BRPI0908079A2 - Conjunto motor para aeronave, e, aeronave - Google Patents
Conjunto motor para aeronave, e, aeronaveInfo
- Publication number
- BRPI0908079A2 BRPI0908079A2 BRPI0908079-1A BRPI0908079A BRPI0908079A2 BR PI0908079 A2 BRPI0908079 A2 BR PI0908079A2 BR PI0908079 A BRPI0908079 A BR PI0908079A BR PI0908079 A2 BRPI0908079 A2 BR PI0908079A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- engine set
- engine
- Prior art date
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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
-
- 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
-
- 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)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0851280A FR2928136B1 (fr) | 2008-02-28 | 2008-02-28 | Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante. |
PCT/FR2009/050320 WO2009112777A2 (fr) | 2008-02-28 | 2009-02-27 | Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0908079A2 true BRPI0908079A2 (pt) | 2015-08-25 |
Family
ID=39810198
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0908079-1A BRPI0908079A2 (pt) | 2008-02-28 | 2009-02-27 | Conjunto motor para aeronave, e, aeronave |
Country Status (9)
Country | Link |
---|---|
US (1) | US9032740B2 (pt) |
EP (1) | EP2244944B1 (pt) |
JP (1) | JP2011513112A (pt) |
CN (1) | CN101945808B (pt) |
BR (1) | BRPI0908079A2 (pt) |
CA (1) | CA2715738C (pt) |
FR (1) | FR2928136B1 (pt) |
RU (1) | RU2487057C2 (pt) |
WO (1) | WO2009112777A2 (pt) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2928180B1 (fr) * | 2008-02-28 | 2010-04-02 | Airbus France | Ensemble moteur pour aeronef comprenant une structure annulaire de transfert d'efforts entourant le carter central d'un turboreacteur. |
FR2963390B1 (fr) * | 2010-07-30 | 2012-08-31 | Snecma | Turboreacteur lateral perfectionne pour limiter ses deformations |
FR2969700B1 (fr) * | 2010-12-23 | 2015-05-15 | Snecma | Systeme propulsif pour aeronef |
FR2975131B1 (fr) * | 2011-05-09 | 2015-12-25 | Snecma | Suspension du canal de flux froid d'un turboreacteur par des biellettes et des chapes radiales sur le carter d'echappement |
FR2981686B1 (fr) * | 2011-10-21 | 2016-05-20 | Snecma | Turbomachine comprenant un recepteur a helices contrarotatives supporte par une enveloppe structurale fixee au carter intermediaire |
WO2015010315A1 (en) | 2013-07-26 | 2015-01-29 | Mra Systems, Inc. | Aircraft engine pylon |
US10654577B2 (en) | 2017-02-22 | 2020-05-19 | General Electric Company | Rainbow flowpath low pressure turbine rotor assembly |
US11421627B2 (en) | 2017-02-22 | 2022-08-23 | General Electric Company | Aircraft and direct drive engine under wing installation |
US10414509B2 (en) * | 2017-02-23 | 2019-09-17 | United Technologies Corporation | Propulsor mounting for advanced body aircraft |
DE102017124043A1 (de) | 2017-10-16 | 2019-04-18 | Rolls-Royce Deutschland Ltd & Co Kg | Strahltriebwerk mit einer Anbindungsvorrichtung |
FR3093704B1 (fr) * | 2019-03-11 | 2021-06-11 | Airbus Operations Sas | Attache moteur arrière d’un ensemble propulsif d’aéronef |
CN110704940B (zh) * | 2019-08-30 | 2023-08-18 | 中国航空工业集团公司沈阳飞机设计研究所 | 飞机发动机安装交点位置偏差处理方法及发动机推力销 |
CN110745250B (zh) * | 2019-11-22 | 2023-04-18 | 中国航发沈阳黎明航空发动机有限责任公司 | 一种航空发动机点火附件装配式安装结构及安装方法 |
CN112572825B (zh) * | 2020-11-27 | 2022-12-13 | 北京星航机电装备有限公司 | 一种飞行器尾舱及其装配方法 |
US11428160B2 (en) | 2020-12-31 | 2022-08-30 | General Electric Company | Gas turbine engine with interdigitated turbine and gear assembly |
US11674414B2 (en) * | 2021-03-19 | 2023-06-13 | Pratt & Whitney Canada Corp. | Gas turbine engine and mount assembly therefor |
US11674415B2 (en) | 2021-08-20 | 2023-06-13 | Raytheon Technologies Corporation | Front section stiffness ratio |
US11555420B1 (en) | 2021-08-20 | 2023-01-17 | Raytheon Technologies Corporation | Frame connection between fan case and core housing in a gas turbine engine |
US11608796B1 (en) | 2021-11-12 | 2023-03-21 | Raytheon Technologies Corporation | Radial strut frame connection between fan case and core housing in a gas turbine engine |
US11686220B2 (en) | 2021-11-12 | 2023-06-27 | Raytheon Technologies Corporation | H-frame connection between fan case and core housing in a gas turbine engine |
US11708772B2 (en) | 2021-11-12 | 2023-07-25 | Raytheon Technologies Corporation | Triangular-frame connection between fan case and core housing in a gas turbine engine |
Family Cites Families (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2753140A (en) * | 1951-07-28 | 1956-07-03 | United Aircraft Corp | Engine mount |
US2949268A (en) * | 1956-07-30 | 1960-08-16 | Snecma | Aircraft jet propulsion unit mount |
US3398535A (en) * | 1966-05-25 | 1968-08-27 | Gen Electric | Engine supporting structure |
GB1516980A (en) * | 1974-12-24 | 1978-07-05 | Rolls Royce | Mounting ducted fan gas turbine engines on aircraft |
US4266741A (en) * | 1978-05-22 | 1981-05-12 | The Boeing Company | Mounting apparatus for fan jet engine having mixed flow nozzle installation |
RU1133819C (pt) * | 1982-12-15 | 2000-11-27 | ||
FR2677953B1 (fr) * | 1991-06-19 | 1993-09-10 | Snecma | Structure de suspension arriere d'un turboreacteur. |
US5226288A (en) * | 1991-06-21 | 1993-07-13 | Rohr, Inc. | Torque link fan jet engine support for reducing engine bending |
US5319922A (en) * | 1992-12-04 | 1994-06-14 | General Electric Company | Aircraft gas turbine engine backbone deflection control |
GB2275308B (en) * | 1993-02-20 | 1997-02-26 | Rolls Royce Plc | A mounting for coupling a turbofan gas turbine engine to an aircraft structure |
US5452575A (en) * | 1993-09-07 | 1995-09-26 | General Electric Company | Aircraft gas turbine engine thrust mount |
GB9602130D0 (en) * | 1996-02-02 | 1996-04-03 | Rolls Royce Plc | Improved method of combining ducted fan gas turbine engine modules and aircraft structure |
JPH09324699A (ja) * | 1996-06-05 | 1997-12-16 | Ishikawajima Harima Heavy Ind Co Ltd | ガスタービンのフレーム構造 |
FR2873985B1 (fr) * | 2004-08-04 | 2006-11-24 | Airbus France Sas | Ensemble moteur pour aeronef |
FR2873986B1 (fr) * | 2004-08-04 | 2007-12-21 | Airbus France Sas | Ensemble moteur pour aeronef |
FR2873987B1 (fr) * | 2004-08-05 | 2006-11-24 | Airbus France Sas | Ensemble moteur pour aeronef |
FR2883839B1 (fr) * | 2005-03-29 | 2007-06-29 | Snecma Moteurs Sa | Suspension arriere de turboreacteur |
FR2885877B1 (fr) * | 2005-05-23 | 2008-12-12 | Airbus France Sas | Mat d'accrochage de turboreacteur pour aeronef |
CN100575690C (zh) * | 2005-09-12 | 2009-12-30 | 波音公司 | 包括锁定机构的反推力装置及其制造方法 |
FR2891244B1 (fr) | 2005-09-26 | 2009-04-03 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef |
FR2891243B1 (fr) | 2005-09-26 | 2009-04-03 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef |
FR2891245B1 (fr) | 2005-09-26 | 2007-10-26 | Airbus France Sas | Procede de montage d'un moteur d'aeronef sur une structure rigide d'un mat d'accrochage du moteur |
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 |
FR2891251B1 (fr) | 2005-09-28 | 2009-04-03 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef |
FR2891526B1 (fr) * | 2005-10-03 | 2007-11-02 | Airbus France Sas | Mat d'accrochage de turboreacteur pour aeronef |
FR2900907B1 (fr) * | 2006-05-09 | 2008-12-19 | Airbus France Sas | Ensemble moteur pour aeronef a nacelle et mat integres |
-
2008
- 2008-02-28 FR FR0851280A patent/FR2928136B1/fr not_active Expired - Fee Related
-
2009
- 2009-02-27 US US12/918,500 patent/US9032740B2/en active Active
- 2009-02-27 BR BRPI0908079-1A patent/BRPI0908079A2/pt not_active IP Right Cessation
- 2009-02-27 CA CA2715738A patent/CA2715738C/fr not_active Expired - Fee Related
- 2009-02-27 WO PCT/FR2009/050320 patent/WO2009112777A2/fr active Application Filing
- 2009-02-27 CN CN2009801060825A patent/CN101945808B/zh not_active Expired - Fee Related
- 2009-02-27 JP JP2010548158A patent/JP2011513112A/ja active Pending
- 2009-02-27 RU RU2010139658/11A patent/RU2487057C2/ru not_active IP Right Cessation
- 2009-02-27 EP EP09720756.7A patent/EP2244944B1/fr not_active Not-in-force
Also Published As
Publication number | Publication date |
---|---|
EP2244944A2 (fr) | 2010-11-03 |
CA2715738A1 (fr) | 2009-09-17 |
FR2928136B1 (fr) | 2010-04-02 |
US9032740B2 (en) | 2015-05-19 |
CN101945808B (zh) | 2013-09-18 |
CA2715738C (fr) | 2015-11-24 |
US20110197595A1 (en) | 2011-08-18 |
FR2928136A1 (fr) | 2009-09-04 |
RU2487057C2 (ru) | 2013-07-10 |
EP2244944B1 (fr) | 2019-01-09 |
RU2010139658A (ru) | 2012-04-10 |
WO2009112777A3 (fr) | 2009-10-29 |
JP2011513112A (ja) | 2011-04-28 |
WO2009112777A2 (fr) | 2009-09-17 |
CN101945808A (zh) | 2011-01-12 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BRPI0908079A2 (pt) | Conjunto motor para aeronave, e, aeronave | |
BRPI0907771A2 (pt) | Conjunto motor para aeronave, e, aeronave | |
BRPI0821929A2 (pt) | Nacela para motor turbojato | |
BRPI0821504A2 (pt) | nacela para motor de avião | |
BRPI0812844A2 (pt) | Estribo de afixação para motor de aeronave, conjunto motor para aeronave, e, aeronave | |
BRPI0922745A2 (pt) | ventoinha para turbomáquina de aeronave e turbomáquina para aeronave. | |
BRPI0717730A2 (pt) | Nacela para motor turbojato de contorno, conjunto de propulsão e avião | |
BRPI0907959A2 (pt) | Conjunto motor para aeronave, e, aeronave | |
BRPI0812818A2 (pt) | Turbo-reator para aeronave | |
BRPI0907309A2 (pt) | transmissão unidirecional para motor | |
DK2481143T3 (da) | Motor | |
BRPI0820878A2 (pt) | fuselagem com atenuação acústica para aeronave | |
DE602008005797D1 (de) | Motor | |
DE602008000573D1 (de) | Triebwerk | |
BRPI0821412A2 (pt) | Configuração otimizada de motores para aeronave | |
BRPI1007029A2 (pt) | conjunto de suspensão para motor turbojato de aeronaves | |
BRPI0810535A2 (pt) | Nacela para turbojato e avião. | |
BRPI0822363A2 (pt) | Nacela de motor turbojato | |
BRPI0822127A2 (pt) | Nacela para motor turbojato e aeronave | |
BR112014013202A2 (pt) | estrutura acústica celular, especificamente para um motor turbojato, e motor turbojato | |
BRPI1009760A2 (pt) | combustível para aviação. | |
ES2388023B2 (es) | Dispositivo de escape para motor. | |
BRPI0914044A2 (pt) | arranjo de entrada de ar para aeronave | |
DE602008002290D1 (de) | Triebwerk | |
BRPI0921772A2 (pt) | nacela de motor turbojato |
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 A 6A ANUIDADE. |
|
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 2344 DE 08-12-2015 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. |