CN103216850B - 微型混合器及包括微型混合器的涡轮机系统 - Google Patents

微型混合器及包括微型混合器的涡轮机系统 Download PDF

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Publication number
CN103216850B
CN103216850B CN201310024296.6A CN201310024296A CN103216850B CN 103216850 B CN103216850 B CN 103216850B CN 201310024296 A CN201310024296 A CN 201310024296A CN 103216850 B CN103216850 B CN 103216850B
Authority
CN
China
Prior art keywords
pipeline
mixer
micro
import
plane
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 - Fee Related
Application number
CN201310024296.6A
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English (en)
Chinese (zh)
Other versions
CN103216850A (zh
Inventor
M.巴蒂娜
A.辛赫
V.纳卡尼
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.)
General Electric Co
Original Assignee
General Electric Co
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.)
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of CN103216850A publication Critical patent/CN103216850A/zh
Application granted granted Critical
Publication of CN103216850B publication Critical patent/CN103216850B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/045—Air inlet arrangements using pipes
    • 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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54—Reverse-flow combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Micromachines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CN201310024296.6A 2012-01-23 2013-01-23 微型混合器及包括微型混合器的涡轮机系统 Expired - Fee Related CN103216850B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/356183 2012-01-23
US13/356,183 US9134030B2 (en) 2012-01-23 2012-01-23 Micromixer of turbine system

Publications (2)

Publication Number Publication Date
CN103216850A CN103216850A (zh) 2013-07-24
CN103216850B true CN103216850B (zh) 2016-08-17

Family

ID=47563291

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310024296.6A Expired - Fee Related CN103216850B (zh) 2012-01-23 2013-01-23 微型混合器及包括微型混合器的涡轮机系统

Country Status (5)

Country Link
US (1) US9134030B2 (https=)
EP (1) EP2618057B1 (https=)
JP (1) JP6106441B2 (https=)
CN (1) CN103216850B (https=)
RU (1) RU2013102629A (https=)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10274200B2 (en) * 2013-10-18 2019-04-30 Mitsubishi Heavy Industries, Ltd. Fuel injector, combustor, and gas turbine
US10041681B2 (en) * 2014-08-06 2018-08-07 General Electric Company Multi-stage combustor with a linear actuator controlling a variable air bypass
US9581335B2 (en) 2014-08-07 2017-02-28 General Electric Company Fuel nozzle tube retention
US9631816B2 (en) 2014-11-26 2017-04-25 General Electric Company Bundled tube fuel nozzle
US10344982B2 (en) 2016-12-30 2019-07-09 General Electric Company Compact multi-residence time bundled tube fuel nozzle having transition portions of different lengths
US11525578B2 (en) 2017-08-16 2022-12-13 General Electric Company Dynamics-mitigating adapter for bundled tube fuel nozzle
US11434831B2 (en) 2018-05-23 2022-09-06 General Electric Company Gas turbine combustor having a plurality of angled vanes circumferentially spaced within the combustor
US11162681B2 (en) 2019-10-28 2021-11-02 King Fahd University Of Petroleum And Minerals Integrated ITM micromixer burner of shell and tube design for clean combustion in gas turbines
US12553385B2 (en) 2020-03-30 2026-02-17 Ge Vernova Infrastructure Technology Llc Compact turbomachine combustor
GB2596339B (en) * 2020-06-26 2023-03-01 Gkn Aerospace Sweden Ab Modified air bleed arrangement
KR102599921B1 (ko) * 2022-03-21 2023-11-07 두산에너빌리티 주식회사 연소기용 노즐, 연소기, 및 이를 포함하는 가스 터빈
US12379107B2 (en) 2023-12-01 2025-08-05 Doosan Enerbility Co., Ltd. Combustor nozzle, combustor and gas turbine including same
US12339007B2 (en) 2023-12-01 2025-06-24 Doosan Enerbility Co., Ltd. Combustor nozzle, combustor and gas turbine including same

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB579424A (en) * 1943-09-29 1946-08-02 Lucas Ltd Joseph Improvements relating to liquid fuel combustion apparatus for generating gases for power purposes
EP1174662A1 (en) * 2000-07-21 2002-01-23 Mitsubishi Heavy Industries, Ltd. Apparatus to reduce the vibrations of a turbine combustor
US20030167771A1 (en) * 2002-03-08 2003-09-11 National Aerospace Laboratory Of Japan Gas turbine combustor
US20040216463A1 (en) * 2003-04-30 2004-11-04 Harris Mark M. Combustor system for an expendable gas turbine engine
WO2011139309A2 (en) * 2009-12-29 2011-11-10 Rolls-Royce North American Technologies, Inc. Gas turbine engine and combustor

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4087962A (en) * 1976-07-26 1978-05-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Direct heating surface combustor
JP2865684B2 (ja) * 1989-01-06 1999-03-08 株式会社日立製作所 ガスタービン燃焼器
JPH05196232A (ja) * 1991-08-01 1993-08-06 General Electric Co <Ge> 耐逆火性燃料ステージング式予混合燃焼器
US5361586A (en) * 1993-04-15 1994-11-08 Westinghouse Electric Corporation Gas turbine ultra low NOx combustor
US8147121B2 (en) * 2008-07-09 2012-04-03 General Electric Company Pre-mixing apparatus for a turbine engine
US8209986B2 (en) * 2008-10-29 2012-07-03 General Electric Company Multi-tube thermal fuse for nozzle protection from a flame holding or flashback event
US8402763B2 (en) 2009-10-26 2013-03-26 General Electric Company Combustor headend guide vanes to reduce flow maldistribution into multi-nozzle arrangement
JP5372815B2 (ja) * 2010-03-17 2013-12-18 株式会社日立製作所 ガスタービン燃焼器
US8322143B2 (en) * 2011-01-18 2012-12-04 General Electric Company System and method for injecting fuel

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB579424A (en) * 1943-09-29 1946-08-02 Lucas Ltd Joseph Improvements relating to liquid fuel combustion apparatus for generating gases for power purposes
EP1174662A1 (en) * 2000-07-21 2002-01-23 Mitsubishi Heavy Industries, Ltd. Apparatus to reduce the vibrations of a turbine combustor
US20030167771A1 (en) * 2002-03-08 2003-09-11 National Aerospace Laboratory Of Japan Gas turbine combustor
US20040216463A1 (en) * 2003-04-30 2004-11-04 Harris Mark M. Combustor system for an expendable gas turbine engine
WO2011139309A2 (en) * 2009-12-29 2011-11-10 Rolls-Royce North American Technologies, Inc. Gas turbine engine and combustor

Also Published As

Publication number Publication date
EP2618057B1 (en) 2018-03-14
JP6106441B2 (ja) 2017-03-29
RU2013102629A (ru) 2014-07-27
US9134030B2 (en) 2015-09-15
JP2013148345A (ja) 2013-08-01
EP2618057A1 (en) 2013-07-24
US20130186092A1 (en) 2013-07-25
CN103216850A (zh) 2013-07-24

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Granted publication date: 20160817

Termination date: 20220123

CF01 Termination of patent right due to non-payment of annual fee