CA993667A - Combustion apparatus for gas turbine engines - Google Patents

Combustion apparatus for gas turbine engines

Info

Publication number
CA993667A
CA993667A CA196,144A CA196144A CA993667A CA 993667 A CA993667 A CA 993667A CA 196144 A CA196144 A CA 196144A CA 993667 A CA993667 A CA 993667A
Authority
CA
Canada
Prior art keywords
gas turbine
combustion apparatus
turbine engines
engines
combustion
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.)
Expired
Application number
CA196,144A
Other versions
CA196144S (en
Inventor
Arthur H. Lefebvre
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation 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 Motors Liquidation Co filed Critical Motors Liquidation Co
Application granted granted Critical
Publication of CA993667A publication Critical patent/CA993667A/en
Expired 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
    • 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
    • F23R3/045—Air inlet arrangements using pipes

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)
CA196,144A 1973-07-27 1974-03-27 Combustion apparatus for gas turbine engines Expired CA993667A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US38332873A 1973-07-27 1973-07-27

Publications (1)

Publication Number Publication Date
CA993667A true CA993667A (en) 1976-07-27

Family

ID=23512630

Family Applications (1)

Application Number Title Priority Date Filing Date
CA196,144A Expired CA993667A (en) 1973-07-27 1974-03-27 Combustion apparatus for gas turbine engines

Country Status (2)

Country Link
CA (1) CA993667A (en)
GB (1) GB1462903A (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4475344A (en) * 1982-02-16 1984-10-09 Westinghouse Electric Corp. Low smoke combustor for land based combustion turbines
GB2278431A (en) * 1993-05-24 1994-11-30 Rolls Royce Plc A gas turbine engine combustion chamber
FR2748088B1 (en) * 1996-04-24 1998-05-29 Snecma OPTIMIZATION OF THE MIXTURE OF BURNED GASES IN AN ANNULAR COMBUSTION CHAMBER
US6606861B2 (en) 2001-02-26 2003-08-19 United Technologies Corporation Low emissions combustor for a gas turbine engine
GB2391297A (en) * 2002-07-24 2004-02-04 Rolls Royce Plc Gas supply assembly
FR2958012B1 (en) * 2010-03-23 2013-12-13 Snecma TURBOMACHINE COMBUSTION CHAMBER
EP2966356B1 (en) * 2014-07-10 2020-01-08 Ansaldo Energia Switzerland AG Sequential combustor arrangement with a mixer
CN107575889B (en) * 2017-09-05 2023-05-16 中国联合重型燃气轮机技术有限公司 Fuel nozzle of gas turbine
US11572835B2 (en) * 2021-05-11 2023-02-07 General Electric Company Combustor dilution hole

Also Published As

Publication number Publication date
GB1462903A (en) 1977-01-26

Similar Documents

Publication Publication Date Title
CA1013153A (en) Combustion apparatus for a gas turbine engine
CA985514A (en) Combustion apparatus for gas turbine
CA1022350A (en) Combustion method and apparatus for gas turbine engine
CA982831A (en) Combustion apparatus for an engine with hot combustion air
CA988309A (en) Impingement-convective cooling system for a gas turbine engine
CA1020423A (en) Exhaust gas recirculation for three-valve engine
JPS5236210A (en) Fuel system for gas turbine engine
CA987918A (en) Gas turbine engine combustion equipment
GB1552132A (en) Combustion chambers for gas turbine engines
CA993668A (en) Combustion apparatus air supply for gas turbine engine
CA993667A (en) Combustion apparatus for gas turbine engines
CA985918A (en) Gas turbine engine combustion equipment
CA1002034A (en) Pressurized strongback regenerator for gas turbine engines
CA1023567A (en) Combustion chamber for a gas turbine engine
CA1005994A (en) Exhaust gas reactor for internal combustion engines
CA1031973A (en) Combustion chamber for a gas turbine engine
CA1009854A (en) Regenerator for gas turbine engine
CA1007331A (en) Device for controlling gas turbine engines
CA981920A (en) Compressor geometry control apparatus for gas turbine engine
CA970593A (en) Temperature measurement system for gas turbine engines
CA948698A (en) Transistorized ignition system for gas turbine engines
GB1556266A (en) Gas turbine engines
CA986319A (en) Gas turbine engine for subsonic flight
CA836231A (en) Combustion apparatus for gas turbine engines
CA843080A (en) Combustion apparatus for gas turbine engines