US20160195268A1 - Burner nozzle - Google Patents

Burner nozzle Download PDF

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Publication number
US20160195268A1
US20160195268A1 US14/907,297 US201414907297A US2016195268A1 US 20160195268 A1 US20160195268 A1 US 20160195268A1 US 201414907297 A US201414907297 A US 201414907297A US 2016195268 A1 US2016195268 A1 US 2016195268A1
Authority
US
United States
Prior art keywords
outlet
passage
combustion supporting
supporting agent
fuel
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.)
Abandoned
Application number
US14/907,297
Inventor
Yu SHANDONG
Original Assignee
Liang Yu
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
Priority to CN201320446743.2 priority Critical
Priority to CN 201320446743 priority patent/CN203442826U/en
Priority to CN201310315933.5A priority patent/CN104344405A/en
Priority to CN201310315933.5 priority
Application filed by Liang Yu filed Critical Liang Yu
Priority to PCT/CN2014/082835 priority patent/WO2015010622A1/en
Publication of US20160195268A1 publication Critical patent/US20160195268A1/en
Application status is Abandoned legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/48Nozzles
    • F23D14/58Nozzles characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration
    • 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
    • F23D11/36Details, e.g. burner cooling means, noise reduction means
    • F23D11/38Nozzles; Cleaning devices therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/20Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/48Nozzles

Abstract

A burner nozzle, comprised by a fuel passage (7) and combustion supporting agent passage (2), where the combustion supporting agent passage (2) is inside fuel passage (7), the inner wall of the outer annual ring of nozzle outlet (8) and the outer wall of the combustion supporting agent passage outlet (4) comprise annular ring outlet is the fuel outlet (6). The burner nozzle can create favorable conditions for combustion.

Description

    TECHNICAL FIELD
  • The invention relates to burner nozzles.
  • BACKGROUND ART
  • Currently fuel burner nozzles are devices for fuel supply.
  • SUMMARY OF INVENTION Technical Problem
  • But their functions can not supply very favorable conditions for burning.
  • Solution to Problem
  • The present invention is used to provide a burner nozzle, which is achieved by the following technical scheme: the nozzle body has a combustion supporting agent passage and a fuel passage. The fuel passage is inside the combustion supporting agent passage. One end of the combustion supporting agent passage is the combustion supporting agent inlet, the other end of the combustion supporting agent passage is the combustion supporting agent outlet. The nozzle has a fuel inlet, the outlet of nozzle comprised by combustion supporting agent passage outlet and fuel passage outlet, of which the inner wall of the outer annular ring of nozzle outlet and outer wall of the combustion supporting agent passage outlet comprise the annular ring outlet is the fuel outlet.
  • Advantageous Effects of Invention
  • The nozzle can create favorable conditions for combustion.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a schematic diagram.
  • Of which: 1, nozzle body 2, combustion supporting agent passage 3, combustion supporting agent inlet 4, combustion supporting agent outlet 5, fuel passage inlet 6, fuel passage outlet 7, fuel passage 8, outer annular ring of the nozzle outlet.
  • DESCRIPTION OF EMBODIMENTS
  • As shown in FIG. 1, the combustion supporting agent flow through the combustion supporting agent inlet 3 into the combustion supporting agent passage 2 which is inside the nozzle body 1 and flow out from the combustion supporting agent outlet 4. The fuel flow through fuel passage inlet 5 into fuel passage 7 which is inside the nozzle body 1 and flow out from fuel passage outlet 6. The fuel passage outlet 6 is an annular ring outlet comprised by inner wall of the outer annular ring of nozzle outlet 8 and outer wall of the combustion supporting agent passage outlet 4.
  • EXAMPLES
  • As shown in FIG. 1, the combustion supporting agent flow through the combustion supporting agent inlet 3 into the combustion supporting agent passage 2 which is inside the nozzle body 1 and flow out from the combustion supporting agent outlet 4. The fuel flow through fuel passage inlet 5 into fuel passage 7 which is inside the nozzle body 1 and flow out from fuel passage outlet 6. The fuel passage outlet 6 is an annular ring outlet comprised by inner wall of the outer annular ring of nozzle outlet 8 and outer wall of the combustion supporting agent passage outlet 4. The thickness and radius of the annular ring orifice are adjustable.
  • The above is only a preferred embodiment of the present invention, but the scope of the present invention is not limited to this, the equivalent replacement or change according to the present invention and the inventive concept should be encompassed by the present invention within the scope of protection.
  • INDUSTRIAL APPLICABILITY
  • The present invention can improve combustion efficiency, while industrial application is very easy to install and maintain.

Claims (1)

1] A burner nozzle, comprised by a fuel passage (7) and combustion supporting agent passage (2), where the combustion supporting agent passage (2) is inside fuel passage (7), the inner wall of the outer annular ring of nozzle outlet (8) and the outer wall of the combustion supporting agent passage outlet (4) comprise annular ring outlet is the fuel outlet (6).
US14/907,297 2013-07-25 2014-07-23 Burner nozzle Abandoned US20160195268A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
CN201320446743.2 2013-07-25
CN 201320446743 CN203442826U (en) 2013-07-25 2013-07-25 Combustor nozzle
CN201310315933.5A CN104344405A (en) 2013-07-25 2013-07-25 Burner nozzle
CN201310315933.5 2013-07-25
PCT/CN2014/082835 WO2015010622A1 (en) 2013-07-25 2014-07-23 Burner nozzle

Publications (1)

Publication Number Publication Date
US20160195268A1 true US20160195268A1 (en) 2016-07-07

