GB2030653B - Gas turbine engine combustion gas temperature variation - Google Patents

Gas turbine engine combustion gas temperature variation

Info

Publication number: GB2030653B
Authority: GB; United Kingdom
Prior art keywords: turbine engine; temperature variation; engine combustion; gas turbine; combustion gas
Prior art date: 1978-10-02
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

GB7925598A

Other versions

GB2030653A (en

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.)

1978-10-02

Filing date

1979-07-23

Publication date

1983-05-05

1979-07-23 Application filed by General Electric Co filed Critical General Electric Co

1980-04-10 Publication of GB2030653A publication Critical patent/GB2030653A/en

1983-05-05 Application granted granted Critical

1983-05-05 Publication of GB2030653B publication Critical patent/GB2030653B/en

Status Expired 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/06—Arrangement of apertures along the flame tube
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
- 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)
Turbine Rotor Nozzle Sealing (AREA)

GB7925598A 1978-10-02 1979-07-23 Gas turbine engine combustion gas temperature variation Expired GB2030653B (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US94791978A	1978-10-02	1978-10-02

Publications (2)

Publication Number	Publication Date
GB2030653A GB2030653A (en)	1980-04-10
GB2030653B true GB2030653B (en)	1983-05-05

Family

ID=25486990

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
GB7925598A Expired GB2030653B (en)	1978-10-02	1979-07-23	Gas turbine engine combustion gas temperature variation

Country Status (6)

Country	Link
JP (1)	JPS5560625A (en)
CA (1)	CA1148755A (en)
DE (1)	DE2939563A1 (en)
FR (1)	FR2438166B1 (en)
GB (1)	GB2030653B (en)
IT (1)	IT1165348B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2727193B1 (en) *	1994-11-23	1996-12-20	Snecma	TWO-HEAD COMBUSTION CHAMBER OPERATING AT FULL GAS SLOW MOTION
US7234304B2 (en)	2002-10-23	2007-06-26	Pratt & Whitney Canada Corp	Aerodynamic trip to improve acoustic transmission loss and reduce noise level for gas turbine engine
FR2948987B1 (en) *	2009-08-04	2011-12-09	Snecma	TURBOMACHINE COMBUSTION CHAMBER HAVING IMPROVED AIR INLET ORIFICES
US20220225736A1 (en) *	2019-06-13	2022-07-21	Asics Corporation	Shoe

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3126705A (en) *	1956-03-26	1964-03-31		Combustion system
NL108658C (en) *	1958-07-31
DE1199541B (en) *	1961-12-04	1965-08-26	Jan Jerie Dr Ing	Propellant gas collector for the stator of gas turbines
US3608310A (en) *	1966-06-27	1971-09-28	Gen Motors Corp	Turbine stator-combustor structure

1979
- 1979-07-23 GB GB7925598A patent/GB2030653B/en not_active Expired
- 1979-09-14 JP JP11742379A patent/JPS5560625A/en active Granted
- 1979-09-21 CA CA000336140A patent/CA1148755A/en not_active Expired
- 1979-09-28 IT IT26087/79A patent/IT1165348B/en active
- 1979-09-29 DE DE19792939563 patent/DE2939563A1/en not_active Withdrawn
- 1979-10-01 FR FR7924380A patent/FR2438166B1/en not_active Expired

Also Published As

Publication number	Publication date
IT1165348B (en)	1987-04-22
GB2030653A (en)	1980-04-10
FR2438166A1 (en)	1980-04-30
DE2939563A1 (en)	1980-04-17
CA1148755A (en)	1983-06-28
IT7926087A0 (en)	1979-09-28
JPS6236142B2 (en)	1987-08-05
FR2438166B1 (en)	1986-07-11
JPS5560625A (en)	1980-05-07

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Legal Events

Date	Code	Title	Description
1992-03-18	PCNP	Patent ceased through non-payment of renewal fee