FR2132380A1 - - Google Patents
Info
- Publication number
- FR2132380A1 FR2132380A1 FR7211639A FR7211639A FR2132380A1 FR 2132380 A1 FR2132380 A1 FR 2132380A1 FR 7211639 A FR7211639 A FR 7211639A FR 7211639 A FR7211639 A FR 7211639A FR 2132380 A1 FR2132380 A1 FR 2132380A1
- Authority
- FR
- France
- 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.)
- Granted
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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Exhaust Silencers (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB828371A GB1386232A (en) | 1971-03-31 | 1971-03-31 | Fluid propulsion systems |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2132380A1 true FR2132380A1 (en) | 1972-11-17 |
FR2132380B1 FR2132380B1 (en) | 1977-01-14 |
Family
ID=9849544
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7211639A Expired FR2132380B1 (en) | 1971-03-31 | 1972-03-31 |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE2216220A1 (en) |
FR (1) | FR2132380B1 (en) |
GB (1) | GB1386232A (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2405366A1 (en) * | 1977-10-05 | 1979-05-04 | Rolls Royce | IMPROVEMENTS TO THE FLOW DEVIATION DEVICES |
FR2496766A1 (en) * | 1980-12-23 | 1982-06-25 | Snecma | MOBILE FAIRING GUIDING DEVICE OF A PUSH REVERSING SYSTEM |
EP0191204A1 (en) * | 1983-05-19 | 1986-08-20 | The Boeing Company | A removable slider shoe for a translating sleeve used on a jet engine cowl and duct |
FR2812035A1 (en) | 2000-07-24 | 2002-01-25 | Hurel Dubois Avions | IMPROVEMENTS ON DRIVE INVERTERS FOR JET ENGINES OF THE GRID TYPE |
WO2008043890A1 (en) * | 2006-10-11 | 2008-04-17 | Aircelle | Cascade-type thrust reverser for jet engine |
FR2925607A1 (en) * | 2007-12-21 | 2009-06-26 | Aircelle Sa | NACELLE FOR AIRCRAFT ENGINE WITH VARIABLE SECTION TUBE |
EP2175123A3 (en) * | 2008-10-13 | 2011-05-11 | Goodrich Actuation Systems Ltd. | Actuator and corresponding thrust reverser system |
WO2013021136A1 (en) * | 2011-08-08 | 2013-02-14 | Snecma | Thrust reverser device for compact jet pipe |
FR2999239A1 (en) * | 2012-12-12 | 2014-06-13 | Aircelle Sa | PLATFORM PUSH INVERTER AND NACELLE EQUIPPED WITH AT LEAST ONE INVERTER |
WO2014132011A1 (en) * | 2013-03-01 | 2014-09-04 | Aircelle | Thrust reverser device |
WO2015028755A1 (en) * | 2013-08-30 | 2015-03-05 | Aircelle | Nacelle comprising a thrust reverser device with maintained mobile grids |
CN104712456A (en) * | 2013-12-12 | 2015-06-17 | 中航商用航空发动机有限责任公司 | Engine mobile cover and engine reverse thrust device |
WO2023026014A1 (en) * | 2021-08-25 | 2023-03-02 | Safran Nacelles | Reverser with movable cascades for an aircraft propulsion assembly, comprising a system for limiting the buckling of an actuator of the reverser |
FR3136517A1 (en) * | 2022-06-14 | 2023-12-15 | Airbus Operations | Aircraft engine nacelle provided with a thrust reverser with a movable ejection structure. |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4373328A (en) * | 1980-10-22 | 1983-02-15 | United Technologies Corporation | Thrust reverser |
GB2156004A (en) * | 1984-03-15 | 1985-10-02 | Gen Electric | Thrust modulation device for a gas turbine engine |
GB2189550A (en) * | 1986-04-25 | 1987-10-28 | Rolls Royce | A gas turbine engine powerplant with flow control devices |
