JPS5582231A - Gas turbine engine combustor - Google Patents

Gas turbine engine combustor

Info

Publication number
JPS5582231A
JPS5582231A JP13998779A JP13998779A JPS5582231A JP S5582231 A JPS5582231 A JP S5582231A JP 13998779 A JP13998779 A JP 13998779A JP 13998779 A JP13998779 A JP 13998779A JP S5582231 A JPS5582231 A JP S5582231A
Authority
JP
Japan
Prior art keywords
gas turbine
turbine engine
engine combustor
combustor
gas
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.)
Pending
Application number
JP13998779A
Other languages
English (en)
Japanese (ja)
Inventor
Shiyaaman Hofuman Jiyakobu
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 JPS5582231A publication Critical patent/JPS5582231A/ja
Pending 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
    • 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
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
    • 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)
JP13998779A 1978-11-03 1979-10-31 Gas turbine engine combustor Pending JPS5582231A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US95759178A 1978-11-03 1978-11-03

Publications (1)

Publication Number Publication Date
JPS5582231A true JPS5582231A (en) 1980-06-20

Family

ID=25499810

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13998779A Pending JPS5582231A (en) 1978-11-03 1979-10-31 Gas turbine engine combustor

Country Status (5)

Country Link
JP (1) JPS5582231A (fr)
DE (1) DE2944139A1 (fr)
FR (1) FR2440524A1 (fr)
GB (1) GB2034874A (fr)
IT (1) IT1124886B (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2161914B (en) * 1980-12-10 1986-06-11 Rolls Royce Combustion equipment for a gas turbine engine
GB2125950B (en) * 1982-08-16 1986-09-24 Gen Electric Gas turbine combustor
GB2134243A (en) * 1983-01-27 1984-08-08 Rolls Royce Combustion equipment for a gas turbine engine
US4566280A (en) * 1983-03-23 1986-01-28 Burr Donald N Gas turbine engine combustor splash ring construction
FR2604509B1 (fr) * 1986-09-25 1988-11-18 Snecma Procede de realisation d'un film de refroidissement pour chambre de combustion de turbomachine, film ainsi realise et chambre de combustion le comportant
US4916906A (en) * 1988-03-25 1990-04-17 General Electric Company Breach-cooled structure
IT1255613B (it) * 1992-09-24 1995-11-09 Eniricerche Spa Sistema di combustione a basse emissioni inquinanti per turbine a gas
DE19547703C2 (de) * 1995-12-20 1999-02-18 Mtu Muenchen Gmbh Brennkammer, insbesondere Ringbrennkammer, für Gasturbinentriebwerke
DE10048864A1 (de) 2000-10-02 2002-04-11 Rolls Royce Deutschland Brennkammerkopf für eine Gasturbine
JP2002317650A (ja) * 2001-04-24 2002-10-31 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器
FR2901349B1 (fr) * 2006-05-19 2008-09-05 Snecma Sa Chambre de combustion d'une turbomachine
EP2261565A1 (fr) * 2009-06-09 2010-12-15 Siemens Aktiengesellschaft Chambre de combustion de turbine à gaz et turbine à gaz
RU2451881C2 (ru) * 2009-10-06 2012-05-27 Открытое акционерное общество "Всероссийский дважды ордена Трудового Красного Знамени теплотехнический научно-исследовательский институт" Камера сгорания предварительного смешения газотурбинной установки

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2482E (fr) * 1902-04-30 1904-04-27 Gaston Charles Emile De Bonnec Système de turbo-moteur à combustion continue
CH255541A (de) * 1947-05-12 1948-06-30 Bbc Brown Boveri & Cie Gekühlte metallische Brennkammer zur Erzeugung von Heiz- und Treibgasen.
US2729062A (en) * 1951-07-06 1956-01-03 Dresser Operations Inc Power plant combustion chamber
US2974485A (en) * 1958-06-02 1961-03-14 Gen Electric Combustor for fluid fuels
GB845971A (en) * 1958-07-21 1960-08-24 Gen Electric Improvements relating to combustion chambers for gas turbine engines
US3338051A (en) * 1965-05-28 1967-08-29 United Aircraft Corp High velocity ram induction burner
US3369363A (en) * 1966-01-19 1968-02-20 Gen Electric Integral spacing rings for annular combustion chambers
FR2055720A1 (fr) * 1969-08-01 1971-04-30 Snecma
CA980584A (en) * 1972-11-10 1975-12-30 Edward E. Ekstedt Double walled impingement cooled combustor
US3986347A (en) * 1973-12-06 1976-10-19 Phillips Petroleum Company Combustor process for low-level NOx and CO emissions
GB1498269A (en) * 1975-05-23 1978-01-18 Snecma Gas turbine combustion chambers
DE2636520A1 (de) * 1976-08-13 1978-02-16 Daimler Benz Ag Brennkammer, insbesondere fuer gasturbinen

Also Published As

Publication number Publication date
IT1124886B (it) 1986-05-14
FR2440524A1 (fr) 1980-05-30
GB2034874A (en) 1980-06-11
IT7926982A0 (it) 1979-10-31
DE2944139A1 (de) 1980-05-14

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