FR2901244B1 - Dispositif d'articulation de portes d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation - Google Patents

Dispositif d'articulation de portes d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation

Info

Publication number
FR2901244B1
FR2901244B1 FR0651760A FR0651760A FR2901244B1 FR 2901244 B1 FR2901244 B1 FR 2901244B1 FR 0651760 A FR0651760 A FR 0651760A FR 0651760 A FR0651760 A FR 0651760A FR 2901244 B1 FR2901244 B1 FR 2901244B1
Authority
FR
France
Prior art keywords
nacelle
doors
joining
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
FR0651760A
Other languages
English (en)
Other versions
FR2901244A1 (fr
Inventor
Guillaume Bulin
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 FR0651760A priority Critical patent/FR2901244B1/fr
Priority to US11/798,375 priority patent/US7703716B2/en
Publication of FR2901244A1 publication Critical patent/FR2901244A1/fr
Application granted granted Critical
Publication of FR2901244B1 publication Critical patent/FR2901244B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • B64D29/08—Inspection panels for power plants
FR0651760A 2006-05-16 2006-05-16 Dispositif d'articulation de portes d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation Expired - Fee Related FR2901244B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0651760A FR2901244B1 (fr) 2006-05-16 2006-05-16 Dispositif d'articulation de portes d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation
US11/798,375 US7703716B2 (en) 2006-05-16 2007-05-14 Hinged device for doors of an aircraft nacelle and nacelle equipped with said hinged device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0651760A FR2901244B1 (fr) 2006-05-16 2006-05-16 Dispositif d'articulation de portes d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation

Publications (2)

Publication Number Publication Date
FR2901244A1 FR2901244A1 (fr) 2007-11-23
FR2901244B1 true FR2901244B1 (fr) 2009-01-09

Family

ID=37686088

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0651760A Expired - Fee Related FR2901244B1 (fr) 2006-05-16 2006-05-16 Dispositif d'articulation de portes d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation

Country Status (2)

Country Link
US (1) US7703716B2 (fr)
FR (1) FR2901244B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104870310A (zh) * 2012-12-12 2015-08-26 埃尔塞乐公司 用于飞机的推进组件

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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
FR2920133B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Nacelle de turboreacteur, destinee a equiper un aeronef
FR2920179B1 (fr) * 2007-08-20 2013-11-15 Aircelle Sa Dispositif de verrouillage
FR2926790B1 (fr) * 2008-01-30 2010-02-12 Aircelle Sa Systeme de guidage pour la maintenance d'une nacelle d'aeronef
FR2933073B1 (fr) * 2008-06-25 2010-06-04 Aircelle Sa Ensemble d'entree d'air de nacelle de moteur d'avion
FR2936492B1 (fr) * 2008-10-01 2011-04-01 Aircelle Sa Nacelle pour turboreacteur.
FR2938237B1 (fr) * 2008-11-13 2011-05-20 Aircelle Sa Nacelle pour turboreacteur a capot amont translatable
ES2345808B1 (es) * 2009-03-31 2011-07-28 Airbus Operations, S.L. Cono de cola de una aeronave con carena movil deslizante.
ES2350429B1 (es) * 2009-05-28 2011-11-18 Airbus Operations, S.L. Cono de cola de una aeronave con carena movil abatible
US8876042B2 (en) * 2009-12-21 2014-11-04 General Electric Company Integrated nacelle assembly
FR2989952B1 (fr) * 2012-04-27 2014-04-18 Aircelle Sa Nacelle de turboreacteur a section aval
US9279342B2 (en) 2012-11-21 2016-03-08 General Electric Company Turbine casing with service wedge
WO2014120126A1 (fr) 2013-01-29 2014-08-07 United Technologies Corporation Capot avec verrou actionné par pression
US9845708B2 (en) 2013-01-29 2017-12-19 United Technologies Corporation Cowl with rate limited lock
US9260281B2 (en) 2013-03-13 2016-02-16 General Electric Company Lift efficiency improvement mechanism for turbine casing service wedge
FR3005453B1 (fr) * 2013-05-13 2016-10-07 Airbus Operations Sas Nacelle de turboreacteur d'aeronef
GB201322380D0 (en) * 2013-12-18 2014-02-05 Rolls Royce Plc Gas turbine cowl
PL3059157T3 (pl) * 2015-02-23 2018-08-31 Airbus Helicopters Deutschland GmbH Wiropłat z osłoną mogącą obracać się i przesuwać względem kadłuba
FR3033545B1 (fr) 2015-03-12 2018-08-10 Airbus Operations Nacelle pour ensemble moteur d'aeronef comprenant au moins un capot de nacelle articule a son extremite avant
KR101979332B1 (ko) * 2016-08-23 2019-08-28 에어버스 헬리콥터스 회전익기
US10173783B2 (en) * 2016-08-23 2019-01-08 Airbus Helicopters Rotorcraft with cowling able to rotate and translate relative to the fuselage
FR3079878A1 (fr) * 2018-04-05 2019-10-11 Airbus Operations Turboreacteur comportant une nacelle equipee d'un systeme inverseur comportant un capot articule
US10830177B2 (en) 2018-05-01 2020-11-10 Rohr, Inc. Articulating pivot point post-exit thrust reverser
US10724474B2 (en) 2018-05-01 2020-07-28 Rohr, Inc. Hybrid articulating/translating trailing edge reverser
FR3081837B1 (fr) 2018-06-05 2020-11-27 Airbus Operations Sas Ensemble turbomachine d'aeronef comportant un capot articule
FR3085353A1 (fr) * 2018-09-04 2020-03-06 Airbus Operations 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
FR3134080A1 (fr) * 2022-03-31 2023-10-06 Safran Nacelles Ensemble propulsif pour aéronef comprenant un capot intermédiaire de type fixe démontable monté sur un système d’articulation

Family Cites Families (12)

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US2445131A (en) * 1944-08-10 1948-07-13 Yale & Towne Mfg Co Door mounting
IT1027933B (it) * 1974-12-20 1978-12-20 Socimi Porta a battente scorrevole per veicoli
US3935674A (en) * 1974-07-15 1976-02-03 General Motors Corporation Sliding vehicle door
FR2622930B1 (fr) * 1987-11-06 1990-03-23 Aerospatiale Capotage pour turboreacteur a double flux
US5072898A (en) * 1990-08-31 1991-12-17 United Technologies Corporation Engine cowling roller attachment
US5313788A (en) * 1991-08-07 1994-05-24 General Electric Company Thrust reversing arrangement for a long duct mixed flow exhaust turbofan engine
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
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
DE10360484A1 (de) * 2003-12-22 2005-07-28 Airbus Deutschland Gmbh Flugzeugtor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104870310A (zh) * 2012-12-12 2015-08-26 埃尔塞乐公司 用于飞机的推进组件

Also Published As

Publication number Publication date
US20070267539A1 (en) 2007-11-22
FR2901244A1 (fr) 2007-11-23
US7703716B2 (en) 2010-04-27

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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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