GB783599A - Improvements in or relating to gas turbine plant - Google Patents
Improvements in or relating to gas turbine plantInfo
- Publication number
- GB783599A GB783599A GB21006/55A GB2100655A GB783599A GB 783599 A GB783599 A GB 783599A GB 21006/55 A GB21006/55 A GB 21006/55A GB 2100655 A GB2100655 A GB 2100655A GB 783599 A GB783599 A GB 783599A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tube
- gas turbine
- relating
- turbine plant
- july
- 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
- 238000002485 combustion reaction Methods 0.000 abstract 2
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
- 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
-
- 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
- F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
-
- 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
- F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
-
- 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
- F02C7/26—Starting; Ignition
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
Abstract
783,599. Lighting burners. GARRETT CORPORATION. July 20, 1955 [July 30, 1954], No. 21006/55. Class 75(3) [Also in Groups XII, XIII and XXVI] A gas turbine combustion chamber is ignited by inserting a blow lamp 78 into a tube 72 mounted on the side of the combustion chamber casing so as to direct the flame on to the flame tube 43. The end of the tube 72 has a valve 73 which automatically closes the tube when the blow lamp is withdrawn after the engine has started. Specification 783,600 [Group XXVI] is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US783599XA | 1954-07-30 | 1954-07-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB783599A true GB783599A (en) | 1957-09-25 |
Family
ID=22143541
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB21006/55A Expired GB783599A (en) | 1954-07-30 | 1955-07-20 | Improvements in or relating to gas turbine plant |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB783599A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0101942A2 (en) * | 1982-07-28 | 1984-03-07 | Itamar Orian | Gas generator of the turbo-compressor type for low capacity, pressure and temperature |
-
1955
- 1955-07-20 GB GB21006/55A patent/GB783599A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0101942A2 (en) * | 1982-07-28 | 1984-03-07 | Itamar Orian | Gas generator of the turbo-compressor type for low capacity, pressure and temperature |
EP0101942A3 (en) * | 1982-07-28 | 1984-11-14 | Itamar Orian | Gas generator of the turbo-compressor type for low capacity, pressure and temperature |
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