JPS5560625A - Gas turbine engine - Google Patents

Gas turbine engine

Info

Publication number
JPS5560625A
JPS5560625A JP11742379A JP11742379A JPS5560625A JP S5560625 A JPS5560625 A JP S5560625A JP 11742379 A JP11742379 A JP 11742379A JP 11742379 A JP11742379 A JP 11742379A JP S5560625 A JPS5560625 A JP S5560625A
Authority
JP
Japan
Prior art keywords
gas turbine
turbine engine
engine
gas
turbine
Prior art date
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.)
Granted
Application number
JP11742379A
Other languages
Japanese (ja)
Other versions
JPS6236142B2 (en
Inventor
Ueinsutein Baarii
Uiriamu Budobiaku Jiyon
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.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of JPS5560625A publication Critical patent/JPS5560625A/en
Publication of JPS6236142B2 publication Critical patent/JPS6236142B2/ja
Granted 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
    • 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
JP11742379A 1978-10-02 1979-09-14 Gas turbine engine Granted JPS5560625A (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
JPS5560625A true JPS5560625A (en) 1980-05-07
JPS6236142B2 JPS6236142B2 (en) 1987-08-05

Family

ID=25486990

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11742379A Granted JPS5560625A (en) 1978-10-02 1979-09-14 Gas turbine engine

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
WO2020250389A1 (en) * 2019-06-13 2020-12-17 株式会社アシックス Shoe

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB980363A (en) * 1961-12-04 1965-01-13 Jan Jerie Improvements in or relating to gas turbines

Family Cites Families (3)

* 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
US3608310A (en) * 1966-06-27 1971-09-28 Gen Motors Corp Turbine stator-combustor structure

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB980363A (en) * 1961-12-04 1965-01-13 Jan Jerie Improvements in or relating to gas turbines

Also Published As

Publication number Publication date
FR2438166B1 (en) 1986-07-11
IT7926087A0 (en) 1979-09-28
JPS6236142B2 (en) 1987-08-05
IT1165348B (en) 1987-04-22
GB2030653A (en) 1980-04-10
CA1148755A (en) 1983-06-28
DE2939563A1 (en) 1980-04-17
FR2438166A1 (en) 1980-04-30
GB2030653B (en) 1983-05-05

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