JP4597353B2 - オーグメンタ内で一様な点火をもたらす方法及び装置 - Google Patents

オーグメンタ内で一様な点火をもたらす方法及び装置 Download PDF

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Publication number
JP4597353B2
JP4597353B2 JP2000386191A JP2000386191A JP4597353B2 JP 4597353 B2 JP4597353 B2 JP 4597353B2 JP 2000386191 A JP2000386191 A JP 2000386191A JP 2000386191 A JP2000386191 A JP 2000386191A JP 4597353 B2 JP4597353 B2 JP 4597353B2
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Japan
Prior art keywords
igniter
augmentor
housing
lead
body portion
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
JP2000386191A
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English (en)
Japanese (ja)
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JP2001221103A (ja
JP2001221103A5 (enExample
Inventor
ラリー・リー・ヴァセク
トーマス・チャールズ・ゲレティー
ウィリアム・アール・マスキエル
エルビン・ディー・ヒルトル
リチャード・エム・ホルコンベ
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General Electric Co
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General Electric Co
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
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Publication of JP2001221103A5 publication Critical patent/JP2001221103A5/ja
Application granted granted Critical
Publication of JP4597353B2 publication Critical patent/JP4597353B2/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
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • F02C7/266—Electric
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/90—Mounting on supporting structures or systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spark Plugs (AREA)
  • Air Bags (AREA)
JP2000386191A 1999-12-21 2000-12-20 オーグメンタ内で一様な点火をもたらす方法及び装置 Expired - Fee Related JP4597353B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/467,955 US6438940B1 (en) 1999-12-21 1999-12-21 Methods and apparatus for providing uniform ignition in an augmenter
US09/467955 1999-12-21

Publications (3)

Publication Number Publication Date
JP2001221103A JP2001221103A (ja) 2001-08-17
JP2001221103A5 JP2001221103A5 (enExample) 2008-02-14
JP4597353B2 true JP4597353B2 (ja) 2010-12-15

Family

ID=23857834

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2000386191A Expired - Fee Related JP4597353B2 (ja) 1999-12-21 2000-12-20 オーグメンタ内で一様な点火をもたらす方法及び装置

Country Status (4)

Country Link
US (1) US6438940B1 (enExample)
EP (1) EP1111219B1 (enExample)
JP (1) JP4597353B2 (enExample)
DE (1) DE60032868T2 (enExample)

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ITMI20020910A1 (it) * 2002-04-29 2003-10-29 Nuovo Pignone Spa Dispositivo di tenuta per accoppiamento di una tubazione con un foro
US6920762B2 (en) * 2003-01-14 2005-07-26 General Electric Company Mounting assembly for igniter in a gas turbine engine combustor having a ceramic matrix composite liner
US7153023B2 (en) * 2004-01-12 2006-12-26 General Electric Company Methods and apparatus for installing process instrument probes
US7065956B2 (en) * 2004-09-08 2006-06-27 Howard Johnson Two piece jet engine igniter assembly
US8044319B2 (en) * 2005-02-07 2011-10-25 Pratt & Whitney Canada Corp. Variable arc gap plasma igniter
US7437876B2 (en) * 2005-03-25 2008-10-21 General Electric Company Augmenter swirler pilot
US7637094B2 (en) * 2005-12-16 2009-12-29 General Electric Company Cooling apparatus for a gas turbine engine igniter lead
FR2900976B1 (fr) * 2006-05-11 2008-07-11 Snecma Sa Montage d'une bougie d'allumage dans une chambre de combustion de moteur a turbine a gaz
ATE445772T1 (de) * 2006-12-22 2009-10-15 Siemens Ag Brenner einer gasturbine
US20090293486A1 (en) * 2007-10-26 2009-12-03 Honeywell International, Inc. Combustors with igniters having protrusions
US8171719B2 (en) * 2008-03-21 2012-05-08 Siemens Energy, Inc. Igniter assembly for a gas turbine
FR2952701B1 (fr) * 2009-11-18 2012-11-02 Snecma Guidage d'une bougie d'allumage dans une chambre de combustion d'une turbomachine
FR2952704B1 (fr) * 2009-11-19 2015-08-07 Snecma Guidage rotulant d'une bougie d'allumage dans une chambre de combustion d'une turbomachine
US8726631B2 (en) * 2009-11-23 2014-05-20 Honeywell International Inc. Dual walled combustors with impingement cooled igniters
FR2953908A1 (fr) * 2009-12-16 2011-06-17 Snecma Guidage d'une bougie dans une chambre de combustion de turbomachine
FR2956187B1 (fr) * 2010-02-11 2012-07-06 Snecma Etancheite d'un guide-bougie pour une chambre de combustion de turbomachine
DE102011016917A1 (de) 2011-04-13 2012-10-18 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit einer Halterung einer Dichtung für ein Anbauteil
US9140193B2 (en) * 2011-05-03 2015-09-22 Siemens Energy, Inc. Gas turbine igniter with structure to reduce radial movement of igniter rod
US20130045452A1 (en) * 2011-08-15 2013-02-21 General Electric Company Ignition system for a combustor
US8893502B2 (en) 2011-10-14 2014-11-25 United Technologies Corporation Augmentor spray bar with tip support bushing
US9157638B2 (en) * 2012-01-31 2015-10-13 General Electric Company Adaptor assembly for removable components
US8997453B2 (en) * 2012-06-29 2015-04-07 United Technologies Corporation Igniter for a turbomachine and mounting assembly therefor
US9273867B2 (en) * 2013-02-04 2016-03-01 Air Products And Chemicals, Inc. Retractable ignition system
WO2014137409A1 (en) 2013-03-07 2014-09-12 Rolls-Royce Corporation Flexible bellows igniter seal for a gas turbine with a ceramic combustion liner
US9989254B2 (en) * 2013-06-03 2018-06-05 General Electric Company Combustor leakage control system
US20160003150A1 (en) * 2014-07-03 2016-01-07 General Electric Company Igniter tip with cooling passage
CN105091029B (zh) * 2014-07-07 2017-10-10 池州中宏运环保设备有限公司 一种点火器伸缩装置
US9897319B2 (en) 2015-02-25 2018-02-20 United Technologies Corporation Igniter position for a combustor of a gas turbine engine
JP6388421B2 (ja) * 2015-03-03 2018-09-12 東芝エネルギーシステムズ株式会社 点火装置およびガスタービン燃焼器
US10041413B2 (en) 2015-06-05 2018-08-07 General Electric Company Igniter assembly for a gas turbine engine
CN105134385B (zh) * 2015-09-17 2017-04-19 中国航空工业集团公司沈阳发动机设计研究所 一种伸缩式点火电嘴组件
US10935242B2 (en) * 2016-07-07 2021-03-02 General Electric Company Combustor assembly for a turbine engine
CN106837558B (zh) * 2017-01-19 2018-09-14 新奥能源动力科技（上海）有限公司 一种点火器装置
US11286860B2 (en) 2017-03-03 2022-03-29 General Electric Company Sealing assembly for components penetrating through CMC liner
US10465610B2 (en) 2017-03-03 2019-11-05 General Electric Company Sealing assembly for components penetrating through CMC liner
US11286861B2 (en) * 2018-09-12 2022-03-29 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11268447B2 (en) * 2018-09-12 2022-03-08 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
FR3090747B1 (fr) * 2018-12-21 2021-01-22 Turbotech Chambre de combustion d'une turbomachine
CN117167776A (zh) * 2022-05-25 2023-12-05 中国航发商用航空发动机有限责任公司 点火电嘴安装结构及燃烧室
US12055058B2 (en) * 2022-05-31 2024-08-06 Pratt & Whitney Canada Corp. Joint between gas turbine engine components with a spring element

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US3487636A (en) * 1968-01-02 1970-01-06 Gen Electric Augmentor spark igniter
GB1330638A (en) * 1969-10-10 1973-09-19 Lucas Industries Ltd Gas turbine engine
BE795529A (fr) * 1972-02-17 1973-06-18 Gen Electric Allumeur monte sur un dispositif d'augmentation de la poussee de turboreacteurs et refroidi a l'air
US3793838A (en) * 1972-09-05 1974-02-26 Gen Electric Augmenter fuel injection mounting system
CA992755A (en) * 1972-10-02 1976-07-13 General Electric Company Gas turbine engine igniter assembly
GB1476414A (en) * 1974-04-05 1977-06-16 Gen Motors Corp Combustion apparatus for a gas turbine engine
US3910036A (en) * 1974-04-05 1975-10-07 Gen Motors Corp Igniter installation for combustor with ceramic liner
US4275559A (en) * 1979-08-31 1981-06-30 General Electric Company Retractable igniter device for gas turbines
US5076062A (en) * 1987-11-05 1991-12-31 General Electric Company Gas-cooled flameholder assembly
US4798048A (en) * 1987-12-21 1989-01-17 United Technologies Corporation Augmentor pilot
US4903476A (en) * 1988-12-27 1990-02-27 General Electric Company Gas turbine igniter with ball-joint support
US5115636A (en) * 1990-09-12 1992-05-26 General Electric Company Borescope plug
EP0550126A1 (en) * 1992-01-02 1993-07-07 General Electric Company Thrust augmentor heat shield
US5402637A (en) * 1993-07-13 1995-04-04 Cooper Industries Igniter plug extender for a turbine engine combustor
FR2708072B1 (fr) * 1993-07-21 1995-09-01 Snecma Bouchon amovible de trois trous ménagés dans des parois à températures différentes.
US5813221A (en) * 1997-01-14 1998-09-29 General Electric Company Augmenter with integrated fueling and cooling

Also Published As

Publication number Publication date
DE60032868D1 (de) 2007-02-22
JP2001221103A (ja) 2001-08-17
EP1111219A2 (en) 2001-06-27
US6438940B1 (en) 2002-08-27
EP1111219B1 (en) 2007-01-10
DE60032868T2 (de) 2007-10-25
EP1111219A3 (en) 2003-03-05

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