BR112013014444A2 - nacela para um motor turbojato de fluxo secundário e aeronave incluindo uma asa e uma nacela - Google Patents
nacela para um motor turbojato de fluxo secundário e aeronave incluindo uma asa e uma nacelaInfo
- Publication number
- BR112013014444A2 BR112013014444A2 BR112013014444A BR112013014444A BR112013014444A2 BR 112013014444 A2 BR112013014444 A2 BR 112013014444A2 BR 112013014444 A BR112013014444 A BR 112013014444A BR 112013014444 A BR112013014444 A BR 112013014444A BR 112013014444 A2 BR112013014444 A2 BR 112013014444A2
- Authority
- BR
- Brazil
- Prior art keywords
- nacelle
- wing
- turbojet engine
- aircraft including
- flow turbojet
- Prior art date
Links
Classifications
-
- 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
- F02K1/76—Control or regulation of thrust reversers
- F02K1/766—Control or regulation of thrust reversers with blocking systems or locking devices; Arrangement of locking devices for thrust reversers
-
- 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
- B64D29/06—Attaching of nacelles, fairings or cowlings
-
- 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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- 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
-
- 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
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1060478A FR2968635B1 (fr) | 2010-12-14 | 2010-12-14 | Nacelle pour turboreacteur d’aeronef double flux |
PCT/FR2011/052706 WO2012080604A1 (fr) | 2010-12-14 | 2011-11-18 | Nacelle pour turboreacteur d'aeronef double flux |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112013014444A2 true BR112013014444A2 (pt) | 2016-09-13 |
Family
ID=44275688
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112013014444A BR112013014444A2 (pt) | 2010-12-14 | 2011-11-18 | nacela para um motor turbojato de fluxo secundário e aeronave incluindo uma asa e uma nacela |
Country Status (8)
Country | Link |
---|---|
US (1) | US9334831B2 (pt) |
EP (1) | EP2651764B1 (pt) |
CN (1) | CN103261025B (pt) |
BR (1) | BR112013014444A2 (pt) |
CA (1) | CA2820774A1 (pt) |
FR (1) | FR2968635B1 (pt) |
RU (1) | RU2577741C2 (pt) |
WO (1) | WO2012080604A1 (pt) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8727275B2 (en) | 2012-01-27 | 2014-05-20 | Rohr, Inc. | Nacelle |
US9739235B2 (en) | 2014-03-21 | 2017-08-22 | Rohr, Inc. | Thrust reverser for a turbofan engine |
US9976516B2 (en) | 2014-03-21 | 2018-05-22 | Rohr, Inc. | Thrust reverser for a turbofan engine |
US9938929B2 (en) | 2014-03-21 | 2018-04-10 | Rohr, Inc. | Thrust reverser for a turbofan engine |
US9611808B2 (en) | 2014-03-21 | 2017-04-04 | Rohr, Inc. | Blocker door lock mechanism of a thrust reverser for a turbofan engine |
FR3020344B1 (fr) * | 2014-04-24 | 2016-05-13 | Airbus Operations Sas | Assemblage pour un aeronef comportant un panneau d'acces mobile |
FR3023324B1 (fr) | 2014-07-01 | 2020-04-24 | Safran Nacelles | Inverseur de poussee d’une nacelle de turboreacteur, comprenant des decoupes d’evitement du bec mobile de l’aile |
US9816396B2 (en) | 2014-10-16 | 2017-11-14 | Honeywell International Inc. | Integrated outer flowpath ducting and front frame system for use in a turbofan engine and method for making same |
US9926884B2 (en) | 2015-02-19 | 2018-03-27 | Rohr, Inc. | Slat-thrust reverser clearance |
FR3043655B1 (fr) * | 2015-11-18 | 2019-05-10 | Safran Nacelles | Trappe d’acces a une charniere d’un mat d’une nacelle d’aeronef equipe d’un rabat mobile |
FR3074226B1 (fr) * | 2017-11-30 | 2020-09-25 | Safran Nacelles | Inverseur de poussee d’une nacelle de moteur d’aeronef comprenant un panneau d’evitement d’un bec mobile de l’aile, et nacelle associee |
US11085395B2 (en) | 2017-12-22 | 2021-08-10 | Airbus Operations S.A.S. | Nacelle system and methods of operation |
