FR2958688B1 - Ensemble propulsif pour aeronef muni de moyens d'inversion de poussee - Google Patents
Ensemble propulsif pour aeronef muni de moyens d'inversion de pousseeInfo
- Publication number
- FR2958688B1 FR2958688B1 FR1052689A FR1052689A FR2958688B1 FR 2958688 B1 FR2958688 B1 FR 2958688B1 FR 1052689 A FR1052689 A FR 1052689A FR 1052689 A FR1052689 A FR 1052689A FR 2958688 B1 FR2958688 B1 FR 2958688B1
- Authority
- FR
- France
- Prior art keywords
- inversion means
- aircraft provided
- propulsive assembly
- thrust inversion
- thrust
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired - Fee Related
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
-
- 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
-
- 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)
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1052689A FR2958688B1 (fr) | 2010-04-09 | 2010-04-09 | Ensemble propulsif pour aeronef muni de moyens d'inversion de poussee |
CA 2792288 CA2792288A1 (fr) | 2010-04-09 | 2011-03-10 | Ensemble propulsif pour aeronef muni de moyens d'inversion de poussee |
CN2011800138798A CN102792001A (zh) | 2010-04-09 | 2011-03-10 | 设有反向推力装置的飞行器推进系统 |
RU2012146860/06A RU2012146860A (ru) | 2010-04-09 | 2011-03-10 | Силовая установка летательного аппарата, оснащенная средствами реверса тяги |
PCT/FR2011/050483 WO2011124793A1 (fr) | 2010-04-09 | 2011-03-10 | Ensemble propulsif pour aéronef muni de moyens d'inversion de poussée |
EP11712982A EP2556237A1 (fr) | 2010-04-09 | 2011-03-10 | Ensemble propulsif pour aéronef muni de moyens d'inversion de poussée |
US13/640,070 US9133790B2 (en) | 2010-04-09 | 2011-03-10 | Aircraft propulsion system provided with reverse thrust means |
BR112012022437A BR112012022437A2 (pt) | 2010-04-09 | 2011-03-10 | sistema de propulsão |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1052689A FR2958688B1 (fr) | 2010-04-09 | 2010-04-09 | Ensemble propulsif pour aeronef muni de moyens d'inversion de poussee |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2958688A1 FR2958688A1 (fr) | 2011-10-14 |
FR2958688B1 true FR2958688B1 (fr) | 2013-02-22 |
Family
ID=43086911
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1052689A Expired - Fee Related FR2958688B1 (fr) | 2010-04-09 | 2010-04-09 | Ensemble propulsif pour aeronef muni de moyens d'inversion de poussee |
Country Status (8)
Country | Link |
---|---|
US (1) | US9133790B2 (fr) |
EP (1) | EP2556237A1 (fr) |
CN (1) | CN102792001A (fr) |
BR (1) | BR112012022437A2 (fr) |
CA (1) | CA2792288A1 (fr) |
FR (1) | FR2958688B1 (fr) |
RU (1) | RU2012146860A (fr) |
WO (1) | WO2011124793A1 (fr) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9109462B2 (en) * | 2011-12-15 | 2015-08-18 | United Technologies Corporation | Energy-absorbing fan case for a gas turbine engine |
DE102014210025A1 (de) * | 2014-05-26 | 2015-12-17 | Rolls-Royce Deutschland Ltd & Co Kg | Schubumkehrkaskadenelement einer Fluggasturbine |
US10539095B2 (en) * | 2016-04-06 | 2020-01-21 | Rolls-Royce Plc | Aircraft gas turbine engine nacelle |
PL417832A1 (pl) * | 2016-07-04 | 2018-01-15 | General Electric Company | Zespół rozszerzenia kielichowego, zwłaszcza do dyszy i sposób jego rozkładania oraz silnik turbowentylatorowy zawierający ten zespół |
US10252790B2 (en) * | 2016-08-11 | 2019-04-09 | General Electric Company | Inlet assembly for an aircraft aft fan |
US10259565B2 (en) * | 2016-08-11 | 2019-04-16 | General Electric Company | Inlet assembly for an aircraft aft fan |
