DE60026235D1 - Gasturbine und deren Regelung - Google Patents

Gasturbine und deren Regelung

Info

Publication number
DE60026235D1
DE60026235D1 DE60026235T DE60026235T DE60026235D1 DE 60026235 D1 DE60026235 D1 DE 60026235D1 DE 60026235 T DE60026235 T DE 60026235T DE 60026235 T DE60026235 T DE 60026235T DE 60026235 D1 DE60026235 D1 DE 60026235D1
Authority
DE
Germany
Prior art keywords
regulation
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.)
Expired - Lifetime
Application number
DE60026235T
Other languages
English (en)
Other versions
DE60026235T2 (de
Inventor
Jeffrey Douglas Willis
James Melville
Paul Fletcher
Philip Patrick Walsh
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of DE60026235D1 publication Critical patent/DE60026235D1/de
Application granted granted Critical
Publication of DE60026235T2 publication Critical patent/DE60026235T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
    • 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
    • F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/20—Control of working fluid flow by throttling; by adjusting vanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Supercharger (AREA)
DE60026235T 1999-05-22 2000-04-25 Gasturbine und deren Regelung Expired - Lifetime DE60026235T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB9911871 1999-05-22
GBGB9911871.3A GB9911871D0 (en) 1999-05-22 1999-05-22 A gas turbine engine and a method of controlling a gas turbine engine

Publications (2)

Publication Number Publication Date
DE60026235D1 true DE60026235D1 (de) 2006-04-27
DE60026235T2 DE60026235T2 (de) 2006-11-23

Family

ID=10853918

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60026235T Expired - Lifetime DE60026235T2 (de) 1999-05-22 2000-04-25 Gasturbine und deren Regelung

Country Status (4)

Country Link
US (1) US6324828B1 (de)
EP (1) EP1055809B1 (de)
DE (1) DE60026235T2 (de)
GB (1) GB9911871D0 (de)

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US6550253B2 (en) 2001-09-12 2003-04-22 General Electric Company Apparatus and methods for controlling flow in turbomachinery
GB2388160A (en) * 2002-05-03 2003-11-05 Rolls Royce Plc A gas turbine engine and fuel cell stack combination
DE60313392T2 (de) * 2002-05-16 2007-08-09 Rolls-Royce Plc Gasturbine
US20050034446A1 (en) * 2003-08-11 2005-02-17 Fielder William Sheridan Dual capture jet turbine and steam generator
US6897578B1 (en) 2003-12-08 2005-05-24 Ingersoll-Rand Energy Systems Corporation Integrated microturbine gearbox generator assembly
US20060291997A1 (en) * 2004-10-26 2006-12-28 Wilson Erich A Fluid Flow Chambers and Bridges in Bladeless Compressors, Turbines and Pumps
US20060216149A1 (en) * 2004-10-26 2006-09-28 Wilson Erich A Fluid Flow Channels in Bladeless Compressors, Turbines and Pumps
US20080016876A1 (en) * 2005-06-02 2008-01-24 General Electric Company Method and apparatus for reducing gas turbine engine emissions
US7478990B2 (en) * 2005-10-25 2009-01-20 Wilson Erich A Bracket/spacer optimization in bladeless turbines, compressors and pumps
US8915086B2 (en) * 2006-08-07 2014-12-23 General Electric Company System for controlling combustion dynamics and method for operating the same
GB0616832D0 (en) 2006-08-25 2006-10-04 Alstom Technology Ltd Turbomachine
US8382436B2 (en) 2009-01-06 2013-02-26 General Electric Company Non-integral turbine blade platforms and systems
US8262345B2 (en) 2009-02-06 2012-09-11 General Electric Company Ceramic matrix composite turbine engine
WO2010132439A1 (en) 2009-05-12 2010-11-18 Icr Turbine Engine Corporation Gas turbine energy storage and conversion system
US8866334B2 (en) 2010-03-02 2014-10-21 Icr Turbine Engine Corporation Dispatchable power from a renewable energy facility
IT1401425B1 (it) 2010-06-24 2013-07-26 Nuovo Pignone Spa Turboespansore e metodo per usare palette direttrici di ingresso mobili all'ingresso di un compressore
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
AU2011295668A1 (en) 2010-09-03 2013-05-02 Icr Turbine Engine Corporation Gas turbine engine configurations
US9228497B2 (en) * 2010-12-30 2016-01-05 Rolls-Royce Corporation Gas turbine engine with secondary air flow circuit
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
WO2013002664A1 (en) * 2011-06-28 2013-01-03 General Electric Company Rational late lean injection
US9243802B2 (en) * 2011-12-07 2016-01-26 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9097424B2 (en) * 2012-03-12 2015-08-04 General Electric Company System for supplying a fuel and working fluid mixture to a combustor
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
AT514480A1 (de) * 2013-06-27 2015-01-15 Preglau Otto Dr Wirkungsgradverbesserung beim Düsenantrieb im Kraftfahrzeugbau
EP3022491B1 (de) 2013-07-15 2019-10-16 United Technologies Corporation Befestigung einer drallvorrichtung an einer gasturbinenbrennkammer
US10088166B2 (en) 2013-07-15 2018-10-02 United Technologies Corporation Swirler mount interface for gas turbine engine combustor
WO2015030928A1 (en) 2013-08-30 2015-03-05 United Technologies Corporation Swirler mount interface for a gas turbine engine combustor
EP3102887B1 (de) 2014-01-24 2023-11-15 RTX Corporation Axiale gestufte brennkammer mit beschränktem hauptbrennstoffinjektor
US9869190B2 (en) 2014-05-30 2018-01-16 General Electric Company Variable-pitch rotor with remote counterweights
GB201414662D0 (en) * 2014-08-19 2014-10-01 Rolls Royce Plc Method of operation of a gas turbine engine
GB201414661D0 (en) * 2014-08-19 2014-10-01 Rolls Royce Plc Gas turbine engine and method of operation
US10072510B2 (en) 2014-11-21 2018-09-11 General Electric Company Variable pitch fan for gas turbine engine and method of assembling the same
US10119592B2 (en) * 2015-03-06 2018-11-06 Elwha Llc Vehicle drivetrain with active magnetic bearings
EP3130539B1 (de) 2015-08-12 2020-04-08 Rolls-Royce North American Technologies, Inc. Wärmetauscher für ein gasturbinenmotorantriebssystem
US10100653B2 (en) 2015-10-08 2018-10-16 General Electric Company Variable pitch fan blade retention system
US10801728B2 (en) 2016-12-07 2020-10-13 Raytheon Technologies Corporation Gas turbine engine combustor main mixer with vane supported centerbody
US11149952B2 (en) 2016-12-07 2021-10-19 Raytheon Technologies Corporation Main mixer in an axial staged combustor for a gas turbine engine
US11174816B2 (en) 2019-02-25 2021-11-16 Rolls-Royce Corporation Bypass duct conformal heat exchanger array
US11674435B2 (en) 2021-06-29 2023-06-13 General Electric Company Levered counterweight feathering system
US11795964B2 (en) 2021-07-16 2023-10-24 General Electric Company Levered counterweight feathering system

