JPS5596837A - Burner structure and operating method thereof - Google Patents

Burner structure and operating method thereof

Info

Publication number
JPS5596837A
JPS5596837A JP17403079A JP17403079A JPS5596837A JP S5596837 A JPS5596837 A JP S5596837A JP 17403079 A JP17403079 A JP 17403079A JP 17403079 A JP17403079 A JP 17403079A JP S5596837 A JPS5596837 A JP S5596837A
Authority
JP
Japan
Prior art keywords
operating method
burner structure
burner
operating
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
JP17403079A
Other languages
Japanese (ja)
Inventor
Jiyon Sutaagesu Jiefurei
Rindozei Mooton Haamon
Rii Maashiyaru Richiyaado
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of JPS5596837A publication Critical patent/JPS5596837A/en
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

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)
JP17403079A 1979-01-15 1979-12-28 Burner structure and operating method thereof Pending JPS5596837A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US345779A 1979-01-15 1979-01-15

Publications (1)

Publication Number Publication Date
JPS5596837A true JPS5596837A (en) 1980-07-23

Family

ID=21705966

Family Applications (1)

Application Number Title Priority Date Filing Date
JP17403079A Pending JPS5596837A (en) 1979-01-15 1979-12-28 Burner structure and operating method thereof

Country Status (3)

Country Link
JP (1) JPS5596837A (en)
FR (1) FR2446442A1 (en)
GB (1) GB2039359A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2683891B1 (en) * 1991-11-20 1995-03-24 Snecma TURBOMACHINE COMPRISING A DEVICE FOR REDUCING THE EMISSION OF NITROGEN OXIDES.
US6606861B2 (en) 2001-02-26 2003-08-19 United Technologies Corporation Low emissions combustor for a gas turbine engine
US6672067B2 (en) * 2002-02-27 2004-01-06 General Electric Company Corrugated cowl for combustor of a gas turbine engine and method for configuring same
EA008046B1 (en) * 2005-02-22 2007-02-27 Александр Владимирович Клюев Method of burning fuel and burner therefor

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR962862A (en) * 1946-10-26 1950-06-22
FR1206830A (en) * 1958-05-19 1960-02-11 Rolls Royce Improvements to combustion equipment for gas turbine engines
US3653207A (en) * 1970-07-08 1972-04-04 Gen Electric High fuel injection density combustion chamber for a gas turbine engine
JPS5129726A (en) * 1974-09-06 1976-03-13 Mitsubishi Heavy Ind Ltd
FR2357738A1 (en) * 1976-07-07 1978-02-03 Snecma Combustion chamber for gas turbine engine - uses air streams ensuring stoichiometric mixture for all turbine speeds
US4122670A (en) * 1977-02-04 1978-10-31 General Motors Corporation Parallel stage fuel combustion system

Also Published As

Publication number Publication date
FR2446442A1 (en) 1980-08-08
GB2039359A (en) 1980-08-06

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