FR2277238A1 - Perfectionnements aux tuyeres a configuration reglable, notamment pour propulseur a reaction - Google Patents
Perfectionnements aux tuyeres a configuration reglable, notamment pour propulseur a reactionInfo
- Publication number
- FR2277238A1 FR2277238A1 FR7423232A FR7423232A FR2277238A1 FR 2277238 A1 FR2277238 A1 FR 2277238A1 FR 7423232 A FR7423232 A FR 7423232A FR 7423232 A FR7423232 A FR 7423232A FR 2277238 A1 FR2277238 A1 FR 2277238A1
- Authority
- FR
- France
- Prior art keywords
- linkage
- diagonals
- exhaust duct
- jet engine
- variable diameter
- 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.)
- Granted
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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Rigid Pipes And Flexible Pipes (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7423232A FR2277238A1 (fr) | 1974-07-04 | 1974-07-04 | Perfectionnements aux tuyeres a configuration reglable, notamment pour propulseur a reaction |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7423232A FR2277238A1 (fr) | 1974-07-04 | 1974-07-04 | Perfectionnements aux tuyeres a configuration reglable, notamment pour propulseur a reaction |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2277238A1 true FR2277238A1 (fr) | 1976-01-30 |
FR2277238B1 FR2277238B1 (xx) | 1976-12-24 |
Family
ID=9140870
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7423232A Granted FR2277238A1 (fr) | 1974-07-04 | 1974-07-04 | Perfectionnements aux tuyeres a configuration reglable, notamment pour propulseur a reaction |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2277238A1 (xx) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0509757A1 (en) * | 1991-04-15 | 1992-10-21 | General Electric Company | Jet engine exhaust nozzle |
FR2723145A1 (fr) * | 1981-11-24 | 1996-02-02 | Snecma | Tuyere convergente-divergente, en particulier pour turboreacteur |
FR2732408A1 (fr) * | 1983-03-16 | 1996-10-04 | Snecma | Tuyere, en particulier pour turboreacteur |
RU2684362C1 (ru) * | 2018-02-13 | 2019-04-08 | Государственный научный центр Российской Федерации-федеральное государственное унитарное предприятие "Исследовательский Центр имени М.В. Келдыша" | Разрезное регулируемое сопло для прямоточного воздушно-реактивного двигателя |
-
1974
- 1974-07-04 FR FR7423232A patent/FR2277238A1/fr active Granted
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2723145A1 (fr) * | 1981-11-24 | 1996-02-02 | Snecma | Tuyere convergente-divergente, en particulier pour turboreacteur |
FR2732408A1 (fr) * | 1983-03-16 | 1996-10-04 | Snecma | Tuyere, en particulier pour turboreacteur |
EP0509757A1 (en) * | 1991-04-15 | 1992-10-21 | General Electric Company | Jet engine exhaust nozzle |
RU2684362C1 (ru) * | 2018-02-13 | 2019-04-08 | Государственный научный центр Российской Федерации-федеральное государственное унитарное предприятие "Исследовательский Центр имени М.В. Келдыша" | Разрезное регулируемое сопло для прямоточного воздушно-реактивного двигателя |
Also Published As
Publication number | Publication date |
---|---|
FR2277238B1 (xx) | 1976-12-24 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CA1004477A (en) | Diverter valve for a gas turbine with an augmenter | |
GB1092170A (en) | Improvements in thrust reversers for jet propulsion powerplants | |
GB1368353A (en) | Actuation ring for variable geometry axial flow compressors | |
US3837580A (en) | Nozzles having an adjustable cross-section | |
SE8206771D0 (sv) | Axially translatable variable area convergent/divergent nozzle | |
FR2277238A1 (fr) | Perfectionnements aux tuyeres a configuration reglable, notamment pour propulseur a reaction | |
ES356313A1 (es) | Perfeccionamientos en dispositivos de accionamiento de val-vulas de caja giratoria. | |
US3949550A (en) | Engine exhaust flow diverter | |
GB852670A (en) | Improvements in or relating to mechanical linkage structures | |
GB1211447A (en) | Turbine having variable angle nozzle guide vanes | |
GB825547A (en) | Turbine with variable admission | |
GB1332278A (en) | Variable area and reversing jet propulsion nozzles | |
SE8206772D0 (sv) | Three-dimensional auxially translatable convergent/divergent nozzle assembly | |
US2928234A (en) | Exhaust nozzle | |
GB871016A (en) | Gas turbine jet propulsion engines | |
US3752597A (en) | Flow path deflector for axial flow reversing gas turbine | |
GB1476277A (en) | Tyre building drum | |
US3154241A (en) | Compressors of gas turbine engines | |
GB1142150A (en) | An arrangement for supporting and guiding flexible power lines | |
GB1430609A (en) | Variable angle turbine nozzle actuating mechanism | |
GB797874A (en) | Variable configuration discharge nozzles for propulsive jets | |
GB768014A (en) | Improvements in or relating to variable area propulsion nozzles | |
US3286982A (en) | Reversible axial flow gas turbine | |
GB946995A (en) | Fluid flow machine such as a gas turbine engine | |
GB1299196A (en) | Annular spring disc for a disc valve |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |