CA963672A - Gas turbine recirculating combustor - Google Patents

Gas turbine recirculating combustor

Info

Publication number: CA963672A
Authority: CA; Canada
Prior art keywords: gas turbine; recirculating; combustor; recirculating combustor; turbine
Prior art date: 1972-01-25
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

CA155,632A

Inventor

Richard J. Stettler

Albert J. Verdouw

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.)

Motors Liquidation Co

Original Assignee

Motors Liquidation 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.)

1972-01-25

Filing date

1972-11-06

Publication date

1975-03-04

1972-11-06 Application filed by Motors Liquidation Co filed Critical Motors Liquidation Co

1975-03-04 Application granted granted Critical

1975-03-04 Publication of CA963672A publication Critical patent/CA963672A/en

Status Expired 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C9/00—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber
- F23C9/006—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber the recirculation taking place in the combustion chamber
- 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
- F23R3/005—Combined with pressure or heat exchangers
- 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
- F23R3/16—Continuous 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
- 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
- F23R3/26—Controlling the air flow
- 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
- F05B2250/00—Geometry
- F05B2250/40—Movement of component
- F05B2250/41—Movement of component with one degree of freedom
- F05B2250/411—Movement of component with one degree of freedom in rotation
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2202/00—Fluegas recirculation
- F23C2202/30—Premixing fluegas with combustion air
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2202/00—Fluegas recirculation
- F23C2202/50—Control of recirculation rate

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Combustion Of Fluid Fuel (AREA)
Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

CA155,632A 1972-01-25 1972-11-06 Gas turbine recirculating combustor Expired CA963672A (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US22060772A	1972-01-25	1972-01-25

Publications (1)

Publication Number	Publication Date
CA963672A true CA963672A (en)	1975-03-04

Family

ID=22824206

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
CA155,632A Expired CA963672A (en)	1972-01-25	1972-11-06	Gas turbine recirculating combustor

Country Status (8)

Country	Link
US (1)	US3744242A (en)
JP (1)	JPS4883212A (en)
AU (1)	AU446216B2 (en)
CA (1)	CA963672A (en)
DE (1)	DE2301572A1 (en)
FR (1)	FR2169053B1 (en)
GB (1)	GB1352823A (en)
IT (1)	IT976740B (en)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3814575A (en) *	1973-04-25	1974-06-04	Us Air Force	Combustion device
US3826083A (en) *	1973-07-16	1974-07-30	Gen Motors Corp	Recirculating combustion apparatus jet pump
US3880570A (en) *	1973-09-04	1975-04-29	Babcock & Wilcox Co	Method and apparatus for reducing nitric in combustion furnaces
DE2511172A1 (en) *	1975-03-14	1976-09-30	Daimler Benz Ag	FILM EVAPORATION COMBUSTION CHAMBER
US4255927A (en) *	1978-06-29	1981-03-17	General Electric Company	Combustion control system
US4385490A (en) *	1978-08-14	1983-05-31	Phillips Petroleum Company	Combustors and methods of operating same
US4318355A (en) *	1979-09-12	1982-03-09	Nelson Wilbert K	Burner structure for particulate fuels
US4345426A (en) *	1980-03-27	1982-08-24	Egnell Rolf A	Device for burning fuel with air
US4498287A (en) *	1980-12-23	1985-02-12	Phillips Petroleum Company	Combustors and methods of operating same
US4944149A (en) *	1988-12-14	1990-07-31	General Electric Company	Combustor liner with air staging for NOx control
US5094082A (en) *	1989-12-22	1992-03-10	Sundstrand Corporation	Stored energy combustor
FR2723177B1 (en) *	1994-07-27	1996-09-06	Snecma	COMBUSTION CHAMBER COMPRISING A DOUBLE WALL
DE59810347D1 (en)	1998-09-10	2004-01-15	Alstom Switzerland Ltd	Vibration damping in combustion chambers
US6609362B2 (en)	2001-07-13	2003-08-26	Pratt & Whitney Canada Corp.	Apparatus for adjusting combustor cycle
SE523082C2 (en) *	2001-11-20	2004-03-23	Volvo Aero Corp	Device at a combustion chamber of a gas turbine for controlling gas inflow to the combustion zone of the combustion chamber
US6848631B2 (en)	2002-01-23	2005-02-01	Robert James Monson	Flat fan device
US8266911B2 (en) *	2005-11-14	2012-09-18	General Electric Company	Premixing device for low emission combustion process
DE102006041955A1 (en) *	2006-08-30	2008-03-20	Deutsches Zentrum für Luft- und Raumfahrt e.V.	Method for controlling combustion in a combustion chamber and combustion chamber device
US8171732B2 (en) *	2006-09-08	2012-05-08	General Electric Company	Turbocharger for a vehicle with a coanda device
US7685804B2 (en) *	2006-09-08	2010-03-30	General Electric Company	Device for enhancing efficiency of an energy extraction system
US9347375B2 (en) *	2012-06-22	2016-05-24	General Electronic Company	Hot EGR driven by turbomachinery
US9869279B2 (en)	2012-11-02	2018-01-16	General Electric Company	System and method for a multi-wall turbine combustor
US10774685B2 (en) *	2018-04-30	2020-09-15	Ratheon Technologies Corporation	Gas turbine engine exhaust component
US11079111B2 (en) *	2019-04-29	2021-08-03	Solar Turbines Incorporated	Air tube

