GB0709126D0 - Turbine engine nozzle - Google Patents
Turbine engine nozzleInfo
- Publication number
- GB0709126D0 GB0709126D0 GBGB0709126.7A GB0709126A GB0709126D0 GB 0709126 D0 GB0709126 D0 GB 0709126D0 GB 0709126 A GB0709126 A GB 0709126A GB 0709126 D0 GB0709126 D0 GB 0709126D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine engine
- engine nozzle
- nozzle
- turbine
- engine
- 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
- 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
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0709126A GB2437418B (en) | 2003-07-07 | 2004-07-06 | Turbine engine nozzle |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/614,632 US6871797B2 (en) | 2003-07-07 | 2003-07-07 | Turbine engine nozzle |
GB0709126A GB2437418B (en) | 2003-07-07 | 2004-07-06 | Turbine engine nozzle |
GB0415187A GB2403775B (en) | 2003-07-07 | 2004-07-06 | Turbine engine nozzle |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0709126D0 true GB0709126D0 (en) | 2007-06-20 |
GB2437418A GB2437418A (en) | 2007-10-24 |
GB2437418B GB2437418B (en) | 2008-03-19 |
Family
ID=38529964
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0709126A Expired - Fee Related GB2437418B (en) | 2003-07-07 | 2004-07-06 | Turbine engine nozzle |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2437418B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB202213334D0 (en) * | 2022-09-13 | 2022-10-26 | Rolls Royce Plc | A variable-geometry convergent-divergent exhaust nozzle |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB839230A (en) * | 1956-01-12 | 1960-06-29 | Gen Motors Corp | Improvements relating to variable jet nozzles |
FR1215237A (en) * | 1958-11-12 | 1960-04-15 | Snecma | Variable geometry nozzle |
GB1100656A (en) * | 1965-10-04 | 1968-01-24 | Rolls Royce | Jet propulsion nozzle |
US3454227A (en) * | 1966-08-19 | 1969-07-08 | United Aircraft Corp | Free floating articulate ejector nozzle |
US4141501A (en) * | 1975-05-09 | 1979-02-27 | Rolls-Royce (1971) Limited | Nozzles for gas turbine engines |
US7225622B2 (en) * | 2003-07-21 | 2007-06-05 | United Technologies Corporation | Turbine engine nozzle |
-
2004
- 2004-07-06 GB GB0709126A patent/GB2437418B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB2437418A (en) | 2007-10-24 |
GB2437418B (en) | 2008-03-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20130706 |