CN109956044B (zh) * | 2017-12-22 | 2022-03-11 | 空中客车运营简化股份公司 | 喷气发动机的短舱 |
US11002222B2 (en) * | 2018-03-21 | 2021-05-11 | Honeywell International Inc. | Systems and methods for thrust reverser with temperature and fluid management |
FR3085726B1 (fr) * | 2018-09-07 | 2020-12-11 | Safran Nacelles | Inverseur de poussee a structure mobile en c pour ensemble propulsif d’aeronef, et procede de maintenance s’y rapportant |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3344604A (en) * | 1965-12-14 | 1967-10-03 | Gen Dynamics Corp | Apparatus for selectively reversing the thrust of front fan jet engines |
US4629146A (en) * | 1985-01-30 | 1986-12-16 | Rohr Industries, Inc. | Hold open rod for hinged section of nacelle system |
US4884772A (en) * | 1986-07-28 | 1989-12-05 | The Boeing Company | Cantilevered vortex control device |
US5046689A (en) * | 1989-04-19 | 1991-09-10 | The Boeing Company | Cowling interlock system |
FR2740834B1 (fr) * | 1995-11-02 | 1997-12-05 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a double flux muni de portes secondaires |
EP0852290A1 (en) * | 1996-12-19 | 1998-07-08 | SOCIETE DE CONSTRUCTION DES AVIONS HUREL-DUBOIS (société anonyme) | Thrust reverser for high bypass fan engine |
WO2008045070A1 (en) * | 2006-10-12 | 2008-04-17 | United Technologies Corporation | Variable area fan nozzle thrust reverser |
FR2911372B1 (fr) * | 2007-01-15 | 2009-02-27 | Aircelle Sa | Inverseur de poussee translatable pour moteur a reaction |
US20080258016A1 (en) * | 2007-04-23 | 2008-10-23 | Gukeisen Robert L | Nacelle assembly without lower bi-fi splitter |
FR2920408B1 (fr) * | 2007-08-30 | 2010-02-19 | Snecma | Pylone de suspension d'un moteur sous une aile d'avion |
US8127531B2 (en) * | 2008-11-11 | 2012-03-06 | The Boeing Company | Radially translating fan nozzle nacelle |
US8316632B2 (en) * | 2009-02-25 | 2012-11-27 | Spirit Aerosystems, Inc. | Thrust reverser configuration for a short fan duct |
US8443586B2 (en) * | 2009-11-24 | 2013-05-21 | United Technologies Corporation | Variable area fan nozzle bearing track |
US8875486B2 (en) * | 2010-05-17 | 2014-11-04 | Rohr, Inc. | Guide system for nacelle assembly |
FR2962977B1 (fr) * | 2010-07-20 | 2012-08-17 | Airbus Operations Sas | Nacelle pour aeronef |
US8727275B2 (en) * | 2012-01-27 | 2014-05-20 | Rohr, Inc. | Nacelle |
US20140216005A1 (en) * | 2012-09-28 | 2014-08-07 | United Technologies Corporation | Gas Turbine Engine Assembly Including A Thrust Reverser |
US9670876B2 (en) * | 2013-02-22 | 2017-06-06 | United Technologies Corporation | Tandem thrust reverser with sliding rails |
-
2010
- 2010-12-14 FR FR1060478A patent/FR2968635B1/fr active Active
-
2011
- 2011-11-18 CN CN201180060165.2A patent/CN103261025B/zh not_active Expired - Fee Related
- 2011-11-18 CA CA2820774A patent/CA2820774A1/fr not_active Abandoned
- 2011-11-18 EP EP11802482.7A patent/EP2651764B1/fr active Active
- 2011-11-18 BR BR112013014444A patent/BR112013014444A2/pt not_active IP Right Cessation
- 2011-11-18 RU RU2013131841/11A patent/RU2577741C2/ru not_active IP Right Cessation
- 2011-11-18 WO PCT/FR2011/052706 patent/WO2012080604A1/fr active Application Filing
-
2013
- 2013-06-14 US US13/917,905 patent/US9334831B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR2968635B1 (fr) | 2012-12-14 |
EP2651764A1 (fr) | 2013-10-23 |
EP2651764B1 (fr) | 2016-12-14 |
FR2968635A1 (fr) | 2012-06-15 |
US9334831B2 (en) | 2016-05-10 |
CN103261025A (zh) | 2013-08-21 |
US20130280052A1 (en) | 2013-10-24 |
CA2820774A1 (fr) | 2012-06-21 |
CN103261025B (zh) | 2015-11-25 |
RU2577741C2 (ru) | 2016-03-20 |
RU2013131841A (ru) | 2015-01-20 |
WO2012080604A1 (fr) | 2012-06-21 |
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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] | ||
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |