BRPI0813602A2 - "dispositivo de travamento, nacela de turbojato e aeronave" - Google Patents

"dispositivo de travamento, nacela de turbojato e aeronave"

Info

Publication number
BRPI0813602A2
BRPI0813602A2 BRPI0813602-5A2A BRPI0813602A BRPI0813602A2 BR PI0813602 A2 BRPI0813602 A2 BR PI0813602A2 BR PI0813602 A BRPI0813602 A BR PI0813602A BR PI0813602 A2 BRPI0813602 A2 BR PI0813602A2
Authority
BR
Brazil
Prior art keywords
turbojet
nipple
aircraft
locking device
locking
Prior art date
Application number
BRPI0813602-5A2A
Other languages
English (en)
Inventor
Pascal-Marie Paul Marcel Soulier
Aurelie De Sorbay
Original Assignee
Aircelle Sa
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 Aircelle Sa filed Critical Aircelle Sa
Publication of BRPI0813602A2 publication Critical patent/BRPI0813602A2/pt

Links

Classifications

    • 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
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B63/00—Locks or fastenings with special structural characteristics
    • E05B63/18—Locks or fastenings with special structural characteristics with arrangements independent of the locking mechanism for retaining the bolt or latch in the retracted position
    • E05B63/185—Preventing actuation of a bolt when the wing is open
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/70—Interfitted members
    • Y10T403/7075—Interfitted members including discrete retainer
BRPI0813602-5A2A 2007-08-20 2008-08-08 "dispositivo de travamento, nacela de turbojato e aeronave" BRPI0813602A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0705928A FR2920171B1 (fr) 2007-08-20 2007-08-20 Dispositif de verrouillage concu pour etre dispose dans une zone de jonction d'une nacelle
PCT/EP2008/060460 WO2009024487A1 (fr) 2007-08-20 2008-08-08 Dispositif de verrouillage conçu pour etre disposé dans une zone de jonction d'une nacelle

Publications (1)

Publication Number Publication Date
BRPI0813602A2 true BRPI0813602A2 (pt) 2014-12-30

Family

ID=39322887

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0813602-5A2A BRPI0813602A2 (pt) 2007-08-20 2008-08-08 "dispositivo de travamento, nacela de turbojato e aeronave"

Country Status (8)

Country Link
US (1) US8573934B2 (pt)
EP (1) EP2178759B1 (pt)
CN (1) CN101778762B (pt)
BR (1) BRPI0813602A2 (pt)
CA (1) CA2696720C (pt)
FR (1) FR2920171B1 (pt)
RU (1) RU2469921C2 (pt)
WO (1) WO2009024487A1 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2991669B1 (fr) * 2012-06-11 2014-07-11 Lisi Aerospace Verrou a crochet
FR3018845A1 (fr) 2014-03-20 2015-09-25 Aircelle Sa Dispositif pour le verrouillage securise de deux parties d'une nacelle de turboreacteur
US9617767B1 (en) * 2014-11-06 2017-04-11 Avibank Manufacturing, Inc. Latch mechanism
ES2876924T3 (es) * 2015-09-01 2021-11-15 Hartwell Corp Pestillo de gancho de enlace único
EP3426870B1 (en) 2016-03-10 2020-05-06 Hartwell Corporation High offset hook latch
FR3059299B1 (fr) * 2016-11-30 2021-11-12 Safran Nacelles Nacelle de turboreacteur d’aeronef, ensemble propulsif et aeronef comportant une telle nacelle
CN107387490B (zh) * 2017-09-18 2023-07-28 贵州航天天马机电科技有限公司 一种起竖系统锁定及解锁装置
US11142326B2 (en) * 2018-07-27 2021-10-12 The Boeing Company Mechanism for indicating position of a latch mechanism for an aircraft nacelle
US11149564B2 (en) * 2019-06-24 2021-10-19 Rohr, Inc. Nacelle thrust reverser compression rod supporting system
US11866189B2 (en) * 2020-03-26 2024-01-09 Hartwell Corporation Latching system with movable anti-shear mechanism

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3259412A (en) * 1963-12-17 1966-07-05 Camloc Fastener Corp Safety device for toggle latch
SU580142A1 (ru) * 1976-05-25 1977-11-15 Предприятие П/Я А-3395 Ст жной замок
US4127215A (en) * 1978-02-06 1978-11-28 Kaiser Aerospace & Electronics Corporation Access port covering device
US4759574A (en) * 1987-07-15 1988-07-26 Hartwell Corporation Latch assembly
JPH06509305A (ja) * 1992-05-22 1994-10-20 ショート　ブラザーズ　ピーエルシー 閉鎖不履行表示装置
US5984382A (en) * 1998-03-13 1999-11-16 Hartwell Corporation Extended reach latch
US6042156A (en) * 1998-08-11 2000-03-28 Hartwell Corporation Overcenter double jaw latch mechanism
US6279971B1 (en) * 1999-10-05 2001-08-28 Hartwell Corporation Latch with sensor
US6325428B1 (en) * 1999-11-10 2001-12-04 Hartwell Corporation Latch assembly including sensor
FR2800707B1 (fr) * 1999-11-10 2002-01-18 Aerospatiale Matra Airbus Indicateur de defaut de fermeture, notamment pour des capots de nacelle d'un moteur d'avion
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
US6517027B1 (en) * 2001-12-03 2003-02-11 Pratt & Whitney Canada Corp. Flexible/fixed support for engine cowl
FR2857400B1 (fr) * 2003-07-10 2005-10-21 Hurel Hispano Verrou destine a relier deux panneaux d'une structure d'aeroplane
US7252311B2 (en) * 2003-09-17 2007-08-07 Hartwell Corporation Motor driven latch

Also Published As

Publication number Publication date
WO2009024487A1 (fr) 2009-02-26
CA2696720C (fr) 2014-12-09
RU2469921C2 (ru) 2012-12-20
CA2696720A1 (fr) 2009-02-26
US20110293414A1 (en) 2011-12-01
CN101778762A (zh) 2010-07-14
US8573934B2 (en) 2013-11-05
EP2178759B1 (fr) 2018-04-11
CN101778762B (zh) 2014-06-11
FR2920171B1 (fr) 2017-01-13
FR2920171A1 (fr) 2009-02-27
EP2178759A1 (fr) 2010-04-28
RU2010109780A (ru) 2011-09-27

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Legal Events

Date Code Title Description
B08F Application fees: application dismissed [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]