BE698900A - - Google Patents
Info
- Publication number
- BE698900A BE698900A BE698900DA BE698900A BE 698900 A BE698900 A BE 698900A BE 698900D A BE698900D A BE 698900DA BE 698900 A BE698900 A BE 698900A
- Authority
- BE
- Belgium
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
- F02K1/68—Reversers mounted on the engine housing downstream of the fan exhaust section
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Professional, Industrial, Or Sporting Protective Garments (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US554036A US3330115A (en) | 1966-05-31 | 1966-05-31 | Turbofan thrust reverser |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE698900A true BE698900A (xx) | 1967-11-03 |
Family
ID=24211789
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE698900D BE698900A (xx) | 1966-05-31 | 1967-05-24 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US3330115A (xx) |
| BE (1) | BE698900A (xx) |
| DE (1) | DE1506612B1 (xx) |
| FR (1) | FR1526550A (xx) |
| GB (1) | GB1190627A (xx) |
| NL (1) | NL6707588A (xx) |
| SE (1) | SE315505B (xx) |
Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3386247A (en) * | 1966-09-09 | 1968-06-04 | Gen Electric | Powerplant with thrust reverser |
| US4005836A (en) * | 1975-12-22 | 1977-02-01 | Rohr Industries, Inc. | Target thrust reverser |
| US4326686A (en) * | 1980-02-15 | 1982-04-27 | Runge Thomas M | Fan jet engine bypass air delivery system for blown wing aircraft lift augmentation device |
| US4698964A (en) * | 1985-09-06 | 1987-10-13 | The Boeing Company | Automatic deflector for a jet engine bleed air exhaust system |
| FR2717859B1 (fr) * | 1994-03-28 | 1996-05-31 | Sud Ouest Conception Aeronauti | Turbomoteur à double flux équipé d'un système d'inversion de poussée et d'un dispositif de restriction du canal d'éjection des gaz froids, et dispositif de restriction équipant un tel turbomoteur. |
| FR2737256B1 (fr) * | 1995-07-26 | 1997-10-17 | Aerospatiale | Turboreacteur a double flux a portes d'inversion de poussee non soumises au flux secondaire dans leur position inactive |
| US7874477B2 (en) * | 2003-02-06 | 2011-01-25 | Graphic Packaging International, Inc. | Carton with top dispensing feature |
| FR3087848B1 (fr) * | 2018-10-30 | 2020-10-23 | Safran Nacelles | Inverseur de poussee comprenant une membrane souple de deviation d'air |
| FR3096087B1 (fr) * | 2019-05-14 | 2021-06-04 | Safran Nacelles | Porte pour inverseur de poussée d’ensemble propulsif d’aéronef, comportant un déflecteur souple |
| FR3112816A1 (fr) * | 2020-07-21 | 2022-01-28 | Airbus Operations | Turboréacteur double flux comportant un système d’obturation de la veine du flux secondaire comportant des voiles |
| FR3119203A1 (fr) * | 2021-01-22 | 2022-07-29 | Airbus Operations | Turboréacteur double flux comportant un système d’obturation de la veine du flux secondaire comportant des voiles |
| FR3131757B1 (fr) * | 2022-01-10 | 2023-11-24 | Safran Nacelles | Inverseur de poussee comprenant des grilles mobiles et une membrane d’obturation |
| FR3135757A1 (fr) * | 2022-05-20 | 2023-11-24 | Safran Nacelles | Inverseur de poussee comprenant une membrane d’obturation a deploiement simplifie |
| FR3145780A1 (fr) * | 2023-02-10 | 2024-08-16 | Safran Nacelles | Inverseur de poussee pour turbomachine d’aeronef comprenant des moyens de deploiement et de retrait a cable d’une membrane d’obturation de la veine secondaire |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB765582A (en) * | 1954-06-18 | 1957-01-09 | Power Jets Res & Dev Ltd | A jet deflecting device for jet propelled aircraft |
| US3280561A (en) * | 1965-06-07 | 1966-10-25 | Gen Electric | Thrust reverser mechanism |
| US3302404A (en) * | 1965-06-30 | 1967-02-07 | Gen Electric | Lightweight thrust reverser |
-
1966
- 1966-05-31 US US554036A patent/US3330115A/en not_active Expired - Lifetime
-
1967
- 1967-05-10 GB GB21818/67A patent/GB1190627A/en not_active Expired
- 1967-05-23 DE DE19671506612 patent/DE1506612B1/de not_active Withdrawn
- 1967-05-24 BE BE698900D patent/BE698900A/xx unknown
- 1967-05-25 SE SE7386/67A patent/SE315505B/xx unknown
- 1967-05-31 FR FR5117A patent/FR1526550A/fr not_active Expired
- 1967-05-31 NL NL6707588A patent/NL6707588A/xx unknown
Also Published As
| Publication number | Publication date |
|---|---|
| US3330115A (en) | 1967-07-11 |
| DE1506612B1 (de) | 1969-09-04 |
| NL6707588A (xx) | 1967-12-01 |
| FR1526550A (fr) | 1968-05-24 |
| GB1190627A (en) | 1970-05-06 |
| SE315505B (xx) | 1969-09-29 |