GB2265188B - Turbo-jet nozzle - Google Patents
Turbo-jet nozzleInfo
- Publication number
- GB2265188B GB2265188B GB8124084A GB8124084A GB2265188B GB 2265188 B GB2265188 B GB 2265188B GB 8124084 A GB8124084 A GB 8124084A GB 8124084 A GB8124084 A GB 8124084A GB 2265188 B GB2265188 B GB 2265188B
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbo
- jet nozzle
- jet
- nozzle
- 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
- 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
- F02K1/15—Control or regulation
-
- 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)
- Transmission Devices (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8018329 | 1980-08-22 |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2265188A GB2265188A (en) | 1993-09-22 |
GB2265188B true GB2265188B (en) | 1994-05-11 |
Family
ID=9245347
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8124084A Expired - Fee Related GB2265188B (en) | 1980-08-22 | 1981-08-06 | Turbo-jet nozzle |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE3132961C1 (en) |
GB (1) | GB2265188B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2714422A1 (en) * | 1983-01-13 | 1995-06-30 | Snecma | Convergent-divergent nozzle, particularly for jet engines |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2858668A (en) * | 1952-09-27 | 1958-11-04 | Curtiss Wright Corp | Control for variable area convergentdivergent exhaust nozzle |
FR1562941A (en) * | 1968-01-19 | 1969-04-11 | ||
FR2474592A1 (en) * | 1980-01-25 | 1981-07-31 | Snecma | TURBOREACTOR TUBE DEVICE |
-
1981
- 1981-08-06 GB GB8124084A patent/GB2265188B/en not_active Expired - Fee Related
- 1981-08-20 DE DE19813132961 patent/DE3132961C1/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE3132961C1 (en) | 1993-04-22 |
GB2265188A (en) | 1993-09-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19970806 |