DE68915000T2 - Flügel schubdüse. - Google Patents
Flügel schubdüse.Info
- Publication number
- DE68915000T2 DE68915000T2 DE68915000T DE68915000T DE68915000T2 DE 68915000 T2 DE68915000 T2 DE 68915000T2 DE 68915000 T DE68915000 T DE 68915000T DE 68915000 T DE68915000 T DE 68915000T DE 68915000 T2 DE68915000 T2 DE 68915000T2
- Authority
- DE
- Germany
- Prior art keywords
- wing sheet
- sheet nozzle
- nozzle
- wing
- sheet
- 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.)
- Expired - Fee Related
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
-
- 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
- F02K1/006—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 within one plane only
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/60—Steering arrangements
- F42B10/66—Steering by varying intensity or direction of thrust
- F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Nozzles (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US1989/003602 WO1989012741A1 (en) | 1989-08-21 | 1989-08-21 | Vane-type thrust vectoring nozzle |
Publications (2)
Publication Number | Publication Date |
---|---|
DE68915000D1 DE68915000D1 (de) | 1994-06-01 |
DE68915000T2 true DE68915000T2 (de) | 1994-11-03 |
Family
ID=22215179
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE68915000T Expired - Fee Related DE68915000T2 (de) | 1989-08-21 | 1989-08-21 | Flügel schubdüse. |
Country Status (4)
Country | Link |
---|---|
US (1) | US5110047A (de) |
EP (1) | EP0442899B1 (de) |
DE (1) | DE68915000T2 (de) |
WO (1) | WO1989012741A1 (de) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5294055A (en) * | 1992-09-08 | 1994-03-15 | Mcdonnell Douglas Corporation | Rotatable arms for thrust vectoring and changing the area of a nozzle throat |
GB2277559A (en) * | 1993-04-30 | 1994-11-02 | Marconi Gec Ltd | Variable area convergent-divergent nozzle. |
DE4426195C2 (de) * | 1994-07-23 | 1998-02-05 | Daimler Benz Aerospace Ag | Schubdüse in Rechteckbauweise für Strahltriebwerke |
US6681560B2 (en) | 2002-01-08 | 2004-01-27 | Atlantic Research Corporation | Nozzle throat area control apparatus and method |
SE527787C2 (sv) * | 2004-11-05 | 2006-06-07 | Volvo Aero Corp | Utloppsanordning till en jetmotor och en jetmotor innefattande sådan utloppsanordning |
US7493914B2 (en) * | 2005-07-20 | 2009-02-24 | Welker, Inc. | Newtonian thrust cowl array |
US7842898B2 (en) * | 2007-10-19 | 2010-11-30 | Honeywell International Inc. | Variable orifice torch |
FR2945316B1 (fr) * | 2009-01-27 | 2013-01-04 | Michel Aguilar | Reacteur, notamment reacteur pour aeronef |
CN103303451B (zh) * | 2013-06-17 | 2015-09-23 | 北京理工大学 | 一种液压驱动的全矢量喷水推进器喷口 |
CN107313875A (zh) * | 2017-06-16 | 2017-11-03 | 李新亚 | 潜水船装喷气发动机的矢量喷管 |
CN110657043B (zh) * | 2019-09-09 | 2022-02-08 | 南京航空航天大学 | 一种机械扰动式喉道偏移式气动矢量喷管 |
CN113685272B (zh) * | 2021-10-26 | 2021-12-24 | 中国航发四川燃气涡轮研究院 | 一种大尺寸薄壁非对称对开的圆转方机匣 |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2366264A (en) * | 1943-06-04 | 1945-01-02 | Mack Mfg Corp | Nozzle |
US2799989A (en) * | 1954-09-24 | 1957-07-23 | Peter G Kappus | Variable area jet nozzle |
GB874427A (en) * | 1958-06-03 | 1961-08-10 | Alec Tucker | New or improved speed and direction control means for water craft |
US3302890A (en) * | 1964-07-10 | 1967-02-07 | Atlantic Res Corp | Rocket nozzle |
US3304865A (en) * | 1965-04-21 | 1967-02-21 | Robert L Gungle | Self-sealing, unbonded, rocket motor nozzle closure |
US3979067A (en) * | 1975-04-28 | 1976-09-07 | General Electric Company | Actuating means for a thrust vectoring gas turbine engine exhaust nozzle |
GB2155552B (en) * | 1981-02-24 | 1986-02-26 | Rolls Royce | Adjustable jet propulsion nozzle |
GB2194597B (en) * | 1986-08-29 | 1990-07-25 | Rolls Royce Plc | A variable area exhaust nozzle for a gas turbine engine |
US4763840A (en) * | 1987-04-09 | 1988-08-16 | United Technologies Corporation | Thrust vectoring exhaust nozzle arrangement |
US4798328A (en) * | 1987-05-22 | 1989-01-17 | United Technologies Corporation | Area controlled, thrust vectoring vane cascade with nutating control vane |
-
1989
- 1989-08-21 DE DE68915000T patent/DE68915000T2/de not_active Expired - Fee Related
- 1989-08-21 US US07/474,744 patent/US5110047A/en not_active Expired - Fee Related
- 1989-08-21 EP EP89911315A patent/EP0442899B1/de not_active Expired - Lifetime
- 1989-08-21 WO PCT/US1989/003602 patent/WO1989012741A1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
EP0442899A1 (de) | 1991-08-28 |
WO1989012741A1 (en) | 1989-12-28 |
US5110047A (en) | 1992-05-05 |
DE68915000D1 (de) | 1994-06-01 |
EP0442899B1 (de) | 1994-04-27 |
EP0442899A4 (en) | 1992-01-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |