CN103998745B - 在燃气轮机上使用的具有分级切向燃料‑空气喷嘴的筒状环形燃烧室 - Google Patents

在燃气轮机上使用的具有分级切向燃料‑空气喷嘴的筒状环形燃烧室 Download PDF

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Publication number
CN103998745B
CN103998745B CN201180073013.6A CN201180073013A CN103998745B CN 103998745 B CN103998745 B CN 103998745B CN 201180073013 A CN201180073013 A CN 201180073013A CN 103998745 B CN103998745 B CN 103998745B
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air
nozzle
jet
fuel
cylinder volume
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CN103998745A (zh
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马吉德·托甘
布伦特·阿伦·格雷戈里
乔纳森·达维德·赖盖莱
里安·萨多·亚马内
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    • 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
    • F23R3/34—Feeding into different combustion zones
    • F23R3/346—Feeding into different combustion zones for staged combustion
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/44—Combustion chambers comprising a single tubular flame tube within a tubular casing
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/58—Cyclone or vortex type combustion chambers
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
CN201180073013.6A 2011-08-22 2011-08-22 在燃气轮机上使用的具有分级切向燃料‑空气喷嘴的筒状环形燃烧室 Active CN103998745B (zh)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2011/048612 WO2013028167A2 (en) 2011-08-22 2011-08-22 Can-annular combustor with staged and tangential fuel-air nozzles for use on gas turbine engines

Publications (2)

Publication Number Publication Date
CN103998745A CN103998745A (zh) 2014-08-20
CN103998745B true CN103998745B (zh) 2017-02-15

Family

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Application Number Title Priority Date Filing Date
CN201180073013.6A Active CN103998745B (zh) 2011-08-22 2011-08-22 在燃气轮机上使用的具有分级切向燃料‑空气喷嘴的筒状环形燃烧室

Country Status (7)

Country Link
EP (1) EP2748444B1 (ru)
JP (1) JP6086391B2 (ru)
KR (1) KR101774093B1 (ru)
CN (1) CN103998745B (ru)
PL (1) PL2748444T3 (ru)
RU (1) RU2611217C2 (ru)
WO (1) WO2013028167A2 (ru)

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* Cited by examiner, † Cited by third party
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US10139111B2 (en) 2014-03-28 2018-11-27 Siemens Energy, Inc. Dual outlet nozzle for a secondary fuel stage of a combustor of a gas turbine engine
FR3032781B1 (fr) * 2015-02-17 2018-07-06 Safran Helicopter Engines Systeme de combustion a volume constant pour turbomachine de moteur d'aeronef
WO2018090383A1 (zh) * 2016-11-21 2018-05-24 深圳智慧能源技术有限公司 燃气轮机燃烧室及其喷嘴
CN106439914A (zh) * 2016-11-21 2017-02-22 深圳智慧能源技术有限公司 燃气轮机燃烧室
WO2018090384A1 (zh) * 2016-11-21 2018-05-24 深圳智慧能源技术有限公司 燃气轮机燃烧室
US11174792B2 (en) 2019-05-21 2021-11-16 General Electric Company System and method for high frequency acoustic dampers with baffles
US11156164B2 (en) 2019-05-21 2021-10-26 General Electric Company System and method for high frequency accoustic dampers with caps
KR102265626B1 (ko) * 2020-09-25 2021-06-16 박재현 샌드 스프레이 시험 장치
CN114135901A (zh) * 2021-11-08 2022-03-04 中国航发四川燃气涡轮研究院 一种防烧蚀的火焰筒大孔射流套筒
CN114427689A (zh) * 2022-01-20 2022-05-03 中国空气动力研究与发展中心空天技术研究所 一种可实现超声速流场观测的圆盘形旋转爆震燃烧室
CN114857617B (zh) * 2022-05-20 2023-07-14 南昌航空大学 一种带锯齿型凹槽涡流发生器的支板火焰稳定器

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JPH0375414A (ja) * 1989-08-15 1991-03-29 Nissan Motor Co Ltd ガスタービン燃焼器
US5113647A (en) * 1989-12-22 1992-05-19 Sundstrand Corporation Gas turbine annular combustor
GB2295887A (en) * 1994-12-08 1996-06-12 Rolls Royce Plc Combustor assembly
US6453658B1 (en) * 2000-02-24 2002-09-24 Capstone Turbine Corporation Multi-stage multi-plane combustion system for a gas turbine engine
JP4608154B2 (ja) * 2001-09-27 2011-01-05 大阪瓦斯株式会社 ガスタービン用燃焼装置及びそれを備えたガスタービン
US6751961B2 (en) * 2002-05-14 2004-06-22 United Technologies Corporation Bulkhead panel for use in a combustion chamber of a gas turbine engine
JP3959632B2 (ja) * 2002-09-04 2007-08-15 石川島播磨重工業株式会社 拡散燃焼方式低ＮＯｘ燃焼器
JP3901629B2 (ja) * 2002-11-11 2007-04-04 石川島播磨重工業株式会社 アニュラ型渦巻き拡散火炎燃焼器
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Also Published As

Publication number Publication date
RU2014110628A (ru) 2015-09-27
WO2013028167A3 (en) 2014-03-20
JP6086391B2 (ja) 2017-03-01
JP2014526029A (ja) 2014-10-02
EP2748444A4 (en) 2015-05-27
KR20140082658A (ko) 2014-07-02
RU2611217C2 (ru) 2017-02-21
CN103998745A (zh) 2014-08-20
WO2013028167A2 (en) 2013-02-28
PL2748444T3 (pl) 2019-11-29
EP2748444A2 (en) 2014-07-02
EP2748444B1 (en) 2019-02-13
KR101774093B1 (ko) 2017-09-12

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