ATE224833T1 - Verriegelungsvorrichtung für das fahrwerk eines flugzeugs - Google Patents

Verriegelungsvorrichtung für das fahrwerk eines flugzeugs

Info

Publication number
ATE224833T1
ATE224833T1 AT00901751T AT00901751T ATE224833T1 AT E224833 T1 ATE224833 T1 AT E224833T1 AT 00901751 T AT00901751 T AT 00901751T AT 00901751 T AT00901751 T AT 00901751T AT E224833 T1 ATE224833 T1 AT E224833T1
Authority
AT
Austria
Prior art keywords
lock member
aircraft
roller
locking device
undercarriage
Prior art date
Application number
AT00901751T
Other languages
English (en)
Inventor
Trevor Anthony Brighton
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 ATE224833T1 publication Critical patent/ATE224833T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18—Operating mechanisms
    • B64C25/26—Control or locking systems therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lock And Its Accessories (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
  • Transmission Devices (AREA)
  • Braking Arrangements (AREA)
  • Retarders (AREA)
  • General Details Of Gearings (AREA)
  • Body Structure For Vehicles (AREA)
AT00901751T 1999-02-16 2000-02-02 Verriegelungsvorrichtung für das fahrwerk eines flugzeugs ATE224833T1 (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 (1)

Publication Number Publication Date
ATE224833T1 true ATE224833T1 (de) 2002-10-15

Family

ID=10847756

Family Applications (1)

Application Number Title Priority Date Filing Date
AT00901751T ATE224833T1 (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 (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
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
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
US6824092B1 (en) 2003-10-30 2004-11-30 Supersonic Aerospace International, Llc Aircraft tail configuration for sonic boom reduction
US6921045B2 (en) 2003-10-30 2005-07-26 Supersonic Aerospace International, Llc Supersonic aircraft with channel relief control
WO2009146148A2 (en) * 2008-04-04 2009-12-03 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
EP3751161B1 (de) * 2019-06-14 2023-09-27 Safran Landing Systems UK Ltd Selbstschmierende buchsenanordnung
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
EP1150884B1 (de) 2002-09-25
DE60000504D1 (de) 2002-10-31
JP3540748B2 (ja) 2004-07-07
AU2305300A (en) 2000-09-04
WO2000048903A1 (en) 2000-08-24
EP1150884A1 (de) 2001-11-07
JP2002537172A (ja) 2002-11-05
DE60000504T2 (de) 2003-01-23
ES2179014T3 (es) 2003-01-16
GB9903353D0 (en) 1999-04-07
US6279853B1 (en) 2001-08-28
CA2361921A1 (en) 2000-08-24

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Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties