CH700993A8 - System mit einem Turbinentriebwerk und einem Luftstromkonditionierer. - Google Patents

System mit einem Turbinentriebwerk und einem Luftstromkonditionierer. Download PDF

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Publication number
CH700993A8
CH700993A8 CH00631/10A CH6312010A CH700993A8 CH 700993 A8 CH700993 A8 CH 700993A8 CH 00631/10 A CH00631/10 A CH 00631/10A CH 6312010 A CH6312010 A CH 6312010A CH 700993 A8 CH700993 A8 CH 700993A8
Authority
CH
Switzerland
Prior art keywords
airflow
conditioner
turbine engine
airflow conditioner
turbine combustor
Prior art date
Application number
CH00631/10A
Other languages
German (de)
English (en)
Other versions
CH700993A2 (de
Inventor
Jonathan Dwight Berry
Jason Thurman Stewart
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 CH700993A2 publication Critical patent/CH700993A2/de
Publication of CH700993A8 publication Critical patent/CH700993A8/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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • 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
    • F23M9/00—Baffles or deflectors for air or combustion products; Flame shields
    • F23M9/02—Baffles or deflectors for air or combustion products; Flame shields in air inlets

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Nozzles (AREA)
CH00631/10A 2009-05-01 2010-04-28 System mit einem Turbinentriebwerk und einem Luftstromkonditionierer. CH700993A8 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/434,505 US8234872B2 (en) 2009-05-01 2009-05-01 Turbine air flow conditioner

Publications (2)

Publication Number Publication Date
CH700993A2 CH700993A2 (de) 2010-11-15
CH700993A8 true CH700993A8 (de) 2011-01-31

Family

ID=42813871

Family Applications (1)

Application Number Title Priority Date Filing Date
CH00631/10A CH700993A8 (de) 2009-05-01 2010-04-28 System mit einem Turbinentriebwerk und einem Luftstromkonditionierer.

Country Status (5)

Country Link
US (1) US8234872B2 (enExample)
JP (1) JP5485006B2 (enExample)
CN (1) CN101876437A (enExample)
CH (1) CH700993A8 (enExample)
DE (1) DE102010016543A1 (enExample)

