GB635195A - Improvements in and relating to gas turbine power plant - Google Patents
Improvements in and relating to gas turbine power plantInfo
- Publication number
- GB635195A GB635195A GB10245/45A GB1024545A GB635195A GB 635195 A GB635195 A GB 635195A GB 10245/45 A GB10245/45 A GB 10245/45A GB 1024545 A GB1024545 A GB 1024545A GB 635195 A GB635195 A GB 635195A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- tubes
- supplied
- steam
- heat exchanger
- 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
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
- F02C7/27—Fluid drives
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K21/00—Steam engine plants not otherwise provided for
- F01K21/04—Steam engine plants not otherwise provided for using mixtures of steam and gas; Plants generating or heating steam by bringing water or steam into direct contact with hot gas
- F01K21/047—Steam engine plants not otherwise provided for using mixtures of steam and gas; Plants generating or heating steam by bringing water or steam into direct contact with hot gas having at least one combustion gas turbine
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
635,195. Elastic fluid turbines. BRITISH THOMSON-HOUSTON CO., Ltd., April 24, 1945, No. 10245. Convention date, April 26, 1944. [Class 110(iii)] In a power plant, which may form part of a locomotive engine; comprising a gas turbine driving a compressor which supplies air through a heat exchanger to one or more combustion chambers supplying gas to the turbine, the exhaust gases from the latter passing through the heat exchanger and through a boiler to raise steam, the turbine also provides. the output power and has starting nozzles through which steam from the boiler can be supplied for starting the plant. Air from an axial flow compressor 6 passes through the tubes 33 of the heat exchanger to an annular chamber 23, from which it enters a series of combustion chambers 12 through concentric walls 13, 14 and openings 16. Fuel is supplied through nozzles 17. The exhaust gases leaving the blades 19 of the turbine are discharged to a chamber defined by walls 27, 28, 29, and flow across the heat exchanger tubes 33, boiler tubes 39 and superheater tubes 45. The boiler tubes are connected by headers 37, 38 and pipes 41, 42 to a water drum 40. The latter may be supplied with water through a pipe 43. Steam passes from a steam dome 40<1> to the superheater tubes, from which it may be supplied through pipe 50 for heating and other purposes and through pipe 46 to a nozzle box 48 to assist in driving the turbine. The plant is started by steam raised by an auxiliary combustion chamber 52, air for this purpose being supplied by a motordriven centrifugal compressor 54. The latter and a motor-driven starting fuel pump may be operated by an electric storage battery. The normal running fuel pump and other auxiliaries may be driven from the turbine shaft through gearing. Specification 413,697 is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US635195XA | 1944-04-26 | 1944-04-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB635195A true GB635195A (en) | 1950-04-05 |
Family
ID=22049753
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB10245/45A Expired GB635195A (en) | 1944-04-26 | 1945-04-24 | Improvements in and relating to gas turbine power plant |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB635195A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0372472A1 (en) * | 1988-12-09 | 1990-06-13 | Hitachi, Ltd. | Method and device for starting a gas turbine |
GB2326197A (en) * | 1997-06-11 | 1998-12-16 | Solar Turbines Inc | Gas turbine engine with recuperator |
WO2006015857A1 (en) * | 2004-08-11 | 2006-02-16 | Airbus Deutschland Gmbh | Compressed-air generating system |
EP1790834A1 (en) * | 2005-04-18 | 2007-05-30 | ALSTOM Technology Ltd | Turbosatz mit Vorrichtung zum Hochfahren |
-
1945
- 1945-04-24 GB GB10245/45A patent/GB635195A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0372472A1 (en) * | 1988-12-09 | 1990-06-13 | Hitachi, Ltd. | Method and device for starting a gas turbine |
GB2326197A (en) * | 1997-06-11 | 1998-12-16 | Solar Turbines Inc | Gas turbine engine with recuperator |
WO2006015857A1 (en) * | 2004-08-11 | 2006-02-16 | Airbus Deutschland Gmbh | Compressed-air generating system |
CN101014760B (en) * | 2004-08-11 | 2012-04-04 | 空中客车德国运营有限责任公司 | Compressed air generating system |
EP1790834A1 (en) * | 2005-04-18 | 2007-05-30 | ALSTOM Technology Ltd | Turbosatz mit Vorrichtung zum Hochfahren |
CH697636B1 (en) * | 2005-04-18 | 2008-12-31 | Alstom Technology Ltd | Turbine group with starting device. |
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