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DE3364029D1 - Combustor - Google Patents

Combustor

Info

Publication number
DE3364029D1
DE3364029D1 DE8383301586T DE3364029T DE3364029D1 DE 3364029 D1 DE3364029 D1 DE 3364029D1 DE 8383301586 T DE8383301586 T DE 8383301586T DE 3364029 T DE3364029 T DE 3364029T DE 3364029 D1 DE3364029 D1 DE 3364029D1
Authority
DE
Germany
Prior art keywords
combustor
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
DE8383301586T
Other languages
German (de)
Inventor
Hukam C Mongia
Edwin B Coleman
Thomas W Bruce
Harry A Elliot
John T White
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.)
Garrett Corp
Original Assignee
Garrett 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
Priority claimed from US06/400,578 external-priority patent/US4497170A/en
Priority claimed from US06/400,580 external-priority patent/US4532762A/en
Application filed by Garrett Corp filed Critical Garrett Corp
Application granted granted Critical
Publication of DE3364029D1 publication Critical patent/DE3364029D1/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
    • F23R3/26—Controlling the air flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
DE8383301586T 1982-07-22 1983-03-22 Combustor Expired DE3364029D1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/400,578 US4497170A (en) 1982-07-22 1982-07-22 Actuation system for a variable geometry combustor
US06/400,580 US4532762A (en) 1982-07-22 1982-07-22 Gas turbine engine variable geometry combustor apparatus

Publications (1)

Publication Number Publication Date
DE3364029D1 true DE3364029D1 (en) 1986-07-17

Family

ID=27017100

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8383301586T Expired DE3364029D1 (en) 1982-07-22 1983-03-22 Combustor

Country Status (2)

Country Link
EP (1) EP0100135B1 (en)
DE (1) DE3364029D1 (en)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3942451A1 (en) * 1989-12-22 1991-06-27 Daimler Benz Ag DEVICE FOR ADJUSTING THE SECOND AIR FLOW ON A GAS TURBINE COMBUSTION CHAMBER
FR2690977B1 (en) * 1992-05-06 1995-09-01 Snecma COMBUSTION CHAMBER COMPRISING ADJUSTABLE PASSAGES FOR THE ADMISSION OF PRIMARY FUEL.
FR2704628B1 (en) * 1993-04-29 1995-06-09 Snecma Combustion chamber comprising an oxidizer injection system with variable geometry.
US6220034B1 (en) 1993-07-07 2001-04-24 R. Jan Mowill Convectively cooled, single stage, fully premixed controllable fuel/air combustor
US5638674A (en) * 1993-07-07 1997-06-17 Mowill; R. Jan Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
US5572862A (en) * 1993-07-07 1996-11-12 Mowill Rolf Jan Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules
RU2112181C1 (en) * 1994-06-10 1998-05-27 Ставропольское высшее авиационное инженерное училище противовоздушной обороны им.Маршала авиации Судца В.А. Gas-turbine engine combustion chamber
RU2163991C2 (en) * 1995-12-19 2001-03-10 Акционерное общество открытого типа "Самарский научно-технический комплекс "Двигатели НК" Combustion chamber of gas-turbine engine with controller distribution of air
RU2158881C2 (en) * 1996-01-10 2000-11-10 Ставропольское высшее авиационное инженерное училище ПВО им.маршала авиации Судца В.А. Combustion chamber front system for high- temperature gas-turbine engine
RU2159898C2 (en) * 1996-01-10 2000-11-27 Ставропольское высшее авиационное инженерное училище ПВО им.маршала авиации В.А.Судца Main combustion chamber diffuser for aircraft gas- turbine engine
US5924276A (en) * 1996-07-17 1999-07-20 Mowill; R. Jan Premixer with dilution air bypass valve assembly
FR2780488B1 (en) * 1998-06-24 2000-10-13 Pillard Chauffage IMPROVEMENT IN COMBUSTION APPARATUSES COMPRISING SEVERAL FUEL TRANSPORT LINES
RU2286513C1 (en) * 2005-05-05 2006-10-27 Сергей Александрович Маяцкий Device for fuel combustion in gas-turbine engine
RU2311589C1 (en) * 2006-05-04 2007-11-27 Сергей Александрович Маяцкий Combustion chamber for gas turbine engine
RU2325588C2 (en) * 2006-07-13 2008-05-27 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Device to control low emission combustion chamber of gas turbine
RU2376528C1 (en) * 2008-03-31 2009-12-20 Денис Сергеевич Легконогих Method of increasing survivability of gas turbine engine combustion chamber
RU2378576C1 (en) * 2008-04-02 2010-01-10 Закрытое акционерное общество "Энергомаш (Холдинг)" Combustion chamber burner device of gas turbine equipment
RU2400673C1 (en) * 2009-01-11 2010-09-27 Открытое акционерное общество "Климов" Combustion chamber with optimum operating mode
RU2505749C1 (en) * 2012-07-27 2014-01-27 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Gas turbine engine combustion chamber and method of its operation
RU2513527C1 (en) * 2012-12-20 2014-04-20 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Gas turbine engine combustion chamber and method of its operation
RU2531477C1 (en) * 2013-08-30 2014-10-20 Федеральное государственное казенное военное образовательное учреждение высшего профессионального образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации Device to burn fuel in gas turbine engine
RU2625076C1 (en) * 2016-02-08 2017-07-11 Николай Борисович Болотин Combustion chamber of gas turbine engine and means of air activation
CN115949509B (en) * 2023-01-09 2025-09-05 中国航发湖南动力机械研究所 Ignition starting device and gas turbine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3927520A (en) * 1974-02-04 1975-12-23 Gen Motors Corp Combustion apparatus with combustion and dilution air modulating means
US3919838A (en) * 1974-11-04 1975-11-18 Gen Motors Corp Combustion control
US3930368A (en) * 1974-12-12 1976-01-06 General Motors Corporation Combustion liner air valve
US4263780A (en) * 1979-09-28 1981-04-28 General Motors Corporation Lean prechamber outflow combustor with sets of primary air entrances

Also Published As

Publication number Publication date
EP0100135B1 (en) 1986-06-11
EP0100135A1 (en) 1984-02-08

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee