C (https=)
BR (1) BRPI0610450B1 (https=)
CA (1) CA2602667C (https=)
DE (2) DE102005017307A1 (https=)
RU (1) RU2399554C2 (https=)
WO (1) WO2006108648A1 (https=)

Families Citing this family (14)

* 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
DE102007036996A1 (de) * 2007-08-06 2009-02-19 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug
US8451144B2 (en) * 2009-02-04 2013-05-28 Honeywell International Inc. Flaps overspeed advisory system
GB0906270D0 (en) * 2009-04-14 2009-05-20 Ge Aviat Systems Ltd High lift devices for aircraft
DE102010025475A1 (de) * 2010-06-29 2011-12-29 Airbus Operations Gmbh Stellsystem eines Flugzeugs mit einer Stellklappe
FR2972175B1 (fr) * 2011-03-01 2013-10-25 Sagem Defense Securite Procede de commande simultanee d'actionneurs de deplacement de volets d'aeronef, dispositif de motorisation de volets d'aeronef et aeronef pourvu d'un tel dispositif
US8438743B2 (en) * 2011-06-01 2013-05-14 Hamilton Sundstrand Corporation Resolver type skew sensor with gimbal attachment
GB201117340D0 (en) * 2011-10-07 2011-11-23 Airbus Uk Ltd Flat support
DE102012111690A1 (de) * 2012-11-30 2014-06-05 Airbus Operations Gmbh Formvariabler aerodynamischer Verkleidungskörper für einen Klappen-Verstellmechanismus eines Luftfahrzeugs
US9073643B2 (en) 2013-03-28 2015-07-07 The Boeing Company Monitoring of high-lift systems for aircraft
EP3025955B1 (de) * 2014-11-26 2019-06-19 Airbus Defence and Space GmbH Hochauftriebssystem
CN108263596A (zh) * 2018-03-07 2018-07-10 陕西金色科技有限公司 一种自动调整机翼位置的快拆机构及其调整方法
CN109895995B (zh) * 2019-04-10 2025-08-26 珠海市海卫科技有限公司 一种轻型运动飞机的襟翼控制机构
US12491989B2 (en) 2022-05-02 2025-12-09 The Boeing Company Systems and methods for controlling a flight control surface of an aircraft

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0411680A1 (en) * 1989-07-31 1991-02-06 The Boeing Company Extending bent shaft flap drive
CN2345452Y (zh) * 1998-07-16 1999-10-27 孙卫东 可伸缩机翼的飞机
CN2574996Y (zh) * 2002-07-11 2003-09-24 广州天象地效飞行器股份有限公司 一种动力增升型地效飞行器地效过渡区的操纵装置
EP1462361A1 (de) * 2003-03-27 2004-09-29 Airbus Deutschland GmbH Klappensystem am Tragflügel eines Starrflügel-Flugzeuges
WO2005021375A1 (de) * 2003-08-25 2005-03-10 Mt Aerospace Ag Tragstruktur für eine ein- und ausfahrbare klappe und deren verwendung

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2500691A (en) * 1945-01-22 1950-03-14 Lear Inc Mechanical actuator system
US2826379A (en) * 1956-03-26 1958-03-11 Lockheed Aircraft Corp Aircraft wing flap carriage
DE2914974C2 (de) 1979-04-12 1985-09-12 Dornier Gmbh, 7990 Friedrichshafen Kombinierte Auftriebs- bzw. Steuerklappe, insbesondere an der Hinterkante von Flugzeugtragflügeln
US4471928A (en) * 1980-08-13 1984-09-18 The Boeing Company Extendible airfoil track assembly
US4688744A (en) * 1982-09-03 1987-08-25 Sundstrand Corporation Jam tolerant rotary actuation system
US4575027A (en) * 1983-05-16 1986-03-11 Lockheed Corporation Electromechanical actuator system with anti-jamming features
US5092539A (en) * 1989-10-13 1992-03-03 Bell Helicopter Textron Inc. Jam resistant ball screw actuator
DE4107556C1 (https=) * 1991-03-08 1992-05-14 Deutsche Airbus Gmbh, 2000 Hamburg, De
US5806805A (en) * 1996-08-07 1998-09-15 The Boeing Company Fault tolerant actuation system for flight control actuators
US5788190A (en) * 1996-10-22 1998-08-04 The Boeing Company Slotted cruise trailing edge flap
FR2811780B1 (fr) * 2000-07-13 2002-08-30 Aerospatiale Matra Airbus Procede et dispositif de commande d'organes de manoeuvre d'un aeronef, a modules de secours electriques
RU19650U1 (ru) 2001-03-28 2001-09-20 Государственный космический научно-производственный центр им. М.В. Хруничева Ручной привод закрылков легкого самолета
DE10133920B4 (de) 2001-07-12 2004-05-13 Eads Deutschland Gmbh Auftriebsklappen-Mechanismus
AT410656B (de) 2001-10-24 2003-06-25 Fischer Adv Components Gmbh Trag- bzw. führungsvorrichtung für flugzeugkomponenten
US6755375B2 (en) * 2002-10-22 2004-06-29 The Boeing Company Method and apparatus for controlling aircraft devices with multiple actuators
US20040200928A1 (en) * 2003-04-14 2004-10-14 Arthur Degenholtz Actuator and flap arrangement with actuator interconnection

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0411680A1 (en) * 1989-07-31 1991-02-06 The Boeing Company Extending bent shaft flap drive
CN2345452Y (zh) * 1998-07-16 1999-10-27 孙卫东 可伸缩机翼的飞机
CN2574996Y (zh) * 2002-07-11 2003-09-24 广州天象地效飞行器股份有限公司 一种动力增升型地效飞行器地效过渡区的操纵装置
EP1462361A1 (de) * 2003-03-27 2004-09-29 Airbus Deutschland GmbH Klappensystem am Tragflügel eines Starrflügel-Flugzeuges
WO2005021375A1 (de) * 2003-08-25 2005-03-10 Mt Aerospace Ag Tragstruktur für eine ein- und ausfahrbare klappe und deren verwendung

Also Published As

Publication number Publication date
CA2602667C (en) 2012-12-18
DE602006014117D1 (de) 2010-06-17
BRPI0610450A2 (pt) 2010-06-22
EP1868888B1 (en) 2010-05-05
WO2006108648A1 (en) 2006-10-19
JP4954195B2 (ja) 2012-06-13
RU2007141192A (ru) 2009-05-20
US8157208B2 (en) 2012-04-17
BRPI0610450B1 (pt) 2019-07-16
RU2399554C2 (ru) 2010-09-20
CA2602667A1 (en) 2006-10-19
CN101184664A (zh) 2008-05-21
DE102005017307A1 (de) 2006-10-26
EP1868888A1 (en) 2007-12-26
JP2008535732A (ja) 2008-09-04
US20080191089A1 (en) 2008-08-14

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Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C56 Change in the name or address of the patentee
CP01 Change in the name or title of a patent holder

Address after: hamburg

Co-patentee after: DEUTSCHES ZENTRUM FuR LUFT- UND RAUMFAHRT E.V.

Patentee after: AIRBUS OPERATIONS GmbH

Address before: hamburg

Co-patentee before: DEUTSCHES ZENTRUM FuR LUFT- UND RAUMFAHRT E.V.

Patentee before: AIRBUS DEUTSCHLAND GmbH

CX01 Expiry of patent term

Granted publication date: 20091014