IT1089612B - Apparecchio di combustione per un motore da turbina a gas - Google Patents

Apparecchio di combustione per un motore da turbina a gas

Info

Publication number
IT1089612B
IT1089612B IT31181/77A IT3118177A IT1089612B IT 1089612 B IT1089612 B IT 1089612B IT 31181/77 A IT31181/77 A IT 31181/77A IT 3118177 A IT3118177 A IT 3118177A IT 1089612 B IT1089612 B IT 1089612B
Authority
IT
Italy
Prior art keywords
gas turbine
turbine engine
combustion apparatus
combustion
engine
Prior art date
Application number
IT31181/77A
Other languages
English (en)
Original Assignee
Westinghouse Electric 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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Application granted granted Critical
Publication of IT1089612B publication Critical patent/IT1089612B/it

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F23D17/002—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel
    • 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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/36—Supply of different fuels

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
IT31181/77A 1977-01-21 1977-12-23 Apparecchio di combustione per un motore da turbina a gas IT1089612B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/761,047 US4155220A (en) 1977-01-21 1977-01-21 Combustion apparatus for a gas turbine engine

Publications (1)

Publication Number Publication Date
IT1089612B true IT1089612B (it) 1985-06-18

Family

ID=25060951

Family Applications (1)

Application Number Title Priority Date Filing Date
IT31181/77A IT1089612B (it) 1977-01-21 1977-12-23 Apparecchio di combustione per un motore da turbina a gas

Country Status (8)

Country Link
US (1) US4155220A (it)
JP (1) JPS5392022A (it)
AR (1) AR212792A1 (it)
BE (1) BE863135A (it)
CA (1) CA1071418A (it)
GB (1) GB1543032A (it)
IN (1) IN148367B (it)
IT (1) IT1089612B (it)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4258544A (en) * 1978-09-15 1981-03-31 Caterpillar Tractor Co. Dual fluid fuel nozzle
US4263780A (en) * 1979-09-28 1981-04-28 General Motors Corporation Lean prechamber outflow combustor with sets of primary air entrances
JPS56140324A (en) * 1980-04-02 1981-11-02 Canon Inc Display device
DE3361535D1 (en) * 1982-05-28 1986-01-30 Bbc Brown Boveri & Cie Gas turbine combustion chamber and method of operating it
US4584834A (en) * 1982-07-06 1986-04-29 General Electric Company Gas turbine engine carburetor
JPS59195616U (ja) * 1983-06-14 1984-12-26 松下電器産業株式会社 接続リ−ド
JPH0414949Y2 (it) * 1984-12-29 1992-04-03
JPS63302590A (ja) * 1987-06-02 1988-12-09 Fujikura Ltd フレキシブル回路基板及びその製造方法
JPH01318281A (ja) * 1988-06-20 1989-12-22 Shin Etsu Chem Co Ltd フレキシブル印刷配線基板の製造方法
US5431019A (en) * 1993-04-22 1995-07-11 Alliedsignal Inc. Combustor for gas turbine engine
US5636510A (en) * 1994-05-25 1997-06-10 Westinghouse Electric Corporation Gas turbine topping combustor
US7712313B2 (en) * 2007-08-22 2010-05-11 Pratt & Whitney Canada Corp. Fuel nozzle for a gas turbine engine
US20130189632A1 (en) * 2012-01-23 2013-07-25 General Electric Company Fuel nozzel
US9518739B2 (en) 2013-03-08 2016-12-13 Pratt & Whitney Canada Corp. Combustor heat shield with carbon avoidance feature
FR3022985B1 (fr) * 2014-06-25 2019-06-21 Safran Aircraft Engines Systeme d'injection pour chambre de combustion de turbomachine configure pour une injection directe de deux nappes de carburant coaxiales
RU2598964C2 (ru) * 2014-12-12 2016-10-10 Федеральное агентство научных организаций Федеральное Государственное Бюджетное Научное Учреждение Всероссийский научно-исследовательский институт электрификации сельского хозяйства (ФГБНУ ВИЭСХ) Устройство камеры сгорания с регулируемым зазором подачи охлаждающего воздуха для микрогазотурбинного двигателя
RU170359U1 (ru) * 2016-10-05 2017-04-24 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Форсуночный модуль малоэмиссионной камеры сгорания газотурбинного двигателя

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1536046A (en) * 1920-08-07 1925-05-05 Alfred R Anthony Oil burner
US2515843A (en) * 1945-08-30 1950-07-18 Shell Dev Air register for burners
US3121996A (en) * 1961-10-02 1964-02-25 Lucas Industries Ltd Liquid fuel combustion apparatus
US3215351A (en) * 1963-06-04 1965-11-02 Master Cons Inc Oil burner nozzle
US3498055A (en) * 1968-10-16 1970-03-03 United Aircraft Corp Smoke reduction combustion chamber
FR2122820A5 (it) * 1971-01-22 1972-09-01 Pillard Freres Cie
US3763650A (en) * 1971-07-26 1973-10-09 Westinghouse Electric Corp Gas turbine temperature profiling structure
US3831854A (en) * 1973-02-23 1974-08-27 Hitachi Ltd Pressure spray type fuel injection nozzle having air discharge openings
CA1015093A (en) * 1973-04-23 1977-08-02 Union Carbide Corporation Thermosetting powder coatings
US3853273A (en) * 1973-10-01 1974-12-10 Gen Electric Axial swirler central injection carburetor
US3901446A (en) * 1974-05-09 1975-08-26 Us Air Force Induced vortex swirler
US4044553A (en) * 1976-08-16 1977-08-30 General Motors Corporation Variable geometry swirler

Also Published As

Publication number Publication date
AR212792A1 (es) 1978-09-29
CA1071418A (en) 1980-02-12
IN148367B (it) 1981-01-31
US4155220A (en) 1979-05-22
BE863135A (fr) 1978-07-20
JPS5755972B2 (it) 1982-11-27
JPS5392022A (en) 1978-08-12
GB1543032A (en) 1979-03-28

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