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
English (en)
Japanese (ja)
Other versions
JPS6236142B2 (de
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/ja
Publication of JPS6236142B2 publication Critical patent/JPS6236142B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/06Arrangement of apertures along the flame tube
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/12Cooling of plants
    • F02C7/16Cooling of plants characterised by cooling medium
    • F02C7/18Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
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 (de) 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 (de)
CA (1) CA1148755A (de)
DE (1) DE2939563A1 (de)
FR (1) FR2438166B1 (de)
GB (1) GB2030653B (de)
IT (1) IT1165348B (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2727193B1 (fr) * 1994-11-23 1996-12-20 Snecma Chambre de combustion a deux tetes fonctionnant du ralenti au plein gaz
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 (fr) * 2009-08-04 2011-12-09 Snecma Chambre de combustion de turbomachine comportant des orifices d'entree d'air ameliores
WO2020250389A1 (ja) * 2019-06-13 2020-12-17 株式会社アシックス

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

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