RU96122637A - DEVICE REVERSE DEVICE FOR TURBOJET ENGINE WITH REAR LOCATED Sashes - Google Patents
DEVICE REVERSE DEVICE FOR TURBOJET ENGINE WITH REAR LOCATED SashesInfo
- Publication number
- RU96122637A RU96122637A RU96122637/06A RU96122637A RU96122637A RU 96122637 A RU96122637 A RU 96122637A RU 96122637/06 A RU96122637/06 A RU 96122637/06A RU 96122637 A RU96122637 A RU 96122637A RU 96122637 A RU96122637 A RU 96122637A
- Authority
- RU
- Russia
- Prior art keywords
- turbojet engine
- thrust
- shutter
- rotary axes
- turbojet
- Prior art date
Links
- 230000000875 corresponding Effects 0.000 claims 1
- 238000011144 upstream manufacturing Methods 0.000 claims 1
Claims (2)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9501959 | 1995-02-21 | ||
FR9501959A FR2730763B1 (en) | 1995-02-21 | 1995-02-21 | DOWNSTREAM SHUTTER REVERSER FOR TURBOJET |
PCT/FR1996/000249 WO1996026359A1 (en) | 1995-02-21 | 1996-02-15 | Thrust reverser with downstream flaps for turbojet engines |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2124646C1 RU2124646C1 (en) | 1999-01-10 |
RU96122637A true RU96122637A (en) | 1999-01-20 |
Family
ID=9476336
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU96122637A RU2124646C1 (en) | 1995-02-21 | 1996-02-15 | Draft reversing device for turbojet engine with rear doors |
Country Status (8)
Country | Link |
---|---|
US (1) | US5725182A (en) |
EP (1) | EP0728934B1 (en) |
JP (1) | JPH08240150A (en) |
CA (1) | CA2169874C (en) |
DE (1) | DE69602296T2 (en) |
FR (1) | FR2730763B1 (en) |
RU (1) | RU2124646C1 (en) |
WO (1) | WO1996026359A1 (en) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2887854B1 (en) * | 2005-06-30 | 2008-08-08 | Airbus France Sas | PLATFORM FOR AN AIRCRAFT AND AN AIRCRAFT PROVIDED WITH AT LEAST ONE SUCH NACELLE |
US8015797B2 (en) | 2006-09-21 | 2011-09-13 | Jean-Pierre Lair | Thrust reverser nozzle for a turbofan gas turbine engine |
US7797944B2 (en) * | 2006-10-20 | 2010-09-21 | United Technologies Corporation | Gas turbine engine having slim-line nacelle |
US7870721B2 (en) | 2006-11-10 | 2011-01-18 | United Technologies Corporation | Gas turbine engine providing simulated boundary layer thickness increase |
US8408491B2 (en) * | 2007-04-24 | 2013-04-02 | United Technologies Corporation | Nacelle assembly having inlet airfoil for a gas turbine engine |
US8205430B2 (en) * | 2007-05-16 | 2012-06-26 | United Technologies Corporation | Variable geometry nacelle assembly for a gas turbine engine |
US8402739B2 (en) * | 2007-06-28 | 2013-03-26 | United Technologies Corporation | Variable shape inlet section for a nacelle assembly of a gas turbine engine |
US9004399B2 (en) * | 2007-11-13 | 2015-04-14 | United Technologies Corporation | Nacelle flow assembly |
US7735778B2 (en) | 2007-11-16 | 2010-06-15 | Pratt & Whitney Canada Corp. | Pivoting fairings for a thrust reverser |
US8091827B2 (en) | 2007-11-16 | 2012-01-10 | The Nordam Group, Inc. | Thrust reverser door |
US8051639B2 (en) * | 2007-11-16 | 2011-11-08 | The Nordam Group, Inc. | Thrust reverser |
US8052085B2 (en) | 2007-11-16 | 2011-11-08 | The Nordam Group, Inc. | Thrust reverser for a turbofan gas turbine engine |
US8172175B2 (en) | 2007-11-16 | 2012-05-08 | The Nordam Group, Inc. | Pivoting door thrust reverser for a turbofan gas turbine engine |
US8052086B2 (en) | 2007-11-16 | 2011-11-08 | The Nordam Group, Inc. | Thrust reverser door |
US8192147B2 (en) * | 2007-12-14 | 2012-06-05 | United Technologies Corporation | Nacelle assembly having inlet bleed |
US8186942B2 (en) * | 2007-12-14 | 2012-05-29 | United Technologies Corporation | Nacelle assembly with turbulators |
US8959889B2 (en) | 2008-11-26 | 2015-02-24 | The Boeing Company | Method of varying a fan duct nozzle throat area of a gas turbine engine |
US8127532B2 (en) * | 2008-11-26 | 2012-03-06 | The Boeing Company | Pivoting fan nozzle nacelle |
FR2959488B1 (en) | 2010-04-28 | 2012-05-18 | Aircelle Sa | NACELLE FOR AN AIRCRAFT ENGINE WITH THRUST INVERTER WITH GRIDS AND ADAPTIVE TUBE |
US9038367B2 (en) | 2011-09-16 | 2015-05-26 | United Technologies Corporation | Fan case thrust reverser |
US9097209B2 (en) | 2012-03-27 | 2015-08-04 | United Technologies Corporation | Gas turbine engine thrust reverser system |
US9631578B2 (en) | 2013-02-22 | 2017-04-25 | United Technologies Corporation | Pivot thrust reverser surrounding inner surface of bypass duct |
US9617009B2 (en) | 2013-02-22 | 2017-04-11 | United Technologies Corporation | ATR full ring sliding nacelle |
US11396854B2 (en) * | 2017-10-25 | 2022-07-26 | Rohr, Inc. | Hinge mechanism for pivot door thrust reversers |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1052963A (en) * | 1963-09-30 | |||
US3699682A (en) * | 1971-01-04 | 1972-10-24 | Mc Donnell Douglas Corp | Turbofan engine thrust reverser |
GB1424193A (en) * | 1972-03-21 | 1976-02-11 | Rolls Royce | Gas turbine ducted fan engines |
FR2486153B1 (en) * | 1980-07-04 | 1985-10-04 | Hurel Dubois Avions | DRIVE INVERTER FOR A REACTION ENGINE, IN PARTICULAR FOR EQUIPPING AN AIRCRAFT |
US4407120A (en) * | 1980-08-25 | 1983-10-04 | Rohr Industries, Inc. | Thrust reverser geared linkage |
FR2506843B1 (en) * | 1981-05-29 | 1987-04-24 | Hurel Dubois Avions | PUSH-INVERSION DEVICE FOR AIRPLANE TURBOREACTOR |
US4541673A (en) * | 1983-05-19 | 1985-09-17 | The Boeing Company | Removable slider shoe for a translating sleeve used on a jet engine cowl and duct |
GB2189550A (en) * | 1986-04-25 | 1987-10-28 | Rolls Royce | A gas turbine engine powerplant with flow control devices |
FR2611233B1 (en) * | 1987-02-19 | 1991-05-10 | Hurel Dubois Avions | FAN-TYPE AIRPLANE MOTOR-PROPELLER UNIT EQUIPPED WITH A PUSH-INVERTER WITH DOORS |
FR2622928A1 (en) * | 1987-11-05 | 1989-05-12 | Hispano Suiza Sa | PUSH INVERTER OF DOOR TURBOJET, WITH VARIABLE EJECTION SECTION |
GB2212859B (en) * | 1987-12-02 | 1991-03-06 | Rolls Royce Plc | Ducted fan gas turbine engine with surge controller |
DE3844188C1 (en) * | 1988-12-29 | 1990-05-17 | Mtu Muenchen Gmbh | |
FR2651278B1 (en) * | 1989-08-23 | 1994-05-06 | Hispano Suiza | INVERTER WITH GRIDS WITHOUT SLIDING COVER FOR TURBOREACTOR. |
US5120004A (en) * | 1990-02-05 | 1992-06-09 | Rohr, Inc. | Split door thrust reverser for fan jet aircraft engines |
US5197693A (en) * | 1991-08-15 | 1993-03-30 | Rohr, Inc. | Aircraft turbine engine thrust reverser with sliding hinge actuator |
-
1995
- 1995-02-21 FR FR9501959A patent/FR2730763B1/en not_active Expired - Fee Related
-
1996
- 1996-02-15 RU RU96122637A patent/RU2124646C1/en active
- 1996-02-15 WO PCT/FR1996/000249 patent/WO1996026359A1/en unknown
- 1996-02-15 EP EP96400309A patent/EP0728934B1/en not_active Expired - Lifetime
- 1996-02-15 DE DE69602296T patent/DE69602296T2/en not_active Expired - Lifetime
- 1996-02-20 CA CA002169874A patent/CA2169874C/en not_active Expired - Fee Related
- 1996-02-20 JP JP8032060A patent/JPH08240150A/en active Pending
- 1996-02-20 US US08/603,448 patent/US5725182A/en not_active Expired - Lifetime
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