CH707843A8 - System mit Vielrohr-Brennstoffdüse mit Brennstoffdüsengehäuse. - Google Patents

System mit Vielrohr-Brennstoffdüse mit Brennstoffdüsengehäuse. Download PDF

Info

Publication number
CH707843A8
CH707843A8 CH00392/14A CH3922014A CH707843A8 CH 707843 A8 CH707843 A8 CH 707843A8 CH 00392/14 A CH00392/14 A CH 00392/14A CH 3922014 A CH3922014 A CH 3922014A CH 707843 A8 CH707843 A8 CH 707843A8
Authority
CH
Switzerland
Prior art keywords
fuel nozzle
tube
fuel
wall
extending
Prior art date
Application number
CH00392/14A
Other languages
English (en)
Other versions
CH707843A2 (de
Inventor
Jason Thurman Stewart
Christopher Paul Keener
Heath Michael Ostebee
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of CH707843A2 publication Critical patent/CH707843A2/de
Publication of CH707843A8 publication Critical patent/CH707843A8/de

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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • 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
    • 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
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • 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
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00012—Details of sealing devices
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Gas Burners (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Hydrogen, Water And Hydrids (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Abstract

Ein System enthält mehrere Vielrohr-Brennstoffdüsen (94), die jeweils mehrere Rohre (192) aufweisen, die sich in einer axialen Richtung erstrecken, wobei jedes Rohr (192) von den mehreren Rohren (192) einen Lufteinlass, einen Brennstoffeinlass und einen Brennstoff-Luft-Mischungsauslass aufweist, und ein Brennstoffdüsengehäuse (56) mit einer Aussenwand (120), die sich in Umfangsrichtung um eine Mittelachse (41) erstreckt, mehreren radialen Wänden, die sich von der Aussenwand (120) nach innen zu der Mittelachse hin erstrecken, mehreren Brennstoffdüsenaufnahmen (190), die innerhalb der Aussenwand (120) angeordnet sind, wobei die mehreren radialen Wände die mehreren Brennstoffdüsenaufnahmen (190) voneinander trennen und die mehreren Vielrohr-Brennstoffdüsen (94) in den mehreren Brennstoffdüsenaufnahmen (190) angeordnet sind, einer Befestigungsstruktur, die mehrere radiale Stützarme (124) aufweist, die sich von der Aussenwand (120) nach aussen erstrecken.
CH00392/14A 2013-03-15 2014-03-14 System mit Vielrohr-Brennstoffdüse mit Brennstoffdüsengehäuse. CH707843A8 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13/838,726 US9303873B2 (en) 2013-03-15 2013-03-15 System having a multi-tube fuel nozzle with a fuel nozzle housing

Publications (2)

Publication Number Publication Date
CH707843A2 CH707843A2 (de) 2014-09-15
CH707843A8 true CH707843A8 (de) 2015-01-15

Family

ID=51419083

Family Applications (1)

Application Number Title Priority Date Filing Date
CH00392/14A CH707843A8 (de) 2013-03-15 2014-03-14 System mit Vielrohr-Brennstoffdüse mit Brennstoffdüsengehäuse.

Country Status (5)

Country Link
US (1) US9303873B2 (de)
JP (1) JP6483957B2 (de)
CN (1) CN104048323A (de)
CH (1) CH707843A8 (de)
DE (1) DE102014103085A1 (de)

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US9546789B2 (en) 2013-03-15 2017-01-17 General Electric Company System having a multi-tube fuel nozzle
US9291352B2 (en) 2013-03-15 2016-03-22 General Electric Company System having a multi-tube fuel nozzle with an inlet flow conditioner
US9316397B2 (en) 2013-03-15 2016-04-19 General Electric Company System and method for sealing a fuel nozzle
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KR102459999B1 (ko) 2021-01-13 2022-10-26 두산에너빌리티 주식회사 연소기용 노즐, 연소기, 및 이를 포함하는 가스 터빈
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CN115451432B (zh) * 2022-09-22 2024-03-12 中国联合重型燃气轮机技术有限公司 一种燃气轮机燃烧室燃料的微混喷嘴组件及系统

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US9534787B2 (en) 2013-03-12 2017-01-03 General Electric Company Micromixing cap assembly
US9528444B2 (en) 2013-03-12 2016-12-27 General Electric Company System having multi-tube fuel nozzle with floating arrangement of mixing tubes
US9784452B2 (en) 2013-03-15 2017-10-10 General Electric Company System having a multi-tube fuel nozzle with an aft plate assembly
US9316397B2 (en) 2013-03-15 2016-04-19 General Electric Company System and method for sealing a fuel nozzle
US9291352B2 (en) 2013-03-15 2016-03-22 General Electric Company System having a multi-tube fuel nozzle with an inlet flow conditioner
US9546789B2 (en) 2013-03-15 2017-01-17 General Electric Company System having a multi-tube fuel nozzle

Also Published As

Publication number Publication date
US20140338344A1 (en) 2014-11-20
DE102014103085A1 (de) 2014-09-18
US9303873B2 (en) 2016-04-05
JP2014181900A (ja) 2014-09-29
JP6483957B2 (ja) 2019-03-13
CH707843A2 (de) 2014-09-15
CN104048323A (zh) 2014-09-17

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PK Correction

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NV New agent

Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH

AZW Rejection (application)