BE694091A - - Google Patents
Info
- Publication number
- BE694091A BE694091A BE694091DA BE694091A BE 694091 A BE694091 A BE 694091A BE 694091D A BE694091D A BE 694091DA BE 694091 A BE694091 A BE 694091A
- 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
- F02K1/52—Nozzles specially constructed for positioning adjacent to another nozzle or to a fixed member, e.g. fairing
-
- 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
- F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
- F02K1/004—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector by using one or more swivable nozzles rotating about their own axis
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Exhaust Silencers (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US551397A US3416754A (en) | 1966-05-19 | 1966-05-19 | Vectorable exhaust nozzle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE694091A true BE694091A (US20100056889A1-20100304-C00004.png) | 1967-08-16 |
Family
ID=24201108
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE694091D BE694091A (US20100056889A1-20100304-C00004.png) | 1966-05-19 | 1967-02-15 |
Country Status (5)
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1277679B (de) * | 1967-04-28 | 1968-09-12 | Entwicklungsring Sued G M B H | Strahltriebwerk, insbesondere fuer senkrecht startende und landende Flugzeuge, mit schwenkbarer Primaerduese und Zusatzluft ansaugender Sekundaerduese |
| DE1756879A1 (de) * | 1968-07-26 | 1970-10-01 | Karl Jaeger | Flugscheibe |
| US4478377A (en) * | 1980-12-22 | 1984-10-23 | British Aerospace Public Limited Company | Aircraft |
| US4506848A (en) * | 1980-12-22 | 1985-03-26 | British Aerospace Public Limited Company | Aircraft configuration and control arrangement therefor |
| US4579299A (en) * | 1982-04-22 | 1986-04-01 | Morton Thiokol, Inc. | Quick turn, 90 degree omniaxial nozzle thrust control system |
| US4840329A (en) * | 1986-04-08 | 1989-06-20 | Rolls-Royce Inc. | Aircraft with stowable vectorable nozzle and ejector thrust augmentation |
| GB2188887B (en) * | 1986-04-08 | 1989-11-29 | Rolls Royce Plc | Aircraft with stowable vectorable nozzle and ejector thrust augmentation |
| US4713935A (en) * | 1986-04-08 | 1987-12-22 | Rolls-Royce Inc. | Vectorable nozzles for aircraft |
| GB8812978D0 (en) * | 1988-06-01 | 1988-11-16 | British Aerospace | Nozzle assembly for aircraft |
| US4901947A (en) * | 1989-02-27 | 1990-02-20 | Lockheed Corporation | Reverse engine VSTOL |
| US5351888A (en) * | 1993-05-14 | 1994-10-04 | General Electric Company | Multi-axis vectorable exhaust nozzle |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3025667A (en) * | 1957-07-22 | 1962-03-20 | Boeing Co | Rotary turret reversible thrust noise suppression jet engine nozzles |
| DE1066428B (US20100056889A1-20100304-C00004.png) * | 1959-01-17 | |||
| GB915400A (en) * | 1960-02-03 | 1963-01-09 | Bristol Siddeley Engines Ltd | Improvements in or relating to jet propulsion power plants for aircraft |
| GB1019303A (en) * | 1961-07-31 | 1966-02-02 | Bristol Siddeley Engines Ltd | Improvements in nozzle systems of jet propulsion engines |
| FR1304094A (fr) * | 1961-08-04 | 1962-09-21 | Snecma | Moteur à réaction convertible de propulsion et de sustentation |
| GB976854A (en) * | 1961-12-07 | 1964-12-02 | Havilland Engine Co Ltd | Aircraft propulsion apparatus |
| GB991220A (en) * | 1963-04-25 | 1965-05-05 | Rolls Royce | Aircraft |
-
1966
- 1966-05-19 US US551397A patent/US3416754A/en not_active Expired - Lifetime
-
1967
- 1967-01-04 CH CH5867A patent/CH466721A/de unknown
- 1967-02-15 BE BE694091D patent/BE694091A/xx unknown
- 1967-02-16 DE DE19671481568 patent/DE1481568A1/de active Pending
- 1967-02-17 GB GB7610/67A patent/GB1161949A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| US3416754A (en) | 1968-12-17 |
| CH466721A (de) | 1968-12-15 |
| GB1161949A (en) | 1969-08-20 |
| DE1481568A1 (de) | 1969-05-29 |
