EP1224422A1 - LUFT GESTUFTER BRENNER MIT NIEDRIGEM NOx-AUSSTOSS - Google Patents

LUFT GESTUFTER BRENNER MIT NIEDRIGEM NOx-AUSSTOSS

Info

Publication number
EP1224422A1
EP1224422A1 EP00989709A EP00989709A EP1224422A1 EP 1224422 A1 EP1224422 A1 EP 1224422A1 EP 00989709 A EP00989709 A EP 00989709A EP 00989709 A EP00989709 A EP 00989709A EP 1224422 A1 EP1224422 A1 EP 1224422A1
Authority
EP
European Patent Office
Prior art keywords
air
burner
secondary air
fuel
nox
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Withdrawn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
EP00989709A
Other languages
English (en)
French (fr)
Inventor
Stephen P. Pisano
Anthony G. Fennell
John R. Hemmerlin
Glenn W. Baggley
John C. Dormire
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.)
Bloom Engineering Co Inc
Original Assignee
Bloom Engineering Co 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 Bloom Engineering Co Inc filed Critical Bloom Engineering Co Inc
Publication of EP1224422A1 publication Critical patent/EP1224422A1/de
Withdrawn legal-status Critical Current

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
    • 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 
    • F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
    • F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
    • F23C6/045—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure
    • 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
    • F23C7/02—Disposition of air supply not passing through burner
    • F23C7/06—Disposition of air supply not passing through burner for heating the incoming air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • F23M5/02—Casings; Linings; Walls characterised by the shape of the bricks or blocks used
    • F23M5/025—Casings; Linings; Walls characterised by the shape of the bricks or blocks used specially adapted for burner openings
    • 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 
    • F23C2201/00—Staged combustion
    • F23C2201/20—Burner staging
    • 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 
    • F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
    • F23C2900/06041—Staged supply of oxidant

Definitions

  • the present invention relates to low-NOx burners, and, in particular, to
  • Oxides of nitrogen (NOx) are produced from the burning of fuels during
  • primary air is provided in an amount that
  • the secondary air is introduced in a
  • the present invention uses staged air combustion to reduce the production
  • invention also includes a fuel passageway connecting a fuel source to a burner throat.
  • Primary air jets are connected to an air source and inject air into a primary combustion
  • This primary combustion region is in the burner throat.
  • the primary air jets can be
  • a dish surface is located in the port block; the dish surface extending in an
  • the present invention utilizes secondary air jets connected to an air source.
  • secondary air jets extend through the port block and inject secondary air into a secondary
  • combustion region located downstream from the primary combustion region.
  • the present invention also includes a method of reducing NOx emissions
  • Fuel is fed into the burner and proceeds to the throat
  • Air is introduced into the secondary
  • Fig. 1 is a side view of a single stage burner design according to the prior
  • Fig. 2 is a side view of a first embodiment according to the present
  • Fig. 3 is a side view of a second embodiment according to the present
  • Fig. 4 is a side view of a third embodiment according to the present
  • Fig. 5 is a front view of the present invention illustrating a secondary air
  • Fig. 6 is a front view of the present invention illustrating a further
  • FIG. 7 is a front view of the present invention illustrating a still further
  • Fig. 8 is a side view of the present invention illustrating the use of
  • Fig. 9 is a front view of the present invention illustrating a swirling
  • Fig. 10 is a side view of the present invention illustrating a two direction
  • Fig. 11 is a table illustrating the NOx emissions of the present invention
  • Fig. 12 is a side view of a further embodiment according to the present
  • a typical prior art burner includes a burner
  • passageway 14 may have an optional heat storing media 18 area, depending upon the
  • Fuel is introduced into the fuel passageway 12, which directs the fuel
  • combustion air enters through an air entrance 16, runs through the air passageway 14 and
  • the burner body 10 is fixed to
  • a port block 42 The fuel and air initially mix in a burner throat 40 of the burner.
  • Combustion occurs in the burner throat 40 and continues into cup 26 and from these to
  • the present invention is an apparatus and method directed to an air-staged
  • the first embodiment is illustrated in Fig. 2.
  • the air flows through the air passageway 14 and is split into primary air (i.e., the first air to be introduced to the fuel), which exits through the primary air jets
  • Fig. 9 preferable angular orientation of the primary air jets 20 is illustrated in Fig. 9.
  • the combustion process is initiated by spark, pilot flame or another
  • combustion occurs in the primary combustion region 24.
  • the fuel-rich condition allows the combustion
  • the dish surface 28 extends in
  • angle of divergence between the dish surface 28 and centerline 35 may be between
  • the dish surface 28 may have a continuously
  • trumpet-like shaped dish surface 28 of Fig. 12 still allows for the required Coanda effect
  • these secondary air jets 34 are oriented in a divergent manner.
  • the secondary air jets 34 are divergent with respect to the
  • divergence ⁇ between the secondary air jets 34 and centerline 35 may be between 1° and
  • burner throat 40 as well as the fuel passageway 12 extend perpendicularly to the port block 42 in a normal burner configuration.
  • the primary air jets 20 and the secondary air jets 34 are controlled as to
  • the air split ratio be within the limits of 40/60 (primary air/secondary
  • FIG. 3 Another embodiment of the present invention is illustrated in Fig. 3. This
  • the secondary air jets 34 open at a hot face 30 in a divergent
  • the third embodiment of the present invention is illustrated in Fig. 4.
  • the secondary air jets 34 enter the hot face 30 in an
  • the air may be supplied through
  • the secondary air jets 34 can be supplied through a different air source.
  • a secondary air inlet 46 can be utilized, allowing secondary air to flow through
  • each of the secondary air jets 34 may have
  • Fig. 5 shows a first
  • FIG. 6 shows a second secondary air jet configuration, using four
  • FIG. 7 shows a third
  • air jets 34 used, and their relative location, can vary.
  • the preferred arrangement is with
  • FIG. 10 Another arrangement for adjusting flame stability is seen in Fig. 10.
  • the swirling effect in the burner throat 40 could be any swirling effect in the burner throat 40
EP00989709A 1999-10-27 2000-10-26 LUFT GESTUFTER BRENNER MIT NIEDRIGEM NOx-AUSSTOSS Withdrawn EP1224422A1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US16201899P 1999-10-27 1999-10-27
US162018P 1999-10-27
PCT/US2000/041596 WO2001035022A1 (en) 1999-10-27 2000-10-26 AIR STAGED LOW-NOx BURNER

