ATE316601T1 - Flugzeugmotorgondel mit verschlussfehleranzeiger - Google Patents

Flugzeugmotorgondel mit verschlussfehleranzeiger

Info

Publication number
ATE316601T1
ATE316601T1 AT02292913T AT02292913T ATE316601T1 AT E316601 T1 ATE316601 T1 AT E316601T1 AT 02292913 T AT02292913 T AT 02292913T AT 02292913 T AT02292913 T AT 02292913T AT E316601 T1 ATE316601 T1 AT E316601T1
Authority
AT
Austria
Prior art keywords
aircraft engine
fault indicator
closing fault
engine gondola
flap
Prior art date
Application number
AT02292913T
Other languages
English (en)
Inventor
Alain Porte
Original Assignee
Airbus France
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 Airbus France filed Critical Airbus France
Application granted granted Critical
Publication of ATE316601T1 publication Critical patent/ATE316601T1/de

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B41/00Locks with visible indication as to whether the lock is locked or unlocked
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings or cowlings
    • B64D29/06Attaching of nacelles, fairings or cowlings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05CBOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C19/00Other devices specially designed for securing wings, e.g. with suction cups
    • E05C19/10Hook fastenings; Fastenings in which a link engages a fixed hook-like member
    • E05C19/12Hook fastenings; Fastenings in which a link engages a fixed hook-like member pivotally mounted around an axis
    • E05C19/14Hook fastenings; Fastenings in which a link engages a fixed hook-like member pivotally mounted around an axis with toggle action
    • E05C19/145Hook fastenings; Fastenings in which a link engages a fixed hook-like member pivotally mounted around an axis with toggle action flush
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S292/00Closure fasteners
    • Y10S292/65Emergency or safety
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T292/00Closure fasteners
    • Y10T292/08Bolts
    • Y10T292/0911Hooked end
    • Y10T292/0913Sliding and swinging
    • Y10T292/0914Operating means
    • Y10T292/0917Lever
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T292/00Closure fasteners
    • Y10T292/08Bolts
    • Y10T292/1043Swinging
    • Y10T292/1062Spring retracted

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
  • Superstructure Of Vehicle (AREA)
  • Infusion, Injection, And Reservoir Apparatuses (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Measuring Fluid Pressure (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Preventing Unauthorised Actuation Of Valves (AREA)
  • Displays For Variable Information Using Movable Means (AREA)
  • Centrifugal Separators (AREA)
AT02292913T 2001-11-27 2002-11-25 Flugzeugmotorgondel mit verschlussfehleranzeiger ATE316601T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0115300A FR2832752B1 (fr) 2001-11-27 2001-11-27 Dispositif indicateur de defaut de fermeture d'au moins un mecanisme de verrouillage interpose entre deux elements

Publications (1)

Publication Number Publication Date
ATE316601T1 true ATE316601T1 (de) 2006-02-15

Family

ID=8869817

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02292913T ATE316601T1 (de) 2001-11-27 2002-11-25 Flugzeugmotorgondel mit verschlussfehleranzeiger

Country Status (7)

