BR112014008570A2 - reversor de empuxo para uma nacela de um motor turbojato e nacela para uma aeronave turbojato - Google Patents
reversor de empuxo para uma nacela de um motor turbojato e nacela para uma aeronave turbojatoInfo
- Publication number
- BR112014008570A2 BR112014008570A2 BR112014008570A BR112014008570A BR112014008570A2 BR 112014008570 A2 BR112014008570 A2 BR 112014008570A2 BR 112014008570 A BR112014008570 A BR 112014008570A BR 112014008570 A BR112014008570 A BR 112014008570A BR 112014008570 A2 BR112014008570 A2 BR 112014008570A2
- Authority
- BR
- Brazil
- Prior art keywords
- turbojet
- nacelle
- thrust reverser
- aircraft
- turbojet engine
- 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
- F02K1/64—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
- 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
- F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
-
- 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
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
- Body Structure For Vehicles (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1159867A FR2981989B1 (fr) | 2011-10-31 | 2011-10-31 | Inverseur de poussee a grilles mobiles et capot mobile monobloc |
PCT/FR2012/052340 WO2013064762A1 (fr) | 2011-10-31 | 2012-10-15 | Inverseur de poussée à grilles mobiles et capot mobile monobloc |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112014008570A2 true BR112014008570A2 (pt) | 2017-04-11 |
Family
ID=47143175
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014008570A BR112014008570A2 (pt) | 2011-10-31 | 2012-10-15 | reversor de empuxo para uma nacela de um motor turbojato e nacela para uma aeronave turbojato |
Country Status (9)
Country | Link |
---|---|
US (1) | US9366201B2 (pt) |
EP (1) | EP2773861B1 (pt) |
CN (1) | CN104024618B (pt) |
BR (1) | BR112014008570A2 (pt) |
CA (1) | CA2850704A1 (pt) |
ES (1) | ES2560966T3 (pt) |
FR (1) | FR2981989B1 (pt) |
RU (1) | RU2014120988A (pt) |
WO (1) | WO2013064762A1 (pt) |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104712455B (zh) * | 2013-12-12 | 2017-07-04 | 中航商用航空发动机有限责任公司 | 涡扇发动机的反推力装置和用于该反推力装置的反推叶栅 |
DE102013226770A1 (de) * | 2013-12-19 | 2015-06-25 | Liebherr-Aerospace Lindenberg Gmbh | Fluggasturbine mit einer Triebwerksverkleidung mit Schubumkehrvorrichtung |
DE102013226767A1 (de) * | 2013-12-19 | 2015-07-09 | Liebherr-Aerospace Lindenberg Gmbh | Fluggasturbine mit einer Schubumkehrvorrichtung mit Kaskadenelementen und integriertem Zahnstangenantrieb |
US9915225B2 (en) | 2015-02-06 | 2018-03-13 | United Technologies Corporation | Propulsion system arrangement for turbofan gas turbine engine |
US10184426B2 (en) * | 2015-06-22 | 2019-01-22 | Rohr, Inc. | Thrust reverser with forward positioned blocker doors |
FR3047522B1 (fr) | 2016-02-04 | 2018-03-16 | Safran Aircraft Engines | Ensemble propulsif pour aeronef |
US20170283081A1 (en) * | 2016-04-05 | 2017-10-05 | Rohr, Inc. | Securing a translating fanlet for an aircraft propulsion system nacelle |
EP3228854B1 (en) | 2016-04-06 | 2019-10-02 | Rolls-Royce plc | Aircraft gas turbine engine nacelle |
FR3059368A1 (fr) * | 2016-11-28 | 2018-06-01 | Airbus Operations | Nacelle d'un turboreacteur comportant un volet inverseur |
FR3065260B1 (fr) * | 2017-04-14 | 2020-10-09 | Safran Aircraft Engines | Systeme inverseur de poussee pour turboreacteur |
US10436112B2 (en) * | 2017-06-26 | 2019-10-08 | The Boeing Company | Translating turning vanes for a nacelle inlet |
US10570854B2 (en) * | 2017-08-18 | 2020-02-25 | Woodward, Inc. | Three actuator cascade type thrust reverser actuation system |
FR3073010B1 (fr) * | 2017-10-27 | 2020-06-19 | Safran Nacelles | Systeme verrouillable et deverrouillable sous charge |
US11053888B2 (en) * | 2017-11-01 | 2021-07-06 | The Boeing Company | Fan cowl with a serrated trailing edge providing attached flow in reverse thrust mode |
FR3073572B1 (fr) * | 2017-11-16 | 2020-10-02 | Safran Nacelles | Inverseur de poussee a grilles mobiles pour ensemble propulsif d’aeronef et procedes de montage et demontage s’y rapportant |
FR3075886B1 (fr) * | 2017-12-22 | 2019-12-27 | Safran Nacelles | Nacelle de turboreacteur comportant des ouvertures de capots avant d'acces a des points de fixation de la nacelle |
US10704497B2 (en) | 2018-01-10 | 2020-07-07 | Woodward, Inc. | Thrust reverser velocity control valve |
FR3078108B1 (fr) * | 2018-02-20 | 2020-01-31 | Safran Nacelles | Ensemble propulsif comportant des points de levage disposes sur des supports de verins d’inverseur de poussee |
FR3078998B1 (fr) * | 2018-03-19 | 2020-03-06 | Safran Aircraft Engines | Ensemble propulsif a double flux, comprenant un inverseur de poussee a grilles mobiles |
FR3089207A1 (fr) * | 2018-11-30 | 2020-06-05 | Airbus Operations | système de propulsion d’un aeronef comportant un capot mobile et articule |
