CH304500A - Gas turbine plant. - Google Patents
Gas turbine plant.Info
- Publication number
- CH304500A CH304500A CH304500DA CH304500A CH 304500 A CH304500 A CH 304500A CH 304500D A CH304500D A CH 304500DA CH 304500 A CH304500 A CH 304500A
- Authority
- CH
- Switzerland
- Prior art keywords
- gas turbine
- turbine plant
- plant
- gas
- turbine
- Prior art date
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
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
-
- 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
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
-
- 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
- F02K3/075—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 controlling flow ratio between flows
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB18370/51A GB712633A (en) | 1952-07-22 | 1952-07-22 | Improvements relating to gas-turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
CH304500A true CH304500A (en) | 1955-01-15 |
Family
ID=32011990
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH304500D CH304500A (en) | 1952-07-22 | 1952-08-01 | Gas turbine plant. |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH304500A (en) |
FR (1) | FR1066903A (en) |
GB (1) | GB712633A (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB805418A (en) * | 1955-10-05 | 1958-12-03 | Power Jets Res & Dev Ltd | Jet propulsion plant |
DE1276969B (en) * | 1962-10-30 | 1968-09-05 | Bristol Siddeley Engines Ltd | Gas turbine jet engine |
US4064692A (en) * | 1975-06-02 | 1977-12-27 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Variable cycle gas turbine engines |
US4142365A (en) * | 1976-11-01 | 1979-03-06 | General Electric Company | Hybrid mixer for a high bypass ratio gas turbofan engine |
FR2713749B1 (en) * | 1993-12-15 | 1996-01-12 | Snecma | Post-combustion chamber of gas turbine. |
-
1952
- 1952-07-22 GB GB18370/51A patent/GB712633A/en not_active Expired
- 1952-07-31 FR FR1066903D patent/FR1066903A/en not_active Expired
- 1952-08-01 CH CH304500D patent/CH304500A/en unknown
Also Published As
Publication number | Publication date |
---|---|
FR1066903A (en) | 1954-06-10 |
GB712633A (en) | 1954-07-28 |
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