PL2748444T3 - Komora spalania cylindryczno-pierścieniowa z rozstawionymi, stycznymi dyszami paliwowo-powietrznymi do zastosowania w silnikach turbinowych - Google Patents

Komora spalania cylindryczno-pierścieniowa z rozstawionymi, stycznymi dyszami paliwowo-powietrznymi do zastosowania w silnikach turbinowych

Info

Publication number
PL2748444T3
PL2748444T3 PL11871243T PL11871243T PL2748444T3 PL 2748444 T3 PL2748444 T3 PL 2748444T3 PL 11871243 T PL11871243 T PL 11871243T PL 11871243 T PL11871243 T PL 11871243T PL 2748444 T3 PL2748444 T3 PL 2748444T3
Authority
PL
Poland
Prior art keywords
staged
gas turbine
turbine engines
air nozzles
annular combustor
Prior art date
Application number
PL11871243T
Other languages
English (en)
Inventor
Majed Toqan
Brent Allan Gregory
Jonathan David Regele
Ryan Sadao Yamane
Original Assignee
Majed Toqan
Brent Allan Gregory
Jonathan David Regele
Ryan Sadao Yamane
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 Majed Toqan, Brent Allan Gregory, Jonathan David Regele, Ryan Sadao Yamane filed Critical Majed Toqan
Publication of PL2748444T3 publication Critical patent/PL2748444T3/pl

Links

Classifications

    • 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
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34Feeding into different combustion zones
    • F23R3/346Feeding into different combustion zones for staged combustion
    • 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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/44Combustion chambers comprising a single tubular flame tube within a tubular casing
    • 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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/58Cyclone or vortex type combustion chambers
    • 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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50Combustion chambers comprising an annular flame tube within an annular casing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
PL11871243T 2011-08-22 2011-08-22 Komora spalania cylindryczno-pierścieniowa z rozstawionymi, stycznymi dyszami paliwowo-powietrznymi do zastosowania w silnikach turbinowych PL2748444T3 (pl)

Applications Claiming Priority (2)

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
EP11871243.9A EP2748444B1 (en) 2011-08-22 2011-08-22 Can-annular combustor with staged and tangential fuel-air nozzles for use on gas turbine engines

Publications (1)

Publication Number Publication Date
PL2748444T3 true PL2748444T3 (pl) 2019-11-29

Family

ID=47747020

Family Applications (1)

Application Number Title Priority Date Filing Date
PL11871243T PL2748444T3 (pl) 2011-08-22 2011-08-22 Komora spalania cylindryczno-pierścieniowa z rozstawionymi, stycznymi dyszami paliwowo-powietrznymi do zastosowania w silnikach turbinowych

Country Status (7)

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

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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
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
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
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
CN114427689B (zh) * 2022-01-20 2024-07-12 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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US5113647A (en) * 1989-12-22 1992-05-19 Sundstrand Corporation Gas turbine annular combustor
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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
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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
EP2748444B1 (en) 2019-02-13
CN103998745B (zh) 2017-02-15
KR20140082658A (ko) 2014-07-02
EP2748444A2 (en) 2014-07-02
WO2013028167A3 (en) 2014-03-20
JP2014526029A (ja) 2014-10-02
RU2611217C2 (ru) 2017-02-21
JP6086391B2 (ja) 2017-03-01
EP2748444A4 (en) 2015-05-27
KR101774093B1 (ko) 2017-09-12
CN103998745A (zh) 2014-08-20
WO2013028167A2 (en) 2013-02-28

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