DE602004000560D1 - Verriegelungseinrichtung für die Verkleidung einer Triebwerkgondel - Google Patents

Verriegelungseinrichtung für die Verkleidung einer Triebwerkgondel

Info

Publication number
DE602004000560D1
DE602004000560D1 DE602004000560T DE602004000560T DE602004000560D1 DE 602004000560 D1 DE602004000560 D1 DE 602004000560D1 DE 602004000560 T DE602004000560 T DE 602004000560T DE 602004000560 T DE602004000560 T DE 602004000560T DE 602004000560 D1 DE602004000560 D1 DE 602004000560D1
Authority
DE
Germany
Prior art keywords
lining
locking device
engine nacelle
nacelle
engine
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.)
Active
Application number
DE602004000560T
Other languages
English (en)
Other versions
DE602004000560T2 (de
Inventor
Robert Halin
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of DE602004000560D1 publication Critical patent/DE602004000560D1/de
Application granted granted Critical
Publication of DE602004000560T2 publication Critical patent/DE602004000560T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C19/00—Other devices specially designed for securing wings, e.g. with suction cups
    • E05C19/10—Hook fastenings; Fastenings in which a link engages a fixed hook-like member
    • E05C19/12—Hook fastenings; Fastenings in which a link engages a fixed hook-like member pivotally mounted around an axis
    • E05C19/14—Hook fastenings; Fastenings in which a link engages a fixed hook-like member pivotally mounted around an axis with toggle action
    • E05C19/145—Hook fastenings; Fastenings in which a link engages a fixed hook-like member pivotally mounted around an axis with toggle action flush
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C3/00—Fastening devices with bolts moving pivotally or rotatively
    • E05C3/02—Fastening devices with bolts moving pivotally or rotatively without latching action
    • E05C3/06—Fastening devices with bolts moving pivotally or rotatively without latching action with operating handle or equivalent member moving otherwise than rigidly with the bolt
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B15/00—Other details of locks; Parts for engagement by bolts of fastening devices
    • E05B15/0086—Toggle levers
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B63/00—Locks or fastenings with special structural characteristics
    • E05B63/24—Arrangements in which the fastening members which engage one another are mounted respectively on the wing and the frame and are both movable, e.g. for release by moving either of them

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lock And Its Accessories (AREA)
  • Superstructure Of Vehicle (AREA)
  • Catching Or Destruction (AREA)
  • Orthopedics, Nursing, And Contraception (AREA)
  • Wind Motors (AREA)
DE602004000560T 2003-07-04 2004-06-17 Verriegelungseinrichtung für die Verkleidung einer Triebwerkgondel Active DE602004000560T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0308155 2003-07-04
FR0308155A FR2857048B1 (fr) 2003-07-04 2003-07-04 Verrouillage des capots de nacelle d'un turboreacteur

Publications (2)

Publication Number Publication Date
DE602004000560D1 true DE602004000560D1 (de) 2006-05-18
DE602004000560T2 DE602004000560T2 (de) 2007-03-08

Family

ID=33427688

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004000560T Active DE602004000560T2 (de) 2003-07-04 2004-06-17 Verriegelungseinrichtung für die Verkleidung einer Triebwerkgondel

Country Status (9)

