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FR2622930B1 - Capotage pour turboreacteur a double flux - Google Patents

Capotage pour turboreacteur a double flux

Info

Publication number
FR2622930B1
FR2622930B1 FR8715434A FR8715434A FR2622930B1 FR 2622930 B1 FR2622930 B1 FR 2622930B1 FR 8715434 A FR8715434 A FR 8715434A FR 8715434 A FR8715434 A FR 8715434A FR 2622930 B1 FR2622930 B1 FR 2622930B1
Authority
FR
France
Prior art keywords
hood
double
flow turboreactor
turboreactor
flow
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 - Lifetime
Application number
FR8715434A
Other languages
English (en)
Other versions
FR2622930A1 (fr
Inventor
Alain Garcia
Jean-Claude Tchavdarov
Alain Porte
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 Group SAS
Original Assignee
Airbus Group 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 Group SAS filed Critical Airbus Group SAS
Priority to FR8715434A priority Critical patent/FR2622930B1/fr
Priority to GB8825416A priority patent/GB2212218B/en
Priority to US07/267,458 priority patent/US4920744A/en
Publication of FR2622930A1 publication Critical patent/FR2622930A1/fr
Application granted granted Critical
Publication of FR2622930B1 publication Critical patent/FR2622930B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
FR8715434A 1987-11-06 1987-11-06 Capotage pour turboreacteur a double flux Expired - Lifetime FR2622930B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR8715434A FR2622930B1 (fr) 1987-11-06 1987-11-06 Capotage pour turboreacteur a double flux
GB8825416A GB2212218B (en) 1987-11-06 1988-10-31 Ducted fan turbine engines
US07/267,458 US4920744A (en) 1987-11-06 1988-11-04 Ducted fan turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8715434A FR2622930B1 (fr) 1987-11-06 1987-11-06 Capotage pour turboreacteur a double flux

Publications (2)

Publication Number Publication Date
FR2622930A1 FR2622930A1 (fr) 1989-05-12
FR2622930B1 true FR2622930B1 (fr) 1990-03-23

Family

ID=9356579

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8715434A Expired - Lifetime FR2622930B1 (fr) 1987-11-06 1987-11-06 Capotage pour turboreacteur a double flux

Country Status (3)

Country Link
US (1) US4920744A (fr)
FR (1) FR2622930B1 (fr)
GB (1) GB2212218B (fr)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5350136A (en) * 1993-05-14 1994-09-27 United Technologies Corporation Nacelle arrangement
GB9723022D0 (en) 1997-11-01 1998-01-07 Rolls Royce Plc Gas turbine apparatus
US6220546B1 (en) * 1999-12-29 2001-04-24 The Boeing Company Aircraft engine and associated aircraft engine cowl
FR2825976B1 (fr) * 2001-06-13 2003-09-05 Eads Airbus Sa Dispositif de reprise d'efforts generes par un moteur d'aeronef
US6860131B2 (en) * 2002-09-26 2005-03-01 Newfrey Llc Rekeying a lock assembly
US7494318B2 (en) * 2005-02-11 2009-02-24 General Electric Company Methods and apparatus useful for servicing engines
FR2897339B1 (fr) * 2006-02-16 2008-04-11 Aircelle Sa Nacelle de turboreacteur a ouverture laterale des capots
FR2901244B1 (fr) 2006-05-16 2009-01-09 Airbus France Sas Dispositif d'articulation de portes d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation
FR2901245B1 (fr) 2006-05-22 2008-12-26 Airbus France Sas Dispositif d'articulation d'une porte d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation
FR2912378B1 (fr) * 2007-02-14 2009-03-20 Aircelle Sa Nacelle de moteur a reaction pour un avion
FR2914700B1 (fr) * 2007-04-04 2009-05-22 Aircelle Sa Inverseur de poussee pour moteur a reaction
US20080258016A1 (en) * 2007-04-23 2008-10-23 Gukeisen Robert L Nacelle assembly without lower bi-fi splitter
FR2920177B1 (fr) * 2007-08-20 2009-09-18 Aircelle Sa Dispositif de liaison, destine a relier un premier et second elements mobiles l'un par rapport a l'autre
FR2920145B1 (fr) * 2007-08-20 2009-09-18 Aircelle Sa Nacelle de turboreacteur a amortisseurs pour demi-coquilles
US8438859B2 (en) * 2008-01-08 2013-05-14 Rolls-Royce North American Technologies, Inc. Integrated bypass engine structure
FR2926790B1 (fr) 2008-01-30 2010-02-12 Aircelle Sa Systeme de guidage pour la maintenance d'une nacelle d'aeronef
ES2350429B1 (es) * 2009-05-28 2011-11-18 Airbus Operations, S.L. Cono de cola de una aeronave con carena movil abatible
FR2999155B1 (fr) * 2012-12-12 2014-11-21 Aircelle Sa Ensemble propulsif pour aeronef
EP2951091B1 (fr) 2013-01-29 2019-01-09 United Technologies Corporation Capot avec verrou à taux limité
EP2951090B1 (fr) 2013-01-29 2019-01-16 United Technologies Corporation Capot avec verrou actionné par pression
US9822734B2 (en) 2013-02-22 2017-11-21 United Technologies Corporation Tandem thrust reverser with multi-bar linkage
US9617009B2 (en) * 2013-02-22 2017-04-11 United Technologies Corporation ATR full ring sliding nacelle
US20140352797A1 (en) * 2013-06-04 2014-12-04 Rohr, Inc. Aircraft jet engine
FR3007739B1 (fr) * 2013-07-01 2016-02-05 Aircelle Sa Dispositif d’assistance pour la manœuvre d’un capot et nacelle de turboreacteur ainsi equipee
DE102015206093A1 (de) * 2015-04-02 2016-10-06 Rolls-Royce Deutschland Ltd & Co Kg Triebwerksverkleidung einer Fluggasturbine
FR3037039B1 (fr) 2015-06-03 2017-06-02 Aircelle Sa Dispositif de verrouillage de capots pivotants d’un inverseur de poussee
FR3075176B1 (fr) 2017-12-18 2020-11-06 Safran Aircraft Engines Ensemble de capot ouvrant et mecanisme de deploiement
FR3085353A1 (fr) * 2018-09-04 2020-03-06 Airbus Operations Ensemble turbomachine d'aeronef comportant un capot articule
FR3087497B1 (fr) * 2018-10-23 2020-09-25 Safran Nacelles Retention axiale haute pour un inverseur a grilles coulissantes a structure en d
GB201909171D0 (en) 2019-06-26 2019-08-07 Rolls Royce Plc Gas turbine engine cowl doors
FR3110547B1 (fr) * 2020-05-20 2022-04-22 Safran Nacelles Nacelle pour ensemble propulsif à très grand taux de dilution, comprenant une structure interne avant amovible et structurelle
FR3142455A1 (fr) * 2022-11-28 2024-05-31 Airbus Operations Système de propulsion d’un aéronef comportant une nacelle asymétrique

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2863620A (en) * 1952-10-04 1958-12-09 Sud Aviation Jet-propelled aircraft
US2879959A (en) * 1955-02-17 1959-03-31 Boeing Co Cowl securing means
US3541794A (en) * 1969-04-23 1970-11-24 Gen Electric Bifurcated fan duct thrust reverser
US4055041A (en) * 1974-11-08 1977-10-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Integrated gas turbine engine-nacelle
FR2291091A1 (fr) * 1974-11-13 1976-06-11 Snecma Dispositif de montage sur avion d'un turboreacteur
US4043522A (en) * 1975-12-22 1977-08-23 The Boeing Company Common pod for housing a plurality of different turbofan jet propulsion engines
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
US4278220A (en) * 1979-03-30 1981-07-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thrust reverser for a long duct fan engine
US4506850A (en) * 1983-01-04 1985-03-26 The Boeing Company Engine installation for aircraft
JPH0717238B2 (ja) * 1983-07-14 1995-03-01 ユナイテツド・テクノロジ−ズ・コ−ポレイシヨン 荷重分担アダプタを備えたガスタービンエンジン
FR2560854B1 (fr) * 1984-03-07 1986-09-12 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
US4585189A (en) * 1984-10-22 1986-04-29 Lockheed Corporation Counterbalanced cowling assembly for a pylon-mounted engine and nacelle therefor
US4825648A (en) * 1987-03-02 1989-05-02 General Electric Company Turbofan engine having a split cowl

Also Published As

Publication number Publication date
GB2212218A (en) 1989-07-19
GB2212218B (en) 1992-07-22
US4920744A (en) 1990-05-01
FR2622930A1 (fr) 1989-05-12
GB8825416D0 (en) 1988-11-30

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Legal Events

Date Code Title Description
CD Change of name or company name
TP Transmission of property