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FR2901245B1 - Dispositif d'articulation d'une porte d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation - Google Patents

Dispositif d'articulation d'une porte d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation

Info

Publication number
FR2901245B1
FR2901245B1 FR0651872A FR0651872A FR2901245B1 FR 2901245 B1 FR2901245 B1 FR 2901245B1 FR 0651872 A FR0651872 A FR 0651872A FR 0651872 A FR0651872 A FR 0651872A FR 2901245 B1 FR2901245 B1 FR 2901245B1
Authority
FR
France
Prior art keywords
nacelle
joining
door
aircraft
articulation
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 - Fee Related
Application number
FR0651872A
Other languages
English (en)
Other versions
FR2901245A1 (fr
Inventor
Patrick Oberle
Joel Bourgault
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 SAS
Original Assignee
Airbus Operations 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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR0651872A priority Critical patent/FR2901245B1/fr
Priority to US11/802,132 priority patent/US7789347B2/en
Publication of FR2901245A1 publication Critical patent/FR2901245A1/fr
Application granted granted Critical
Publication of FR2901245B1 publication Critical patent/FR2901245B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64D29/00Power-plant nacelles, fairings or cowlings
    • B64D29/08Inspection panels for power plants
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00Suspension arrangements for wings
    • E05D15/06Suspension arrangements for wings for wings sliding horizontally more or less in their own plane
    • E05D15/10Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane
    • E05D15/1005Suspension arrangements for wings for wings sliding horizontally more or less in their own plane movable out of one plane into a second parallel plane the wing being supported on arms movable in horizontal planes
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05DHINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D15/00Suspension arrangements for wings
    • E05D15/28Suspension arrangements for wings supported on arms movable in horizontal plane
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2900/00Application of doors, windows, wings or fittings thereof
    • E05Y2900/50Application of doors, windows, wings or fittings thereof for vehicles
    • E05Y2900/502Application of doors, windows, wings or fittings thereof for vehicles for aircraft or spacecraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Wind Motors (AREA)
FR0651872A 2006-05-22 2006-05-22 Dispositif d'articulation d'une porte d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation Expired - Fee Related FR2901245B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0651872A FR2901245B1 (fr) 2006-05-22 2006-05-22 Dispositif d'articulation d'une porte d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation
US11/802,132 US7789347B2 (en) 2006-05-22 2007-05-21 Device for articulating a door of a nacelle of an aircraft and nacelle provided with said articulation device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0651872A FR2901245B1 (fr) 2006-05-22 2006-05-22 Dispositif d'articulation d'une porte d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation

Publications (2)

Publication Number Publication Date
FR2901245A1 FR2901245A1 (fr) 2007-11-23
FR2901245B1 true FR2901245B1 (fr) 2008-12-26

Family

ID=37654799

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0651872A Expired - Fee Related FR2901245B1 (fr) 2006-05-22 2006-05-22 Dispositif d'articulation d'une porte d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation

Country Status (2)

Country Link
US (1) US7789347B2 (fr)
FR (1) FR2901245B1 (fr)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2890378B1 (fr) * 2005-09-08 2009-01-16 Airbus France Sas Capot de nacelle pour turboreacteur et nacelle comportant au moins un tel capot.
FR2897339B1 (fr) * 2006-02-16 2008-04-11 Aircelle Sa Nacelle de turboreacteur a ouverture laterale des capots
FR2905991B1 (fr) * 2006-09-20 2012-01-13 Snecma Systeme propulsif integre comportant un moteur a turboreacteur a double flux.
FR2912378B1 (fr) * 2007-02-14 2009-03-20 Aircelle Sa Nacelle de moteur a reaction pour un avion
FR2916737B1 (fr) * 2007-06-01 2010-05-28 Airbus France Ensemble moteur pour aeronef a nacelle coulissante.
FR2920140B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Nacelle de turboreacteur, destinee a equiper un aeronef
FR2926285B1 (fr) * 2008-01-15 2009-12-11 Aircelle Sa Nacelle a capotage simplifie
US9188025B2 (en) * 2008-11-26 2015-11-17 Mra Systems, Inc. Apparatus for facilitating access to a nacelle interior
US8220738B2 (en) * 2008-11-26 2012-07-17 Mra Systems, Inc. Nacelle and method of assembling the same
US9188026B2 (en) * 2008-11-26 2015-11-17 Mra Systems, Inc. Apparatus for facilitating access to a nacelle interior and method of assembling the same
FR2961788B1 (fr) * 2010-06-29 2012-06-15 Aircelle Sa Nacelle de turboreacteur
US9217390B2 (en) 2012-06-28 2015-12-22 United Technologies Corporation Thrust reverser maintenance actuation system
US9279342B2 (en) 2012-11-21 2016-03-08 General Electric Company Turbine casing with service wedge
US9260281B2 (en) 2013-03-13 2016-02-16 General Electric Company Lift efficiency improvement mechanism for turbine casing service wedge
FR3010049B1 (fr) * 2013-09-04 2017-03-31 Snecma Structure de liaison moteur-nacelle a secteurs de virole pivotants
CN106573682B (zh) 2014-08-20 2020-03-27 庞巴迪公司 用于飞机高温排气的致动出口门
DE102015206093A1 (de) * 2015-04-02 2016-10-06 Rolls-Royce Deutschland Ltd & Co Kg Triebwerksverkleidung einer Fluggasturbine
FR3036382B1 (fr) * 2015-05-21 2017-06-16 Airbus Operations Sas Nacelle d'aeronef comportant au moins un capot monte rotatif autour de l'axe longitudinal de la nacelle
FR3075761A1 (fr) * 2017-12-21 2019-06-28 Airbus Operations Partie anterieure de nacelle d'un ensemble propulsif comportant un cadre de rigidification incline
FR3079500A1 (fr) * 2018-03-29 2019-10-04 Airbus Operations Nacelle d'aeronef a capot de soufflante rotatif integrant une trappe d'acces
FR3087422B1 (fr) * 2018-10-23 2021-10-01 Airbus Operations Sas Ensemble turbomachine d’aeronef comportant un capot articule
FR3088906A1 (fr) * 2018-11-22 2020-05-29 Airbus Operations Nacelle d’aéronef comportant un capot a deux vantaux articulés
FR3090048A1 (fr) * 2018-12-13 2020-06-19 Airbus Operations Turboreacteur double flux comportant une serie de lames rotatives pour obturer la veine du flux secondaire
EP3733525B1 (fr) * 2019-04-29 2023-08-09 Rohr, Inc. Dispositifs de retenue de fixation de capot de soufflante
US11414200B2 (en) 2019-04-29 2022-08-16 Rohr, Inc. Fan cowl securement retainers
US11702196B2 (en) * 2020-06-25 2023-07-18 Textron Innovations Inc. Rotor system with reconfigurable duct
DE102020134638B3 (de) 2020-12-22 2022-05-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Außenverkleidung für Flugobjekte
DE102020134661B3 (de) 2020-12-22 2022-03-17 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zur Herstellung einer Außenverkleidung sowie eine Außenverkleidung
DE102020134629A1 (de) 2020-12-22 2022-06-23 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zur Herstellung einer Außenverkleidung für Flugobjekte
DE102021117594B4 (de) 2021-07-07 2023-05-17 Deutsches Zentrum für Luft- und Raumfahrt e.V. Außenverkleidung für Flugobjekte sowie Verfahren zu dessen Herstellung
FR3151837A1 (fr) * 2023-08-01 2025-02-07 Airbus Operations Ensemble de positionnement ameliore de capot mobile d’aeronef et aeronef muni d’un tel ensemble.

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3164956A (en) * 1963-03-14 1965-01-12 Boeing Co Two part thrust reverser
FR2622930B1 (fr) * 1987-11-06 1990-03-23 Aerospatiale Capotage pour turboreacteur a double flux
US5181677A (en) * 1991-09-26 1993-01-26 Kaplan Abraham M Sliding aircraft door
US5350136A (en) * 1993-05-14 1994-09-27 United Technologies Corporation Nacelle arrangement
GB9407632D0 (en) * 1994-04-18 1994-06-08 Short Brothers Plc An aircraft propulsive power unit
FR2734540B1 (fr) * 1995-05-24 1997-08-08 Aerospatiale Nacelle de moteur d'aeronef comportant un capot de nacelle
FR2771459B1 (fr) * 1997-11-27 2000-02-04 Aerospatiale Bielle telescopique d'ouverture d'un capot mobile, notamment 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
US6311928B1 (en) * 2000-01-05 2001-11-06 Stage Iii Technologies, L.C. Jet engine cascade thrust reverser for use with mixer/ejector noise suppressor
US6340135B1 (en) * 2000-05-30 2002-01-22 Rohr, Inc. Translating independently mounted air inlet system for aircraft turbofan jet engine

Also Published As

Publication number Publication date
US7789347B2 (en) 2010-09-07
US20070278345A1 (en) 2007-12-06
FR2901245A1 (fr) 2007-11-23

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Legal Events

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CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

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