GB9102205D0 - Thrust reverser - Google Patents
Thrust reverserInfo
- Publication number
- GB9102205D0 GB9102205D0 GB919102205A GB9102205A GB9102205D0 GB 9102205 D0 GB9102205 D0 GB 9102205D0 GB 919102205 A GB919102205 A GB 919102205A GB 9102205 A GB9102205 A GB 9102205A GB 9102205 D0 GB9102205 D0 GB 9102205D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- thrust reverser
- reverser
- 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.)
- Withdrawn
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
- F02K1/56—Reversing jet main flow
- F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
- F02K1/605—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers the aft end of the engine cowling being movable to uncover openings for the reversed flow
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Supercharger (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9102205A GB2252279A (en) | 1991-02-01 | 1991-02-01 | Thrust reverser |
DE19924200645 DE4200645A1 (en) | 1991-02-01 | 1992-01-13 | DRAWER REVERSE |
FR9200955A FR2672339A1 (en) | 1991-02-01 | 1992-01-29 | PUSH INVERTER. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9102205A GB2252279A (en) | 1991-02-01 | 1991-02-01 | Thrust reverser |
Publications (2)
Publication Number | Publication Date |
---|---|
GB9102205D0 true GB9102205D0 (en) | 1991-07-10 |
GB2252279A GB2252279A (en) | 1992-08-05 |
Family
ID=10689378
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9102205A Withdrawn GB2252279A (en) | 1991-02-01 | 1991-02-01 | Thrust reverser |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE4200645A1 (en) |
FR (1) | FR2672339A1 (en) |
GB (1) | GB2252279A (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5181676A (en) * | 1992-01-06 | 1993-01-26 | Lair Jean Pierre | Thrust reverser integrating a variable exhaust area nozzle |
FR2727468B1 (en) * | 1994-11-30 | 1996-12-27 | Hispano Suiza Sa | DOWNSTREAM OBSTACLE TURBOREACTOR DRIVER |
FR2736390B1 (en) * | 1995-07-05 | 1997-08-08 | Hispano Suiza Sa | PUSH INVERTER OF A SHELL TURBOREACTOR |
FR2768773B1 (en) * | 1997-09-25 | 1999-11-05 | Hispano Suiza Sa | INTERNAL SHELL TURBOREACTOR DRIVE INVERTER |
FR2774431B1 (en) | 1998-02-04 | 2000-03-03 | Hispano Suiza Sa | DOWNSTREAM OBSTACLE TURBOREACTOR DRIVER |
FR3057617B1 (en) * | 2016-10-17 | 2020-10-16 | Airbus | NACELLE OF A TURBOREACTOR CONTAINING A INVERTER FLAP |
RU2663249C1 (en) | 2017-03-16 | 2018-08-03 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Method for manufacturing sections of a thrust reverser bearing grid |
US10641208B2 (en) * | 2017-11-27 | 2020-05-05 | Rohr, Inc. | Translating nozzle for mixed flow turbofan engine |
US10724474B2 (en) | 2018-05-01 | 2020-07-28 | Rohr, Inc. | Hybrid articulating/translating trailing edge reverser |
US11053887B2 (en) * | 2018-07-02 | 2021-07-06 | Rohr, Inc. | Thrust reverser with displaceable trailing edge body |
US11155343B2 (en) | 2018-12-17 | 2021-10-26 | The Boeing Company | Brake systems for aircraft and related methods |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3020712A (en) * | 1959-06-22 | 1962-02-13 | Boeing Co | Reversible-thrust sound suppression jet nozzles with movable ejector rings |
GB1062839A (en) * | 1965-11-26 | 1967-03-22 | Rolls Royce | Improvements relating to thrust reversers |
GB1150012A (en) * | 1966-09-12 | 1969-04-30 | Rolls Royce | Fluid Flow Duct Including Thrust Reversing Means |
US4340178A (en) * | 1980-05-05 | 1982-07-20 | Rohr Industries, Inc. | Thrust reverser - cascade type |
FR2486153B1 (en) * | 1980-07-04 | 1985-10-04 | Hurel Dubois Avions | DRIVE INVERTER FOR A REACTION ENGINE, IN PARTICULAR FOR EQUIPPING AN AIRCRAFT |
DE3844188C1 (en) * | 1988-12-29 | 1990-05-17 | Mtu Muenchen Gmbh |
-
1991
- 1991-02-01 GB GB9102205A patent/GB2252279A/en not_active Withdrawn
-
1992
- 1992-01-13 DE DE19924200645 patent/DE4200645A1/en not_active Withdrawn
- 1992-01-29 FR FR9200955A patent/FR2672339A1/en active Pending
Also Published As
Publication number | Publication date |
---|---|
DE4200645A1 (en) | 1992-08-06 |
FR2672339A1 (en) | 1992-08-07 |
GB2252279A (en) | 1992-08-05 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |