DE69500969D1 - Vormischung für ein Einspritzsystem - Google Patents

Vormischung für ein Einspritzsystem

Info

Publication number
DE69500969D1
DE69500969D1 DE69500969T DE69500969T DE69500969D1 DE 69500969 D1 DE69500969 D1 DE 69500969D1 DE 69500969 T DE69500969 T DE 69500969T DE 69500969 T DE69500969 T DE 69500969T DE 69500969 D1 DE69500969 D1 DE 69500969D1
Authority
DE
Germany
Prior art keywords
premix
injection system
injection
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 - Lifetime
Application number
DE69500969T
Other languages
English (en)
Other versions
DE69500969T2 (de
Inventor
Denis Roger Henri Ansart
Patrice Andre Commaret
Etienne Simon Rene David
Michel Andre Albert Desaulty
Bruno Michel Marc Quinquenneau
Denis Sandelis
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=9460869&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE69500969(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of DE69500969D1 publication Critical patent/DE69500969D1/de
Publication of DE69500969T2 publication Critical patent/DE69500969T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F23R3/02Continuous 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
    • 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
    • F23R3/286Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • 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
    • F23R3/32Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
    • 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)
  • Spray-Type Burners (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Nozzles (AREA)
DE69500969T 1994-03-10 1995-03-08 Vormischung für ein Einspritzsystem Expired - Lifetime DE69500969T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9402750A FR2717250B1 (fr) 1994-03-10 1994-03-10 Système d'injection à prémélange.

Publications (2)

Publication Number Publication Date
DE69500969D1 true DE69500969D1 (de) 1997-12-11
DE69500969T2 DE69500969T2 (de) 1998-03-26

Family

ID=9460869

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69500969T Expired - Lifetime DE69500969T2 (de) 1994-03-10 1995-03-08 Vormischung für ein Einspritzsystem

Country Status (5)

Country Link
US (1) US5592819A (de)
EP (1) EP0671590B1 (de)
JP (1) JP3305909B2 (de)
DE (1) DE69500969T2 (de)
FR (1) FR2717250B1 (de)

