FR1199576A - Improvements made to power plants with gas turbines, in particular for jet propulsion - Google Patents
Improvements made to power plants with gas turbines, in particular for jet propulsionInfo
- Publication number
- FR1199576A FR1199576A FR1199576DA FR1199576A FR 1199576 A FR1199576 A FR 1199576A FR 1199576D A FR1199576D A FR 1199576DA FR 1199576 A FR1199576 A FR 1199576A
- Authority
- FR
- France
- Prior art keywords
- power plants
- improvements made
- gas turbines
- jet propulsion
- propulsion
- 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
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors
-
- 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
- F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
- F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB738457A GB838602A (en) | 1957-03-06 | 1957-03-06 | Improvements in or relating to gas turbine plant |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1199576A true FR1199576A (en) | 1959-12-15 |
Family
ID=9832098
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1199576D Expired FR1199576A (en) | 1957-03-06 | 1958-03-06 | Improvements made to power plants with gas turbines, in particular for jet propulsion |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1199576A (en) |
GB (1) | GB838602A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3095696A (en) * | 1959-09-25 | 1963-07-02 | Roy W Rumble | Combustion-engine exhaust systems |
DE1270891B (en) * | 1963-12-17 | 1968-06-20 | Hans Georg Muenzberg | Gas turbine engine with a short axial length |
FR2378182A1 (en) * | 1977-01-19 | 1978-08-18 | Rolls Royce | GAS TURBINE PROPELLER IMPROVEMENTS |
EP0022692A1 (en) * | 1979-07-16 | 1981-01-21 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Turbofan with variable by-pass ratio |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1483743A (en) * | 1965-12-02 | 1967-06-09 | Snecma | Turbomachine with contra-rotating compressor |
DE1626110B1 (en) * | 1966-03-02 | 1969-12-18 | Rolls Royce | Gas turbine fan engine |
US3375997A (en) * | 1966-06-10 | 1968-04-02 | Gen Electric | Compound aircraft and propulsion system |
FR2181472B1 (en) * | 1972-04-25 | 1975-08-29 | Snecma | |
GB2309745A (en) * | 1996-02-02 | 1997-08-06 | John Peter Miller | Multi-stage compressor |
JP2016509153A (en) * | 2013-01-18 | 2016-03-24 | ゼネラル・エレクトリック・カンパニイ | Engine configuration with reverse rotation integrated drive and vaneless turbine |
CN108757509B (en) * | 2018-05-30 | 2020-09-29 | 中国航发动力股份有限公司 | Low-pressure compressor structure of gas turbine |
-
1957
- 1957-03-06 GB GB738457A patent/GB838602A/en not_active Expired
-
1958
- 1958-03-06 FR FR1199576D patent/FR1199576A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3095696A (en) * | 1959-09-25 | 1963-07-02 | Roy W Rumble | Combustion-engine exhaust systems |
DE1270891B (en) * | 1963-12-17 | 1968-06-20 | Hans Georg Muenzberg | Gas turbine engine with a short axial length |
FR2378182A1 (en) * | 1977-01-19 | 1978-08-18 | Rolls Royce | GAS TURBINE PROPELLER IMPROVEMENTS |
EP0022692A1 (en) * | 1979-07-16 | 1981-01-21 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Turbofan with variable by-pass ratio |
FR2461820A1 (en) * | 1979-07-16 | 1981-02-06 | Snecma | MULTIFLUX TURBOREACTOR WITH A DILUTION RATE |
Also Published As
Publication number | Publication date |
---|---|
GB838602A (en) | 1960-06-22 |
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