Publications (1)

Publication Number Publication Date
EP1224422A1 true EP1224422A1 (de) 2002-07-24

Family

ID=22583815

Family Applications (1)

Application Number Title Priority Date Filing Date
EP00989709A Withdrawn EP1224422A1 (de) 1999-10-27 2000-10-26 LUFT GESTUFTER BRENNER MIT NIEDRIGEM NOx-AUSSTOSS

Country Status (4)

Country Link
EP (1) EP1224422A1 (de)
CZ (1) CZ20021421A3 (de)
RU (1) RU2242674C2 (de)
WO (1) WO2001035022A1 (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004333073A (ja) * 2003-05-12 2004-11-25 Chugai Ro Co Ltd 燃焼装置
US7163392B2 (en) 2003-09-05 2007-01-16 Feese James J Three stage low NOx burner and method
US8485813B2 (en) 2008-01-11 2013-07-16 Hauck Manufacturing Company Three stage low NOx burner system with controlled stage air separation
US7874157B2 (en) * 2008-06-05 2011-01-25 General Electric Company Coanda pilot nozzle for low emission combustors
US8176739B2 (en) 2008-07-17 2012-05-15 General Electric Company Coanda injection system for axially staged low emission combustors
US8769955B2 (en) * 2010-06-02 2014-07-08 Siemens Energy, Inc. Self-regulating fuel staging port for turbine combustor
US20130244187A1 (en) * 2012-03-19 2013-09-19 Honeywell International Inc. HIGH EFFICIENCY LOW NOx EMISSION BURNER APPARATUS
CN104633658B (zh) * 2015-02-15 2016-11-02 重庆赛迪热工环保工程技术有限公司 一种低氧化氮烧嘴

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4004875A (en) 1975-01-23 1977-01-25 John Zink Company Low nox burner
JPS5414028A (en) * 1977-07-01 1979-02-01 Chugai Ro Kogyo Kaisha Ltd Low nox burner
US4347052A (en) 1978-06-19 1982-08-31 John Zink Company Low NOX burner
EP0124146A1 (de) * 1983-03-30 1984-11-07 Shell Internationale Researchmaatschappij B.V. Verfahren und Gerät zum Verbrennen von Brennstoff mit niedriger NOx-, Russ- und Teilchenemission
US4983118A (en) 1988-03-16 1991-01-08 Bloom Engineering Company, Inc. Low NOx regenerative burner
DE4130922C2 (de) * 1991-09-17 2001-02-08 Gaswaerme Inst Ev Brenner für Hochtemperaturprozesse sowie Verfahren zum Betreiben des Brenners
GB2283311B (en) * 1993-10-07 1997-11-05 Stordy Combustion Eng Burner and method of burning a fuel
DE69521707T2 (de) * 1995-11-14 2002-05-08 Pillard Chauffage Brenner für flüssigen oder gasförmigen Brennstoff mit sehr niedriger Stickoxidemission
GB9709205D0 (en) * 1997-05-07 1997-06-25 Boc Group Plc Oxy/oil swirl burner

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO0135022A1 *

Also Published As

Publication number Publication date
RU2242674C2 (ru) 2004-12-20
WO2001035022A1 (en) 2001-05-17
CZ20021421A3 (cs) 2003-01-15

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