GB2038425B - Gas turbine engine - Google Patents
Gas turbine engineInfo
- Publication number
- GB2038425B GB2038425B GB7849998A GB7849998A GB2038425B GB 2038425 B GB2038425 B GB 2038425B GB 7849998 A GB7849998 A GB 7849998A GB 7849998 A GB7849998 A GB 7849998A GB 2038425 B GB2038425 B GB 2038425B
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- turbine engine
- engine
- gas
- turbine
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
- F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
- F04D29/684—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps by fluid injection
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB7849998A GB2038425B (en) | 1978-12-27 | 1978-12-27 | Gas turbine engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB7849998A GB2038425B (en) | 1978-12-27 | 1978-12-27 | Gas turbine engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB2038425A GB2038425A (en) | 1980-07-23 |
| GB2038425B true GB2038425B (en) | 1982-12-01 |
Family
ID=10501939
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB7849998A Expired GB2038425B (en) | 1978-12-27 | 1978-12-27 | Gas turbine engine |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2038425B (en) |
Families Citing this family (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2046843B (en) * | 1979-04-17 | 1983-01-26 | Rolls Royce | Gas turbine engines-de-icing-icing |
| GB2251031B (en) * | 1990-12-19 | 1995-01-18 | Rolls Royce Plc | Cooling air pick up |
| WO2000029721A1 (en) * | 1998-11-13 | 2000-05-25 | Siemens Aktiengesellschaft | Turbo-machine, especially a turbo-generator comprising a turbo-machine and an electric machine |
| GB9828812D0 (en) * | 1998-12-29 | 1999-02-17 | Rolls Royce Plc | Gas turbine nose cone assembly |
| US6561760B2 (en) * | 2001-08-17 | 2003-05-13 | General Electric Company | Booster compressor deicer |
| GB2442967B (en) * | 2006-10-21 | 2011-02-16 | Rolls Royce Plc | An engine arrangement |
| EP1923574B1 (en) * | 2006-11-20 | 2014-10-29 | Siemens Aktiengesellschaft | Compressor, turbine and method for supplying heating gas |
| US10393019B2 (en) * | 2016-07-28 | 2019-08-27 | Pratt & Whitney Canada Corp. | Assembly and method for influencing flow through a fan of a gas turbine engine |
| CN107061013B (en) * | 2017-03-30 | 2019-05-24 | 中国航发沈阳发动机研究所 | A kind of hot air anti-icing method for engine intake rotary rectifier calotte |
| US10900414B2 (en) * | 2018-11-23 | 2021-01-26 | Pratt & Whitney Canada Corp. | Fan assembly having flow recirculation circuit with guide vanes |
| US11499475B2 (en) | 2018-11-23 | 2022-11-15 | Pratt & Whitney Canada Corp. | Fan assembly having flow recirculation circuit with rotating airfoils |
| US11156093B2 (en) | 2019-04-18 | 2021-10-26 | Pratt & Whitney Canada Corp. | Fan blade ice protection using hot air |
| US11098646B2 (en) | 2019-07-08 | 2021-08-24 | Pratt & Whitney Canada Corp. | Gas turbine impeller nose cone |
| US11118457B2 (en) * | 2019-10-21 | 2021-09-14 | Pratt & Whitney Canada Corp. | Method for fan blade heating using coanda effect |
| US12416262B2 (en) | 2023-02-17 | 2025-09-16 | General Electric Company | Reverse flow gas turbine engine having electric machine |
| US12221894B2 (en) * | 2023-03-20 | 2025-02-11 | General Electric Company Polska Sp. Z O.O. | Compressor with anti-ice inlet |
-
1978
- 1978-12-27 GB GB7849998A patent/GB2038425B/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB2038425A (en) | 1980-07-23 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |