IL62557A - Combustor liner construction for gas turbine engines - Google Patents

Combustor liner construction for gas turbine engines

Info

Publication number: IL62557A
Authority: IL; Israel
Prior art keywords: gas turbine; turbine engines; combustor liner; liner construction; construction
Prior art date: 1980-04-02

Application number

IL62557A

Other languages

English (en)

Other versions

IL62557A0 (en

Original Assignee

United Technologies Corp

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.)

1980-04-02

Filing date

1981-04-02

Publication date

1984-01-31

1981-04-02 Application filed by United Technologies Corp filed Critical United Technologies Corp

1981-06-29 Publication of IL62557A0 publication Critical patent/IL62557A0/xx

1984-01-31 Publication of IL62557A publication Critical patent/IL62557A/xx

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
- F05B2260/221—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
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Gas Burners (AREA)
Spray-Type Burners (AREA)
Laminated Bodies (AREA)
Turbine Rotor Nozzle Sealing (AREA)

IL62557A 1980-04-02 1981-04-02 Combustor liner construction for gas turbine engines IL62557A (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US06/136,848 US4361010A (en)	1980-04-02	1980-04-02	Combustor liner construction

Publications (2)

Publication Number	Publication Date
IL62557A0 IL62557A0 (en)	1981-06-29
IL62557A true IL62557A (en)	1984-01-31

Family

ID=22474647

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
IL62557A IL62557A (en)	1980-04-02	1981-04-02	Combustor liner construction for gas turbine engines

Country Status (8)

