DE4200645A1 - Schubumkehrvorrichtung - Google Patents
SchubumkehrvorrichtungInfo
- Publication number
- DE4200645A1 DE4200645A1 DE19924200645 DE4200645A DE4200645A1 DE 4200645 A1 DE4200645 A1 DE 4200645A1 DE 19924200645 DE19924200645 DE 19924200645 DE 4200645 A DE4200645 A DE 4200645A DE 4200645 A1 DE4200645 A1 DE 4200645A1
- Authority
- DE
- Germany
- Prior art keywords
- doors
- sealing body
- thrust reverser
- deflecting
- movement
- 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- Withdrawn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)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9102205A GB2252279A (en) | 1991-02-01 | 1991-02-01 | Thrust reverser |
Publications (1)
Publication Number | Publication Date |
---|---|
DE4200645A1 true DE4200645A1 (de) | 1992-08-06 |
Family
ID=10689378
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19924200645 Withdrawn DE4200645A1 (de) | 1991-02-01 | 1992-01-13 | Schubumkehrvorrichtung |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE4200645A1 (fr) |
FR (1) | FR2672339A1 (fr) |
GB (1) | GB2252279A (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2018169453A2 (fr) | 2017-03-16 | 2018-09-20 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Procédé de fabrication de sections de la grille porteuse d'un inverseur de poussée |
Families Citing this family (10)
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 (fr) | 1994-11-30 | 1996-12-27 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a obstacles aval |
FR2736390B1 (fr) * | 1995-07-05 | 1997-08-08 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a une coquille |
FR2768773B1 (fr) * | 1997-09-25 | 1999-11-05 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a coquilles internes |
FR2774431B1 (fr) | 1998-02-04 | 2000-03-03 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a obstacles aval |
FR3057617B1 (fr) * | 2016-10-17 | 2020-10-16 | Airbus | Nacelle d'un turboreacteur comportant un volet inverseur |
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 (fr) * | 1980-07-04 | 1985-10-04 | Hurel Dubois Avions | Inverseur de poussee pour moteur a reaction, destine notamment a equiper un aeronef |
DE3844188C1 (fr) * | 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/de not_active Withdrawn
- 1992-01-29 FR FR9200955A patent/FR2672339A1/fr active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2018169453A2 (fr) | 2017-03-16 | 2018-09-20 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Procédé de fabrication de sections de la grille porteuse d'un inverseur de poussée |
Also Published As
Publication number | Publication date |
---|---|
FR2672339A1 (fr) | 1992-08-07 |
GB2252279A (en) | 1992-08-05 |
GB9102205D0 (en) | 1991-07-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8139 | Disposal/non-payment of the annual fee |