DE69625744T2 - Magervormischbrenner mit niedrigem NOx-Ausstoss für industrielle Gasturbinen - Google Patents

Magervormischbrenner mit niedrigem NOx-Ausstoss für industrielle Gasturbinen

Info

Publication number
DE69625744T2
DE69625744T2 DE69625744T DE69625744T DE69625744T2 DE 69625744 T2 DE69625744 T2 DE 69625744T2 DE 69625744 T DE69625744 T DE 69625744T DE 69625744 T DE69625744 T DE 69625744T DE 69625744 T2 DE69625744 T2 DE 69625744T2
Authority
DE
Germany
Prior art keywords
gas turbines
nox emissions
industrial gas
low nox
premix burner
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
DE69625744T
Other languages
English (en)
Other versions
DE69625744D1 (de
Inventor
Rahul Puri
Mohan K Razdan
Duane A Smith
David M Stansel
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.)
Rolls Royce Corp
Original Assignee
Rolls Royce Corp
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 Rolls Royce Corp filed Critical Rolls Royce Corp
Publication of DE69625744D1 publication Critical patent/DE69625744D1/de
Application granted granted Critical
Publication of DE69625744T2 publication Critical patent/DE69625744T2/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
    • F23R3/34Feeding into different combustion zones
    • F23R3/346Feeding into different combustion zones for staged combustion
    • 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
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03041Effusion cooled combustion chamber walls or domes
    • 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
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03342Arrangement of silo-type combustion chambers
    • 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
DE69625744T 1995-06-05 1996-06-05 Magervormischbrenner mit niedrigem NOx-Ausstoss für industrielle Gasturbinen Expired - Lifetime DE69625744T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US46452695A 1995-06-05 1995-06-05

Publications (2)

Publication Number Publication Date
DE69625744D1 DE69625744D1 (de) 2003-02-20
DE69625744T2 true DE69625744T2 (de) 2003-10-16

Family

ID=23844285

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69625744T Expired - Lifetime DE69625744T2 (de) 1995-06-05 1996-06-05 Magervormischbrenner mit niedrigem NOx-Ausstoss für industrielle Gasturbinen

Country Status (4)

Country Link
US (1) US6094916A (de)
EP (1) EP0747635B1 (de)
JP (1) JPH09119641A (de)
DE (1) DE69625744T2 (de)

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EP0747635A2 (de) 1996-12-11
JPH09119641A (ja) 1997-05-06
EP0747635A3 (de) 1998-09-02
DE69625744D1 (de) 2003-02-20
US6094916A (en) 2000-08-01
EP0747635B1 (de) 2003-01-15

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