GB2309296B - Gas turbine engine combuster - Google Patents

Gas turbine engine combuster

Info

Publication number
GB2309296B
GB2309296B GB9520778A GB9520778A GB2309296B GB 2309296 B GB2309296 B GB 2309296B GB 9520778 A GB9520778 A GB 9520778A GB 9520778 A GB9520778 A GB 9520778A GB 2309296 B GB2309296 B GB 2309296B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
combuster
engine combuster
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
GB9520778A
Other versions
GB2309296A (en
GB9520778D0 (en
Inventor
R Noden
Eric Roy Norster
Simon Mario Depietro
Michael Craig 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.)
Alstom Power UK Holdings Ltd
Original Assignee
Alstom Power UK Holdings Ltd
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 Alstom Power UK Holdings Ltd filed Critical Alstom Power UK Holdings Ltd
Priority to GB9520778A priority Critical patent/GB2309296B/en
Publication of GB9520778D0 publication Critical patent/GB9520778D0/en
Publication of GB2309296A publication Critical patent/GB2309296A/en
Application granted granted Critical
Publication of GB2309296B publication Critical patent/GB2309296B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/06Arrangement of apertures along the flame tube
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/24Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants of the fluid-screen type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/20Heat transfer, e.g. cooling
    • F05B2260/201Heat transfer, e.g. cooling by impingement of a fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/96Preventing, counteracting or reducing vibration or noise
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03041Effusion cooled combustion chamber walls or domes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03044Impingement cooled combustion chamber walls or subassemblies
GB9520778A 1995-10-11 1995-10-11 Gas turbine engine combuster Expired - Lifetime GB2309296B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9520778A GB2309296B (en) 1995-10-11 1995-10-11 Gas turbine engine combuster

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9520778A GB2309296B (en) 1995-10-11 1995-10-11 Gas turbine engine combuster

Publications (3)

Publication Number Publication Date
GB9520778D0 GB9520778D0 (en) 1995-12-13
GB2309296A GB2309296A (en) 1997-07-23
GB2309296B true GB2309296B (en) 2000-02-09

Family

ID=10782120

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9520778A Expired - Lifetime GB2309296B (en) 1995-10-11 1995-10-11 Gas turbine engine combuster

Country Status (1)

Country Link
GB (1) GB2309296B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110848030A (en) * 2019-11-25 2020-02-28 东方电气集团东方汽轮机有限公司 Optimization method for gas turbine combustor flame tube impingement cooling system

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE59809097D1 (en) * 1998-09-30 2003-08-28 Alstom Switzerland Ltd Combustion chamber for a gas turbine
EP1221574B2 (en) * 2001-01-09 2017-12-20 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor
US6351947B1 (en) 2000-04-04 2002-03-05 Abb Alstom Power (Schweiz) Combustion chamber for a gas turbine
US6530221B1 (en) 2000-09-21 2003-03-11 Siemens Westinghouse Power Corporation Modular resonators for suppressing combustion instabilities in gas turbine power plants
JP2002195565A (en) 2000-12-26 2002-07-10 Mitsubishi Heavy Ind Ltd Gas turbine
JP3962554B2 (en) 2001-04-19 2007-08-22 三菱重工業株式会社 Gas turbine combustor and gas turbine
ITMI20012785A1 (en) * 2001-12-21 2003-06-23 Nuovo Pignone Spa IMPIANT PIPE OR "LINER" IMPROVED FOR A COMBUSTION CHAMBER OF A LOW-EMISSION GAS TURBINE
US6964170B2 (en) 2003-04-28 2005-11-15 Pratt & Whitney Canada Corp. Noise reducing combustor
DE102005059184B3 (en) * 2005-12-02 2007-09-06 Deutsches Zentrum für Luft- und Raumfahrt e.V. Apparatus and method for damping thermoacoustic resonances in combustion chambers
EP1832812A3 (en) * 2006-03-10 2012-01-04 Rolls-Royce Deutschland Ltd & Co KG Gas turbine combustion chamber wall with absorption of combustion chamber vibrations
EP2644995A1 (en) 2012-03-27 2013-10-02 Siemens Aktiengesellschaft An improved hole arrangement of liners of a combustion chamber of a gas turbine engine with low combustion dynamics and emissions
DE102019205540A1 (en) * 2019-04-17 2020-10-22 Siemens Aktiengesellschaft Resonator, method for producing such and burner arrangement provided with such

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB816878A (en) * 1956-04-18 1959-07-22 Rolls Royce Improvements in or relating to combustion equipment
GB2169696A (en) * 1984-12-17 1986-07-16 Gen Electric Gas turbine augmentor

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB816878A (en) * 1956-04-18 1959-07-22 Rolls Royce Improvements in or relating to combustion equipment
GB2169696A (en) * 1984-12-17 1986-07-16 Gen Electric Gas turbine augmentor
GB2206686A (en) * 1984-12-17 1989-01-11 Gen Electric Gas-turbine augmentor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110848030A (en) * 2019-11-25 2020-02-28 东方电气集团东方汽轮机有限公司 Optimization method for gas turbine combustor flame tube impingement cooling system
CN110848030B (en) * 2019-11-25 2021-09-21 东方电气集团东方汽轮机有限公司 Optimization method for gas turbine combustor flame tube impingement cooling system

Also Published As

Publication number Publication date
GB2309296A (en) 1997-07-23
GB9520778D0 (en) 1995-12-13

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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)

Free format text: REGISTERED BETWEEN 20140904 AND 20140910

PE20 Patent expired after termination of 20 years

Expiry date: 20151010