FR1588791A - - Google Patents
Info
- Publication number
- FR1588791A FR1588791A FR1588791DA FR1588791A FR 1588791 A FR1588791 A FR 1588791A FR 1588791D A FR1588791D A FR 1588791DA FR 1588791 A FR1588791 A FR 1588791A
- Authority
- FR
- France
- 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
-
- 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
- F02K1/1292—Varying effective area of jet pipe or nozzle by means of pivoted flaps of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, the internal downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series and at their downstream ends on the downstream ends of the flaps of the external downstream series hinged at their upstream ends on a substantially axially movable structure
-
- 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
- F02K1/1223—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series
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)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR136775 | 1968-01-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1588791A true FR1588791A (de) | 1970-03-16 |
Family
ID=8644841
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1588791D Expired FR1588791A (de) | 1968-01-19 | 1968-01-19 |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1588791A (de) |
GB (1) | GB1254175A (de) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2524937A1 (fr) * | 1982-04-07 | 1983-10-14 | Nightingale Douglas | Tuyere d'ejection a geometrie variable pour turbomachines |
FR2602274A1 (fr) * | 1986-07-30 | 1988-02-05 | Snecma | Tuyere de reacteur convergente-divergente a section reglable |
WO1990008254A1 (de) * | 1989-01-19 | 1990-07-26 | Mtu Motoren- Und Turbinen Union München Gmbh | Schubdüse |
FR2691508A1 (fr) * | 1992-05-20 | 1993-11-26 | Snecma | Vérin à fluide sous pression et tuyère à section variable en faisant application. |
FR2698409A1 (fr) * | 1992-11-25 | 1994-05-27 | Snecma | Tuyère d'éjection de turboréacteur. |
FR2714422A1 (fr) * | 1983-01-13 | 1995-06-30 | Snecma | Tuyère convergente-divergente, en particulier pour turboréacteur. |
FR2724977A1 (fr) * | 1980-12-30 | 1996-03-29 | Snecma | Tuyere convergente-divergente en particulier pour turboreacteur |
US5934564A (en) * | 1996-06-20 | 1999-08-10 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) | Variable geometry turbojet engine exhaust nozzle |
-
1968
- 1968-01-19 FR FR1588791D patent/FR1588791A/fr not_active Expired
-
1969
- 1969-01-20 GB GB323169A patent/GB1254175A/en not_active Expired
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2724977A1 (fr) * | 1980-12-30 | 1996-03-29 | Snecma | Tuyere convergente-divergente en particulier pour turboreacteur |
FR2524937A1 (fr) * | 1982-04-07 | 1983-10-14 | Nightingale Douglas | Tuyere d'ejection a geometrie variable pour turbomachines |
FR2714422A1 (fr) * | 1983-01-13 | 1995-06-30 | Snecma | Tuyère convergente-divergente, en particulier pour turboréacteur. |
FR2602274A1 (fr) * | 1986-07-30 | 1988-02-05 | Snecma | Tuyere de reacteur convergente-divergente a section reglable |
US5186390A (en) * | 1989-01-16 | 1993-02-16 | Mtu Motoren-Und Turbinen-Union Munchen Gmbh | Propelling nozzle |
WO1990008254A1 (de) * | 1989-01-19 | 1990-07-26 | Mtu Motoren- Und Turbinen Union München Gmbh | Schubdüse |
FR2691508A1 (fr) * | 1992-05-20 | 1993-11-26 | Snecma | Vérin à fluide sous pression et tuyère à section variable en faisant application. |
FR2698409A1 (fr) * | 1992-11-25 | 1994-05-27 | Snecma | Tuyère d'éjection de turboréacteur. |
US5359851A (en) * | 1992-11-25 | 1994-11-01 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation (S.N.E.C.M.A.) | Variable geometry exhaust nozzle for a turbojet engine |
US5934564A (en) * | 1996-06-20 | 1999-08-10 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) | Variable geometry turbojet engine exhaust nozzle |
Also Published As
Publication number | Publication date |
---|---|
GB1254175A (en) | 1971-11-17 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |