JP4659201B2 - 低エミッション燃焼器 - Google Patents

低エミッション燃焼器 Download PDF

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Publication number
JP4659201B2
JP4659201B2 JP2000331593A JP2000331593A JP4659201B2 JP 4659201 B2 JP4659201 B2 JP 4659201B2 JP 2000331593 A JP2000331593 A JP 2000331593A JP 2000331593 A JP2000331593 A JP 2000331593A JP 4659201 B2 JP4659201 B2 JP 4659201B2
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JP
Japan
Prior art keywords
cone
combustor
flare
flared
heat shield
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 - Fee Related
Application number
JP2000331593A
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English (en)
Japanese (ja)
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JP2001147018A (ja
JP2001147018A5 (enExample
Inventor
ジョセフ・ダグラス・モンティー
ジョン・カール・ジャコブソン
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General Electric Co
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General Electric Co
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Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of JP2001147018A publication Critical patent/JP2001147018A/ja
Publication of JP2001147018A5 publication Critical patent/JP2001147018A5/ja
Application granted granted Critical
Publication of JP4659201B2 publication Critical patent/JP4659201B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
JP2000331593A 1999-11-01 2000-10-31 低エミッション燃焼器 Expired - Fee Related JP4659201B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/431464 1999-11-01
US09/431,464 US6279323B1 (en) 1999-11-01 1999-11-01 Low emissions combustor

Publications (3)

Publication Number Publication Date
JP2001147018A JP2001147018A (ja) 2001-05-29
JP2001147018A5 JP2001147018A5 (enExample) 2007-12-13
JP4659201B2 true JP4659201B2 (ja) 2011-03-30

Family

ID=23712059

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2000331593A Expired - Fee Related JP4659201B2 (ja) 1999-11-01 2000-10-31 低エミッション燃焼器

Country Status (4)

Country Link
US (1) US6279323B1 (enExample)
EP (1) EP1096206B1 (enExample)
JP (1) JP4659201B2 (enExample)
DE (1) DE60029897T2 (enExample)

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US20040202977A1 (en) * 2003-04-08 2004-10-14 Ken Walkup Low NOx burner
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US7185497B2 (en) * 2004-05-04 2007-03-06 Honeywell International, Inc. Rich quick mix combustion system
US7013649B2 (en) * 2004-05-25 2006-03-21 General Electric Company Gas turbine engine combustor mixer
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US7246494B2 (en) * 2004-09-29 2007-07-24 General Electric Company Methods and apparatus for fabricating gas turbine engine combustors
US7421843B2 (en) * 2005-01-15 2008-09-09 Siemens Power Generation, Inc. Catalytic combustor having fuel flow control responsive to measured combustion parameters
US7386980B2 (en) * 2005-02-02 2008-06-17 Power Systems Mfg., Llc Combustion liner with enhanced heat transfer
US7316117B2 (en) * 2005-02-04 2008-01-08 Siemens Power Generation, Inc. Can-annular turbine combustors comprising swirler assembly and base plate arrangements, and combinations
FR2886714B1 (fr) * 2005-06-07 2007-09-07 Snecma Moteurs Sa Systeme d'injection anti-rotatif pour turbo-reacteur
US7673460B2 (en) * 2005-06-07 2010-03-09 Snecma System of attaching an injection system to a turbojet combustion chamber base
US7513098B2 (en) 2005-06-29 2009-04-07 Siemens Energy, Inc. Swirler assembly and combinations of same in gas turbine engine combustors
US7464553B2 (en) * 2005-07-25 2008-12-16 General Electric Company Air-assisted fuel injector for mixer assembly of a gas turbine engine combustor
FR2894327B1 (fr) 2005-12-05 2008-05-16 Snecma Sa Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
FR2903172B1 (fr) * 2006-06-29 2008-10-17 Snecma Sa Agencement pour chambre de combustion de turbomachine ayant un defecteur a collerette
FR2906350B1 (fr) * 2006-09-22 2009-03-20 Snecma Sa Chambre de combustion annulaire d'une turbomachine
FR2908867B1 (fr) * 2006-11-16 2012-06-15 Snecma Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
US8707704B2 (en) * 2007-05-31 2014-04-29 General Electric Company Method and apparatus for assembling turbine engines
FR2921462B1 (fr) * 2007-09-21 2012-08-24 Snecma Chambre de combustion annulaire de moteur a turbine a gaz
US20090165435A1 (en) * 2008-01-02 2009-07-02 Michal Koranek Dual fuel can combustor with automatic liquid fuel purge
US8096132B2 (en) * 2008-02-20 2012-01-17 Flexenergy Energy Systems, Inc. Air-cooled swirlerhead
US20090255118A1 (en) * 2008-04-11 2009-10-15 General Electric Company Method of manufacturing mixers
US8281597B2 (en) * 2008-12-31 2012-10-09 General Electric Company Cooled flameholder swirl cup
US8443610B2 (en) * 2009-11-25 2013-05-21 United Technologies Corporation Low emission gas turbine combustor
FR2955375B1 (fr) * 2010-01-18 2012-06-15 Turbomeca Dispositif d'injection et chambre de combustion de turbomachine equipee d'un tel dispositif d'injection
GB201116608D0 (en) * 2011-09-27 2011-11-09 Rolls Royce Plc A method of operating a combustion chamber
US10378775B2 (en) * 2012-03-23 2019-08-13 Pratt & Whitney Canada Corp. Combustor heat shield
US9021812B2 (en) 2012-07-27 2015-05-05 Honeywell International Inc. Combustor dome and heat-shield assembly
US9803498B2 (en) * 2012-10-17 2017-10-31 United Technologies Corporation One-piece fuel nozzle for a thrust engine
BR112015011109A2 (pt) * 2012-11-15 2017-12-05 Gen Electric aparelho de blindagem termorresistente, aparelho de bocal de combustível, método para reparar o aparelho e método para montar um bocal de combustível
US10260748B2 (en) 2012-12-21 2019-04-16 United Technologies Corporation Gas turbine engine combustor with tailored temperature profile
WO2014123850A1 (en) 2013-02-06 2014-08-14 United Technologies Corporation Gas turbine engine component with upstream-directed cooling film holes
US10174949B2 (en) 2013-02-08 2019-01-08 United Technologies Corporation Gas turbine engine combustor liner assembly with convergent hyperbolic profile
WO2014160299A1 (en) 2013-03-14 2014-10-02 United Technologies Corporation Combustor panel with increased durability
JP6470135B2 (ja) 2014-07-14 2019-02-13 ユナイテッド テクノロジーズ コーポレイションＵｎｉｔｅｄ Ｔｅｃｈｎｏｌｏｇｉｅｓ Ｃｏｒｐｏｒａｔｉｏｎ 付加製造された表面仕上げ
CN107250673A (zh) * 2014-12-15 2017-10-13 诺沃皮尼奥内股份有限公司 燃烧器衬套柔性支撑及方法
US10309654B2 (en) * 2016-07-27 2019-06-04 Honda Motor Co., Ltd. Structure for cooling gas turbine engine
US10816202B2 (en) 2017-11-28 2020-10-27 General Electric Company Combustor liner for a gas turbine engine and an associated method thereof
FR3082284B1 (fr) * 2018-06-07 2020-12-11 Safran Aircraft Engines Chambre de combustion pour une turbomachine
CN110657452B (zh) 2018-06-29 2020-10-27 中国航发商用航空发动机有限责任公司 低污染燃烧室及其燃烧控制方法
US11255543B2 (en) 2018-08-07 2022-02-22 General Electric Company Dilution structure for gas turbine engine combustor
CN111829012B (zh) * 2019-04-17 2022-04-08 中国航发湖南动力机械研究所 火焰筒
US11686474B2 (en) * 2021-03-04 2023-06-27 General Electric Company Damper for swirl-cup combustors
US11719438B2 (en) * 2021-03-15 2023-08-08 General Electric Company Combustion liner
US11859819B2 (en) 2021-10-15 2024-01-02 General Electric Company Ceramic composite combustor dome and liners
US12072099B2 (en) * 2021-12-21 2024-08-27 General Electric Company Gas turbine fuel nozzle having a lip extending from the vanes of a swirler
US20230212984A1 (en) * 2021-12-30 2023-07-06 General Electric Company Engine fuel nozzle and swirler
US11774100B2 (en) * 2022-01-14 2023-10-03 General Electric Company Combustor fuel nozzle assembly
US12092324B2 (en) * 2022-03-17 2024-09-17 General Electric Company Flare cone for a mixer assembly of a gas turbine combustor
US12429216B2 (en) * 2023-02-23 2025-09-30 Rtx Corporation Turbine engine fuel injector assembly with annular fuel outlet

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US3853273A (en) * 1973-10-01 1974-12-10 Gen Electric Axial swirler central injection carburetor
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US4315405A (en) * 1978-12-09 1982-02-16 Rolls-Royce Limited Combustion apparatus
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DE3545524C2 (de) * 1985-12-20 1996-02-29 Siemens Ag Mehrstufenbrennkammer für die Verbrennung von stickstoffhaltigem Gas mit verringerter NO¶x¶-Emission und Verfahren zu ihrem Betrieb
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US5117637A (en) * 1990-08-02 1992-06-02 General Electric Company Combustor dome assembly
DE4110507C2 (de) 1991-03-30 1994-04-07 Mtu Muenchen Gmbh Brenner für Gasturbinentriebwerke mit mindestens einer für die Zufuhr von Verbrennungsluft lastabhängig regulierbaren Dralleinrichtung
IT1273369B (it) * 1994-03-04 1997-07-08 Nuovo Pignone Spa Sistema perfezionato combustione a basse emissioni inquinanti per turbine a gas
DE69506308T2 (de) 1994-04-20 1999-08-26 Rolls-Royce Plc Brennstoffeinspritzdüse für Gasturbinentriebwerke
FR2751054B1 (fr) 1996-07-11 1998-09-18 Snecma Chambre de combustion anti-nox a injection de carburant de type annulaire
FR2753779B1 (fr) * 1996-09-26 1998-10-16 Systeme d'injection aerodynamique d'un melange air carburant
US5970716A (en) * 1997-10-02 1999-10-26 General Electric Company Apparatus for retaining centerbody between adjacent domes of multiple annular combustor employing interference and clamping fits
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US6101814A (en) * 1999-04-15 2000-08-15 United Technologies Corporation Low emissions can combustor with dilution hole arrangement for a turbine engine

Also Published As

Publication number Publication date
JP2001147018A (ja) 2001-05-29
DE60029897D1 (de) 2006-09-21
US6279323B1 (en) 2001-08-28
EP1096206A1 (en) 2001-05-02
EP1096206B1 (en) 2006-08-09
DE60029897T2 (de) 2007-03-08

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