DE60000504D1 - Verriegelungsvorrichtung für das fahrwerk eines flugzeugs - Google Patents

Verriegelungsvorrichtung für das fahrwerk eines flugzeugs

Info

Publication number
DE60000504D1
DE60000504D1 DE60000504T DE60000504T DE60000504D1 DE 60000504 D1 DE60000504 D1 DE 60000504D1 DE 60000504 T DE60000504 T DE 60000504T DE 60000504 T DE60000504 T DE 60000504T DE 60000504 D1 DE60000504 D1 DE 60000504D1
Authority
DE
Germany
Prior art keywords
lock member
undercarriage
roller
aircraft
locking device
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
DE60000504T
Other languages
English (en)
Other versions
DE60000504T2 (de
Inventor
Trevor Anthony Brighton
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 Ltd
Original Assignee
BAE Systems PLC
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 BAE Systems PLC filed Critical BAE Systems PLC
Application granted granted Critical
Publication of DE60000504D1 publication Critical patent/DE60000504D1/de
Publication of DE60000504T2 publication Critical patent/DE60000504T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18Operating mechanisms
    • B64C25/26Control or locking systems therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lock And Its Accessories (AREA)
  • Transmission Devices (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
  • Body Structure For Vehicles (AREA)
  • Retarders (AREA)
  • General Details Of Gearings (AREA)
  • Braking Arrangements (AREA)
DE60000504T 1999-02-16 2000-02-02 Verriegelungsvorrichtung für das fahrwerk eines flugzeugs Expired - Lifetime DE60000504T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB9903353.2A GB9903353D0 (en) 1999-02-16 1999-02-16 Aircraft undercarriage mechanism
PCT/GB2000/000292 WO2000048903A1 (en) 1999-02-16 2000-02-02 Aircraft undercarriage lock mechanism

Publications (2)

Publication Number Publication Date
DE60000504D1 true DE60000504D1 (de) 2002-10-31
DE60000504T2 DE60000504T2 (de) 2003-01-23

Family

ID=10847756

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60000504T Expired - Lifetime DE60000504T2 (de) 1999-02-16 2000-02-02 Verriegelungsvorrichtung für das fahrwerk eines flugzeugs

Country Status (10)

Country Link
US (1) US6279853B1 (de)
EP (1) EP1150884B1 (de)
JP (1) JP3540748B2 (de)
AT (1) ATE224833T1 (de)
AU (1) AU2305300A (de)
CA (1) CA2361921A1 (de)
DE (1) DE60000504T2 (de)
ES (1) ES2179014T3 (de)
GB (1) GB9903353D0 (de)
WO (1) WO2000048903A1 (de)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2836668B1 (fr) * 2002-03-04 2004-12-03 Messier Bugatti Dispositif d'accrochage, notamment pour l'accrochage d'un train d'atterrissage d'aeronef ou d'une trappe de train d'atterrissage d'aeronef, et procede de fonctionnement dudit dispositif
FR2836669B1 (fr) * 2002-03-04 2004-12-03 Messier Bugatti Dispositif d'accrochage, notamment pour l'accrochage d'un train d'atterrissage d'aeronef ou d'une trappe de train d'atterrissage d'aeronef
US6942182B2 (en) 2003-05-13 2005-09-13 Supersonic Aerospace International, Llc Forward inboard retracting main landing gear
US7216830B2 (en) * 2003-09-05 2007-05-15 Supersonic Aerospace International, Llc Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction
US6921045B2 (en) 2003-10-30 2005-07-26 Supersonic Aerospace International, Llc Supersonic aircraft with channel relief control
US6824092B1 (en) 2003-10-30 2004-11-30 Supersonic Aerospace International, Llc Aircraft tail configuration for sonic boom reduction
US8814094B2 (en) * 2008-04-04 2014-08-26 Tactair Fluid Controls, Inc. Locking mechanism with bi-modal actuator
FR2944076B1 (fr) * 2009-04-06 2012-09-21 Messier Dowty Sa Dispositif de transmission selective d'effort, et un atterrisseur faisant application
FR3003234B1 (fr) * 2013-03-12 2015-04-10 Messier Bugatti Dowty Atterrisseur d'aeronef muni d'une olive reglable.
EP3135581B1 (de) * 2015-08-25 2018-03-21 Safran Landing Systems UK Limited Flugzeugfahrwerkanordnung
EP3213992B1 (de) * 2016-03-04 2018-04-25 Safran Landing Systems UK Limited Flugzeugfahrwerkanordnung
EP3587252A1 (de) * 2018-06-28 2020-01-01 Airbus Operations GmbH Arretiersystem zum arretieren einer ersten flugzeugkomponente in bezug auf eine zweite flugzeugkomponente
FR3109366B1 (fr) * 2020-04-20 2022-03-18 Safran Landing Systems Agencement de blocage d’un axe d’atterrisseur d’aéronef
FR3144809A1 (fr) * 2023-01-06 2024-07-12 Safran Landing Systems Dispositif pour le crochetage d’un élément mobile

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2567114A (en) * 1945-05-07 1951-09-04 Curtiss Wright Corp Latch mechanism
US2661171A (en) 1951-10-11 1953-12-01 Glenn L Martin Co Up and down lock mechanism for retractable landing gear for aircraft
US2720369A (en) * 1953-09-01 1955-10-11 North American Aviation Inc Locking mechanism for retractable landing gears
US4568045A (en) * 1983-08-17 1986-02-04 The Boeing Company Door operated linkage for support of retracted airplane landing gear
GB2161202A (en) * 1984-07-05 1986-01-08 Dowty Rotol Ltd Locking means for retractable devices
GB8625505D0 (en) 1986-10-24 1986-11-26 Dowty Rotol Ltd Locking mechanisms
EP0384919A1 (de) * 1989-02-27 1990-09-05 Feinmechanische Werke Mainz GmbH Greif- und Verriegelungseinrichtung für Flugzeugklappen oder -fahrwerke
US5022609A (en) * 1990-01-10 1991-06-11 Lockheed Corporation Landing gear
US5100083A (en) * 1990-02-13 1992-03-31 The Boeing Company Retractable landing gear with self-braced folding strut
FR2686854B1 (fr) * 1992-02-03 1994-04-01 Messier Bugatti Train d'atterrissage relevable equipe d'une contre-fiche articulee a double alignement.
FR2688190A1 (fr) * 1992-03-03 1993-09-10 Messier Bugatti Train d'atterrissage relevable.

Also Published As

Publication number Publication date
DE60000504T2 (de) 2003-01-23
JP2002537172A (ja) 2002-11-05
CA2361921A1 (en) 2000-08-24
EP1150884B1 (de) 2002-09-25
US6279853B1 (en) 2001-08-28
ATE224833T1 (de) 2002-10-15
EP1150884A1 (de) 2001-11-07
WO2000048903A1 (en) 2000-08-24
JP3540748B2 (ja) 2004-07-07
ES2179014T3 (es) 2003-01-16
GB9903353D0 (en) 1999-04-07
AU2305300A (en) 2000-09-04

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS UK LTD., BRISTOL, GB

R082 Change of representative

Ref document number: 1150884

Country of ref document: EP

Representative=s name: G. KOCH UND KOLLEGEN, 80339 MUENCHEN, DE