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DE19547913A1 (de) * 1995-12-21 1997-06-26 Abb Research Ltd Brenner für einen Wärmeerzeuger
DE19547912A1 (de) * 1995-12-21 1997-06-26 Abb Research Ltd Brenner für einen Wärmeerzeuger
JPH09259239A (ja) * 1996-03-25 1997-10-03 Toshiba Corp Icカード用携帯端末装置
US5850732A (en) * 1997-05-13 1998-12-22 Capstone Turbine Corporation Low emissions combustion system for a gas turbine engine
FR2770283B1 (fr) * 1997-10-29 1999-11-19 Snecma Chambre de combustion pour turbomachine
US6550251B1 (en) 1997-12-18 2003-04-22 General Electric Company Venturiless swirl cup
US6453658B1 (en) 2000-02-24 2002-09-24 Capstone Turbine Corporation Multi-stage multi-plane combustion system for a gas turbine engine
DE10026122A1 (de) * 2000-05-26 2001-11-29 Abb Alstom Power Nv Brenner für einen Wärmeerzeuger
US6427446B1 (en) * 2000-09-19 2002-08-06 Power Systems Mfg., Llc Low NOx emission combustion liner with circumferentially angled film cooling holes
US6360776B1 (en) 2000-11-01 2002-03-26 Rolls-Royce Corporation Apparatus for premixing in a gas turbine engine
US6508061B2 (en) * 2001-04-25 2003-01-21 Pratt & Whitney Canada Corp Diffuser combustor
US6539721B2 (en) 2001-07-10 2003-04-01 Pratt & Whitney Canada Corp. Gas-liquid premixer
US6691515B2 (en) * 2002-03-12 2004-02-17 Rolls-Royce Corporation Dry low combustion system with means for eliminating combustion noise
US6928822B2 (en) * 2002-05-28 2005-08-16 Lytesyde, Llc Turbine engine apparatus and method
CA2537949C (en) * 2003-09-05 2011-01-11 Delavan Inc. Device for stabilizing combustion in gas turbine engines
US7093441B2 (en) * 2003-10-09 2006-08-22 United Technologies Corporation Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume
FR2875584B1 (fr) * 2004-09-23 2009-10-30 Snecma Moteurs Sa Injecteur a effervescence pour systeme aeromecanique d'injection air/carburant dans une chambre de combustion de turbomachine
JP4703250B2 (ja) * 2005-04-28 2011-06-15 ダイニチ工業株式会社 燃料電池用水素供給装置の燃焼装置
US7954325B2 (en) * 2005-12-06 2011-06-07 United Technologies Corporation Gas turbine combustor
NO325990B1 (no) * 2006-06-23 2008-09-01 Rolf B Rummelhoff Etterbrenner for gass fra gassifiseringsanlegg for trebrensel
FR2903169B1 (fr) * 2006-06-29 2011-11-11 Snecma Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
EP1975506A1 (de) * 2007-03-30 2008-10-01 Siemens Aktiengesellschaft Vorverbrennungskammer
FR2920032B1 (fr) * 2007-08-13 2014-08-22 Snecma Diffuseur d'une turbomachine
US8151716B2 (en) * 2007-09-13 2012-04-10 General Electric Company Feed injector cooling apparatus and method of assembly
FR2925146B1 (fr) * 2007-12-14 2009-12-25 Snecma Systeme d'injection d'un melange d'air et de carburant dans une chambre de combustion de turbomachine
EP2252831B1 (de) * 2008-03-07 2013-05-08 Alstom Technology Ltd Brenneranordnung sowie anwendung einer solchen brenner-anordnung
EP2257736B1 (de) * 2008-03-07 2015-11-25 Alstom Technology Ltd Verfahren zum erzeugen von heissgas
US8113000B2 (en) * 2008-09-15 2012-02-14 Siemens Energy, Inc. Flashback resistant pre-mixer assembly
CN101922735B (zh) * 2009-06-15 2013-04-24 叶民主 一种具有分隔火焰盘的涡轮发动机燃料混合室
KR20130113317A (ko) 2010-04-30 2013-10-15 클린 커런트 리미티드 파트너쉽 강화된 덕트, 블레이드 및 발전기를 가진 단방향 수력 터빈
US8850819B2 (en) * 2010-06-25 2014-10-07 United Technologies Corporation Swirler, fuel and air assembly and combustor
US20120023951A1 (en) * 2010-07-29 2012-02-02 Nishant Govindbhai Parsania Fuel nozzle with air admission shroud
US8800289B2 (en) 2010-09-08 2014-08-12 General Electric Company Apparatus and method for mixing fuel in a gas turbine nozzle
US20120198850A1 (en) * 2010-12-28 2012-08-09 Jushan Chin Gas turbine engine and fuel injection system
US8479521B2 (en) 2011-01-24 2013-07-09 United Technologies Corporation Gas turbine combustor with liner air admission holes associated with interspersed main and pilot swirler assemblies
US9958162B2 (en) 2011-01-24 2018-05-01 United Technologies Corporation Combustor assembly for a turbine engine
US9068748B2 (en) 2011-01-24 2015-06-30 United Technologies Corporation Axial stage combustor for gas turbine engines
US9010083B2 (en) 2011-02-03 2015-04-21 General Electric Company Apparatus for mixing fuel in a gas turbine
US8893500B2 (en) 2011-05-18 2014-11-25 Solar Turbines Inc. Lean direct fuel injector
US8919132B2 (en) 2011-05-18 2014-12-30 Solar Turbines Inc. Method of operating a gas turbine engine
US9506654B2 (en) 2011-08-19 2016-11-29 General Electric Company System and method for reducing combustion dynamics in a combustor
US8984887B2 (en) 2011-09-25 2015-03-24 General Electric Company Combustor and method for supplying fuel to a combustor
US8801428B2 (en) 2011-10-04 2014-08-12 General Electric Company Combustor and method for supplying fuel to a combustor
US8550809B2 (en) 2011-10-20 2013-10-08 General Electric Company Combustor and method for conditioning flow through a combustor
US9188335B2 (en) 2011-10-26 2015-11-17 General Electric Company System and method for reducing combustion dynamics and NOx in a combustor
US8894407B2 (en) 2011-11-11 2014-11-25 General Electric Company Combustor and method for supplying fuel to a combustor
US9004912B2 (en) 2011-11-11 2015-04-14 General Electric Company Combustor and method for supplying fuel to a combustor
US9033699B2 (en) 2011-11-11 2015-05-19 General Electric Company Combustor
US9182124B2 (en) 2011-12-15 2015-11-10 Solar Turbines Incorporated Gas turbine and fuel injector for the same
US9322557B2 (en) 2012-01-05 2016-04-26 General Electric Company Combustor and method for distributing fuel in the combustor
US9341376B2 (en) 2012-02-20 2016-05-17 General Electric Company Combustor and method for supplying fuel to a combustor
US9052112B2 (en) 2012-02-27 2015-06-09 General Electric Company Combustor and method for purging a combustor
US9121612B2 (en) 2012-03-01 2015-09-01 General Electric Company System and method for reducing combustion dynamics in a combustor
US8511086B1 (en) 2012-03-01 2013-08-20 General Electric Company System and method for reducing combustion dynamics in a combustor
US9366432B2 (en) 2012-05-17 2016-06-14 Capstone Turbine Corporation Multistaged lean prevaporizing premixing fuel injector
JP5991025B2 (ja) * 2012-05-22 2016-09-14 株式会社Ihi バーナ及びガスタービン燃焼器
US9249734B2 (en) 2012-07-10 2016-02-02 General Electric Company Combustor
US8904798B2 (en) 2012-07-31 2014-12-09 General Electric Company Combustor
US9441543B2 (en) 2012-11-20 2016-09-13 Niigata Power Systems Co., Ltd. Gas turbine combustor including a premixing chamber having an inner diameter enlarging portion
EP2735798B1 (de) * 2012-11-23 2020-07-29 IHI Power Systems Co., Ltd. Gasturbinenbrennkammer
US9353950B2 (en) 2012-12-10 2016-05-31 General Electric Company System for reducing combustion dynamics and NOx in a combustor
US9541292B2 (en) 2013-03-12 2017-01-10 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9127843B2 (en) * 2013-03-12 2015-09-08 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9273868B2 (en) 2013-08-06 2016-03-01 General Electric Company System for supporting bundled tube segments within a combustor
KR20160004639A (ko) * 2014-07-03 2016-01-13 한화테크윈 주식회사 연소기 어셈블리
US10184664B2 (en) 2014-08-01 2019-01-22 Capstone Turbine Corporation Fuel injector for high flame speed fuel combustion
US10145561B2 (en) 2016-09-06 2018-12-04 General Electric Company Fuel nozzle assembly with resonator
US10801726B2 (en) 2017-09-21 2020-10-13 General Electric Company Combustor mixer purge cooling structure
US11175046B2 (en) 2019-05-09 2021-11-16 General Electric Company Combustor premixer assembly including inlet lips
GB2585025A (en) * 2019-06-25 2020-12-30 Siemens Ag Combustor for a gas turbine

