YU201686A - Flame stabilizer for additional burning chamber of turbojet engine - Google Patents

Flame stabilizer for additional burning chamber of turbojet engine

Info

Publication number
YU201686A
YU201686A YU02016/86A YU201686A YU201686A YU 201686 A YU201686 A YU 201686A YU 02016/86 A YU02016/86 A YU 02016/86A YU 201686 A YU201686 A YU 201686A YU 201686 A YU201686 A YU 201686A
Authority
YU
Yugoslavia
Prior art keywords
turbojet engine
burning chamber
flame stabilizer
additional burning
additional
Prior art date
Application number
YU02016/86A
Other languages
English (en)
Inventor
T R Clements
J D Blevins
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 YU201686A publication Critical patent/YU201686A/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C1/00Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous 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
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Testing Of Engines (AREA)
  • Control Of Combustion (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
YU02016/86A 1985-11-25 1986-11-25 Flame stabilizer for additional burning chamber of turbojet engine YU201686A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US80164285A 1985-11-25 1985-11-25

Publications (1)

Publication Number Publication Date
YU201686A true YU201686A (en) 1990-06-30

Family

ID=25181670

Family Applications (2)

Application Number Title Priority Date Filing Date
YU02016/86A YU201686A (en) 1985-11-25 1986-11-25 Flame stabilizer for additional burning chamber of turbojet engine
YU02036/86A YU203686A (en) 1985-11-25 1986-11-28 Belt for reinforcing coating of additional burning chamber, with elements for fastening

Family Applications After (1)

Application Number Title Priority Date Filing Date
YU02036/86A YU203686A (en) 1985-11-25 1986-11-28 Belt for reinforcing coating of additional burning chamber, with elements for fastening

Country Status (9)

Country Link
EP (1) EP0224429B1 (xx)
JP (1) JPS62129528A (xx)
KR (1) KR940008267B1 (xx)
CN (1) CN1007640B (xx)
AU (1) AU593858B2 (xx)
CA (1) CA1281554C (xx)
DE (1) DE3675896D1 (xx)
IL (1) IL80634A (xx)
YU (2) YU201686A (xx)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IL93630A0 (en) * 1989-03-27 1990-12-23 Gen Electric Flameholder for gas turbine engine afterburner
JP5375433B2 (ja) * 2009-08-21 2013-12-25 株式会社Ihi アフタバーナ及び航空機エンジン
US20110219776A1 (en) * 2010-03-15 2011-09-15 General Electric Company Aerodynamic flame stabilizer
CN102200292B (zh) * 2010-03-26 2015-01-21 北京航空航天大学 带凹腔的支板火焰稳定装置及火焰稳定方法
JP2013181473A (ja) * 2012-03-02 2013-09-12 Ihi Corp アフタバーナ及び航空機エンジン
CN103884024B (zh) * 2014-04-03 2016-01-20 北京航空航天大学 一种能够组织燃烧并将火焰传导到外涵道气流的联焰装置
CN105546578B (zh) * 2015-12-25 2018-08-24 中国航空工业集团公司沈阳发动机设计研究所 一种火焰稳定器
CN105650642B (zh) * 2016-02-04 2019-04-30 中国科学院工程热物理研究所 一种可形成低速区的喷嘴、喷嘴阵列和燃烧器
CN105841191B (zh) * 2016-03-30 2018-07-06 中国科学院工程热物理研究所 一种v型火焰稳定器尾缘结构
CN106678877A (zh) * 2016-11-15 2017-05-17 西北工业大学 一种加有v型槽环形火焰稳定器的一体化加力燃烧室
CN110486148A (zh) * 2017-08-29 2019-11-22 熵零技术逻辑工程院集团股份有限公司 一种加力燃烧室高负荷响应发动机
CN109611887B (zh) * 2018-11-01 2020-10-09 中国航发沈阳发动机研究所 一种燃烧装置
CN114992674B (zh) * 2022-06-20 2024-03-19 中国航发贵阳发动机设计研究所 一种外置式接力点火及起动供油装置

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB744178A (en) * 1953-03-26 1956-02-01 Rolls Royce Improvements relating to combustion equipment of gas-turbine engines
FR1199822A (fr) * 1958-07-11 1959-12-16 Nord Aviat Perfectionnements aux stabilisateurs de flammes dans les propulseurs à réaction
GB886700A (en) * 1959-11-05 1962-01-10 Rolls Royce Reheat combustion equipment for jet propulsion engines
FR2429326A1 (fr) * 1978-06-22 1980-01-18 Snecma Perfectionnements aux dispositifs accroche-flammes pour chambres de combustion, notamment pour canaux de post-combustion de turboreacteurs
US4423595A (en) * 1982-05-27 1984-01-03 United Technologies Corporation Augmentor residual fuel drain apparatus

Also Published As

Publication number Publication date
CN86108062A (zh) 1987-07-01
EP0224429A3 (en) 1988-09-14
KR940008267B1 (ko) 1994-09-09
AU593858B2 (en) 1990-02-22
IL80634A (en) 1991-12-15
CN1007640B (zh) 1990-04-18
JPS62129528A (ja) 1987-06-11
JPH0587654B2 (xx) 1993-12-17
EP0224429B1 (en) 1990-11-28
DE3675896D1 (de) 1991-01-10
KR870005163A (ko) 1987-06-05
EP0224429A2 (en) 1987-06-03
CA1281554C (en) 1991-03-19
IL80634A0 (en) 1987-02-27
AU6562686A (en) 1987-05-28
YU203686A (en) 1990-06-30

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