DE102009011393A8 - Reinluftstrombrennstoffeinspritzeinrichtung - Google Patents

Reinluftstrombrennstoffeinspritzeinrichtung Download PDF

Info

Publication number
DE102009011393A8
DE102009011393A8 DE102009011393A DE102009011393A DE102009011393A8 DE 102009011393 A8 DE102009011393 A8 DE 102009011393A8 DE 102009011393 A DE102009011393 A DE 102009011393A DE 102009011393 A DE102009011393 A DE 102009011393A DE 102009011393 A8 DE102009011393 A8 DE 102009011393A8
Authority
DE
Germany
Prior art keywords
air flow
fuel injector
clean air
flow fuel
clean
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.)
Withdrawn
Application number
DE102009011393A
Other languages
English (en)
Other versions
DE102009011393A1 (de
Inventor
Gary W. Chew
Viraphand Cholvibul
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Collins Engine Nozzles Inc
Original Assignee
Delavan Inc
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 Delavan Inc filed Critical Delavan Inc
Publication of DE102009011393A1 publication Critical patent/DE102009011393A1/de
Publication of DE102009011393A8 publication Critical patent/DE102009011393A8/de
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/106Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting at the burner outlet
    • F23D11/107Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting at the burner outlet at least one of both being subjected to a swirling motion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/101Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet
    • F23D11/102Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet in an internal mixing chamber
    • F23D11/103Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet in an internal mixing chamber with means creating a swirl inside the mixing chamber
    • 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
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • F23R3/12Air inlet arrangements for primary air inducing a vortex
    • F23R3/14Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • 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
    • F23R3/30Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/11101Pulverising gas flow impinging on fuel from pre-filming surface, e.g. lip atomizers
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Fuel-Injection Apparatus (AREA)
DE102009011393A 2008-03-04 2009-03-03 Reinluftstrombrennstoffeinspritzeinrichtung Withdrawn DE102009011393A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/041,820 US7926282B2 (en) 2008-03-04 2008-03-04 Pure air blast fuel injector
US12/041,820 2008-03-04

Publications (2)

Publication Number Publication Date
DE102009011393A1 DE102009011393A1 (de) 2009-09-10
DE102009011393A8 true DE102009011393A8 (de) 2009-12-31

Family

ID=40580616

Family Applications (1)

Application Number Title Priority Date Filing Date
DE102009011393A Withdrawn DE102009011393A1 (de) 2008-03-04 2009-03-03 Reinluftstrombrennstoffeinspritzeinrichtung

Country Status (4)

Country Link
US (1) US7926282B2 (de)
DE (1) DE102009011393A1 (de)
FR (1) FR2928441B1 (de)
GB (1) GB2458022B (de)

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* Cited by examiner, † Cited by third party
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US20090255258A1 (en) * 2008-04-11 2009-10-15 Delavan Inc Pre-filming air-blast fuel injector having a reduced hydraulic spray angle
US8161750B2 (en) * 2009-01-16 2012-04-24 General Electric Company Fuel nozzle for a turbomachine
US8387393B2 (en) * 2009-06-23 2013-03-05 Siemens Energy, Inc. Flashback resistant fuel injection system
US8899048B2 (en) 2010-11-24 2014-12-02 Delavan Inc. Low calorific value fuel combustion systems for gas turbine engines
US9003804B2 (en) 2010-11-24 2015-04-14 Delavan Inc Multipoint injectors with auxiliary stage
WO2012086006A1 (ja) * 2010-12-20 2012-06-28 トヨタ自動車株式会社 燃料噴射弁
US9644844B2 (en) 2011-11-03 2017-05-09 Delavan Inc. Multipoint fuel injection arrangements
US20140339339A1 (en) * 2011-11-03 2014-11-20 Delavan Inc Airblast injectors for multipoint injection and methods of assembly
US9188063B2 (en) 2011-11-03 2015-11-17 Delavan Inc. Injectors for multipoint injection
US9745936B2 (en) 2012-02-16 2017-08-29 Delavan Inc Variable angle multi-point injection
US9400104B2 (en) * 2012-09-28 2016-07-26 United Technologies Corporation Flow modifier for combustor fuel nozzle tip
WO2014113105A2 (en) * 2012-10-17 2014-07-24 United Technologies Corporation Fuel nozzle for a gas turbine engine
US9488108B2 (en) * 2012-10-17 2016-11-08 Delavan Inc. Radial vane inner air swirlers
US9333518B2 (en) 2013-02-27 2016-05-10 Delavan Inc Multipoint injectors
US10161633B2 (en) 2013-03-04 2018-12-25 Delavan Inc. Air swirlers
EP3039343B8 (de) * 2013-08-30 2021-03-31 Raytheon Technologies Corporation Zweistoffdüse mit axialer wirbelgasinjektion für eine gasturbine und entsprechendes verfahren
US9574776B2 (en) 2013-10-21 2017-02-21 Delavan Inc. Three-piece airblast fuel injector
US10731861B2 (en) * 2013-11-18 2020-08-04 Raytheon Technologies Corporation Dual fuel nozzle with concentric fuel passages for a gas turbine engine
US9689571B2 (en) 2014-01-15 2017-06-27 Delavan Inc. Offset stem fuel distributor
US9618209B2 (en) * 2014-03-06 2017-04-11 Solar Turbines Incorporated Gas turbine engine fuel injector with an inner heat shield
US10252270B2 (en) * 2014-09-08 2019-04-09 Arizona Board Of Regents On Behalf Of Arizona State University Nozzle apparatus and methods for use thereof
CN104759366B (zh) * 2015-03-26 2018-01-02 安徽科创智慧知识产权服务有限公司 一种旋流雾化喷头
CN104759369B (zh) * 2015-03-26 2018-10-30 成都知融智创知识产权运营有限公司 一种蒸汽雾化喷头
US9897321B2 (en) 2015-03-31 2018-02-20 Delavan Inc. Fuel nozzles
US10385809B2 (en) 2015-03-31 2019-08-20 Delavan Inc. Fuel nozzles
US20180238548A1 (en) * 2017-02-22 2018-08-23 Delavan Inc Passive purge injectors
RU180948U1 (ru) * 2017-12-15 2018-07-02 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Форсуночный модуль камеры сгорания
US11118785B2 (en) * 2018-10-26 2021-09-14 Delavan Inc. Fuel injectors for exhaust heaters
US11014054B2 (en) 2019-04-17 2021-05-25 Delavan Inc. Fluid-gas mixer
GB2592254A (en) * 2020-02-21 2021-08-25 Rolls Royce Plc Fuel spray nozzle
US20220099290A1 (en) * 2020-09-29 2022-03-31 Parker-Hannifin Corporation Aircraft fuel nozzle

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US4170108A (en) * 1975-04-25 1979-10-09 Rolls-Royce Limited Fuel injectors for gas turbine engines
US4216652A (en) * 1978-06-08 1980-08-12 General Motors Corporation Integrated, replaceable combustor swirler and fuel injector
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UA82780C2 (uk) * 2004-05-31 2008-05-12 Телесто Сп. З О.О. Головка для створення водяного туману
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US7878000B2 (en) * 2005-12-20 2011-02-01 General Electric Company Pilot fuel injector for mixer assembly of a high pressure gas turbine engine
US7658074B2 (en) * 2006-08-31 2010-02-09 United Technologies Corporation Mid-mount centerbody heat shield for turbine engine fuel nozzle
US20090255258A1 (en) * 2008-04-11 2009-10-15 Delavan Inc Pre-filming air-blast fuel injector having a reduced hydraulic spray angle

Also Published As

Publication number Publication date
GB2458022B (en) 2012-02-22
US20090224080A1 (en) 2009-09-10
FR2928441A1 (fr) 2009-09-11
DE102009011393A1 (de) 2009-09-10
GB0903721D0 (en) 2009-04-15
US7926282B2 (en) 2011-04-19
FR2928441B1 (fr) 2016-01-29
GB2458022A (en) 2009-09-09

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Legal Events

Date Code Title Description
8196 Reprint of faulty title page (publication) german patentblatt: part 1a6
R005 Application deemed withdrawn due to failure to request examination