Country Link
US (1) US7040578B2 (de)
EP (1) EP1493664B1 (de)
JP (1) JP4137852B2 (de)
CA (1) CA2472876C (de)
DE (1) DE602004000560T2 (de)
ES (1) ES2256828T3 (de)
FR (1) FR2857048B1 (de)
RU (1) RU2342287C2 (de)
UA (1) UA80542C2 (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5156184B2 (ja) * 2005-09-12 2013-03-06 ザ・ボーイング・カンパニー 航空機システム、航空機上の逆推力装置を製造するための方法、および逆推力装置上のラッチ機構を動作するための方法
FR2916425B1 (fr) * 2007-05-25 2009-07-03 Aircelle Sa Dispositif de verrouillage d'une partie ouvrante de nacelle de turboreacteur par rapport a une partie fixe,et nacelle equipee d'un tel dispositif
FR2920179B1 (fr) * 2007-08-20 2013-11-15 Aircelle Sa Dispositif de verrouillage
FR2920144B1 (fr) * 2007-08-20 2010-01-08 Aircelle Sa Nacelle equipee d'un dispositif de detection de l'etat de verrouillage d'un dispositif de verrouillage
FR2920170B1 (fr) * 2007-08-20 2009-09-18 Aircelle Sa Dispositif de verrouillage
FR2920174A1 (fr) * 2007-08-20 2009-02-27 Aircelle Sa Dispositif de liaison entre les deux demi-coquilles d'une nacelle de moteur d'aeronef, et nacelle equipee d'un tel dispositif
US20090173823A1 (en) * 2008-01-07 2009-07-09 Rohr, Inc. Method and component for determining load on a latch assembly
FR2953806B1 (fr) * 2009-12-11 2011-12-30 Eurocopter France Train d'atterrissage pour aeronef, a balancier avec pivot et a diabolo articule
WO2014120126A1 (en) 2013-01-29 2014-08-07 United Technologies Corporation Cowl with pressure driven latch
US9845708B2 (en) 2013-01-29 2017-12-19 United Technologies Corporation Cowl with rate limited lock
US10458280B2 (en) * 2013-03-13 2019-10-29 United Technologies Corporation Gas turbine engine hydraulically operated nacelle latch
WO2014151275A1 (en) 2013-03-15 2014-09-25 United Technologies Corporation Nacelle mounted latching system
FR3064601B1 (fr) * 2017-03-30 2021-01-01 Safran Nacelles Nacelle pour turboreacteur reliee au fuselage d'un aeronef, et ensemble propulsif
US11142326B2 (en) * 2018-07-27 2021-10-12 The Boeing Company Mechanism for indicating position of a latch mechanism for an aircraft nacelle
US11338931B2 (en) * 2018-11-20 2022-05-24 Rohr, Inc. High visibility panel latch

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE473228A (de) *
US1907430A (en) * 1931-09-19 1933-05-09 Chicago Forging & Mfg Co Hood latch
US2550337A (en) * 1945-02-07 1951-04-24 Lockheed Aircraft Corp Engine cowling
US2783072A (en) * 1955-05-26 1957-02-26 Boeing Co Dome or cowling latch
US3145021A (en) * 1961-09-21 1964-08-18 Wilmot Castle Co Door locking apparatus
US4549708A (en) * 1982-08-31 1985-10-29 United Technologies Corporation Cowling latch system
US4629146A (en) * 1985-01-30 1986-12-16 Rohr Industries, Inc. Hold open rod for hinged section of nacelle system
US6279971B1 (en) * 1999-10-05 2001-08-28 Hartwell Corporation Latch with sensor
US6513841B1 (en) * 2000-10-10 2003-02-04 Hartwell Corporation Blowout latch
FR2832752B1 (fr) * 2001-11-27 2004-08-06 Airbus France Dispositif indicateur de defaut de fermeture d'au moins un mecanisme de verrouillage interpose entre deux elements

Also Published As

Publication number Publication date
FR2857048A1 (fr) 2005-01-07
US7040578B2 (en) 2006-05-09
JP4137852B2 (ja) 2008-08-20
DE602004000560T2 (de) 2007-03-08
ES2256828T3 (es) 2006-07-16
CA2472876A1 (fr) 2005-01-04
UA80542C2 (uk) 2007-10-10
EP1493664A1 (de) 2005-01-05
JP2005030394A (ja) 2005-02-03
RU2004120264A (ru) 2005-12-10
CA2472876C (fr) 2012-01-03
EP1493664B1 (de) 2006-03-29
US20050045767A1 (en) 2005-03-03
FR2857048B1 (fr) 2005-08-26
RU2342287C2 (ru) 2008-12-27

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition