GB2176274B - Combustor for gas turbine engine - Google Patents

Combustor for gas turbine engine

Info

Publication number: GB2176274B
Authority: GB; United Kingdom
Prior art keywords: combustor; gas turbine; turbine engine; engine; gas
Prior art date: 1985-06-07
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

Application number

GB08515658A

Other versions

GB2176274A (en

Inventor

Michael Francis Cannon

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

Ruston Gas Turbines 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.)

1985-06-07

Filing date

1985-06-20

Publication date

1989-02-01

1985-06-20 Application filed by Ruston Gas Turbines Ltd filed Critical Ruston Gas Turbines Ltd

1986-06-04 Priority to DE8686304249T priority Critical patent/DE3663847D1/en

1986-06-04 Priority to EP86304249A priority patent/EP0204553B1/en

1986-06-04 Priority to US06/870,388 priority patent/US4763481A/en

1986-12-17 Publication of GB2176274A publication Critical patent/GB2176274A/en

1989-02-01 Application granted granted Critical

1989-02-01 Publication of GB2176274B publication Critical patent/GB2176274B/en

Status Expired legal-status Critical Current

Links

Classifications

- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
- F23D11/12—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour characterised by the shape or arrangement of the outlets from the nozzle
- 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
- 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
- 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
- F23R3/36—Supply of different fuels
- 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
- F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]
- 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
- F23R2900/03041—Effusion cooled combustion chamber walls or domes

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Combustion Methods Of Internal-Combustion Engines (AREA)

GB08515658A 1985-06-07 1985-06-20 Combustor for gas turbine engine Expired GB2176274B (en)

Priority Applications (3)

Application Number	Priority Date	Filing Date	Title
DE8686304249T DE3663847D1 (en)	1985-06-07	1986-06-04	Combustor for gas turbine engine
EP86304249A EP0204553B1 (en)	1985-06-07	1986-06-04	Combustor for gas turbine engine
US06/870,388 US4763481A (en)	1985-06-07	1986-06-04	Combustor for gas turbine engine

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
GB8514388		1985-06-07

Publications (2)

Publication Number	Publication Date
GB2176274A GB2176274A (en)	1986-12-17
GB2176274B true GB2176274B (en)	1989-02-01

Family

ID=10580330

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
GB08515658A Expired GB2176274B (en)	1985-06-07	1985-06-20	Combustor for gas turbine engine

Country Status (2)

Country	Link
JP (1)	JPS6229834A (en)
GB (1)	GB2176274B (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB9505067D0 (en) *	1995-03-14	1995-05-03	Europ Gas Turbines Ltd	Combustor and operating method for gas or liquid-fuelled turbine
RU2131557C1 (en) *	1997-08-20	1999-06-10	Общество ограниченной ответственности "Энерго-аудит"	Intermittent air feeder with adjustable amplitude-frequency response (design versions)
RU2151961C1 (en) *	1998-04-30	2000-06-27	Открытое акционерное общество "Авиадвигатель"	Tubular-annular combustion chamber of gas turbine engine
RU2162194C1 (en) *	1999-11-24	2001-01-20	Общество с ограниченной ответственностью Научно-производственное предприятие "ЭСТ"	Combustion chamber
GB2356924A (en)	1999-12-01	2001-06-06	Abb Alstom Power Uk Ltd	Cooling wall structure for combustor
EP2002185B8 (en)	2006-03-31	2016-09-14	General Electric Technology GmbH	Fuel lance for a gas turbine plant and a method of operating a fuel lance
JP5296320B2 (en) *	2007-01-30	2013-09-25	ゼネラル・エレクトリック・カンパニイ	System having backflow injection mechanism and method for injecting fuel and air
US8622737B2 (en)	2008-07-16	2014-01-07	Robert S. Babington	Perforated flame tube for a liquid fuel burner
US8230687B2 (en) *	2008-09-02	2012-07-31	General Electric Company	Multi-tube arrangement for combustor and method of making the multi-tube arrangement
US8590314B2 (en) *	2010-04-09	2013-11-26	General Electric Company	Combustor liner helical cooling apparatus
US9322557B2 (en) *	2012-01-05	2016-04-26	General Electric Company	Combustor and method for distributing fuel in the combustor
US9534787B2 (en) *	2013-03-12	2017-01-03	General Electric Company	Micromixing cap assembly
JP6621658B2 (en) *	2015-12-22	2019-12-18	川崎重工業株式会社	Fuel injection device
JP7205300B2 (en) *	2019-02-28	2023-01-17	株式会社Ihi	Multi-nozzle burner and combustor
CN115325566B (en) *	2022-07-05	2024-05-24	中国航发湖南动力机械研究所	Mixing air inlet structure of combustor flame tube and mounting method thereof

1985
- 1985-06-20 GB GB08515658A patent/GB2176274B/en not_active Expired
1986
- 1986-06-06 JP JP13166986A patent/JPS6229834A/en active Pending

Also Published As

Publication number	Publication date
JPS6229834A (en)	1987-02-07
GB2176274A (en)	1986-12-17

Legal Events

Date	Code	Title	Description
2005-07-13	PE20	Patent expired after termination of 20 years	Effective date: 20050619

Publication	Publication Date	Title
DE3663847D1 (en)	1989-07-13	Combustor for gas turbine engine
GB8602990D0 (en)	1986-03-12	Gas turbine engine
GB2171151B (en)	1988-05-18	Rotors for gas turbine engines
GB2169696B (en)	1989-06-14	Gas turbine engine augmentor
GB8726985D0 (en)	1987-12-23	Turbofan gas turbine engine
GB8624163D0 (en)	1986-11-12	Turbofan gas turbine engine
GB8509675D0 (en)	1985-05-22	Gas turbine engine
EP0213055A3 (en)	1988-10-19	Gas turbine engine assembly
GB2207191B (en)	1992-03-04	Gas turbine engine
GB2190146B (en)	1990-09-19	Gas turbine engines
GB8616153D0 (en)	1986-12-17	Turbofan gas turbine engine
IL77514A (en)	1991-03-10	Combustor liner for a gas turbine engine
JPS57142422A (en)	1982-09-03	Combustor for gas turbine engine
GB8708859D0 (en)	1987-05-20	Gas turbine engine
GB8610180D0 (en)	1986-10-01	Gas turbine engine
GB8700806D0 (en)	1987-02-18	Turbopropeller/gas turbine engine
DE3661224D1 (en)	1988-12-22	Gas turbine combustor
EP0192266A3 (en)	1987-02-25	Gas turbine combustor
GB8527286D0 (en)	1985-12-11	Gas turbine engines
GB2180005B (en)	1989-03-01	Fuel systems for gas turbine engines
EP0259758A3 (en)	1989-02-01	Combustor for gas turbine
GB2238864B (en)	1992-04-22	Gas turbine engine combustors
GB2176274B (en)	1989-02-01	Combustor for gas turbine engine
GB8620199D0 (en)	1986-10-01	Gas turbine engine
GB8619653D0 (en)	1987-01-14	Gas turbine engine