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DE1029195B (de) * 1955-10-01 1958-04-30 Messerschmitt Boelkow Blohm Rohrbrennkammer fuer Brennkraft-Turbinen, insbesondere Flugzeug-Brennkraft-Turbinen
US3899884A (en) * 1970-12-02 1975-08-19 Gen Electric Combustor systems
US3851466A (en) * 1973-04-12 1974-12-03 Gen Motors Corp Combustion apparatus
US3927958A (en) * 1974-10-29 1975-12-23 Gen Motors Corp Recirculating combustion apparatus
CH593457A5 (en) * 1975-08-28 1977-11-30 United Technologies Corp Gas turbine combustor having staged concentric premixing tubes - to control formation of harmful exhaust emissions
US4215535A (en) * 1978-01-19 1980-08-05 United Technologies Corporation Method and apparatus for reducing nitrous oxide emissions from combustors
FR2572463B1 (fr) * 1984-10-30 1989-01-20 Snecma Systeme d'injection a geometrie variable.
US5117636A (en) * 1990-02-05 1992-06-02 General Electric Company Low nox emission in gas turbine system
US5156002A (en) * 1990-03-05 1992-10-20 Rolf J. Mowill Low emissions gas turbine combustor

Also Published As

Publication number Publication date
EP0671590A1 (de) 1995-09-13
DE69500969T2 (de) 1998-03-26
JP3305909B2 (ja) 2002-07-24
FR2717250A1 (fr) 1995-09-15
JPH07260150A (ja) 1995-10-13
EP0671590B1 (de) 1997-11-05
US5592819A (en) 1997-01-14
FR2717250B1 (fr) 1996-04-12

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Legal Events

Date Code Title Description
8363 Opposition against the patent
8365 Fully valid after opposition proceedings
8327 Change in the person/name/address of the patent owner

Owner name: SNECMA MOTEURS, PARIS, FR

8327 Change in the person/name/address of the patent owner

Owner name: SNECMA, PARIS, FR