GB2198999B (en) * | 1986-12-17 | 1990-08-29 | Rolls Royce Plc | Fluid propulsion engine with flow exit control device |
GB2347126B (en) | 1999-02-23 | 2003-02-12 | Rolls Royce Plc | Thrust reverser |
GB0025666D0 (en) * | 2000-10-19 | 2000-12-06 | Short Brothers Plc | Aircraft propulsive power unit |
FR2821892B1 (en) * | 2001-03-08 | 2003-06-13 | Hispano Suiza Sa | SYSTEM FOR ACTUATING THE MOBILE COVERING OF A DRIVE INVERTER IN A TURBOJET |
US6968675B2 (en) * | 2002-10-29 | 2005-11-29 | Rohr, Inc. | Cascadeless fan thrust reverser with plume control |
US6824101B2 (en) * | 2003-02-17 | 2004-11-30 | The Boeing Company | Apparatus and method for mounting a cascade support ring to a thrust reverser |
GB0321139D0 (en) | 2003-09-10 | 2003-10-08 | Short Brothers Plc | A device |
FR2921976B1 (en) | 2007-10-08 | 2009-12-04 | Aircelle Sa | ACTUATOR FOR MOBILE STRUCTURE OF AN AIRCRAFT NACELLE, AND NACELLE COMPRISING AT LEAST ONE ACTUATOR |
FR2959532B1 (en) * | 2010-04-30 | 2013-01-04 | Aircelle Sa | TURBOREACTOR NACELLE |
FR2972224B1 (en) | 2011-03-04 | 2018-04-20 | Safran Aircraft Engines | TUYERE WITH DOWN CORE HAVING A HEAVY CURVATURE |
FR2986212B1 (en) * | 2012-01-26 | 2014-10-10 | Snecma | AIRCRAFT NACELLE WITH A SLIDING REAR PART TO FORM A PUSH INVERTER. |
DE102015203219A1 (en) * | 2015-02-23 | 2016-08-25 | Rolls-Royce Deutschland Ltd & Co Kg | Engine cowling of a gas turbine with thrust reverser and adjustable in cross-section exhaust nozzle |
GB201720950D0 (en) * | 2017-12-15 | 2018-01-31 | Short Brothers Plc | Variable area fan nozzle for turbofan aircraft engine |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB861819A (en) * | 1957-07-29 | 1961-03-01 | Boeing Co | Noise suppressor and thrust reverser for jet propulsion engines |
FR1260040A (en) * | 1960-03-07 | 1961-05-05 | Snecma | Jet diverter device |
-
1971
- 1971-03-31 GB GB828371A patent/GB1386232A/en not_active Expired
-
1972
- 1972-03-31 FR FR7211639A patent/FR2132380B1/fr not_active Expired
- 1972-04-04 DE DE19722216220 patent/DE2216220A1/en active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB861819A (en) * | 1957-07-29 | 1961-03-01 | Boeing Co | Noise suppressor and thrust reverser for jet propulsion engines |
FR1260040A (en) * | 1960-03-07 | 1961-05-05 | Snecma | Jet diverter device |
Cited By (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2405366A1 (en) * | 1977-10-05 | 1979-05-04 | Rolls Royce | IMPROVEMENTS TO THE FLOW DEVIATION DEVICES |
FR2496766A1 (en) * | 1980-12-23 | 1982-06-25 | Snecma | MOBILE FAIRING GUIDING DEVICE OF A PUSH REVERSING SYSTEM |
EP0055163A1 (en) * | 1980-12-23 | 1982-06-30 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Guiderail for the sliding cover of a thrust reverser system |
EP0191204A1 (en) * | 1983-05-19 | 1986-08-20 | The Boeing Company | A removable slider shoe for a translating sleeve used on a jet engine cowl and duct |
FR2812035A1 (en) | 2000-07-24 | 2002-01-25 | Hurel Dubois Avions | IMPROVEMENTS ON DRIVE INVERTERS FOR JET ENGINES OF THE GRID TYPE |
US6438942B2 (en) | 2000-07-24 | 2002-08-27 | Societe De Construction Des Avions Hurel-Dubois (Societe Anonyme) | Cascade-type reversers for jet engines |
US8578698B2 (en) | 2006-10-11 | 2013-11-12 | Aircelle | Cascade-type thrust reverser for jet engine |
WO2008043890A1 (en) * | 2006-10-11 | 2008-04-17 | Aircelle | Cascade-type thrust reverser for jet engine |
FR2907170A1 (en) * | 2006-10-11 | 2008-04-18 | Aircelle Sa | THRUST INVERTER WITH GRIDS FOR REACTION ENGINE |
FR2925607A1 (en) * | 2007-12-21 | 2009-06-26 | Aircelle Sa | NACELLE FOR AIRCRAFT ENGINE WITH VARIABLE SECTION TUBE |
WO2009103905A1 (en) * | 2007-12-21 | 2009-08-27 | Aircelle | Nacelle for aircraft engine having a nozzle with a variable section |
US9133789B2 (en) | 2007-12-21 | 2015-09-15 | Aircelle | Nacelle for aircraft engine having a nozzle with a variable section |
EP2175123A3 (en) * | 2008-10-13 | 2011-05-11 | Goodrich Actuation Systems Ltd. | Actuator and corresponding thrust reverser system |
WO2013021136A1 (en) * | 2011-08-08 | 2013-02-14 | Snecma | Thrust reverser device for compact jet pipe |
FR2978991A1 (en) * | 2011-08-08 | 2013-02-15 | Snecma | THRUST INVERSION DEVICE FOR COMPACT PIPE |
US9856825B2 (en) | 2011-08-08 | 2018-01-02 | Snecma | Thrust reverser device for compact jet pipe |
RU2600825C2 (en) * | 2011-08-08 | 2016-10-27 | Снекма | Thrust reversing device for small-size nozzle |
US9677502B2 (en) | 2012-12-12 | 2017-06-13 | Aircelle | Nacelle thrust reverser and nacelle equipped with at least one reverser |
WO2014091140A1 (en) * | 2012-12-12 | 2014-06-19 | Aircelle | Nacelle thrust reverser and nacelle equipped with at least one reverser |
FR2999239A1 (en) * | 2012-12-12 | 2014-06-13 | Aircelle Sa | PLATFORM PUSH INVERTER AND NACELLE EQUIPPED WITH AT LEAST ONE INVERTER |
CN104854335A (en) * | 2012-12-12 | 2015-08-19 | 埃尔塞乐公司 | Nacelle thrust reverser and nacelle equipped with at least one reverser |
FR3002785A1 (en) * | 2013-03-01 | 2014-09-05 | Aircelle Sa | TRANSLATANT AND FIXED GRIDS WITH A T / R O-DUCT. |
WO2014132011A1 (en) * | 2013-03-01 | 2014-09-04 | Aircelle | Thrust reverser device |
US10190538B2 (en) | 2013-03-01 | 2019-01-29 | Aircelle | Thrust reverser device |
WO2015028755A1 (en) * | 2013-08-30 | 2015-03-05 | Aircelle | Nacelle comprising a thrust reverser device with maintained mobile grids |
FR3010146A1 (en) * | 2013-08-30 | 2015-03-06 | Aircelle Sa | PLATFORM WITH MOBILE SCREEN REVERSE INVERSION DEVICE |
CN104712456A (en) * | 2013-12-12 | 2015-06-17 | 中航商用航空发动机有限责任公司 | Engine mobile cover and engine reverse thrust device |
CN104712456B (en) * | 2013-12-12 | 2017-08-25 | 中国航发商用航空发动机有限责任公司 | Engine movement cover and engine reverse thrust device |
WO2023026014A1 (en) * | 2021-08-25 | 2023-03-02 | Safran Nacelles | Reverser with movable cascades for an aircraft propulsion assembly, comprising a system for limiting the buckling of an actuator of the reverser |
FR3126452A1 (en) * | 2021-08-25 | 2023-03-03 | Safran Nacelles | Reverser with moving grids for an aircraft propulsion system, comprising a system for limiting the buckling of an actuator of the reverser |
FR3136517A1 (en) * | 2022-06-14 | 2023-12-15 | Airbus Operations | Aircraft engine nacelle provided with a thrust reverser with a movable ejection structure. |
EP4293215A1 (en) * | 2022-06-14 | 2023-12-20 | Airbus Operations SAS | Aircraft engine nacelle provided with a thrust reverser with a mobile ejection structure |
Also Published As
Publication number | Publication date |
---|---|
FR2132380B1 (en) | 1977-01-14 |
DE2216220A1 (en) | 1972-10-05 |
GB1386232A (en) | 1975-03-05 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |