ATE549244T1 - Gondel für ein flugzeugtriebwerk - Google Patents

Gondel für ein flugzeugtriebwerk

Info

Publication number
ATE549244T1
ATE549244T1 AT07870326T AT07870326T ATE549244T1 AT E549244 T1 ATE549244 T1 AT E549244T1 AT 07870326 T AT07870326 T AT 07870326T AT 07870326 T AT07870326 T AT 07870326T AT E549244 T1 ATE549244 T1 AT E549244T1
Authority
AT
Austria
Prior art keywords
turbojet
gondola
downstream portion
aircraft engine
nacelle
Prior art date
Application number
AT07870326T
Other languages
English (en)
Inventor
Guy Vauchel
Nicolas Hillereau
Jerome Collier
Pierre-Alain Chouard
Guillaume Lefort
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
Application granted granted Critical
Publication of ATE549244T1 publication Critical patent/ATE549244T1/de

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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)
  • Gear Transmission (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
AT07870326T 2007-02-14 2007-11-23 Gondel für ein flugzeugtriebwerk ATE549244T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0701059A FR2912378B1 (fr) 2007-02-14 2007-02-14 Nacelle de moteur a reaction pour un avion
PCT/FR2007/001923 WO2008102068A1 (fr) 2007-02-14 2007-11-23 Nacelle de moteur a reaction pour un avion

Publications (1)

Publication Number Publication Date
ATE549244T1 true ATE549244T1 (de) 2012-03-15

Family

ID=38291061

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07870326T ATE549244T1 (de) 2007-02-14 2007-11-23 Gondel für ein flugzeugtriebwerk

Country Status (10)

Country Link
US (1) US8951006B2 (de)
EP (1) EP2117932B1 (de)
CN (1) CN101588967B (de)
AT (1) ATE549244T1 (de)
BR (1) BRPI0721237A2 (de)
CA (1) CA2677423C (de)
ES (1) ES2383560T3 (de)
FR (1) FR2912378B1 (de)
RU (1) RU2442726C2 (de)
WO (1) WO2008102068A1 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2916737B1 (fr) * 2007-06-01 2010-05-28 Airbus France Ensemble moteur pour aeronef a nacelle coulissante.
US8426961B2 (en) 2010-06-25 2013-04-23 Taiwan Semiconductor Manufacturing Company, Ltd. Embedded 3D interposer structure
FR2965588B1 (fr) * 2010-10-04 2015-05-01 Aircelle Sa Ensemble propulsif d'aeronef
FR2965589B1 (fr) * 2010-10-04 2015-05-15 Aircelle Sa Inverseur de poussee
CN103029839A (zh) * 2011-12-23 2013-04-10 摩尔动力(北京)技术股份有限公司 外燃飞行器
FR2999155B1 (fr) 2012-12-12 2014-11-21 Aircelle Sa Ensemble propulsif pour aeronef
US9611048B2 (en) 2013-02-22 2017-04-04 United Technologies Corporation ATR axial V-groove
US9822734B2 (en) 2013-02-22 2017-11-21 United Technologies Corporation Tandem thrust reverser with multi-bar linkage
FR3047522B1 (fr) * 2016-02-04 2018-03-16 Safran Aircraft Engines Ensemble propulsif pour aeronef
FR3075176B1 (fr) * 2017-12-18 2020-11-06 Safran Aircraft Engines Ensemble de capot ouvrant et mecanisme de deploiement
GB201806563D0 (en) 2018-04-23 2018-06-06 Rolls Royce Plc Gas turbine engine keel beam
GB201806564D0 (en) * 2018-04-23 2018-06-06 Rolls Royce Plc Gas turbine engine inner barrel
USD885438S1 (en) * 2019-10-05 2020-05-26 Mountain Aerospace Research Solutions, Inc. Engine
US11174817B2 (en) 2020-01-29 2021-11-16 Mountain Aerospace Research Solutions, Inc. Air-Breathing rocket engine
US11002225B1 (en) 2020-01-29 2021-05-11 Mountain Aerospace Research Solutions, Inc. Air-breathing rocket engine
US10961952B1 (en) 2020-01-29 2021-03-30 Mountain Aerospace Research Solutions, Inc. Air-breathing rocket engine
US11220979B1 (en) 2020-11-10 2022-01-11 Mountain Aerospace Research Solutions, Inc. Liquid-cooled air-breathing rocket engine

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2291091A1 (fr) * 1974-11-13 1976-06-11 Snecma Dispositif de montage sur avion d'un turboreacteur
FR2560461B1 (fr) 1984-02-29 1988-03-18 Cem Comp Electro Mec Machine electrodynamique vernier
FR2560854B1 (fr) * 1984-03-07 1986-09-12 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
FR2622930B1 (fr) * 1987-11-06 1990-03-23 Aerospatiale Capotage pour turboreacteur a double flux
GB8822798D0 (en) * 1988-09-28 1988-11-02 Short Brothers Ltd Ducted fan turbine engine
FR2645500B1 (fr) * 1989-04-05 1991-05-31 Hispano Suiza Sa Capotage mobile pour moteur d'avion
JPH0614648Y2 (ja) 1989-04-07 1994-04-20 株式会社吉原 温風パルス発生器
GB9301457D0 (en) * 1993-01-26 1993-03-17 Short Brothers Plc An aircraft propulsuve power unit
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
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

Also Published As

Publication number Publication date
WO2008102068A1 (fr) 2008-08-28
FR2912378B1 (fr) 2009-03-20
CN101588967A (zh) 2009-11-25
CA2677423A1 (fr) 2008-08-28
RU2442726C2 (ru) 2012-02-20
ES2383560T3 (es) 2012-06-22
US20100008772A1 (en) 2010-01-14
US8951006B2 (en) 2015-02-10
FR2912378A1 (fr) 2008-08-15
BRPI0721237A2 (pt) 2014-03-18
EP2117932B1 (de) 2012-03-14
RU2009133821A (ru) 2011-03-20
CA2677423C (fr) 2015-03-24
CN101588967B (zh) 2013-03-27
EP2117932A1 (de) 2009-11-18

Similar Documents

Publication Publication Date Title
ATE549244T1 (de) Gondel für ein flugzeugtriebwerk
WO2009109713A3 (fr) Système de guidage pour la maintenance d'une nacelle d'aéronef
ATE538033T1 (de) Gondelrückseitenbaugruppe für einen turbostrahlmotor
FR2980173B1 (fr) Ensemble arriere de nacelle pour turboreacteur
ATE547324T1 (de) Antriebsanordnung für ein flugzeug mit gleitgondel
ATE535444T1 (de) Anlage für eine flugzeuggondelführungssystem
ATE511011T1 (de) Schubumkehreinheit für ein düsentriebwerk
WO2011066365A3 (en) Variable area fan nozzle bearing track
EP2138697A3 (de) Hinterer Kaskadenring mit Abschnitt zur Strömungsumlenkung, sowie zugehörige Kaskaden-Baugruppe einer Schubumkehrvorrichtung und Gondel eines Flugzeugtriebwerks
ATE540197T1 (de) Laufschaufelanordnung, insbesondere für eine gasturbine
EP1801356A3 (de) Brennkammer-Turbinen-Übergang
EP2527742A3 (de) System und Verfahren zur Strömungssteuerung in einem Gasturbinenmotor
GB201112001D0 (en) Turbine blade assembly including a damper
GB2443982A (en) Bleed off valve system
BR112012013131A2 (pt) estrutura de suporte para uma nacela de motor turbojato, nacela de aeronaves.
EP1895140A3 (de) Lüfterabgasdüse für den Motor eines Turbolüfters
ATE476594T1 (de) Fandüse mit variablem querschnitt für eine gasturbinentriebwerksfangondel mit antriebsringbetätigungssystem
SA515360472B1 (ar) جناح زاوية شفرة توربين بنتوءات ضخ
ATE554271T1 (de) Abgasturbolader für eine brennkraftmaschine
EP2144003A3 (de) Brennkammerwand für einen Gasturbinenmotor
EP1762704A3 (de) Leitschaufelanordnung mit Manschette
EP2402566A3 (de) Hinterkanteneinlagenstützmechanismus und federbelasteter Einlagenstoppmechanismus
BR112014030695A2 (pt) mancal, sistema para mudar o ângulo de inclinação das pás de uma hélice de motor de turboeixo, e, motor de turbina
FR2999651B1 (fr) Extension de carter intermediaire a conception amelioree
BRPI0814918A2 (pt) "nacela para um motor a jato e aeronave"