NO164501C - Hybridbrenner til forblandingsdrift med gass og/eller olje, saerlig for gassturbinanlegg. - Google Patents

Hybridbrenner til forblandingsdrift med gass og/eller olje, saerlig for gassturbinanlegg.

Info

Publication number
NO164501C
NO164501C NO880328A NO880328A NO164501C NO 164501 C NO164501 C NO 164501C NO 880328 A NO880328 A NO 880328A NO 880328 A NO880328 A NO 880328A NO 164501 C NO164501 C NO 164501C
Authority
NO
Norway
Prior art keywords
gas
special
oil
turbin
hybrid burner
Prior art date
Application number
NO880328A
Other languages
English (en)
Other versions
NO164501B (no
NO880328D0 (no
NO880328L (no
Inventor
Helmut Maghon
Original Assignee
Siemens Ag
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 Siemens Ag filed Critical Siemens Ag
Publication of NO880328D0 publication Critical patent/NO880328D0/no
Publication of NO880328L publication Critical patent/NO880328L/no
Publication of NO164501B publication Critical patent/NO164501B/no
Publication of NO164501C publication Critical patent/NO164501C/no

Links

Classifications

    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F23D17/002—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L7/00—Supplying non-combustible liquids or gases, other than air, to the fire, e.g. oxygen, steam
    • 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
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/36—Supply of different fuels

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Hydrogen, Water And Hydrids (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
NO880328A 1987-01-26 1988-01-26 Hybridbrenner til forblandingsdrift med gass og/eller olje, saerlig for gassturbinanlegg. NO164501C (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3702181 1987-01-26

Publications (4)

Publication Number Publication Date
NO880328D0 NO880328D0 (no) 1988-01-26
NO880328L NO880328L (no) 1988-07-27
NO164501B NO164501B (no) 1990-07-02
NO164501C true NO164501C (no) 1990-10-10

Family

ID=6319538

Family Applications (1)

Application Number Title Priority Date Filing Date
NO880328A NO164501C (no) 1987-01-26 1988-01-26 Hybridbrenner til forblandingsdrift med gass og/eller olje, saerlig for gassturbinanlegg.

Country Status (5)

Country Link
US (1) US5062792A (no)
EP (1) EP0276696B1 (no)
JP (1) JPH0735886B2 (no)
DE (1) DE3860569D1 (no)
NO (1) NO164501C (no)

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US6460344B1 (en) 1999-05-07 2002-10-08 Parker-Hannifin Corporation Fuel atomization method for turbine combustion engines having aerodynamic turning vanes
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US6367262B1 (en) * 2000-09-29 2002-04-09 General Electric Company Multiple annular swirler
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EP1659339A1 (de) * 2004-11-18 2006-05-24 Siemens Aktiengesellschaft Verfahren zum Anfahren eines Brenners
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JP5172468B2 (ja) * 2008-05-23 2013-03-27 川崎重工業株式会社 燃焼装置および燃焼装置の制御方法
EP2312215A1 (de) * 2008-10-01 2011-04-20 Siemens Aktiengesellschaft Brenner und Verfahren zum Betrieb eines Brenners
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US9366432B2 (en) 2012-05-17 2016-06-14 Capstone Turbine Corporation Multistaged lean prevaporizing premixing fuel injector
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WO2014137412A1 (en) * 2013-03-05 2014-09-12 Rolls-Royce Corporation Gas turbine engine fuel air mixer
US9772054B2 (en) 2013-03-15 2017-09-26 Parker-Hannifin Corporation Concentric flexible hose assembly
WO2015076883A2 (en) * 2013-08-30 2015-05-28 United Technologies Corporation Dual fuel nozzle with swirling axial gas injection for a gas turbine engine
US10184664B2 (en) 2014-08-01 2019-01-22 Capstone Turbine Corporation Fuel injector for high flame speed fuel combustion
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CN106524155B (zh) * 2016-11-28 2018-06-05 无锡市莱达热工工程有限公司 低压涡流式烧嘴
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Also Published As

Publication number Publication date
JPS63194114A (ja) 1988-08-11
NO164501B (no) 1990-07-02
US5062792A (en) 1991-11-05
DE3860569D1 (de) 1990-10-18
EP0276696A2 (de) 1988-08-03
JPH0735886B2 (ja) 1995-04-19
EP0276696A3 (en) 1989-04-05
NO880328D0 (no) 1988-01-26
NO880328L (no) 1988-07-27
EP0276696B1 (de) 1990-09-12

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