ATE547324T1 - Antriebsanordnung für ein flugzeug mit gleitgondel - Google Patents

Antriebsanordnung für ein flugzeug mit gleitgondel

Info

Publication number
ATE547324T1
ATE547324T1 AT08760269T AT08760269T ATE547324T1 AT E547324 T1 ATE547324 T1 AT E547324T1 AT 08760269 T AT08760269 T AT 08760269T AT 08760269 T AT08760269 T AT 08760269T AT E547324 T1 ATE547324 T1 AT E547324T1
Authority
AT
Austria
Prior art keywords
turbojet
aircraft
gondola
sliding
drive arrangement
Prior art date
Application number
AT08760269T
Other languages
English (en)
Inventor
Frederic Journade
Laurent Lafont
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
Application granted granted Critical
Publication of ATE547324T1 publication Critical patent/ATE547324T1/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
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • 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
    • F05D2250/00—Geometry
    • F05D2250/40—Movement of components
    • F05D2250/41—Movement of components with one degree of freedom
    • 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
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Wrappers (AREA)
AT08760269T 2007-06-01 2008-05-30 Antriebsanordnung für ein flugzeug mit gleitgondel ATE547324T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0755409A FR2916737B1 (fr) 2007-06-01 2007-06-01 Ensemble moteur pour aeronef a nacelle coulissante.
PCT/EP2008/056680 WO2008145725A1 (fr) 2007-06-01 2008-05-30 Ensemble moteur pour aeronef a nacelle coulissante

Publications (1)

Publication Number Publication Date
ATE547324T1 true ATE547324T1 (de) 2012-03-15

Family

ID=38926103

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08760269T ATE547324T1 (de) 2007-06-01 2008-05-30 Antriebsanordnung für ein flugzeug mit gleitgondel

Country Status (10)

Country Link
US (1) US8226027B2 (de)
EP (1) EP2152582B1 (de)
JP (1) JP2010529346A (de)
CN (1) CN101678897A (de)
AT (1) ATE547324T1 (de)
BR (1) BRPI0811239A2 (de)
CA (1) CA2689111C (de)
FR (1) FR2916737B1 (de)
RU (1) RU2472678C2 (de)
WO (1) WO2008145725A1 (de)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2926790B1 (fr) * 2008-01-30 2010-02-12 Aircelle Sa Systeme de guidage pour la maintenance d'une nacelle d'aeronef
FR2933144B1 (fr) * 2008-06-26 2012-08-17 Airbus France Nacelle pour aeronef comportant des moyens inverseurs de poussee et aeronef comportant au moins une telle nacelle
US8713910B2 (en) 2009-07-31 2014-05-06 General Electric Company Integrated thrust reverser/pylon assembly
FR2965859B1 (fr) * 2010-10-07 2012-11-02 Snecma Dispositif de traitement acoustique du bruit emis par un turboreacteur
FR2969122B1 (fr) 2010-12-20 2012-12-28 Aircelle Sa Structure interne pour une nacelle pour un turboreacteur double flux d'un aeronef
FR2978126B1 (fr) * 2011-07-22 2013-09-27 Airbus Operations Sas Nacelle pour ensemble propulsif a tuyere a section variable
FR2979613B1 (fr) * 2011-09-01 2014-06-13 Snecma Ensemble forme par un turbomoteur et son systeme d'attache a une structure d'aeronef
CN102621899B (zh) * 2011-11-07 2014-12-10 中国商用飞机有限责任公司 一种打开飞机动力装置反推系统的方法
FR2989952B1 (fr) * 2012-04-27 2014-04-18 Aircelle Sa Nacelle de turboreacteur a section aval
US10145335B2 (en) * 2012-09-28 2018-12-04 United Technologies Corporation Turbomachine thrust reverser
US10006405B2 (en) 2012-11-30 2018-06-26 General Electric Company Thrust reverser system with translating-rotating blocker doors and method of operation
US20140151497A1 (en) * 2012-12-04 2014-06-05 Ge Aviation Systems Llc Engine pylon for an aircraft
FR2999155B1 (fr) * 2012-12-12 2014-11-21 Aircelle Sa Ensemble propulsif pour aeronef
CN103047012B (zh) * 2013-01-11 2017-02-08 中国兵器工业集团第七0研究所 一种引射中冷燃气轮机
FR3002288B1 (fr) * 2013-02-20 2022-11-25 Snecma Suspension d'un turboreacteur par double support arriere
US9611048B2 (en) 2013-02-22 2017-04-04 United Technologies Corporation ATR axial V-groove
US9435293B2 (en) * 2013-02-22 2016-09-06 United Technologies Corporation Full ring sliding nacelle with thrust reverser
US9822734B2 (en) 2013-02-22 2017-11-21 United Technologies Corporation Tandem thrust reverser with multi-bar linkage
US8979056B2 (en) * 2013-05-24 2015-03-17 Hamilton Sundstrand Corporation Cabin air compressor support bracket
WO2015054233A1 (en) * 2013-10-07 2015-04-16 Rohr, Inc. Hybrid inner fixed structure with metallic and composite construction
FR3039228B1 (fr) * 2015-07-22 2020-01-03 Safran Aircraft Engines Aeronef comprenant un propulseur arriere carene avec stator d'entree comprenant une fonction soufflage
US10040560B2 (en) * 2015-09-30 2018-08-07 The Boeing Company Trailing edge core compartment vent for an aircraft engine
US10752371B2 (en) * 2016-09-30 2020-08-25 General Electric Company Translating nacelle wall for an aircraft tail mounted fan section
FR3097260B1 (fr) * 2019-06-12 2021-06-11 Safran Aircraft Engines Carter de soufflante de turboréacteur
US11149564B2 (en) * 2019-06-24 2021-10-19 Rohr, Inc. Nacelle thrust reverser compression rod supporting system
CN111846251B (zh) * 2020-07-10 2024-03-19 山东太古飞机工程有限公司 一种用于发动机进气口、排气及尾喷嘴的防沙保护装置
CN115196024B (zh) * 2022-09-16 2022-12-09 中国航空工业集团公司西安飞机设计研究所 一种用于飞行器的动力设备

Family Cites Families (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3067968A (en) * 1958-12-29 1962-12-11 Heppenstall Charles William Retractable jet engine noise suppressor
GB1130268A (en) * 1967-07-01 1968-10-16 Rolls Royce Improvements in or relating to gas turbine by-pass engines
US3541794A (en) * 1969-04-23 1970-11-24 Gen Electric Bifurcated fan duct thrust reverser
US3614037A (en) * 1969-09-22 1971-10-19 Boeing Co Aircraft combination thrust reverser and sound suppressor and a particular full range balanced thrust reverser
US3598318A (en) * 1970-04-10 1971-08-10 Boeing Co Movable acoustic splitter for nozzle area control and thrust reversal
GB1375868A (de) * 1972-09-22 1974-11-27
US3829020A (en) * 1973-06-13 1974-08-13 Boeing Co Translating sleeve variable area nozzle and thrust reverser
US3897001A (en) * 1974-06-12 1975-07-29 Gen Electric Nozzle and auxiliary inlet arrangement for gas turbine engine
US4005822A (en) * 1975-12-22 1977-02-01 Rohr Industries, Inc. Fan duct thrust reverser
FR2349738A1 (fr) * 1976-04-28 1977-11-25 Gen Electric Mecanisme d'inversion de poussee
US4228651A (en) * 1977-11-29 1980-10-21 Rolls-Royce Limited Ducted fan gas turbine engine
CA1185101A (en) * 1980-03-03 1985-04-09 Daniel J. Lahti Drag-reducing nacelle
US4373328A (en) * 1980-10-22 1983-02-15 United Technologies Corporation Thrust reverser
FR2496766A1 (fr) * 1980-12-23 1982-06-25 Snecma Dispositif de guidage de carenage mobile d'un systeme d'inversion de poussee
US4506850A (en) * 1983-01-04 1985-03-26 The Boeing Company Engine installation for aircraft
US4533098A (en) * 1983-06-20 1985-08-06 General Electric Company Thrust reverser attachment
FR2560854B1 (fr) * 1984-03-07 1986-09-12 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
US4600619A (en) * 1984-12-31 1986-07-15 The Boeing Company Continuously wound filament structure for use in noise attenuation element
SU1320997A1 (ru) * 1985-04-01 2004-12-20 В.Ф. Гордеев Створка гондолы летательного аппарата
US4825648A (en) * 1987-03-02 1989-05-02 General Electric Company Turbofan engine having a split cowl
FR2613773B1 (fr) * 1987-04-08 1990-11-30 Snecma Panneau acoustique pour garniture insonorisante et turboreacteur comportant une telle garniture
FR2645500B1 (fr) * 1989-04-05 1991-05-31 Hispano Suiza Sa Capotage mobile pour moteur d'avion
EP0591154B1 (de) * 1989-11-06 1996-08-14 THE NORDAM GROUP, Inc. Schalldämpfer mit zentralkörper für ein mantelstromtriebwerk
US5060471A (en) * 1989-11-06 1991-10-29 501 Nordam Jet engine noise reduction system
US5228641A (en) * 1991-08-15 1993-07-20 Rohr, Inc. Cascade type aircraft engine thrust reverser with hidden link actuator
US5251435A (en) 1991-10-30 1993-10-12 General Electric Company Reverser inner cowl with integral bifurcation walls and core cowl
US5782082A (en) * 1996-06-13 1998-07-21 The Boeing Company Aircraft engine acoustic liner
US5806302A (en) * 1996-09-24 1998-09-15 Rohr, Inc. Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
US5975237A (en) * 1997-07-30 1999-11-02 The Boeing Company Reinforcing structure for engine nacelle acoustic panel
US6170254B1 (en) * 1998-12-18 2001-01-09 Rohr, Inc. Translating sleeve for cascade type thrust reversing system for fan gas turbine engine for an aircraft
US6340135B1 (en) * 2000-05-30 2002-01-22 Rohr, Inc. Translating independently mounted air inlet system for aircraft turbofan jet engine
US6557799B1 (en) * 2001-11-09 2003-05-06 The Boeing Company Acoustic treated thrust reverser bullnose fairing assembly
US20060145001A1 (en) * 2004-12-30 2006-07-06 Smith Matthew C Fan cowl door elimination
FR2891250B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
FR2891248B1 (fr) * 2005-09-28 2009-05-01 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
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

Also Published As

Publication number Publication date
CN101678897A (zh) 2010-03-24
CA2689111C (fr) 2014-10-21
FR2916737A1 (fr) 2008-12-05
FR2916737B1 (fr) 2010-05-28
US20100170984A1 (en) 2010-07-08
WO2008145725A1 (fr) 2008-12-04
RU2009149458A (ru) 2011-07-20
US8226027B2 (en) 2012-07-24
JP2010529346A (ja) 2010-08-26
RU2472678C2 (ru) 2013-01-20
EP2152582B1 (de) 2012-02-29
EP2152582A1 (de) 2010-02-17
CA2689111A1 (fr) 2008-12-04
BRPI0811239A2 (pt) 2014-11-04

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