Country Link
US (1) US6824175B2 (de)
EP (1) EP1314839B1 (de)
AT (1) ATE316601T1 (de)
CA (1) CA2412714C (de)
DE (1) DE60208872T2 (de)
ES (1) ES2256429T3 (de)
FR (1) FR2832752B1 (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2857048B1 (fr) 2003-07-04 2005-08-26 Snecma Moteurs Verrouillage des capots de nacelle d'un turboreacteur
FR2907759B1 (fr) * 2006-10-31 2008-12-12 Aircelle Sa Nacelle pour turboreacteur a ouverture laterale
FR2920171B1 (fr) 2007-08-20 2017-01-13 Aircelle Sa Dispositif de verrouillage concu pour etre dispose dans une zone de jonction d'une nacelle
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
FR2926285B1 (fr) * 2008-01-15 2009-12-11 Aircelle Sa Nacelle a capotage simplifie
ES2359305B1 (es) * 2008-07-09 2012-03-23 Eads Construcciones Aeronauticas, S.A. Dispositivo para una unidad de propulsión de una aeronave.
FR2953491B1 (fr) * 2009-12-08 2011-12-09 Airbus Operations Sas Nacelle d'aeronef incorporant un dispositif pour proteger un volet d'acces a un systeme de verrouillage
FR2970513B1 (fr) * 2011-01-14 2015-07-31 Aircelle Sa Dispositif de liaison d'un cadre avant a un carter de soufflante
FR2973421B1 (fr) * 2011-03-29 2013-04-05 Aircelle Sa Dispositif de verrouillage a detection mecanique de fermeture et ouverture
FR2979369B1 (fr) * 2011-08-22 2013-08-23 Aircelle Sa Dispositif de verrouillage a detection mecanique de fermeture et ouverture
EP2586707B1 (de) * 2011-10-27 2016-01-20 Airbus Defence and Space SA Sicherheitsverriegelung für die Klappe einer Flugzeugtriebwerksgondel
FR3015435B1 (fr) * 2013-12-20 2016-02-05 Aircelle Sa Nacelle de turboreacteur comprenant un verrou de demi-parties arriere securise
FR3015952B1 (fr) 2014-01-02 2018-01-26 Airbus Operations Systeme de verrouillage de capots
FR3016157B1 (fr) * 2014-01-07 2018-03-02 Airbus Operations (S.A.S) Nacelle d'aeronef comprenant un dispositif visuel d'alerte de defaut de verrouillage des capots.
FR3024435B1 (fr) * 2014-07-31 2016-08-26 Airbus Operations Sas Capot de soufflante pliable guide, pour ensemble moteur d'aeronef
WO2016040501A1 (en) 2014-09-09 2016-03-17 Hartwell Corporation Clevis sensing lock
US9945150B2 (en) * 2015-03-27 2018-04-17 Rohr, Inc. High visibility latch handle
JP6664233B2 (ja) * 2016-02-19 2020-03-13 三菱航空機株式会社 航空機
CN110114542B (zh) * 2016-10-21 2021-08-10 索斯科公司 箱子闩锁
US10267060B2 (en) * 2016-12-21 2019-04-23 The Boeing Company Apparatuses and methods for cowl latch indication
GB2561383A (en) 2017-04-13 2018-10-17 Airbus Operations Ltd Aircraft uplock
US10710736B2 (en) 2017-10-30 2020-07-14 The Boeing Company Latch indication system and method for a fan cowl of an air vehicle
US11142326B2 (en) * 2018-07-27 2021-10-12 The Boeing Company Mechanism for indicating position of a latch mechanism for an aircraft nacelle
FR3085702B1 (fr) * 2018-09-12 2022-05-20 Airbus Operations Sas Systeme de verrouillage d'un capot
US11338931B2 (en) * 2018-11-20 2022-05-24 Rohr, Inc. High visibility panel latch
US20210285269A1 (en) * 2020-03-13 2021-09-16 Rohr, Inc. Latch assembly
US11866189B2 (en) * 2020-03-26 2024-01-09 Hartwell Corporation Latching system with movable anti-shear mechanism
FR3144975A1 (fr) * 2023-01-17 2024-07-19 Airbus Operations (S.A.S.) Aéronef comportant un dispositif de verrouillage ainsi qu’un système d’indication visuelle de l’état dudit dispositif de verrouillage

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3194595A (en) * 1962-08-21 1965-07-13 Camloc Fastener Corp Safety device for cowling latch
US4086670A (en) * 1976-12-06 1978-05-02 Kaiser Aerospace & Electronics Corporation Aircraft toilet drain assembly
US4428609A (en) * 1980-09-15 1984-01-31 The Boeing Company Latch for flexibly joining trailing edge access doors on an aircraft engine support pylon
US4365775A (en) * 1980-12-08 1982-12-28 The Boeing Company Cowl structure alignment and shear device
US4613099A (en) * 1982-02-05 1986-09-23 The Boeing Company Latch signal and cowling structure
US4531769A (en) 1982-08-25 1985-07-30 The Boeing Company Hook latch for an engine cowling
US4679750A (en) * 1984-06-20 1987-07-14 The Boeing Company Latch system
DE69303253D1 (de) 1992-05-22 1996-07-25 Short Brothers Plc Fehleranzeige für schliessvorrichtung
FR2765917B1 (fr) * 1997-07-10 1999-08-20 Hispano Suiza Sa Inverseur de poussee a visualisation de verrouillage
US5915765A (en) * 1998-03-17 1999-06-29 The Boeing Company Opposing hook 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
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
US6220546B1 (en) * 1999-12-29 2001-04-24 The Boeing Company Aircraft engine and associated aircraft engine cowl

Also Published As

Publication number Publication date
US6824175B2 (en) 2004-11-30
DE60208872T2 (de) 2006-09-07
DE60208872D1 (de) 2006-04-13
CA2412714A1 (en) 2003-05-27
ES2256429T3 (es) 2006-07-16
FR2832752A1 (fr) 2003-05-30
US20040104583A1 (en) 2004-06-03
EP1314839B1 (de) 2006-01-25
EP1314839A1 (de) 2003-05-28
FR2832752B1 (fr) 2004-08-06
CA2412714C (en) 2011-04-12

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Legal Events

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