Families Citing this family (59)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8522555B2 (en) * 2009-05-20 2013-09-03 General Electric Company Multi-premixer fuel nozzle support system
US20110000215A1 (en) * 2009-07-01 2011-01-06 General Electric Company Combustor Can Flow Conditioner
CN102422083B (zh) * 2009-08-13 2014-07-16 三菱重工业株式会社 燃烧器
US8590311B2 (en) * 2010-04-28 2013-11-26 General Electric Company Pocketed air and fuel mixing tube
US8991187B2 (en) * 2010-10-11 2015-03-31 General Electric Company Combustor with a lean pre-nozzle fuel injection system
US9423132B2 (en) * 2010-11-09 2016-08-23 Opra Technologies B.V. Ultra low emissions gas turbine combustor
TWI429854B (zh) * 2010-12-17 2014-03-11 Grand Mate Co Ltd Detection and Compensation of Gas Safety Supply
CN103930723A (zh) * 2011-08-22 2014-07-16 马吉德·托甘 在燃气涡轮机上使用的、具有预混合的燃料和空气的切向环形燃烧器
US8899975B2 (en) 2011-11-04 2014-12-02 General Electric Company Combustor having wake air injection
US9267687B2 (en) 2011-11-04 2016-02-23 General Electric Company Combustion system having a venturi for reducing wakes in an airflow
US9033699B2 (en) * 2011-11-11 2015-05-19 General Electric Company Combustor
US8438851B1 (en) * 2012-01-03 2013-05-14 General Electric Company Combustor assembly for use in a turbine engine and methods of assembling same
US9134023B2 (en) * 2012-01-06 2015-09-15 General Electric Company Combustor and method for distributing fuel in the combustor
US20130192234A1 (en) * 2012-01-26 2013-08-01 General Electric Company Bundled multi-tube nozzle assembly
US9163839B2 (en) * 2012-03-19 2015-10-20 General Electric Company Micromixer combustion head end assembly
US9353949B2 (en) 2012-04-17 2016-05-31 Siemens Energy, Inc. Device for improved air and fuel distribution to a combustor
US9534781B2 (en) 2012-05-10 2017-01-03 General Electric Company System and method having multi-tube fuel nozzle with differential flow
US20140182304A1 (en) * 2012-12-28 2014-07-03 Exxonmobil Upstream Research Company System and method for a turbine combustor
US9631815B2 (en) * 2012-12-28 2017-04-25 General Electric Company System and method for a turbine combustor
US9803865B2 (en) 2012-12-28 2017-10-31 General Electric Company System and method for a turbine combustor
WO2014071120A2 (en) * 2012-11-02 2014-05-08 General Electric Company System and method for a turbine combustor
WO2014071123A2 (en) * 2012-11-02 2014-05-08 General Electric Company System and method for a turbine combustor
US20140123649A1 (en) * 2012-11-07 2014-05-08 Juan E. Portillo Bilbao Acoustic damping system for a combustor of a gas turbine engine
US9151503B2 (en) 2013-01-04 2015-10-06 General Electric Company Coaxial fuel supply for a micromixer
US9228747B2 (en) * 2013-03-12 2016-01-05 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9651259B2 (en) 2013-03-12 2017-05-16 General Electric Company Multi-injector micromixing system
US9534787B2 (en) 2013-03-12 2017-01-03 General Electric Company Micromixing cap assembly
US9765973B2 (en) 2013-03-12 2017-09-19 General Electric Company System and method for tube level air flow conditioning
US9528444B2 (en) 2013-03-12 2016-12-27 General Electric Company System having multi-tube fuel nozzle with floating arrangement of mixing tubes
US9671112B2 (en) 2013-03-12 2017-06-06 General Electric Company Air diffuser for a head end of a combustor
US9759425B2 (en) * 2013-03-12 2017-09-12 General Electric Company System and method having multi-tube fuel nozzle with multiple fuel injectors
US9303873B2 (en) 2013-03-15 2016-04-05 General Electric Company System having a multi-tube fuel nozzle with a fuel nozzle housing
US9784452B2 (en) 2013-03-15 2017-10-10 General Electric Company System having a multi-tube fuel nozzle with an aft plate assembly
JP6239247B2 (ja) * 2013-03-15 2017-11-29 三菱重工業株式会社 ガスタービン燃焼器
US9316397B2 (en) 2013-03-15 2016-04-19 General Electric Company System and method for sealing a fuel nozzle
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
US9739201B2 (en) 2013-05-08 2017-08-22 General Electric Company Wake reducing structure for a turbine system and method of reducing wake
US9322553B2 (en) 2013-05-08 2016-04-26 General Electric Company Wake manipulating structure for a turbine system
US9435221B2 (en) 2013-08-09 2016-09-06 General Electric Company Turbomachine airfoil positioning
EP3068975B1 (en) * 2013-11-11 2020-11-25 United Technologies Corporation Gas turbine engine component and corresponding methods of manufacturing
US20150338101A1 (en) * 2014-05-21 2015-11-26 General Electric Company Turbomachine combustor including a combustor sleeve baffle
US9803864B2 (en) * 2014-06-24 2017-10-31 General Electric Company Turbine air flow conditioner
US9964308B2 (en) * 2014-08-19 2018-05-08 General Electric Company Combustor cap assembly
US9835333B2 (en) * 2014-12-23 2017-12-05 General Electric Company System and method for utilizing cooling air within a combustor
US10139109B2 (en) 2016-01-07 2018-11-27 Siemens Energy, Inc. Can-annular combustor burner with non-uniform airflow mitigation flow conditioner
US20170226929A1 (en) * 2016-02-09 2017-08-10 General Electric Company Fuel injector covers and methods of fabricating same
JP6723768B2 (ja) * 2016-03-07 2020-07-15 三菱重工業株式会社 バーナアセンブリ、燃焼器、及びガスタービン
CN108869041B (zh) * 2017-05-12 2020-07-14 中国联合重型燃气轮机技术有限公司 用于燃气轮机的前端转向勺状件
CN107166389A (zh) * 2017-06-29 2017-09-15 佛山市豹鼎厨具设备有限公司 一种燃气炉头
US10969107B2 (en) * 2017-09-15 2021-04-06 General Electric Company Turbine engine assembly including a rotating detonation combustor
US10890329B2 (en) 2018-03-01 2021-01-12 General Electric Company Fuel injector assembly for gas turbine engine
US10935245B2 (en) 2018-11-20 2021-03-02 General Electric Company Annular concentric fuel nozzle assembly with annular depression and radial inlet ports
US11286884B2 (en) 2018-12-12 2022-03-29 General Electric Company Combustion section and fuel injector assembly for a heat engine
US11073114B2 (en) 2018-12-12 2021-07-27 General Electric Company Fuel injector assembly for a heat engine
US11156360B2 (en) 2019-02-18 2021-10-26 General Electric Company Fuel nozzle assembly
JP6841968B1 (ja) * 2020-09-04 2021-03-10 三菱パワー株式会社 ガスタービン燃焼器の多孔板、ガスタービン燃焼器及びガスタービン
CN113091093A (zh) * 2021-05-13 2021-07-09 中国联合重型燃气轮机技术有限公司 燃气轮机的空气整流罩及喷嘴
US12215866B2 (en) 2022-02-18 2025-02-04 General Electric Company Combustor for a turbine engine having a fuel-air mixer including a set of mixing passages

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0936406B1 (en) * 1998-02-10 2004-05-06 General Electric Company Burner with uniform fuel/air premixing for low emissions combustion
JP3364169B2 (ja) * 1999-06-09 2003-01-08 三菱重工業株式会社 ガスタービン及びその燃焼器
DE10050248A1 (de) * 2000-10-11 2002-04-18 Alstom Switzerland Ltd Brenner
US6438959B1 (en) * 2000-12-28 2002-08-27 General Electric Company Combustion cap with integral air diffuser and related method
US7377036B2 (en) * 2004-10-05 2008-05-27 General Electric Company Methods for tuning fuel injection assemblies for a gas turbine fuel nozzle
US8062027B2 (en) * 2005-08-11 2011-11-22 Elster Gmbh Industrial burner and method for operating an industrial burner
US7770395B2 (en) * 2006-02-27 2010-08-10 Mitsubishi Heavy Industries, Ltd. Combustor
US7762074B2 (en) * 2006-04-04 2010-07-27 Siemens Energy, Inc. Air flow conditioner for a combustor can of a gas turbine engine
US20080104961A1 (en) * 2006-11-08 2008-05-08 Ronald Scott Bunker Method and apparatus for enhanced mixing in premixing devices
US8117845B2 (en) * 2007-04-27 2012-02-21 General Electric Company Systems to facilitate reducing flashback/flame holding in combustion systems
US20100260591A1 (en) * 2007-06-08 2010-10-14 General Electric Company Spanwise split variable guide vane and related method

Also Published As

Publication number Publication date
CH700993A2 (de) 2010-11-15
DE102010016543A1 (de) 2010-11-04
US20100275601A1 (en) 2010-11-04
CN101876437A (zh) 2010-11-03
US8234872B2 (en) 2012-08-07
JP5485006B2 (ja) 2014-05-07
JP2010261706A (ja) 2010-11-18

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