FR1434703A - Tuyère à réaction - Google Patents
Tuyère à réactionInfo
- Publication number
- FR1434703A FR1434703A FR17504A FR17504A FR1434703A FR 1434703 A FR1434703 A FR 1434703A FR 17504 A FR17504 A FR 17504A FR 17504 A FR17504 A FR 17504A FR 1434703 A FR1434703 A FR 1434703A
- Authority
- FR
- France
- Prior art keywords
- reaction nozzle
- nozzle
- reaction
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
- B64C29/0058—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with vertical jet
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/38—Jet flaps
-
- 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
- F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
- F02K1/30—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for varying effective area of jet pipe or nozzle
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Extrusion Moulding Of Plastics Or The Like (AREA)
- Advancing Webs (AREA)
- Looms (AREA)
- Jet Pumps And Other Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB25312/64A GB1019203A (en) | 1964-06-18 | 1964-06-18 | Jet nozzle |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1434703A true FR1434703A (fr) | 1966-04-08 |
Family
ID=10225673
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR17504A Expired FR1434703A (fr) | 1964-06-18 | 1965-05-18 | Tuyère à réaction |
Country Status (3)
Country | Link |
---|---|
US (1) | US3288373A (fr) |
FR (1) | FR1434703A (fr) |
GB (1) | GB1019203A (fr) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5435489A (en) * | 1994-01-13 | 1995-07-25 | Bell Helicopter Textron Inc. | Engine exhaust gas deflection system |
US5863229A (en) * | 1996-06-11 | 1999-01-26 | Bombardier, Inc. | Variable venturi |
US5727381A (en) * | 1997-02-19 | 1998-03-17 | The United States Of America As Represented By Secretary Of The Navy | Duct flow control system |
US5996936A (en) * | 1997-09-29 | 1999-12-07 | General Electric Company | Fluidic throat exhaust nozzle |
US6021637A (en) * | 1997-09-29 | 2000-02-08 | General Electric Company | Integrated fluidic CD nozzle for gas turbine engine |
US6336319B1 (en) | 2000-05-26 | 2002-01-08 | General Electric Company | Fluidic nozzle control system |
US6442941B1 (en) * | 2000-09-11 | 2002-09-03 | General Electric Company | Compressor discharge bleed air circuit in gas turbine plants and related method |
FR2903455B1 (fr) * | 2006-07-05 | 2013-01-18 | Airbus France | Procede pour inverser la poussee produite par un ensemble propulsif d'un aeronef, dispositif pour sa mise en oeuvre, nacelle equipee dudit dispositif |
US8001762B2 (en) * | 2006-08-04 | 2011-08-23 | Efremkin Artem P | Method and device to increase thrust and efficiency of jet engine |
WO2008045074A1 (fr) * | 2006-10-12 | 2008-04-17 | United Technologies Corporation | Turboréacteur à double flux présentant une surface de sortie de tuyère de dilution variable et procédé permettant de le faire fonctionner |
FR2910937B1 (fr) * | 2007-01-02 | 2009-04-03 | Airbus France Sas | Nacelle de reacteur d'aeronef et aeronef comportant une telle nacelle |
CN103899433A (zh) * | 2014-03-31 | 2014-07-02 | 西北工业大学 | 一种新型激波控制推力矢量喷管结构 |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2943821A (en) * | 1950-12-30 | 1960-07-05 | United Aircraft Corp | Directional control means for a supersonic vehicle |
US3024602A (en) * | 1952-04-22 | 1962-03-13 | Snecma | Arrangements for deflecting the jet expelled from a discharge nozzle or from a reaction-propulsion unit |
US3016699A (en) * | 1952-10-10 | 1962-01-16 | Snecma | Aerodynamically acting jet deflecting device |
FR1111633A (fr) * | 1954-09-17 | 1956-03-02 | Snecma | Dispositif de réglage de la section d'une tuyère |
-
1964
- 1964-06-18 GB GB25312/64A patent/GB1019203A/en not_active Expired
-
1965
- 1965-04-12 US US447250A patent/US3288373A/en not_active Expired - Lifetime
- 1965-05-18 FR FR17504A patent/FR1434703A/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US3288373A (en) | 1966-11-29 |
GB1019203A (en) | 1966-02-02 |
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