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FR2695191B1 - Bruleur pour propulseurs a turbines a gaz. - Google Patents

Bruleur pour propulseurs a turbines a gaz.

Info

Publication number
FR2695191B1
FR2695191B1 FR9310305A FR9310305A FR2695191B1 FR 2695191 B1 FR2695191 B1 FR 2695191B1 FR 9310305 A FR9310305 A FR 9310305A FR 9310305 A FR9310305 A FR 9310305A FR 2695191 B1 FR2695191 B1 FR 2695191B1
Authority
FR
France
Prior art keywords
burner
gas turbine
turbine propellers
propellers
gas
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
FR9310305A
Other languages
English (en)
Other versions
FR2695191A1 (fr
Inventor
Nikolaos Zarzalis
Franz Joos
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of FR2695191A1 publication Critical patent/FR2695191A1/fr
Application granted granted Critical
Publication of FR2695191B1 publication Critical patent/FR2695191B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

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
    • F23R3/10—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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
    • F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
    • F23C7/006—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes adjustable
    • 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
    • F23R3/26—Controlling the air flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
FR9310305A 1992-08-29 1993-08-27 Bruleur pour propulseurs a turbines a gaz. Expired - Fee Related FR2695191B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4228816A DE4228816C2 (de) 1992-08-29 1992-08-29 Brenner für Gasturbinentriebwerke

Publications (2)

Publication Number Publication Date
FR2695191A1 FR2695191A1 (fr) 1994-03-04
FR2695191B1 true FR2695191B1 (fr) 1996-03-22

Family

ID=6466742

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9310305A Expired - Fee Related FR2695191B1 (fr) 1992-08-29 1993-08-27 Bruleur pour propulseurs a turbines a gaz.

Country Status (4)

Country Link
US (1) US5373693A (fr)
DE (1) DE4228816C2 (fr)
FR (1) FR2695191B1 (fr)
GB (1) GB2270974B (fr)

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RU2442932C1 (ru) * 2010-06-01 2012-02-20 Общество с ограниченной ответственностью "Новые технологии" Малоэмиссионная горелка

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EP0895024B1 (fr) * 1993-07-30 2003-01-02 United Technologies Corporation Mélangeur à tourbillon pour une chambre de combustion
EP0678708B1 (fr) * 1994-04-20 1998-12-02 ROLLS-ROYCE plc Injecteur de carburant pour turbines à gaz
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DE10348604A1 (de) * 2003-10-20 2005-07-28 Rolls-Royce Deutschland Ltd & Co Kg Kraftstoffeinspritzdüse mit filmartiger Kraftstoffplatzierung
US7117678B2 (en) * 2004-04-02 2006-10-10 Pratt & Whitney Canada Corp. Fuel injector head
US7065972B2 (en) * 2004-05-21 2006-06-27 Honeywell International, Inc. Fuel-air mixing apparatus for reducing gas turbine combustor exhaust emissions
US7628019B2 (en) * 2005-03-21 2009-12-08 United Technologies Corporation Fuel injector bearing plate assembly and swirler assembly
DE102005022772A1 (de) * 2005-05-12 2007-01-11 Universität Karlsruhe Brenner mit Teilvormischung und -vorverdampfung des flüssigen Brennstoffs
US7703288B2 (en) * 2005-09-30 2010-04-27 Solar Turbines Inc. Fuel nozzle having swirler-integrated radial fuel jet
US20070074518A1 (en) * 2005-09-30 2007-04-05 Solar Turbines Incorporated Turbine engine having acoustically tuned fuel nozzle
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US20080280238A1 (en) * 2007-05-07 2008-11-13 Caterpillar Inc. Low swirl injector and method for low-nox combustor
DE102007025051B4 (de) * 2007-05-29 2011-06-01 Hitachi Power Europe Gmbh Hüttengasbrenner
DE102007043626A1 (de) 2007-09-13 2009-03-19 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenmagerbrenner mit Kraftstoffdüse mit kontrollierter Kraftstoffinhomogenität
EP2312215A1 (fr) * 2008-10-01 2011-04-20 Siemens Aktiengesellschaft Brûleur et procédé de fonctionnement d'un brûleur
US8215116B2 (en) * 2008-10-02 2012-07-10 General Electric Company System and method for air-fuel mixing in gas turbines
US20100175380A1 (en) * 2009-01-13 2010-07-15 General Electric Company Traversing fuel nozzles in cap-less combustor assembly
US8689563B2 (en) * 2009-07-13 2014-04-08 United Technologies Corporation Fuel nozzle guide plate mistake proofing
US8365534B2 (en) 2011-03-15 2013-02-05 General Electric Company Gas turbine combustor having a fuel nozzle for flame anchoring
RU2011115528A (ru) 2011-04-21 2012-10-27 Дженерал Электрик Компани (US) Топливная форсунка, камера сгорания и способ работы камеры сгорания
US9134023B2 (en) * 2012-01-06 2015-09-15 General Electric Company Combustor and method for distributing fuel in the combustor
CN105899878B (zh) * 2013-06-18 2018-11-13 伍德沃德有限公司 燃气涡轮燃烧室组件及发动机及相关联的操作方法
US9482433B2 (en) 2013-11-11 2016-11-01 Woodward, Inc. Multi-swirler fuel/air mixer with centralized fuel injection
US9587833B2 (en) 2014-01-29 2017-03-07 Woodward, Inc. Combustor with staged, axially offset combustion
EP3062019B1 (fr) * 2015-02-27 2018-11-21 Ansaldo Energia Switzerland AG Procédé et dispositif de stabilisation de flamme dans un brûleur d'un moteur à combustion stationnaire
RU173463U1 (ru) * 2017-02-14 2017-08-29 Публичное акционерное общество "Научно-производственное объединение "Сатурн" Топливовоздушная горелка камеры сгорания газотурбинного двигателя
CN108731029B (zh) 2017-04-25 2021-10-29 帕克-汉尼芬公司 喷气燃料喷嘴
DE102017120370B4 (de) * 2017-09-05 2019-06-06 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennerkopf, Brennersystem und Verfahren zum Betreiben des Brennersystems
US10890329B2 (en) 2018-03-01 2021-01-12 General Electric Company Fuel injector assembly for gas turbine engine
US10935245B2 (en) 2018-11-20 2021-03-02 General Electric Company Annular concentric fuel nozzle assembly with annular depression and radial inlet ports
US11073114B2 (en) 2018-12-12 2021-07-27 General Electric Company Fuel injector assembly for a heat engine
US11286884B2 (en) 2018-12-12 2022-03-29 General Electric Company Combustion section and fuel injector assembly for a heat engine
US11156360B2 (en) 2019-02-18 2021-10-26 General Electric Company Fuel nozzle assembly
US11378275B2 (en) * 2019-12-06 2022-07-05 Raytheon Technologies Corporation High shear swirler with recessed fuel filmer for a gas turbine engine
CN114321978B (zh) * 2021-11-29 2022-10-21 南京航空航天大学 一种扩压器出口流量分配智能调节系统及调节方法
US12123592B2 (en) * 2022-01-12 2024-10-22 General Electric Company Fuel nozzle and swirler
US12215866B2 (en) 2022-02-18 2025-02-04 General Electric Company Combustor for a turbine engine having a fuel-air mixer including a set of mixing passages
US12007115B1 (en) * 2023-02-28 2024-06-11 Rtx Corporation High shear swirler for gas turbine engine
FR3146493B1 (fr) * 2023-03-09 2025-02-28 Safran Aircraft Engines Ensemble pour turbomachine et turbomachine associee

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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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2442932C1 (ru) * 2010-06-01 2012-02-20 Общество с ограниченной ответственностью "Новые технологии" Малоэмиссионная горелка

Also Published As

Publication number Publication date
GB9317914D0 (en) 1993-10-13
DE4228816A1 (de) 1994-03-03
DE4228816C2 (de) 1998-08-06
US5373693A (en) 1994-12-20
FR2695191A1 (fr) 1994-03-04
GB2270974A (en) 1994-03-30
GB2270974B (en) 1995-11-22

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20080430