FR3094698B1 (fr) * | 2019-04-02 | 2022-09-09 | Safran Aircraft Engines | Manche d’entree d’air pour une nacelle d’un ensemble propulsif d’aeronef |
US11441482B2 (en) * | 2019-06-04 | 2022-09-13 | Rohr, Inc. | Single track translating inlet |
US11421463B2 (en) | 2019-09-09 | 2022-08-23 | Hamilton Sundstrand Corporation | One-way clutch for use in a no-back clutch design |
FR3105304B1 (fr) * | 2019-12-19 | 2021-12-10 | Safran Nacelles | Inverseur de poussée avec système d’actionnement anti-flambage |
FR3110639B1 (fr) * | 2020-05-20 | 2022-09-16 | Safran Nacelles | Inverseur de poussee pour une nacelle d’un turboreacteur a double flux d’aeronef |
US11781506B2 (en) | 2020-06-03 | 2023-10-10 | Rtx Corporation | Splitter and guide vane arrangement for gas turbine engines |
RU2745276C1 (ru) * | 2020-06-03 | 2021-03-23 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Капот газогенератора турбореактивного двигателя |
US11473658B2 (en) | 2020-11-30 | 2022-10-18 | Woodward, Inc. | Locking compound rotary actuator |
FR3121713B1 (fr) | 2021-04-13 | 2023-11-24 | Safran Nacelles | Inverseur de poussée à grilles mobiles comprenant une structure fixe plurifonctionnelle |
FR3122904B1 (fr) | 2021-05-17 | 2023-04-28 | Safran Nacelles | Inverseur de poussée à grilles mobiles, comprenant une structure arrière de support de grilles intégrant une fonction acoustique |
FR3126452A1 (fr) | 2021-08-25 | 2023-03-03 | Safran Nacelles | Inverseur à grilles mobiles pour ensemble propulsif d’aéronef, comprenant un système pour limiter le flambage d’un actionneur de l’inverseur |
FR3127479B1 (fr) | 2021-09-24 | 2023-09-01 | Safran Nacelles | Nacelle pour ensemble propulsif d’aéronef, comprenant un inverseur de poussée à grilles mobiles, et de préférence au moins un capot de soufflante pivotant |
FR3128207A1 (fr) * | 2021-10-15 | 2023-04-21 | Airbus Operations | Turboréacteur double flux comportant des déflecteurs mobiles et un système d’actionnement des déflecteurs |
FR3131757B1 (fr) | 2022-01-10 | 2023-11-24 | Safran Nacelles | Inverseur de poussee comprenant des grilles mobiles et une membrane d’obturation |
FR3131758B1 (fr) * | 2022-01-10 | 2023-11-24 | Safran Nacelles | Inverseur de poussee comprenant des grilles fixes et une membrane d’obturation |
FR3132545A1 (fr) | 2022-02-04 | 2023-08-11 | Safran Nacelles | Ensemble propulsif pour aeronef comprenant un inverseur de poussee a grilles mobiles et a actionneur monte de maniere optimisee |
WO2023198962A1 (fr) | 2022-04-15 | 2023-10-19 | General Electric Company | Suspension d'une turbomachine d'aeronef a triple flux |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5778659A (en) * | 1994-10-20 | 1998-07-14 | United Technologies Corporation | Variable area fan exhaust nozzle having mechanically separate sleeve and thrust reverser actuation systems |
FR2911372B1 (fr) * | 2007-01-15 | 2009-02-27 | Aircelle Sa | Inverseur de poussee translatable pour moteur a reaction |
US8109466B2 (en) * | 2008-06-23 | 2012-02-07 | Rohr, Inc. | Thrust reverser cascade assembly and AFT cascade ring with flow deflector portion |
FR2952681B1 (fr) * | 2009-11-18 | 2017-10-06 | Aircelle Sa | Inverseur de poussee |
FR2952908B1 (fr) * | 2009-11-26 | 2011-11-25 | Aircelle Sa | Ensemble pour turboreacteur d'aeronef |
FR2965589B1 (fr) * | 2010-10-04 | 2015-05-15 | Aircelle Sa | Inverseur de poussee |
-
2011
- 2011-10-31 FR FR1159867A patent/FR2981989B1/fr not_active Expired - Fee Related
-
2012
- 2012-10-15 RU RU2014120988/06A patent/RU2014120988A/ru not_active Application Discontinuation
- 2012-10-15 BR BR112014008570A patent/BR112014008570A2/pt not_active IP Right Cessation
- 2012-10-15 EP EP12781394.7A patent/EP2773861B1/fr active Active
- 2012-10-15 WO PCT/FR2012/052340 patent/WO2013064762A1/fr active Application Filing
- 2012-10-15 CN CN201280053439.XA patent/CN104024618B/zh not_active Expired - Fee Related
- 2012-10-15 CA CA2850704A patent/CA2850704A1/fr not_active Abandoned
- 2012-10-15 ES ES12781394.7T patent/ES2560966T3/es active Active
-
2014
- 2014-04-28 US US14/263,290 patent/US9366201B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
WO2013064762A1 (fr) | 2013-05-10 |
EP2773861A1 (fr) | 2014-09-10 |
CN104024618B (zh) | 2015-08-19 |
RU2014120988A (ru) | 2015-12-10 |
FR2981989B1 (fr) | 2013-11-01 |
CN104024618A (zh) | 2014-09-03 |
EP2773861B1 (fr) | 2015-11-18 |
CA2850704A1 (fr) | 2013-05-10 |
US20150285185A1 (en) | 2015-10-08 |
ES2560966T3 (es) | 2016-02-23 |
FR2981989A1 (fr) | 2013-05-03 |
US9366201B2 (en) | 2016-06-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application fees: dismissal - article 86 of industrial property law | ||
B08K | Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87) |