CN106927016B (zh) * | 2017-04-18 | 2023-08-08 | 河北天启通宇航空器材科技发展有限公司 | 旋翼机舱的强制通风机构以及旋翼机 |
FR3078951B1 (fr) * | 2018-03-13 | 2020-02-28 | Airbus Operations | Turboreacteur comportant une nacelle equipee d'un carter de soufflante et d'une structure fixe |
FR3090048A1 (fr) * | 2018-12-13 | 2020-06-19 | Airbus Operations | Turboreacteur double flux comportant une serie de lames rotatives pour obturer la veine du flux secondaire |
FR3092145A1 (fr) * | 2019-01-24 | 2020-07-31 | Airbus Operations | Turboreacteur double flux comportant une serie de lames rotatives pour obturer la veine du flux secondaire |
FR3104211B1 (fr) * | 2019-12-10 | 2021-12-17 | Airbus Operations Sas | Turboreacteur double flux comportant une serie de lames rotatives pour obturer la veine du flux secondaire |
CN112977847A (zh) * | 2021-03-10 | 2021-06-18 | 陕西北斗金箭航空科技有限公司 | 一种高可靠性无叶电推进器 |
GB202210040D0 (en) | 2022-05-20 | 2022-08-24 | Rolls Royce Plc | Gas turbine engine |
GB202210039D0 (en) * | 2022-05-20 | 2022-08-24 | Rolls Royce Plc | Gas turbine engine |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3040524A (en) * | 1961-07-28 | 1962-06-26 | United Aircraft Corp | Ducted fan engine thrust reverser |
GB1197028A (en) * | 1968-10-24 | 1970-07-01 | Rolls Royce | Thrust Reverser for Jet-Propulsion Engines |
GB1365491A (en) * | 1971-01-02 | 1974-09-04 | Dowty Rotol Ltd | Gas turbine ducted fan engines and fans therefor |
US3946554A (en) * | 1974-09-06 | 1976-03-30 | General Electric Company | Variable pitch turbofan engine and a method for operating same |
US4030290A (en) * | 1974-11-06 | 1977-06-21 | The Boeing Company | Jet engine thrust reverser |
US4030291A (en) | 1976-01-02 | 1977-06-21 | General Electric Company | Thrust reverser for a gas turbofan engine |
US5315821A (en) * | 1993-02-05 | 1994-05-31 | General Electric Company | Aircraft bypass turbofan engine thrust reverser |
US5706649A (en) * | 1995-04-03 | 1998-01-13 | Boeing North American, Inc. | Multi axis thrust vectoring for turbo fan engines |
GB0001279D0 (en) * | 2000-01-21 | 2000-03-08 | Rolls Royce Plc | A flow directing element and a method of manufacturing a flow directing element |
FR2871776B1 (fr) * | 2004-06-21 | 2007-11-02 | Snecma Moteurs Sa | Procede de freinage d'un avion et turboreacteur a double flux pour la mise en oeuvre du procede |
US8109466B2 (en) * | 2008-06-23 | 2012-02-07 | Rohr, Inc. | Thrust reverser cascade assembly and AFT cascade ring with flow deflector portion |
-
2010
- 2010-04-09 FR FR1052689A patent/FR2958688B1/fr not_active Expired - Fee Related
-
2011
- 2011-03-10 EP EP11712982A patent/EP2556237A1/fr not_active Withdrawn
- 2011-03-10 RU RU2012146860/06A patent/RU2012146860A/ru not_active Application Discontinuation
- 2011-03-10 CA CA 2792288 patent/CA2792288A1/fr not_active Abandoned
- 2011-03-10 US US13/640,070 patent/US9133790B2/en not_active Expired - Fee Related
- 2011-03-10 CN CN2011800138798A patent/CN102792001A/zh active Pending
- 2011-03-10 BR BR112012022437A patent/BR112012022437A2/pt not_active IP Right Cessation
- 2011-03-10 WO PCT/FR2011/050483 patent/WO2011124793A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
US9133790B2 (en) | 2015-09-15 |
CN102792001A (zh) | 2012-11-21 |
FR2958688A1 (fr) | 2011-10-14 |
BR112012022437A2 (pt) | 2016-07-05 |
WO2011124793A1 (fr) | 2011-10-13 |
RU2012146860A (ru) | 2014-05-20 |
CA2792288A1 (fr) | 2011-10-13 |
US20130025260A1 (en) | 2013-01-31 |
EP2556237A1 (fr) | 2013-02-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 6 |
|
ST | Notification of lapse |
Effective date: 20161230 |