BR112014017430A2 - reversor de empuxo do tipo cascata para um motor turbojato de aeronaves e nacela oara um motor turbojato de aeronaves - Google Patents
reversor de empuxo do tipo cascata para um motor turbojato de aeronaves e nacela oara um motor turbojato de aeronavesInfo
- Publication number
- BR112014017430A2 BR112014017430A2 BR112014017430A BR112014017430A BR112014017430A2 BR 112014017430 A2 BR112014017430 A2 BR 112014017430A2 BR 112014017430 A BR112014017430 A BR 112014017430A BR 112014017430 A BR112014017430 A BR 112014017430A BR 112014017430 A2 BR112014017430 A2 BR 112014017430A2
- Authority
- BR
- Brazil
- Prior art keywords
- turbojet engine
- aircraft turbojet
- nacelle
- thrust reverser
- cascade thrust
- 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
-
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1251605A FR2987080A1 (fr) | 2012-02-22 | 2012-02-22 | Inverseur de poussee a grilles pivotantes |
PCT/FR2013/050289 WO2013124569A1 (fr) | 2012-02-22 | 2013-02-13 | Inverseur de poussée à grilles pivotantes |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112014017430A2 true BR112014017430A2 (pt) | 2017-06-13 |
BR112014017430A8 BR112014017430A8 (pt) | 2017-07-04 |
Family
ID=47843331
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014017430A BR112014017430A8 (pt) | 2012-02-22 | 2013-02-13 | reversor de empuxo do tipo cascata para um motor turbojato de aeronaves e nacela oara um motor turbojato de aeronaves |
Country Status (8)
Country | Link |
---|---|
US (1) | US20150267643A1 (pt) |
EP (1) | EP2817502A1 (pt) |
CN (1) | CN104114842A (pt) |
BR (1) | BR112014017430A8 (pt) |
CA (1) | CA2862589A1 (pt) |
FR (1) | FR2987080A1 (pt) |
RU (1) | RU2014137849A (pt) |
WO (1) | WO2013124569A1 (pt) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9016040B2 (en) * | 2012-11-30 | 2015-04-28 | General Electric Company | Thrust reverser system with translating-rotating cascade and method of operation |
GB201317808D0 (en) | 2013-10-08 | 2013-11-20 | Expro North Sea Ltd | Intervention system and apparatus |
FR3016006A1 (fr) * | 2014-01-02 | 2015-07-03 | Aircelle Sa | Inverseur de poussee de nacelle de turboreacteur comprenant des grilles coulissantes et pivotantes |
FR3018334A1 (fr) * | 2014-03-07 | 2015-09-11 | Aircelle Sa | Raccord hydraulique flexible pour une nacelle de turboreacteur, comportant un reglage de longueur |
US9739235B2 (en) | 2014-03-21 | 2017-08-22 | Rohr, Inc. | Thrust reverser for a turbofan engine |
US9945324B2 (en) * | 2014-11-06 | 2018-04-17 | Rohr, Inc. | Sleeve linkage for thrust reverser |
CN104960669B (zh) * | 2015-06-23 | 2017-04-19 | 中国航空工业集团公司西安飞机设计研究所 | 一种发动机反推力控制系统 |
US10077740B2 (en) * | 2015-10-16 | 2018-09-18 | The Boeing Company | Folding door thrust reversers for aircraft engines |
US10309341B2 (en) * | 2016-01-15 | 2019-06-04 | The Boeing Company | Thrust reverser cascade systems and methods |
US10428763B2 (en) | 2016-04-01 | 2019-10-01 | Rohr, Inc. | Controlling a relative position at an interface between translating structures of an aircraft nacelle |
US11046034B2 (en) | 2016-04-18 | 2021-06-29 | Rohr, Inc. | Manufacturing a fiber-reinforced composite component using mandrels |
FR3052809B1 (fr) | 2016-06-17 | 2019-05-03 | Safran Nacelles | Systeme de guidage axial pour des capots d'inverseur de poussee comprenant un doigt de securite |
FR3059368A1 (fr) * | 2016-11-28 | 2018-06-01 | Airbus Operations | Nacelle d'un turboreacteur comportant un volet inverseur |
FR3062371B1 (fr) * | 2017-01-31 | 2019-03-29 | Airbus | Nacelle d'un turboreacteur comportant un volet inverseur |
US10525636B2 (en) | 2017-06-19 | 2020-01-07 | Rohr, Inc. | Process for forming a fiber-reinforced composite structure |
FR3076323B1 (fr) * | 2017-12-28 | 2020-01-10 | Safran Nacelles | Inverseur de poussee a grilles pour turboreacteur |
US20240035427A1 (en) * | 2022-08-01 | 2024-02-01 | Rohr, Inc. | Thrust reverser cascade with offset vane leading edges |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3241312A (en) * | 1963-09-18 | 1966-03-22 | Gen Electric | Thrust deflector |
FR1407044A (fr) * | 1964-09-10 | 1965-07-23 | Gen Electric | Dispositif déviateur et inverseur de poussée pour moteur à réaction |
US3981451A (en) * | 1975-11-17 | 1976-09-21 | Rohr Industries, Inc. | Fan cascade thrust reverser |
US4073440A (en) * | 1976-04-29 | 1978-02-14 | The Boeing Company | Combination primary and fan air thrust reversal control systems for long duct fan jet engines |
US4807434A (en) * | 1987-12-21 | 1989-02-28 | The Boeing Company | Thrust reverser for high bypass jet engines |
US6546715B1 (en) * | 2001-01-25 | 2003-04-15 | Rohr, Inc. | Cascade-type thrust reverser |
FR2920199B1 (fr) * | 2007-08-20 | 2009-10-30 | Aircelle Sa | Capot mobile d'inverseur de poussee et inverseur de poussee equipe d'un tel capot mobile |
US8201390B2 (en) * | 2007-12-12 | 2012-06-19 | Spirit Aerosystems, Inc. | Partial cascade thrust reverser |
US8316632B2 (en) * | 2009-02-25 | 2012-11-27 | Spirit Aerosystems, Inc. | Thrust reverser configuration for a short fan duct |
-
2012
- 2012-02-22 FR FR1251605A patent/FR2987080A1/fr not_active Withdrawn
-
2013
- 2013-02-13 BR BR112014017430A patent/BR112014017430A8/pt not_active Application Discontinuation
- 2013-02-13 CA CA2862589A patent/CA2862589A1/fr not_active Abandoned
- 2013-02-13 EP EP13708202.0A patent/EP2817502A1/fr not_active Withdrawn
- 2013-02-13 RU RU2014137849A patent/RU2014137849A/ru not_active Application Discontinuation
- 2013-02-13 WO PCT/FR2013/050289 patent/WO2013124569A1/fr active Application Filing
- 2013-02-13 CN CN201380008886.8A patent/CN104114842A/zh active Pending
-
2014
- 2014-08-20 US US14/464,649 patent/US20150267643A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
CN104114842A (zh) | 2014-10-22 |
RU2014137849A (ru) | 2016-04-10 |
FR2987080A1 (fr) | 2013-08-23 |
CA2862589A1 (fr) | 2013-08-29 |
US20150267643A1 (en) | 2015-09-24 |
EP2817502A1 (fr) | 2014-12-31 |
WO2013124569A1 (fr) | 2013-08-29 |
BR112014017430A8 (pt) | 2017-07-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B11A | Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing | ||
B11Y | Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette] | ||
B350 | Update of information on the portal [chapter 15.35 patent gazette] |