DE69111614T2 - Gas turbine combustion chamber and its working methods. - Google Patents

Gas turbine combustion chamber and its working methods.

Info

Publication number
DE69111614T2
DE69111614T2 DE1991611614 DE69111614T DE69111614T2 DE 69111614 T2 DE69111614 T2 DE 69111614T2 DE 1991611614 DE1991611614 DE 1991611614 DE 69111614 T DE69111614 T DE 69111614T DE 69111614 T2 DE69111614 T2 DE 69111614T2
Authority
DE
Germany
Prior art keywords
combustion chamber
gas turbine
turbine combustion
working methods
working
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
DE1991611614
Other languages
German (de)
Other versions
DE69111614D1 (en
Inventor
Ian James Toon
Stephen James O'dell
Jeffrey Willis
Paul Currin
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
Priority to GB909023004A priority Critical patent/GB9023004D0/en
Priority to GB919118945A priority patent/GB9118945D0/en
Application filed by Rolls-Royce PLC filed Critical Rolls-Royce PLC
Priority to PCT/GB1991/001658 priority patent/WO1992007221A1/en
Application granted granted Critical
Publication of DE69111614T2 publication Critical patent/DE69111614T2/en
Anticipated expiration legal-status Critical
Application status is Expired - Lifetime legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F23R3/346—Feeding into different combustion zones for staged combustion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
    • F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
    • F23C6/045—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure
    • F23C6/047—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure with fuel supply in stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
DE1991611614 1990-10-23 1991-09-26 Gas turbine combustion chamber and its working methods. Expired - Lifetime DE69111614T2 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB909023004A GB9023004D0 (en) 1990-10-23 1990-10-23 A gas turbine engine combustion chamber and a method of operating a gas turbine engine combustion chamber
GB919118945A GB9118945D0 (en) 1991-09-05 1991-09-05 A gas turbine engine combustion chamber and a method of operating a gas turbine engine combustion chamber
PCT/GB1991/001658 WO1992007221A1 (en) 1990-10-23 1991-09-26 Gasturbine combustion chamber and method of operation thereof

Publications (1)

Publication Number Publication Date
DE69111614T2 true DE69111614T2 (en) 1995-12-21

Family

ID=26297840

Family Applications (2)

Application Number Title Priority Date Filing Date
DE1991611614 Expired - Fee Related DE69111614D1 (en) 1990-10-23 1991-09-26 Gas turbine combustion chamber and its working methods.
DE1991611614 Expired - Lifetime DE69111614T2 (en) 1990-10-23 1991-09-26 Gas turbine combustion chamber and its working methods.

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE1991611614 Expired - Fee Related DE69111614D1 (en) 1990-10-23 1991-09-26 Gas turbine combustion chamber and its working methods.

Country Status (4)

Country Link
EP (1) EP0554325B1 (en)
JP (1) JP3077939B2 (en)
DE (2) DE69111614D1 (en)
WO (1) WO1992007221A1 (en)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9122965D0 (en) * 1991-10-29 1991-12-18 Rolls Royce Plc Turbine engine control system
GB2278431A (en) * 1993-05-24 1994-11-30 Rolls Royce Plc A gas turbine engine combustion chamber
US5394688A (en) * 1993-10-27 1995-03-07 Westinghouse Electric Corporation Gas turbine combustor swirl vane arrangement
GB2284884B (en) * 1993-12-16 1997-12-10 Rolls Royce Plc A gas turbine engine combustion chamber
GB9410233D0 (en) 1994-05-21 1994-07-06 Rolls Royce Plc A gas turbine engine combustion chamber
DE69428549T2 (en) * 1994-07-13 2002-05-08 Volvo Aero Corp pollutant emission gas turbine chamber low
US5813232A (en) * 1995-06-05 1998-09-29 Allison Engine Company, Inc. Dry low emission combustor for gas turbine engines
DE19532264C2 (en) * 1995-09-01 2001-09-06 Mtu Aero Engines Gmbh Means for preparing a mixture of fuel and air to combustion chambers for gas turbine engines
GB9520002D0 (en) * 1995-09-30 1995-12-06 Rolls Royce Plc Turbine engine control system
GB9611235D0 (en) * 1996-05-30 1996-07-31 Rolls Royce Plc A gas turbine engine combustion chamber and a method of operation thereof
GB9809371D0 (en) 1998-05-02 1998-07-01 Rolls Royce Plc A combustion chamber and a method of operation thereof
GB9813972D0 (en) 1998-06-30 1998-08-26 Rolls Royce Plc A combustion chamber
GB9818160D0 (en) 1998-08-21 1998-10-14 Rolls Royce Plc A combustion chamber
GB9911871D0 (en) 1999-05-22 1999-07-21 Rolls Royce Plc A gas turbine engine and a method of controlling a gas turbine engine
GB9911867D0 (en) 1999-05-22 1999-07-21 Rolls Royce Plc A combustion chamber assembly and a method of operating a combustion chamber assembly
GB9915770D0 (en) 1999-07-07 1999-09-08 Rolls Royce Plc A combustion chamber
GB0019533D0 (en) 2000-08-10 2000-09-27 Rolls Royce Plc A combustion chamber
DE10049205A1 (en) 2000-10-05 2002-05-23 Alstom Switzerland Ltd Process for supplying fuel to a premix burner for operating a gas turbine comprises introducing premix gas separately via two axially divided regions along the burner shell
GB0111788D0 (en) 2001-05-15 2001-07-04 Rolls Royce Plc A combustion chamber
GB0515034D0 (en) 2005-07-21 2005-08-31 Rolls Royce Plc Method and system for operating a multi-stage combustor
US7886539B2 (en) 2007-09-14 2011-02-15 Siemens Energy, Inc. Multi-stage axial combustion system
CN101932792B (en) * 2007-11-12 2013-05-08 格塔斯热力学驱动系统有限责任公司 Axial piston engine and method for operating an axial piston engine
JP5172468B2 (en) * 2008-05-23 2013-03-27 川崎重工業株式会社 The method of the combustion apparatus and the combustion device
US8215116B2 (en) * 2008-10-02 2012-07-10 General Electric Company System and method for air-fuel mixing in gas turbines
WO2011031278A1 (en) * 2009-09-13 2011-03-17 Lean Flame, Inc. Inlet premixer for combustion apparatus
US8866334B2 (en) 2010-03-02 2014-10-21 Icr Turbine Engine Corporation Dispatchable power from a renewable energy facility
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
JP5460846B2 (en) * 2012-12-26 2014-04-02 川崎重工業株式会社 The method of the combustion apparatus and the combustion device
US9534790B2 (en) * 2013-01-07 2017-01-03 General Electric Company Fuel injector for supplying fuel to a combustor
JP6318443B2 (en) * 2013-01-22 2018-05-09 三菱日立パワーシステムズ株式会社 Combustor, and rotary machine
GB201312974D0 (en) * 2013-07-19 2013-09-04 Siemens Ag Turbine engine control system
US20150159877A1 (en) * 2013-12-06 2015-06-11 General Electric Company Late lean injection manifold mixing system

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1039785B (en) * 1957-10-12 1958-09-25 Maschf Augsburg Nuernberg Ag Combustion chamber with high Waermebelastung, in particular for combustion of low calorific value, of gaseous fuels in gas turbine plants
US3605405A (en) * 1970-04-09 1971-09-20 Gen Electric Carbon elimination and cooling improvement to scroll type combustors
US3722216A (en) * 1971-01-04 1973-03-27 Gen Electric Annular slot combustor
US3811278A (en) * 1973-02-01 1974-05-21 Gen Electric Fuel injection apparatus
DE3819898C2 (en) * 1988-06-11 1992-05-27 Daimler-Benz Aktiengesellschaft, 7000 Stuttgart, De
US4910957A (en) * 1988-07-13 1990-03-27 Prutech Ii Staged lean premix low nox hot wall gas turbine combustor with improved turndown capability

Also Published As

Publication number Publication date
JPH06502240A (en) 1994-03-10
EP0554325B1 (en) 1995-07-26
DE69111614D1 (en) 1995-08-31
EP0554325A1 (en) 1993-08-11
WO1992007221A1 (en) 1992-04-30
JP3077939B2 (en) 2000-08-21

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