JP2008535732A5 - - Google Patents

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Publication number
JP2008535732A5
JP2008535732A5 JP2008505814A JP2008505814A JP2008535732A5 JP 2008535732 A5 JP2008535732 A5 JP 2008535732A5 JP 2008505814 A JP2008505814 A JP 2008505814A JP 2008505814 A JP2008505814 A JP 2008505814A JP 2008535732 A5 JP2008535732 A5 JP 2008535732A5
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JP
Japan
Prior art keywords
landing flap
drive system
drive motor
landing
motor
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.)
Granted
Application number
JP2008505814A
Other languages
English (en)
Japanese (ja)
Other versions
JP4954195B2 (ja
JP2008535732A (ja
Filing date
Publication date
Priority claimed from DE102005017307A external-priority patent/DE102005017307A1/de
Application filed filed Critical
Publication of JP2008535732A publication Critical patent/JP2008535732A/ja
Publication of JP2008535732A5 publication Critical patent/JP2008535732A5/ja
Application granted granted Critical
Publication of JP4954195B2 publication Critical patent/JP4954195B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2008505814A 2005-04-14 2006-04-12 ランディングフラップ駆動システム Expired - Fee Related JP4954195B2 (ja)

Applications Claiming Priority (5)

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
PCT/EP2006/003392 WO2006108648A1 (en) 2005-04-14 2006-04-12 Landing flap drive system

Publications (3)

Publication Number Publication Date
JP2008535732A JP2008535732A (ja) 2008-09-04
JP2008535732A5 true JP2008535732A5 (https=) 2009-05-14
JP4954195B2 JP4954195B2 (ja) 2012-06-13

Family

ID=37067742

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008505814A Expired - Fee Related JP4954195B2 (ja) 2005-04-14 2006-04-12 ランディングフラップ駆動システム

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)

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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

Family Cites Families (21)

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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
US5161757A (en) * 1989-07-31 1992-11-10 The Boeing Company Extending bent shaft flap drive
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
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
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
DE10313728B4 (de) 2003-03-27 2011-07-21 Airbus Operations GmbH, 21129 Klappensystem am Tragflügel eines Starrflügel-Flugzeuges
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

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