FR2219311A1 - - Google Patents

Info

Publication number: FR2219311A1
Authority: FR; France
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 Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.): Withdrawn

Application number

FR7406495A

Other languages

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.)

General Electric Co

Original Assignee

General Electric Co

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.)

1973-02-26

Filing date

1974-02-26

Publication date

1974-09-20

1974-02-26 Application filed by General Electric Co filed Critical General Electric Co

1974-09-20 Publication of FR2219311A1 publication Critical patent/FR2219311A1/fr

Status Withdrawn legal-status Critical Current

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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements

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)
Combustion Of Fluid Fuel (AREA)

FR7406495A 1973-02-26 1974-02-26 Withdrawn FR2219311A1 (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US00335684A US3854285A (en)	1973-02-26	1973-02-26	Combustor dome assembly

Publications (1)

Publication Number	Publication Date
FR2219311A1 true FR2219311A1 (en)	1974-09-20

Family

ID=23312822

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
FR7406495A Withdrawn FR2219311A1 (en)	1973-02-26	1974-02-26

Country Status (7)

Country	Link
US (1)	US3854285A (en)
JP (1)	JPS5024617A (en)
BE (1)	BE811568A (en)
CA (1)	CA1005242A (en)
DE (1)	DE2408818A1 (en)
FR (1)	FR2219311A1 (en)
GB (1)	GB1459591A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2334824A1 (en) *	1975-12-11	1977-07-08	Gen Electric	PERFECTED COMBUSTION CHAMBER
FR2431096A1 (en) *	1978-08-14	1980-02-08	Gen Electric	COMBUSTION CHAMBER DOME OF A GAS TURBINE ENGINE
FR2671856A1 (en) *	1991-01-22	1992-07-24	Gen Electric	COMBUSTION SET DOME.
EP1717516A1 (en) *	2005-04-28	2006-11-02	Snecma	Easily disassembled combustion chamber with improved aerodynamic performance
EP1903283B1 (en) *	2006-09-22	2016-03-16	Snecma	Annular combustion chamber of a turbomachine

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB1438379A (en) *	1973-08-16	1976-06-03	Rolls Royce	Cooling arrangement for duct walls
US3903754A (en) *	1974-06-07	1975-09-09	Pino International Ltd	Bicycle crank hub assembly
JPS5363208U (en) *	1976-10-30	1978-05-29
JPS5556521A (en) *	1978-10-23	1980-04-25	Hitachi Ltd	Combustion device
JPS58106541U (en) *	1982-01-13	1983-07-20	アイシン精機株式会社	Combustor for Stirling engine
US4532762A (en) *	1982-07-22	1985-08-06	The Garrett Corporation	Gas turbine engine variable geometry combustor apparatus
US5012645A (en) *	1987-08-03	1991-05-07	United Technologies Corporation	Combustor liner construction for gas turbine engine
US5181377A (en) *	1991-04-16	1993-01-26	General Electric Company	Damped combustor cowl structure
CA2070518C (en) *	1991-07-01	2001-10-02	Adrian Mark Ablett	Combustor dome assembly
JP2597800B2 (en) *	1992-06-12	1997-04-09	ゼネラル・エレクトリック・カンパニイ	Gas turbine engine combustor
US5329772A (en) *	1992-12-09	1994-07-19	General Electric Company	Cast slot-cooled single nozzle combustion liner cap
US5265409A (en) *	1992-12-18	1993-11-30	United Technologies Corporation	Uniform cooling film replenishment thermal liner assembly
DE4244303A1 (en) *	1992-12-28	1994-06-30	Abb Research Ltd	Impact cooling system for cooling surface e.g. of combustion chamber wall
JP3415663B2 (en) *	1992-12-28	2003-06-09	アルストム	Equipment for cooling the cooling surface in an impact manner
DE4244302C2 (en) *	1992-12-28	2002-08-29	Alstom	Impact cooling device
US5924288A (en) *	1994-12-22	1999-07-20	General Electric Company	One-piece combustor cowl
JP3924136B2 (en) *	2001-06-27	2007-06-06	三菱重工業株式会社	Gas turbine combustor
US7013647B2 (en) *	2001-12-21	2006-03-21	Mitsubishi Heavy Industries, Ltd.	Outer casing covering gas turbine combustor
US6672067B2 (en) *	2002-02-27	2004-01-06	General Electric Company	Corrugated cowl for combustor of a gas turbine engine and method for configuring same
US6725667B2 (en)	2002-08-22	2004-04-27	General Electric Company	Combustor dome for gas turbine engine
US6711900B1 (en) *	2003-02-04	2004-03-30	Pratt & Whitney Canada Corp.	Combustor liner V-band design
US7051532B2 (en) *	2003-10-17	2006-05-30	General Electric Company	Methods and apparatus for film cooling gas turbine engine combustors
US7219498B2 (en) *	2004-09-10	2007-05-22	Honeywell International, Inc.	Waffled impingement effusion method
FR2897144B1 (en) *	2006-02-08	2008-05-02	Snecma Sa	COMBUSTION CHAMBER FOR TURBOMACHINE WITH TANGENTIAL SLOTS
FR2897145B1 (en) *	2006-02-08	2013-01-18	Snecma	ANNULAR COMBUSTION CHAMBER FOR TURBOMACHINE WITH ALTERNATE FIXINGS.
FR2905166B1 (en) *	2006-08-28	2008-11-14	Snecma Sa	ANNULAR COMBUSTION CHAMBER OF A TURBOMACHINE.
US7856826B2 (en) *	2006-11-10	2010-12-28	General Electric Company	Combustor dome mixer retaining means
US7765809B2 (en) *	2006-11-10	2010-08-03	General Electric Company	Combustor dome and methods of assembling such
FR2914399B1 (en) *	2007-03-27	2009-10-02	Snecma Sa	FURNITURE FOR BOTTOM OF COMBUSTION CHAMBER.
DE102007050664A1 (en) *	2007-10-24	2009-04-30	Man Turbo Ag	Burner for a turbomachine, baffle for such a burner and a turbomachine with such a burner
US20100050640A1 (en) *	2008-08-29	2010-03-04	General Electric Company	Thermally compliant combustion cap device and system
JP4815513B2 (en) *	2009-07-06	2011-11-16	川崎重工業株式会社	Gas turbine combustor
US8899051B2 (en) *	2010-12-30	2014-12-02	Rolls-Royce Corporation	Gas turbine engine flange assembly including flow circuit
DE102013204307A1 (en) *	2013-03-13	2014-09-18	Siemens Aktiengesellschaft	Jet burner with cooling channel in the base plate
DE102015213629A1 (en) *	2015-07-20	2017-01-26	Rolls-Royce Deutschland Ltd & Co Kg	Cover member and combustion chamber assembly for a gas turbine
US10619856B2 (en) *	2017-03-13	2020-04-14	Rolls-Royce Corporation	Notched gas turbine combustor cowl
US10982852B2 (en)	2018-11-05	2021-04-20	Rolls-Royce Corporation	Cowl integration to combustor wall
US11859819B2 (en)	2021-10-15	2024-01-02	General Electric Company	Ceramic composite combustor dome and liners

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US2549858A (en) *	1946-07-30	1951-04-24	Westinghouse Electric Corp	Annular combustion chamber having telescoping walls with corrugated ends for spacing
US2537033A (en) *	1947-07-18	1951-01-09	Westinghouse Electric Corp	Gas turbine combustion chamber construction
GB697027A (en) *	1950-11-27	1953-09-16	Lucas Ltd Joseph	Combustion chambers for prime movers
GB710353A (en) *	1951-06-18	1954-06-09	Rolls Royce	Improvements in or relating to combustion equipment for gas-turbine engines
GB736028A (en) *	1952-11-29	1955-08-31	Lucas Industries Ltd	Combustion chambers for prime movers
US3038309A (en) *	1959-07-21	1962-06-12	Gen Electric	Cooling liner for jet engine afterburner
US3064425A (en) *	1959-10-05	1962-11-20	Gen Motors Corp	Combustion liner
US3307354A (en) *	1965-10-01	1967-03-07	Gen Electric	Cooling structure for overlapped panels
GB1127637A (en) *	1966-08-18	1968-09-18	Lucas Industries Ltd	Supports for fuel burners
US3385055A (en) *	1966-11-23	1968-05-28	United Aircraft Corp	Combustion chamber with floating swirler rings
US3408812A (en) *	1967-02-24	1968-11-05	Gen Electric	Cooled joint construction for combustion wall means

1973
- 1973-02-26 US US00335684A patent/US3854285A/en not_active Expired - Lifetime
1974
- 1974-02-05 CA CA191,797A patent/CA1005242A/en not_active Expired
- 1974-02-14 GB GB669974A patent/GB1459591A/en not_active Expired
- 1974-02-23 DE DE19742408818 patent/DE2408818A1/en active Pending
- 1974-02-26 FR FR7406495A patent/FR2219311A1/fr not_active Withdrawn
- 1974-02-26 BE BE141381A patent/BE811568A/en unknown
- 1974-02-26 JP JP49022010A patent/JPS5024617A/ja active Pending

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2334824A1 (en) *	1975-12-11	1977-07-08	Gen Electric	PERFECTED COMBUSTION CHAMBER
FR2431096A1 (en) *	1978-08-14	1980-02-08	Gen Electric	COMBUSTION CHAMBER DOME OF A GAS TURBINE ENGINE
FR2671856A1 (en) *	1991-01-22	1992-07-24	Gen Electric	COMBUSTION SET DOME.
EP1717516A1 (en) *	2005-04-28	2006-11-02	Snecma	Easily disassembled combustion chamber with improved aerodynamic performance
FR2885201A1 (en) *	2005-04-28	2006-11-03	Snecma Moteurs Sa	EASILY DISMANTLING COMBUSTION CHAMBER WITH IMPROVED AERODYNAMIC PERFORMANCE
US7637111B2 (en)	2005-04-28	2009-12-29	Snecma	Easily demountable combustion chamber with improved aerodynamic performance
EP1903283B1 (en) *	2006-09-22	2016-03-16	Snecma	Annular combustion chamber of a turbomachine

Also Published As

Publication number	Publication date
BE811568A (en)	1974-06-17
US3854285A (en)	1974-12-17
JPS5024617A (en)	1975-03-15
GB1459591A (en)	1976-12-22
DE2408818A1 (en)	1974-09-05
CA1005242A (en)	1977-02-15

Publication	Publication Date	Title
AR201758A1 (en)	1975-04-15
AU476761B2 (en)	1976-09-30
AU465372B2 (en)	1975-09-25
AR201235Q (en)	1975-02-21
AR201231Q (en)	1975-02-21
AU474593B2 (en)	1976-07-29
AU474511B2 (en)	1976-07-22
AU474838B2 (en)	1976-08-05
AU465453B2 (en)	1975-09-25
AU471343B2 (en)	1976-04-15
AU465434B2 (en)	1975-09-25
AU450229B2 (en)	1974-07-04
AU476714B2 (en)	1976-09-30
AR201229Q (en)	1975-02-21
AU476696B2 (en)	1976-09-30
AU466283B2 (en)	1975-10-23
AU472848B2 (en)	1976-06-03
AR199451A1 (en)	1974-08-30
AU477823B2 (en)	1975-06-19
AU471461B2 (en)	1976-04-29
AR195948A1 (en)	1973-11-15
AU447540B2 (en)	1974-03-25
AU477824B2 (en)	1975-07-17
AU461342B2 (en)	1975-05-22
AR210729A1 (en)	1977-09-15

Legal Events

Date	Code	Title	Description
1979-04-20	ST	Notification of lapse