Country	Link
US (1)	US4361010A (xx)
JP (1)	JPS56168041A (xx)
CA (1)	CA1156843A (xx)
DE (1)	DE3113380A1 (xx)
FR (1)	FR2479951A1 (xx)
GB (1)	GB2074715B (xx)
IL (1)	IL62557A (xx)
SE (1)	SE457372B (xx)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US4622821A (en) *	1985-01-07	1986-11-18	United Technologies Corporation	Combustion liner for a gas turbine engine
US4790140A (en) *	1985-01-18	1988-12-13	Ishikawajima-Harima Jukogyo Kabushiki Kaisha	Liner cooling construction for gas turbine combustor or the like
US4642993A (en) *	1985-04-29	1987-02-17	Avco Corporation	Combustor liner wall
EP0224817B1 (de) *	1985-12-02	1989-07-12	Siemens Aktiengesellschaft	Hitzeschildanordnung, insbesondere für Strukturteile von Gasturbinenanlagen
US4800718A (en) *	1986-12-24	1989-01-31	The United States Of America As Represented By The Secretary Of The Air Force	Surface cooling system
US4928479A (en) *	1987-12-28	1990-05-29	Sundstrand Corporation	Annular combustor with tangential cooling air injection
DE3942271A1 (de) *	1989-12-21	1991-07-04	Mtu Maintenance Gmbh	Verfahren zur reparatur eines flammrohres
DE4242721A1 (de) *	1992-12-17	1994-06-23	Asea Brown Boveri	Gasturbinenbrennkammer
US5363654A (en) *	1993-05-10	1994-11-15	General Electric Company	Recuperative impingement cooling of jet engine components
GB2355301A (en) *	1999-10-13	2001-04-18	Rolls Royce Plc	A wall structure for a combustor of a gas turbine engine
US6345441B1 (en) *	2000-07-18	2002-02-12	General Electric Company	Method of repairing combustion chamber liners
US20020066273A1 (en) *	2000-12-04	2002-06-06	Mitsubishi Heavy Industries, Ltd.	Plate fin and combustor using the plate fin
US6568079B2 (en) *	2001-06-11	2003-05-27	General Electric Company	Methods for replacing combustor liner panels
US6581285B2 (en) *	2001-06-11	2003-06-24	General Electric Co.	Methods for replacing nuggeted combustor liner panels
US6530225B1 (en)	2001-09-21	2003-03-11	Honeywell International, Inc.	Waffle cooling
DE102004001393A1 (de) *	2004-01-09	2005-08-04	Mtu Aero Engines Gmbh	Vorrichtung zur Aufhängung von Gaskanalelementen
US7278256B2 (en) *	2004-11-08	2007-10-09	United Technologies Corporation	Pulsed combustion engine
DE102005059502A1 (de) *	2005-12-06	2007-06-14	Deutsches Zentrum für Luft- und Raumfahrt e.V.	Heißkammer
EP2116770B1 (en) *	2008-05-07	2013-12-04	Siemens Aktiengesellschaft	Combustor dynamic attenuation and cooling arrangement
JP5484707B2 (ja) *	2008-10-10	2014-05-07	三菱重工業株式会社	燃焼器およびガスタービン
US8549861B2 (en) *	2009-01-07	2013-10-08	General Electric Company	Method and apparatus to enhance transition duct cooling in a gas turbine engine
US7712314B1 (en) *	2009-01-21	2010-05-11	Gas Turbine Efficiency Sweden Ab	Venturi cooling system
JP5260402B2 (ja) *	2009-04-30	2013-08-14	三菱重工業株式会社	板状体の製造方法、板状体、ガスタービン燃焼器およびガスタービン
RU2530685C2 (ru) *	2010-03-25	2014-10-10	Дженерал Электрик Компани	Структуры ударного воздействия для систем охлаждения
US8894363B2 (en)	2011-02-09	2014-11-25	Siemens Energy, Inc.	Cooling module design and method for cooling components of a gas turbine system
US8959886B2 (en)	2010-07-08	2015-02-24	Siemens Energy, Inc.	Mesh cooled conduit for conveying combustion gases
US20120227408A1 (en) *	2011-03-10	2012-09-13	Delavan Inc.	Systems and methods of pressure drop control in fluid circuits through swirling flow mitigation
KR20150047565A (ko) *	2012-08-24	2015-05-04	알스톰 테크놀러지 리미티드	희석 가스 혼합기를 갖는 연속 연소
EP3099976B1 (en) *	2014-01-30	2019-03-13	United Technologies Corporation	Cooling flow for leading panel in a gas turbine engine combustor
US10309652B2 (en) *	2014-04-14	2019-06-04	Siemens Energy, Inc.	Gas turbine engine combustor basket with inverted platefins
JP6470135B2 (ja)	2014-07-14	2019-02-13	ユナイテッドテクノロジーズコーポレイションＵｎｉｔｅｄＴｅｃｈｎｏｌｏｇｉｅｓＣｏｒｐｏｒａｔｉｏｎ	付加製造された表面仕上げ
US10480787B2 (en) *	2015-03-26	2019-11-19	United Technologies Corporation	Combustor wall cooling channel formed by additive manufacturing
US10094564B2 (en)	2015-04-17	2018-10-09	Pratt & Whitney Canada Corp.	Combustor dilution hole cooling system
GB202213352D0 (en) *	2022-09-13	2022-10-26	Rolls Royce Plc	A combustor assembly

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
CH255541A (de) *	1947-05-12	1948-06-30	Bbc Brown Boveri & Cie	Gekühlte metallische Brennkammer zur Erzeugung von Heiz- und Treibgasen.
BE535497A (xx) *	1954-02-26
US3064424A (en) *	1959-09-30	1962-11-20	Gen Motors Corp	Flame tube
US3333414A (en) *	1965-10-13	1967-08-01	United Aircraft Canada	Aerodynamic-flow reverser and smoother
US3572031A (en) *	1969-07-11	1971-03-23	United Aircraft Corp	Variable area cooling passages for gas turbine burners
US3706203A (en) *	1970-10-30	1972-12-19	United Aircraft Corp	Wall structure for a gas turbine engine
GB1424197A (en) *	1972-06-09	1976-02-11	Lucas Industries Ltd	Combustion chambers for gas turbine engines
GB1438379A (en) *	1973-08-16	1976-06-03	Rolls Royce	Cooling arrangement for duct walls
GB1552132A (en) *	1975-11-29	1979-09-12	Rolls Royce	Combustion chambers for gas turbine engines
FR2340453A1 (fr) *	1976-02-06	1977-09-02	Snecma	Corps de chambre de combustion, notamment pour turboreacteurs
US4132066A (en) *	1977-09-23	1979-01-02	United Technologies Corporation	Combustor liner for gas turbine engine

1980
- 1980-04-02 US US06/136,848 patent/US4361010A/en not_active Expired - Lifetime
1981
- 1981-03-19 CA CA000373415A patent/CA1156843A/en not_active Expired
- 1981-04-01 GB GB8110149A patent/GB2074715B/en not_active Expired
- 1981-04-02 IL IL62557A patent/IL62557A/xx not_active IP Right Cessation
- 1981-04-02 JP JP5046081A patent/JPS56168041A/ja active Granted
- 1981-04-02 SE SE8102134A patent/SE457372B/sv not_active IP Right Cessation
- 1981-04-02 FR FR8106597A patent/FR2479951A1/fr active Granted
- 1981-04-02 DE DE19813113380 patent/DE3113380A1/de active Granted

Also Published As

Publication number	Publication date
FR2479951B1 (xx)	1984-02-10
SE8102134L (sv)	1981-10-03
DE3113380A1 (de)	1982-04-08
US4361010A (en)	1982-11-30
SE457372B (sv)	1988-12-19
IL62557A0 (en)	1981-06-29
JPH0229935B2 (xx)	1990-07-03
DE3113380C2 (xx)	1990-09-27
FR2479951A1 (fr)	1981-10-09
GB2074715B (en)	1983-10-05
GB2074715A (en)	1981-11-04
CA1156843A (en)	1983-11-15
JPS56168041A (en)	1981-12-24

Legal Events

Date	Code	Title	Description
1999-10-28	KB	Patent renewed
2001-07-24	EXP	Patent expired

Publication	Publication Date	Title
GB2074307B (en)	1983-10-12	Combustor liner construction for gas turbine engine
IL62558A0 (en)	1981-06-29	Combustor liner construction for gas turbine engines
IL62557A (en)	1984-01-31	Combustor liner construction for gas turbine engines
JPS56168040A (en)	1981-12-24	Circular combustor for gas turbine engine
JPS57142422A (en)	1982-09-03	Combustor for gas turbine engine
GB2004592B (en)	1982-01-27	Combustion liner for gas turbine engine
DE3663847D1 (en)	1989-07-13	Combustor for gas turbine engine
JPS5691132A (en)	1981-07-23	Combustor for gas turbine
GB2019947B (en)	1982-07-28	Gas turbine engine combustor assembly
GB2206686B (en)	1989-11-22	Gas turbine engine augmentor
DE3360573D1 (en)	1985-09-19	Combustor for gas turbine
IL62269A (en)	1983-09-30	Anti-coke nozzle for gas turbine combustor
JPS55155118A (en)	1980-12-03	Combustor for gas turbine
GB2043870B (en)	1982-12-22	Flameholder for gas turbine engines
GB2125950B (en)	1986-09-24	Gas turbine combustor
IL83766A0 (en)	1988-02-29	Augmentor liner construction for gas turbine engine
JPS5538494A (en)	1980-03-17	Combustor dome assembly for gas turbine engine
JPS5582231A (en)	1980-06-20	Gas turbine engine combustor
GB2176274B (en)	1989-02-01	Combustor for gas turbine engine
GB2094464B (en)	1984-08-30	Gas turbine combustor
GB2238516B (en)	1991-08-28	Gas turbine engine
GB2251895B (en)	1992-12-09	Gas turbine engine
IL70266A0 (en)	1984-02-29	Combustor for gas turbine engine
GB2095816B (en)	1984-12-12	Gas turbine combustor
GB2102558B (en)	1985-02-13	Combustor for combustion turbine