Family

ID=52392741

Family Applications (1)

Application Number Title Priority Date Filing Date
US14/907,297 Abandoned US20160195268A1 (en) 2013-07-25 2014-07-23 Burner nozzle

Country Status (4)

Country Link
US (1) US20160195268A1 (en)
EP (1) EP3026340A4 (en)
JP (1) JP2017508120A (en)
WO (1) WO2015010622A1 (en)

Citations (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1481419A (en) * 1922-05-11 1924-01-22 Davies Fuel Burners Ltd Oil-fuel burner for use in furnaces, boilers, and the like
US1729677A (en) * 1929-10-01 Gas burner
US4389243A (en) * 1979-05-11 1983-06-21 Dravo Corporation Method for the flash oxidation of metal concentrates
US4428727A (en) * 1980-07-21 1984-01-31 Klockner-Humboldt-Deutz Ag Burner for solid fuels
US5178533A (en) * 1989-10-04 1993-01-12 Enterprise Generale De Chauffage Industries Pillard Process for exploiting a burner and burners for a rotary tubular furnance
US5203692A (en) * 1990-01-29 1993-04-20 F. L. Smidth & Co. A/S Burner for solid and liquid or gaseous fuel
US5408830A (en) * 1994-02-10 1995-04-25 General Electric Company Multi-stage fuel nozzle for reducing combustion instabilities in low NOX gas turbines
US6244860B1 (en) * 1998-11-25 2001-06-12 Messer Griesheim Gmbh Apparatus and process for producing perlite
US6558614B1 (en) * 1998-08-28 2003-05-06 Voest-Alpine Industrieanlagenbau Gmbh Method for producing a metal melt and corresponding multifunction lance
US6773256B2 (en) * 2002-02-05 2004-08-10 Air Products And Chemicals, Inc. Ultra low NOx burner for process heating
US20060001952A1 (en) * 2004-07-02 2006-01-05 Liekki Oy Method and device for producing optical material, and an optical waveguide
US7165425B2 (en) * 2002-07-05 2007-01-23 Fujikura Ltd. Multi-tube burner and glass preform manufacturing method using the same
US20070254251A1 (en) * 2006-04-26 2007-11-01 Jin Cao Ultra-low NOx burner assembly
US8632621B2 (en) * 2010-07-12 2014-01-21 L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Method for melting a solid charge
US8741180B2 (en) * 2010-01-16 2014-06-03 Lurgi Gmbh Process and burner for producing synthesis gas
US9260339B2 (en) * 2008-02-27 2016-02-16 Shin-Etsu Chemical Co., Ltd. Method of fabricating an optical fiber preform and a burner therefor

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004301372A (en) * 2003-03-28 2004-10-28 Osaka Gas Co Ltd Combustion equipment
CN102399593B (en) * 2011-10-13 2014-04-02 东方电气集团东方锅炉股份有限公司 Burner used for gasifier
CN202494101U (en) * 2012-03-07 2012-10-17 广西有色再生金属有限公司 Oven combustion device of top-blown converter
CN203442826U (en) * 2013-07-25 2014-02-19 于良 Combustor nozzle

Patent Citations (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1729677A (en) * 1929-10-01 Gas burner
US1481419A (en) * 1922-05-11 1924-01-22 Davies Fuel Burners Ltd Oil-fuel burner for use in furnaces, boilers, and the like
US4389243A (en) * 1979-05-11 1983-06-21 Dravo Corporation Method for the flash oxidation of metal concentrates
US4428727A (en) * 1980-07-21 1984-01-31 Klockner-Humboldt-Deutz Ag Burner for solid fuels
US5178533A (en) * 1989-10-04 1993-01-12 Enterprise Generale De Chauffage Industries Pillard Process for exploiting a burner and burners for a rotary tubular furnance
US5203692A (en) * 1990-01-29 1993-04-20 F. L. Smidth & Co. A/S Burner for solid and liquid or gaseous fuel
US5408830A (en) * 1994-02-10 1995-04-25 General Electric Company Multi-stage fuel nozzle for reducing combustion instabilities in low NOX gas turbines
US6558614B1 (en) * 1998-08-28 2003-05-06 Voest-Alpine Industrieanlagenbau Gmbh Method for producing a metal melt and corresponding multifunction lance
US6244860B1 (en) * 1998-11-25 2001-06-12 Messer Griesheim Gmbh Apparatus and process for producing perlite
US6773256B2 (en) * 2002-02-05 2004-08-10 Air Products And Chemicals, Inc. Ultra low NOx burner for process heating
US7165425B2 (en) * 2002-07-05 2007-01-23 Fujikura Ltd. Multi-tube burner and glass preform manufacturing method using the same
US20060001952A1 (en) * 2004-07-02 2006-01-05 Liekki Oy Method and device for producing optical material, and an optical waveguide
US20070254251A1 (en) * 2006-04-26 2007-11-01 Jin Cao Ultra-low NOx burner assembly
US9260339B2 (en) * 2008-02-27 2016-02-16 Shin-Etsu Chemical Co., Ltd. Method of fabricating an optical fiber preform and a burner therefor
US8741180B2 (en) * 2010-01-16 2014-06-03 Lurgi Gmbh Process and burner for producing synthesis gas
US8632621B2 (en) * 2010-07-12 2014-01-21 L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude Method for melting a solid charge

Also Published As

Publication number Publication date
EP3026340A1 (en) 2016-06-01
JP2017508120A (en) 2017-03-23
EP3026340A4 (en) 2017-04-19
WO2015010622A1 (en) 2015-01-29

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