JPS5319724B1 - - Google Patents
Info
- Publication number
- JPS5319724B1 JPS5319724B1 JP5815272A JP5815272A JPS5319724B1 JP S5319724 B1 JPS5319724 B1 JP S5319724B1 JP 5815272 A JP5815272 A JP 5815272A JP 5815272 A JP5815272 A JP 5815272A JP S5319724 B1 JPS5319724 B1 JP S5319724B1
- Authority
- JP
- Japan
- 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.)
- Pending
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)
- Control Of Turbines (AREA)
- Supercharger (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2741771A GB1381503A (en) | 1971-06-11 | 1971-06-11 | Variable area nozzle for a gas turbine engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS5319724B1 true JPS5319724B1 (Direct) | 1978-06-22 |
Family
ID=10259237
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP5815272A Pending JPS5319724B1 (Direct) | 1971-06-11 | 1972-06-10 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US3786992A (Direct) |
| JP (1) | JPS5319724B1 (Direct) |
| DE (1) | DE2227279C3 (Direct) |
| FR (1) | FR2140626B1 (Direct) |
| GB (1) | GB1381503A (Direct) |
| IT (1) | IT956132B (Direct) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3989193A (en) * | 1974-03-02 | 1976-11-02 | Motoren- Und Turbinen-Union Munchen Gmbh M.A.N. Maybach Mercedes-Benz | Device for varying the gas exit area of an exhaust nozzle for a jet deflecting device |
| SU571615A2 (ru) * | 1975-08-13 | 1977-09-05 | Всесоюзный научно-исследовательский институт горноспасательного дела | Генератор инертного газа |
| FR2723145B1 (fr) * | 1981-11-24 | 1996-12-13 | Snecma | Tuyere convergente-divergente, en particulier pour turboreacteur |
| US5102050A (en) * | 1991-01-22 | 1992-04-07 | General Electric Company | Divergent flap actuation system for two-dimensional convergent - divergent turbojet exhaust nozzle |
| US5232158A (en) * | 1992-08-11 | 1993-08-03 | United Technologies Corporation | Convergent/divergent nozzle with seal centering |
| US5667140A (en) * | 1994-12-02 | 1997-09-16 | United Technologies Corporation | Engine exhaust nozzle seal |
| US5683034A (en) * | 1995-05-22 | 1997-11-04 | United Technologies Corporation | Engine exhaust nozzle seal |
| US5779152A (en) * | 1997-01-16 | 1998-07-14 | General Electric Company | Coordinated vectoring exhaust nozzle with scissors linkage |
| DE102008022271A1 (de) * | 2008-05-06 | 2009-11-26 | Opara, Günther | Düse für einen Strömungsantrieb |
| US8382436B2 (en) * | 2009-01-06 | 2013-02-26 | General Electric Company | Non-integral turbine blade platforms and systems |
| US8262345B2 (en) * | 2009-02-06 | 2012-09-11 | General Electric Company | Ceramic matrix composite turbine engine |
| US8123150B2 (en) | 2010-03-30 | 2012-02-28 | General Electric Company | Variable area fuel nozzle |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE525114A (Direct) * | 1952-12-16 | |||
| US2934890A (en) * | 1956-08-24 | 1960-05-03 | United Aircraft Corp | Exhaust nozzle flap movement limiting and interflap seal centering means |
| US3685738A (en) * | 1969-12-22 | 1972-08-22 | Heinrich Leibach | Thrust nozzle whose gas discharge cross-section is adapted to be adjusted by means of adjusting flaps |
| US3662957A (en) * | 1970-10-28 | 1972-05-16 | United Aircraft Corp | Low friction track bearing assembly |
-
1971
- 1971-06-11 GB GB2741771A patent/GB1381503A/en not_active Expired
-
1972
- 1972-05-31 US US00258378A patent/US3786992A/en not_active Expired - Lifetime
- 1972-06-03 IT IT25234/72A patent/IT956132B/it active
- 1972-06-05 DE DE2227279A patent/DE2227279C3/de not_active Expired
- 1972-06-09 FR FR7220839A patent/FR2140626B1/fr not_active Expired
- 1972-06-10 JP JP5815272A patent/JPS5319724B1/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| DE2227279A1 (de) | 1973-04-26 |
| FR2140626A1 (Direct) | 1973-01-19 |
| FR2140626B1 (Direct) | 1977-12-23 |
| US3786992A (en) | 1974-01-22 |
| DE2227279B2 (de) | 1974-10-31 |
| IT956132B (it) | 1973-10-10 |
| DE2227279C3 (de) | 1975-06-26 |
| GB1381503A (en) | 1975-01-22 |