GB2242172B - Gas turbine engine - Google Patents
Gas turbine engineInfo
- Publication number
- GB2242172B GB2242172B GB8328254A GB8328254A GB2242172B GB 2242172 B GB2242172 B GB 2242172B GB 8328254 A GB8328254 A GB 8328254A GB 8328254 A GB8328254 A GB 8328254A GB 2242172 B GB2242172 B GB 2242172B
- 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 - Fee Related
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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/13—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having variable working fluid interconnections between turbines or compressors or stages of different rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/328—Application in turbines in gas turbines providing direct vertical lift
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8208521 | 1982-03-23 |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2242172A GB2242172A (en) | 1991-09-25 |
GB2242172B true GB2242172B (en) | 1991-12-11 |
Family
ID=10529218
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8328254A Expired - Fee Related GB2242172B (en) | 1982-03-23 | 1983-03-18 | Gas turbine engine |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE3341126A1 (en) |
FR (1) | FR2665485A1 (en) |
GB (1) | GB2242172B (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2313580B (en) * | 1996-05-31 | 2000-02-23 | Astovl Limited | An aircraft power plant |
AT406574B (en) * | 1999-02-11 | 2000-06-26 | Bobleter Ortwin | DRIVE DEVICE FOR AN AIRCRAFT |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2879014A (en) * | 1957-07-02 | 1959-03-24 | Bell Aircraft Corp | Jet propelled airplane with jet diverter |
GB1389347A (en) * | 1972-05-25 | 1975-04-03 | Rolls Royce | Gas turbine power plant |
GB1415679A (en) * | 1972-11-17 | 1975-11-26 | Rolls Royce | Gas turbine engine powerplant |
US3841091A (en) * | 1973-05-21 | 1974-10-15 | Gen Electric | Multi-mission tandem propulsion system |
US4033119A (en) * | 1973-09-06 | 1977-07-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Dual cycle aircraft turbine engine |
FR2355169A1 (en) * | 1974-03-23 | 1978-01-13 | Rolls Royce | STOL or VTOL aircraft for supersonic flight - has air valve closing thrust unit not contributing to supersonic flight |
US3972349A (en) * | 1974-06-20 | 1976-08-03 | United Technologies Corporation | Variable ratio bypass gas turbine engine with flow diverter |
GB1497153A (en) * | 1975-01-16 | 1978-01-05 | Avon Rubber Co Ltd | Inflatable bung |
GB1511723A (en) * | 1975-05-01 | 1978-05-24 | Rolls Royce | Variable stator vane actuating mechanism |
US4222234A (en) * | 1977-07-25 | 1980-09-16 | General Electric Company | Dual fan engine for VTOL pitch control |
-
1983
- 1983-03-18 DE DE19833341126 patent/DE3341126A1/en active Granted
- 1983-03-18 GB GB8328254A patent/GB2242172B/en not_active Expired - Fee Related
- 1983-11-02 FR FR8317447A patent/FR2665485A1/en active Pending
Also Published As
Publication number | Publication date |
---|---|
FR2665485A1 (en) | 1992-02-07 |
DE3341126C2 (en) | 1993-03-11 |
DE3341126A1 (en) | 1991-12-12 |
GB2242172A (en) | 1991-09-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19970318 |