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3273621A (en) *		1966-09-20		Burner assembly
US2716863A (en) *	1950-07-04	1955-09-06	Onera (Off Nat Aerospatiale)	Continuous flow and internal combustion engines, and in particular turbojets or turbo-props
US2869629A (en) *	1955-12-08	1959-01-20	Gen Electric	Burner assembly
US3306333A (en) *	1964-03-31	1967-02-28	Bendix Corp	Air spray combustor
US3319692A (en) *	1965-06-01	1967-05-16	Iit Res Inst	Oil burner
US3656298A (en) *	1970-11-27	1972-04-18	Gen Motors Corp	Combustion apparatus

1972
- 1972-01-25 US US00220607A patent/US3744242A/en not_active Expired - Lifetime
- 1972-11-06 CA CA155,632A patent/CA963672A/en not_active Expired
- 1972-12-22 AU AU50447/72A patent/AU446216B2/en not_active Expired
1973
- 1973-01-03 IT IT47510/73A patent/IT976740B/en active
- 1973-01-09 FR FR7300565A patent/FR2169053B1/fr not_active Expired
- 1973-01-10 DE DE2301572A patent/DE2301572A1/en active Pending
- 1973-01-11 GB GB147273A patent/GB1352823A/en not_active Expired
- 1973-01-25 JP JP48009970A patent/JPS4883212A/ja active Pending

Also Published As

Publication number	Publication date
GB1352823A (en)	1974-05-15
DE2301572A1 (en)	1973-08-02
JPS4883212A (en)	1973-11-06
FR2169053A1 (en)	1973-09-07
FR2169053B1 (en)	1977-08-05
AU446216B2 (en)	1974-03-14
IT976740B (en)	1974-09-10
US3744242A (en)	1973-07-10
AU5044772A (en)	1974-03-14

Publication	Publication Date	Title
CA963672A (en)	1975-03-04	Gas turbine recirculating combustor
CA986730A (en)	1976-04-06	Modular gas turbine engine
CA965352A (en)	1975-04-01	Gas turbine nozzle vane structure
CA998535A (en)	1976-10-19	Gas turbine engine
CA982829A (en)	1976-02-03	Combustor for a gas turbine engine
AU447212B2 (en)	1974-04-11	Gas turbine engines
CA963673A (en)	1975-03-04	Gas turbine lubrication
CA940051A (en)	1974-01-15	Gas turbine
CA1021315A (en)	1977-11-22	Gas turbine lubricants
CA963674A (en)	1975-03-04	Gas turbine combustion liner
CA1004985A (en)	1977-02-08	Steam turbines
CA974885A (en)	1975-09-23	Axial-flow turbine
CA975183A (en)	1975-09-30	Pollution-free gas turbine system
CA961279A (en)	1975-01-21	Gas turbine control
CA977166A (en)	1975-11-04	Gas turbine engine regenerator
CA971373A (en)	1975-07-22	Gas turbine combustors
CA896905A (en)	1972-04-04	Gas turbine engine
CA999748A (en)	1976-11-16	Gas turbine engine
CA911745A (en)	1972-10-10	Gas turbine engine
CA1022349A (en)	1977-12-13	Gas turbine engine
CA896906A (en)	1972-04-04	Gas turbine engine
CA905690A (en)	1972-07-25	Gas turbine support arrangement
CA834433A (en)	1970-02-17	Gas turbine engines
CA866579A (en)	1971-03-23	Gas turbine
CA851427A (en)	1970-09-15	Gas turbine plants