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US3025688A (en) 1959-06-11 1962-03-20 Draper Corp Pattern mechanism for knitting machines
GB1489339A (en) 1973-11-30 1977-10-19 Rolls Royce Gas turbine engine combustion chambers
US3949548A (en) * 1974-06-13 1976-04-13 Lockwood Jr Hanford N Gas turbine regeneration system
US4178754A (en) * 1976-07-19 1979-12-18 The Hydragon Corporation Throttleable turbine engine
US4145875A (en) 1976-10-15 1979-03-27 General Motors Corporation Variable flow capacity gas turbine engine for improved part load fuel economy
US4215537A (en) * 1978-07-27 1980-08-05 Avco Corporation Apparatus for and method of suppressing infrared radiation emitted from gas turbine engine
JPS5910742A (ja) * 1982-07-08 1984-01-20 Toyota Motor Corp ガスタ−ビン機関の制御装置
GB8722714D0 (en) 1987-09-26 1987-11-04 Rolls Royce Plc Variable guide vane arrangement for compressor
GB9023004D0 (en) * 1990-10-23 1990-12-05 Rolls Royce Plc A gas turbine engine combustion chamber and a method of operating a gas turbine engine combustion chamber
EP0554325B1 (de) 1990-10-23 1995-07-26 ROLLS-ROYCE plc Gasturbinenbrennkammer und deren arbeitsweise
US5224337A (en) * 1991-05-22 1993-07-06 Mitsubishi Jukogyo Kabushiki Kaisha Operating method for gas turbine with variable inlet vanes
US5613357A (en) * 1993-07-07 1997-03-25 Mowill; R. Jan Star-shaped single stage low emission combustor system
JPH07189746A (ja) * 1993-12-28 1995-07-28 Hitachi Ltd ガスタービン燃焼器の制御方法
US5497615A (en) * 1994-03-21 1996-03-12 Noe; James C. Gas turbine generator set
GB2301868B (en) 1995-06-05 1999-08-11 Rolls Royce Plc Improved actuator mechanism for variable angle vane arrays
US6253538B1 (en) * 1999-09-27 2001-07-03 Pratt & Whitney Canada Corp. Variable premix-lean burn combustor

Also Published As

Publication number Publication date
EP1055809A3 (de) 2002-11-27
DE60026235T2 (de) 2006-11-23
EP1055809B1 (de) 2006-03-01
EP1055809A2 (de) 2000-11-29
GB9911871D0 (en) 1999-07-21
US6324828B1 (en) 2001-12-04

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition