DE69204280D1 - GAS TURBINE COMBUSTION CHAMBER. - Google Patents

GAS TURBINE COMBUSTION CHAMBER.

Info

Publication number
DE69204280D1
DE69204280D1 DE69204280T DE69204280T DE69204280D1 DE 69204280 D1 DE69204280 D1 DE 69204280D1 DE 69204280 T DE69204280 T DE 69204280T DE 69204280 T DE69204280 T DE 69204280T DE 69204280 D1 DE69204280 D1 DE 69204280D1
Authority
DE
Germany
Prior art keywords
combustion chamber
gas turbine
turbine combustion
gas
chamber
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
DE69204280T
Other languages
German (de)
Other versions
DE69204280T2 (en
Inventor
Anthony Pidcock
Stephen Cooper
Peter Fry
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=10692006&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE69204280(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of DE69204280D1 publication Critical patent/DE69204280D1/en
Publication of DE69204280T2 publication Critical patent/DE69204280T2/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
    • F05B2260/201—Heat transfer, e.g. cooling by impingement of a fluid
    • 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
    • F05B2260/202—Heat transfer, e.g. cooling by film cooling
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE69204280T 1991-03-22 1992-02-03 GAS TURBINE COMBUSTION CHAMBER. Expired - Lifetime DE69204280T2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB919106085A GB9106085D0 (en) 1991-03-22 1991-03-22 Gas turbine engine combustor
PCT/GB1992/000201 WO1992016798A1 (en) 1991-03-22 1992-02-03 Gas turbine engine combustor

Publications (2)

Publication Number Publication Date
DE69204280D1 true DE69204280D1 (en) 1995-09-28
DE69204280T2 DE69204280T2 (en) 1996-01-25

Family

ID=10692006

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69204280T Expired - Lifetime DE69204280T2 (en) 1991-03-22 1992-02-03 GAS TURBINE COMBUSTION CHAMBER.

Country Status (5)

Country Link
EP (1) EP0576435B1 (en)
JP (1) JPH06507468A (en)
DE (1) DE69204280T2 (en)
GB (1) GB9106085D0 (en)
WO (1) WO1992016798A1 (en)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2723177B1 (en) * 1994-07-27 1996-09-06 Snecma COMBUSTION CHAMBER COMPRISING A DOUBLE WALL
GB2298266A (en) * 1995-02-23 1996-08-28 Rolls Royce Plc A cooling arrangement for heat resistant tiles in a gas turbine engine combustor
US5758503A (en) * 1995-05-03 1998-06-02 United Technologies Corporation Gas turbine combustor
DE19516798A1 (en) * 1995-05-08 1996-11-14 Abb Management Ag Premix burner with axial or radial air flow
FR2752916B1 (en) * 1996-09-05 1998-10-02 Snecma THERMAL PROTECTIVE SHIRT FOR TURBOREACTOR COMBUSTION CHAMBER
US6079199A (en) * 1998-06-03 2000-06-27 Pratt & Whitney Canada Inc. Double pass air impingement and air film cooling for gas turbine combustor walls
DE102007018061A1 (en) 2007-04-17 2008-10-23 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustion chamber wall
US20100263386A1 (en) * 2009-04-16 2010-10-21 General Electric Company Turbine engine having a liner
DE102009032277A1 (en) 2009-07-08 2011-01-20 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber head of a gas turbine
CH703657A1 (en) * 2010-08-27 2012-02-29 Alstom Technology Ltd Method for operating a burner arrangement and burner arrangement for implementing the process.
JP2012145098A (en) * 2010-12-21 2012-08-02 Toshiba Corp Transition piece, and gas turbine
US20120180492A1 (en) * 2011-01-14 2012-07-19 General Electric Company Apparatus for vibration support in combustors and method for forming apparatus
GB201105790D0 (en) 2011-04-06 2011-05-18 Rolls Royce Plc A cooled double walled article
EP2559942A1 (en) 2011-08-19 2013-02-20 Rolls-Royce Deutschland Ltd & Co KG Gas turbine combustion chamber head with cooling and damping
JP5821550B2 (en) * 2011-11-10 2015-11-24 株式会社Ihi Combustor liner
DE102012016493A1 (en) 2012-08-21 2014-02-27 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustor with impingement-cooled bolts of the combustion chamber shingles
DE102012025375A1 (en) 2012-12-27 2014-07-17 Rolls-Royce Deutschland Ltd & Co Kg Method for arranging impingement cooling holes and effusion holes in a combustion chamber wall of a gas turbine
DE102013003444A1 (en) 2013-02-26 2014-09-11 Rolls-Royce Deutschland Ltd & Co Kg Impact-cooled shingle of a gas turbine combustor with extended effusion holes
DE102013222932A1 (en) 2013-11-11 2015-05-28 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustion chamber with shingle for carrying out a spark plug
DE102013226488A1 (en) 2013-12-18 2015-06-18 Rolls-Royce Deutschland Ltd & Co Kg Washer of a combustion chamber shingle of a gas turbine
DE102016222099A1 (en) 2016-11-10 2018-05-17 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber of a gas turbine
JP2024091028A (en) * 2022-12-23 2024-07-04 川崎重工業株式会社 Gas turbine combustor

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1093515A (en) * 1966-04-06 1967-12-06 Rolls Royce Method of producing combustion chambers and similar components for gas turbine engines
US3422620A (en) * 1967-05-04 1969-01-21 Westinghouse Electric Corp Combustion apparatus
GB1552132A (en) * 1975-11-29 1979-09-12 Rolls Royce Combustion chambers for gas turbine engines
GB2087065B (en) * 1980-11-08 1984-11-07 Rolls Royce Wall structure for a combustion chamber
US4422300A (en) * 1981-12-14 1983-12-27 United Technologies Corporation Prestressed combustor liner for gas turbine engine
GB2204672B (en) * 1987-05-06 1991-03-06 Rolls Royce Plc Combustor
GB2221979B (en) * 1988-08-17 1992-03-25 Rolls Royce Plc A combustion chamber for a gas turbine engine

Also Published As

Publication number Publication date
JPH06507468A (en) 1994-08-25
EP0576435A1 (en) 1994-01-05
WO1992016798A1 (en) 1992-10-01
DE69204280T2 (en) 1996-01-25
GB9106085D0 (en) 1991-05-08
EP0576435B1 (en) 1995-08-23

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Legal Events

Date Code Title Description
8363 Opposition against the patent
8365 Fully valid after opposition proceedings