BE682001A - - Google Patents
Info
- Publication number
- BE682001A BE682001A BE682001DA BE682001A BE 682001 A BE682001 A BE 682001A BE 682001D A BE682001D A BE 682001DA BE 682001 A BE682001 A BE 682001A
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US462789A US3280561A (en) | 1965-06-07 | 1965-06-07 | Thrust reverser mechanism |
Publications (1)
Publication Number | Publication Date |
---|---|
BE682001A true BE682001A (es) | 1966-11-14 |
Family
ID=23837759
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE682001D BE682001A (es) | 1965-06-07 | 1966-06-02 |
Country Status (3)
Country | Link |
---|---|
US (1) | US3280561A (es) |
BE (1) | BE682001A (es) |
DE (1) | DE1279478B (es) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3056721A1 (en) * | 2015-02-13 | 2016-08-17 | United Technologies Corporation | Turbine engine with a turbo-compressor |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1111219A (en) * | 1966-02-14 | 1968-04-24 | Rolls Royce | Gas turbine engine |
US3465524A (en) * | 1966-03-02 | 1969-09-09 | Rolls Royce | Fan gas turbine engine |
GB1085619A (en) * | 1966-03-09 | 1967-10-04 | Rolls Royce | Gas turbine engine |
US3476486A (en) * | 1966-04-12 | 1969-11-04 | Dowty Rotol Ltd | Gas turbine engines |
US3366349A (en) * | 1966-05-02 | 1968-01-30 | Gen Dynamics Corp | Centerbody thrust reverser |
US3330115A (en) * | 1966-05-31 | 1967-07-11 | United Aircraft Corp | Turbofan thrust reverser |
US3353355A (en) * | 1966-05-31 | 1967-11-21 | United Aircraft Corp | Turbofan lightweight thrust reverser |
GB1127828A (en) * | 1966-06-29 | 1968-09-18 | Rolls Royce | Fan thrust reverser for jet propulsion plant |
US3531049A (en) * | 1968-09-09 | 1970-09-29 | Rohr Corp | Unitary ejector-thrust reverser assembly for jet-propulsion engines |
US3570767A (en) * | 1969-10-01 | 1971-03-16 | Rohr Corp | Thrust reversing apparatus |
US3874620A (en) * | 1973-03-09 | 1975-04-01 | Boeing Co | Reversing apparatus for a jet engine |
US3981463A (en) * | 1974-03-21 | 1976-09-21 | Rohr Industries, Inc. | Overwing thrust reverser |
US3917198A (en) * | 1974-06-21 | 1975-11-04 | Rohr Industries Inc | Overwing post exit blocker/deflector door thrust reverser |
US4278220A (en) * | 1979-03-30 | 1981-07-14 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thrust reverser for a long duct fan engine |
FR2550821B1 (fr) * | 1983-08-18 | 1985-11-08 | Snecma | Dispositif variateur du flux secondaire d'un turboreacteur multiflux |
FR2618852B1 (fr) * | 1987-07-29 | 1989-11-10 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur muni d'un dispositif redresseur de flux |
FR2625261B1 (fr) * | 1987-12-23 | 1992-11-06 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a obstacles lies au capot primaire |
FR2650861A1 (fr) * | 1989-08-08 | 1991-02-15 | Snecma | Inverseur de poussee de turboreacteur double flux, a obstacles lies au capot primaire |
FR2676780B1 (fr) * | 1991-05-23 | 1993-08-13 | Snecma | Inverseur de poussee pour turbosoufflante a tres grand taux dilution. |
FR2678026B1 (fr) * | 1991-06-24 | 1993-10-15 | Hurel Dubois Avions | Perfectionnement aux inverseurs de poussee de moteur a reaction. |
FR2721977B1 (fr) | 1994-06-30 | 1996-08-02 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a double flux a obstacles lies au capot primaire |
FR2749041B1 (fr) * | 1996-05-23 | 1998-06-26 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a double flux a obstacles lies au capot primaire |
FR2759418B1 (fr) * | 1997-02-13 | 1999-03-19 | Snecma | Inverseur de poussee pour turbosoufflante a tres grand taux de dilution |
EP2395222B1 (en) * | 2006-10-12 | 2019-06-26 | United Technologies Corporation | Gas turbine engine system and corresponding controlling method |
FR2916484B1 (fr) * | 2007-05-21 | 2009-07-24 | Aircelle Sa | Porte a becquet mobile pour inverseur de poussee a porte |
US9650992B2 (en) * | 2013-10-17 | 2017-05-16 | Rohr, Inc. | Core cowl thrust reverser system and apparatus |
US10337401B2 (en) | 2015-02-13 | 2019-07-02 | United Technologies Corporation | Turbine engine with a turbo-compressor |
US10100731B2 (en) | 2015-02-13 | 2018-10-16 | United Technologies Corporation | Turbine engine with a turbo-compressor |
US10041408B2 (en) | 2015-02-13 | 2018-08-07 | United Technologies Corporation | Turbine engine with a turbo-compressor |
US10077740B2 (en) | 2015-10-16 | 2018-09-18 | The Boeing Company | Folding door thrust reversers for aircraft engines |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USRE23198E (en) * | 1950-02-21 | Reaction propelling device for | ||
US2396911A (en) * | 1939-12-04 | 1946-03-19 | Anxionnaz Rene | Reaction propelling device for aircraft |
US2945346A (en) * | 1954-10-04 | 1960-07-19 | Republic Aviat Corp | Reverse thrust brake |
US2929580A (en) * | 1956-06-18 | 1960-03-22 | Piasecki Aircraft Corp | Aircraft for vertical or short takeoff, and integrated propulsion lifting and propeller slip stream deflecting unit therefor |
FR1286886A (fr) * | 1961-01-27 | 1962-03-09 | Nord Aviation | Dispositif d'inversion de poussée pour propulseurs comportant un turbo-réacteur àdouble flux |
US3040524A (en) * | 1961-07-28 | 1962-06-26 | United Aircraft Corp | Ducted fan engine thrust reverser |
-
1965
- 1965-06-07 US US462789A patent/US3280561A/en not_active Expired - Lifetime
-
1966
- 1966-06-02 BE BE682001D patent/BE682001A/xx unknown
- 1966-06-02 DE DEG47046A patent/DE1279478B/de active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3056721A1 (en) * | 2015-02-13 | 2016-08-17 | United Technologies Corporation | Turbine engine with a turbo-compressor |
Also Published As
Publication number | Publication date |
---|---|
DE1279478B (de) | 1968-10-03 |
US3280561A (en) | 1966-10-25 |