BRPI0811239A2 - Conjunto motor para aeronave, e, aeronave - Google Patents

Conjunto motor para aeronave, e, aeronave

Info

Publication number
BRPI0811239A2
BRPI0811239A2 BRPI0811239-8A2A BRPI0811239A BRPI0811239A2 BR PI0811239 A2 BRPI0811239 A2 BR PI0811239A2 BR PI0811239 A BRPI0811239 A BR PI0811239A BR PI0811239 A2 BRPI0811239 A2 BR PI0811239A2
Authority
BR
Brazil
Prior art keywords
turbojet
aircraft
nacelle
attachment pylon
engine
Prior art date
Application number
BRPI0811239-8A2A
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
Publication of BRPI0811239A2 publication Critical patent/BRPI0811239A2/pt

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)
BRPI0811239-8A2A 2007-06-01 2008-05-30 Conjunto motor para aeronave, e, aeronave BRPI0811239A2 (pt)

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
BRPI0811239A2 true BRPI0811239A2 (pt) 2014-11-04

Family

ID=38926103

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0811239-8A2A BRPI0811239A2 (pt) 2007-06-01 2008-05-30 Conjunto motor para aeronave, e, aeronave

Country Status (10)

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

Families Citing this family (27)

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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
US9670876B2 (en) 2013-02-22 2017-06-06 United Technologies Corporation Tandem thrust reverser with sliding rails
US9617009B2 (en) 2013-02-22 2017-04-11 United Technologies Corporation ATR full ring sliding nacelle
US9435293B2 (en) * 2013-02-22 2016-09-06 United Technologies Corporation Full ring sliding nacelle with thrust reverser
US8979056B2 (en) * 2013-05-24 2015-03-17 Hamilton Sundstrand Corporation Cabin air compressor support bracket
CN110259599B (zh) * 2013-10-07 2021-11-09 罗尔公司 具有金属和复合构造的混合式内部固定结构
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

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Also Published As

Publication number Publication date
FR2916737A1 (fr) 2008-12-05
RU2009149458A (ru) 2011-07-20
ATE547324T1 (de) 2012-03-15
JP2010529346A (ja) 2010-08-26
FR2916737B1 (fr) 2010-05-28
US20100170984A1 (en) 2010-07-08
CA2689111C (fr) 2014-10-21
CN101678897A (zh) 2010-03-24
US8226027B2 (en) 2012-07-24
WO2008145725A1 (fr) 2008-12-04
EP2152582A1 (fr) 2010-02-17
EP2152582B1 (fr) 2012-02-29
CA2689111A1 (fr) 2008-12-04
RU2472678C2 (ru) 2013-01-20

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE AS 6A E 7A ANUIDADES.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2343 DE 01-12-2015 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.

B350 Update of information on the portal [chapter 15.35 patent gazette]