DE59208713D1 - Gas turbine combustor - Google Patents

Gas turbine combustor

Info

Publication number
DE59208713D1
DE59208713D1 DE59208713T DE59208713T DE59208713D1 DE 59208713 D1 DE59208713 D1 DE 59208713D1 DE 59208713 T DE59208713 T DE 59208713T DE 59208713 T DE59208713 T DE 59208713T DE 59208713 D1 DE59208713 D1 DE 59208713D1
Authority
DE
Germany
Prior art keywords
gas turbine
turbine combustor
combustor
gas
turbine
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
DE59208713T
Other languages
German (de)
Inventor
Albert Keller
Stefan Tschirren
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.)
Alstom SA
Original Assignee
Asea Brown Boveri AG Switzerland
Asea Brown Boveri AB
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 Asea Brown Boveri AG Switzerland, Asea Brown Boveri AB filed Critical Asea Brown Boveri AG Switzerland
Application granted granted Critical
Publication of DE59208713D1 publication Critical patent/DE59208713D1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/20—Heat transfer, e.g. cooling
    • F05B2260/205—Cooling fluid recirculation, i.e. after having cooled one or more components the cooling fluid is recovered and used elsewhere for other purposes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/20—Heat transfer, e.g. cooling
    • F05B2260/221—Improvement of heat transfer
    • F05B2260/224—Improvement of heat transfer by increasing the heat transfer surface
    • F05B2260/2241—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
DE59208713T 1992-11-09 1992-11-09 Gas turbine combustor Expired - Lifetime DE59208713D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP19920119123 EP0597137B1 (en) 1992-11-09 1992-11-09 Combustion chamber for gas turbine

Publications (1)

Publication Number Publication Date
DE59208713D1 true DE59208713D1 (en) 1997-08-21

Family

ID=8210217

Family Applications (1)

Application Number Title Priority Date Filing Date
DE59208713T Expired - Lifetime DE59208713D1 (en) 1992-11-09 1992-11-09 Gas turbine combustor

Country Status (3)

Country Link
EP (1) EP0597137B1 (en)
JP (1) JP3526895B2 (en)
DE (1) DE59208713D1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998013645A1 (en) * 1996-09-26 1998-04-02 Siemens Aktiengesellschaft Thermal shield component with cooling fluid recirculation and heat shield arrangement for a component circulating hot gas
DE59907940D1 (en) 1998-03-10 2004-01-15 Siemens Ag COMBUSTION CHAMBER AND METHOD FOR OPERATING A COMBUSTION CHAMBER
SE9801822L (en) * 1998-05-25 1999-11-26 Abb Ab combustion device
DE59810344D1 (en) 1998-07-27 2004-01-15 Alstom Switzerland Ltd Process for operating a gas turbine combustor with gaseous fuel
EP1482246A1 (en) 2003-05-30 2004-12-01 Siemens Aktiengesellschaft Combustion chamber
WO2020245537A1 (en) * 2019-06-07 2020-12-10 Safran Helicopter Engines Method for manufacturing a flame tube for a turbomachine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4012902A (en) * 1974-03-29 1977-03-22 Phillips Petroleum Company Method of operating a gas turbine combustor having an independent airstream to remove heat from the primary combustion zone
US4288980A (en) * 1979-06-20 1981-09-15 Brown Boveri Turbomachinery, Inc. Combustor for use with gas turbines
US4414816A (en) * 1980-04-02 1983-11-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Combustor liner construction

Also Published As

Publication number Publication date
JPH06213458A (en) 1994-08-02
EP0597137B1 (en) 1997-07-16
JP3526895B2 (en) 2004-05-17
EP0597137A1 (en) 1994-05-18

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: ALSTOM, PARIS, FR

8328 Change in the person/name/address of the agent

Free format text: ROESLER, U., DIPL.-PHYS.UNIV., PAT.-ANW., 81241 MUENCHEN

8330 Complete disclaimer