RU2399554C2 - Система привода посадочных закрылков - Google Patents

Система привода посадочных закрылков Download PDF

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Publication number
RU2399554C2
RU2399554C2 RU2007141192/11A RU2007141192A RU2399554C2 RU 2399554 C2 RU2399554 C2 RU 2399554C2 RU 2007141192/11 A RU2007141192/11 A RU 2007141192/11A RU 2007141192 A RU2007141192 A RU 2007141192A RU 2399554 C2 RU2399554 C2 RU 2399554C2
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RU
Russia
Prior art keywords
landing flap
drive system
landing
drive
flap
Prior art date
Application number
RU2007141192/11A
Other languages
English (en)
Russian (ru)
Other versions
RU2007141192A (ru
Inventor
Мартин РЕКЗИК (DE)
Мартин РЕКЗИК
Кристоф ГИЕБЕЛЕР (DE)
Кристоф ГИЕБЕЛЕР
Ина БРЮКНЕР (DE)
Ина БРЮКНЕР
Original Assignee
Эйрбас Дойчланд Гмбх
ДОЙЧЕС ЦЕНТРУМ ФЮР ЛЮФТ-УНД РАУМФАРТ э.Ф. (ДРЛ)
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 Эйрбас Дойчланд Гмбх, ДОЙЧЕС ЦЕНТРУМ ФЮР ЛЮФТ-УНД РАУМФАРТ э.Ф. (ДРЛ) filed Critical Эйрбас Дойчланд Гмбх
Publication of RU2007141192A publication Critical patent/RU2007141192A/ru
Application granted granted Critical
Publication of RU2399554C2 publication Critical patent/RU2399554C2/ru

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Classifications

    • 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)
RU2007141192/11A 2005-04-14 2006-04-12 Система привода посадочных закрылков RU2399554C2 (ru)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US67138605P 2005-04-14 2005-04-14
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
RU2007141192A RU2007141192A (ru) 2009-05-20
RU2399554C2 true RU2399554C2 (ru) 2010-09-20

Family

ID=37067742

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2007141192/11A RU2399554C2 (ru) 2005-04-14 2006-04-12 Система привода посадочных закрылков

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 (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4688744A (en) * 1982-09-03 1987-08-25 Sundstrand Corporation Jam tolerant rotary actuation system
EP0411680A1 (en) * 1989-07-31 1991-02-06 The Boeing Company Extending bent shaft flap drive
RU19650U1 (ru) * 2001-03-28 2001-09-20 Государственный космический научно-производственный центр им. М.В. Хруничева Ручной привод закрылков легкого самолета
EP1462361A1 (de) * 2003-03-27 2004-09-29 Airbus Deutschland GmbH Klappensystem am Tragflügel eines Starrflügel-Flugzeuges

Family Cites Families (17)

* 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
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
CN2345452Y (zh) * 1998-07-16 1999-10-27 孙卫东 可伸缩机翼的飞机
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
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
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
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
DE10339030B4 (de) * 2003-08-25 2005-11-03 Man Technologie Ag Tragstruktur für eine ein- und ausfahrbare Klappe und deren Verwendung

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4688744A (en) * 1982-09-03 1987-08-25 Sundstrand Corporation Jam tolerant rotary actuation system
EP0411680A1 (en) * 1989-07-31 1991-02-06 The Boeing Company Extending bent shaft flap drive
RU19650U1 (ru) * 2001-03-28 2001-09-20 Государственный космический научно-производственный центр им. М.В. Хруничева Ручной привод закрылков легкого самолета
EP1462361A1 (de) * 2003-03-27 2004-09-29 Airbus Deutschland GmbH Klappensystem am Tragflügel eines Starrflügel-Flugzeuges

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
CN100548796C (zh) 2009-10-14
RU2007141192A (ru) 2009-05-20
US8157208B2 (en) 2012-04-17
BRPI0610450B1 (pt) 2019-07-16
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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MM4A The patent is invalid due to non-payment of fees

Effective date: 20200413