GB9911677D0 - Method for operating a gas turbine - Google Patents

Method for operating a gas turbine

Info

Publication number
GB9911677D0
GB9911677D0 GBGB9911677.4A GB9911677A GB9911677D0 GB 9911677 D0 GB9911677 D0 GB 9911677D0 GB 9911677 A GB9911677 A GB 9911677A GB 9911677 D0 GB9911677 D0 GB 9911677D0
Authority
GB
United Kingdom
Prior art keywords
operating
gas turbine
turbine
gas
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.)
Withdrawn
Application number
GBGB9911677.4A
Other versions
GB2341641A (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ABB Patent GmbH
Original Assignee
ABB Patent GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by ABB Patent GmbH filed Critical ABB Patent GmbH
Publication of GB9911677D0 publication Critical patent/GB9911677D0/en
Publication of GB2341641A publication Critical patent/GB2341641A/en
Withdrawn legal-status Critical Current

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
    • F02C7/22—Fuel supply systems
    • F02C7/222—Fuel flow conduits, e.g. manifolds
    • 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
    • F02C7/22—Fuel supply systems
    • F02C7/232—Fuel valves; Draining valves or systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)
GB9911677A 1998-06-05 1999-05-19 Ring fuel conduits having switchable valves Withdrawn GB2341641A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1998125335 DE19825335A1 (en) 1998-06-05 1998-06-05 Procedure for operation of gas turbine

Publications (2)

Publication Number Publication Date
GB9911677D0 true GB9911677D0 (en) 1999-07-21
GB2341641A GB2341641A (en) 2000-03-22

Family

ID=7870131

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9911677A Withdrawn GB2341641A (en) 1998-06-05 1999-05-19 Ring fuel conduits having switchable valves

Country Status (3)

Country Link
JP (1) JP2000002421A (en)
DE (1) DE19825335A1 (en)
GB (1) GB2341641A (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2003067055A1 (en) * 2002-02-04 2003-08-14 Alstom Technology Ltd Method for operating a gas turbine having several burners
ES2548236T3 (en) 2004-12-23 2015-10-15 Alstom Technology Ltd Procedure for the operation of a group of gas turbines
GB201000274D0 (en) * 2010-01-11 2010-02-24 Rolls Royce Plc Fuel control arrangement
DE102011117603A1 (en) 2010-11-17 2012-05-24 Alstom Technology Ltd. Combustion chamber and method for damping pulsations
DE102011118411A1 (en) * 2010-12-09 2012-06-14 Alstom Technology Ltd. Combustion chamber and method for supplying fuel to a combustion chamber

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB852290A (en) * 1957-01-28 1960-10-26 Rolls Royce Engine liquid fuel supply system
DE1282356B (en) * 1964-10-06 1968-11-07 Daimler Benz Ag Fuel supply system for gas turbine engines with several fuel return nozzles
US3335567A (en) * 1965-11-19 1967-08-15 Gen Electric Multi-nozzle fuel delivery system
GB2036296B (en) * 1978-11-20 1982-12-01 Rolls Royce Gas turbine
US4903478A (en) * 1987-06-25 1990-02-27 General Electric Company Dual manifold fuel system
US4817389A (en) * 1987-09-24 1989-04-04 United Technologies Corporation Fuel injection system
GB2210446B (en) * 1987-09-30 1991-09-18 Gen Electric Fuel distribution system
US5321949A (en) * 1991-07-12 1994-06-21 General Electric Company Staged fuel delivery system with secondary distribution valve
US5226287A (en) * 1991-07-19 1993-07-13 General Electric Company Compressor stall recovery apparatus
US5339636A (en) * 1992-12-04 1994-08-23 United Technologies Corporation Fuel splitter valve assembly for gas turbine

Also Published As

Publication number Publication date
GB2341641A (en) 2000-03-22
JP2000002421A (en) 2000-01-07
DE19825335A1 (en) 1999-12-09

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Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)