DE112016002108B4 - Brennkammer und Gasturbine - Google Patents

Brennkammer und Gasturbine Download PDF

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Publication number
DE112016002108B4
DE112016002108B4 DE112016002108.9T DE112016002108T DE112016002108B4 DE 112016002108 B4 DE112016002108 B4 DE 112016002108B4 DE 112016002108 T DE112016002108 T DE 112016002108T DE 112016002108 B4 DE112016002108 B4 DE 112016002108B4
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DE
Germany
Prior art keywords
combustion chamber
acoustic device
wall
opening
space
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.)
Active
Application number
DE112016002108.9T
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German (de)
English (en)
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DE112016002108T5 (de
Inventor
Wataru Kugimiya
Taiki Kinoshita
Atsushi Koyama
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.)
Mitsubishi Power Ltd
Original Assignee
Mitsubishi Hitachi Power Systems Ltd
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
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Publication of DE112016002108T5 publication Critical patent/DE112016002108T5/de
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Publication of DE112016002108B4 publication Critical patent/DE112016002108B4/de
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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
    • F23R3/002—Wall structures
    • 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
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • 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
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • G—PHYSICS
    • G10—MUSICAL INSTRUMENTS; ACOUSTICS
    • G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
    • G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
    • G10K11/162—Selection of materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/35—Combustors or associated equipment
    • 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
    • F23R2900/00013—Reducing thermo-acoustic vibrations by active means
    • 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
    • F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Multimedia (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
DE112016002108.9T 2015-07-08 2016-07-06 Brennkammer und Gasturbine Active DE112016002108B4 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2015-137077 2015-07-08
JP2015137077A JP6579834B2 (ja) 2015-07-08 2015-07-08 燃焼器及びガスタービン
PCT/JP2016/070051 WO2017006971A1 (ja) 2015-07-08 2016-07-06 燃焼器及びガスタービン

Publications (2)

Publication Number Publication Date
DE112016002108T5 DE112016002108T5 (de) 2018-03-08
DE112016002108B4 true DE112016002108B4 (de) 2021-02-04

Family

ID=57685119

Family Applications (1)

Application Number Title Priority Date Filing Date
DE112016002108.9T Active DE112016002108B4 (de) 2015-07-08 2016-07-06 Brennkammer und Gasturbine

Country Status (6)

Country Link
US (1) US10712004B2 (enExample)
JP (1) JP6579834B2 (enExample)
KR (1) KR102055493B1 (enExample)
CN (1) CN107407484B (enExample)
DE (1) DE112016002108B4 (enExample)
WO (1) WO2017006971A1 (enExample)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10670271B2 (en) * 2016-09-30 2020-06-02 DOOSAN Heavy Industries Construction Co., LTD Acoustic dampening liner cap and gas turbine combustor including the same
CN110446829B (zh) * 2017-03-30 2021-07-06 西门子股份公司 具有用于双重利用燃气涡轮发动机的燃烧器部段中的冷却流体的导管布置结构的系统
WO2019018673A1 (en) * 2017-07-20 2019-01-24 President And Fellows Of Harvard College ACOUSTICAL SHOCK ABSORBER FOR ORTHOGONAL SLOT GAS TURBINE COMBUSTION CHAMBERS
JP7289752B2 (ja) 2019-08-01 2023-06-12 三菱重工業株式会社 音響減衰器、筒アッセンブリ、燃焼器、ガスタービン及び筒アッセンブリの製造方法
JP7262364B2 (ja) 2019-10-17 2023-04-21 三菱重工業株式会社 ガスタービン燃焼器
CN114502883B (zh) 2019-12-24 2023-08-11 三菱重工业株式会社 燃烧器部件、具备该燃烧器部件的燃烧器及具备该燃烧器的燃气轮机
JP7393262B2 (ja) * 2020-03-23 2023-12-06 三菱重工業株式会社 燃焼器、及びこれを備えるガスタービン
JP6980144B1 (ja) * 2021-03-24 2021-12-15 三菱パワー株式会社 ガスタービン用燃焼器、ガスタービン及びガスタービンの組立方法
JP2023158415A (ja) * 2022-04-18 2023-10-30 三菱重工業株式会社 燃焼器、及びこれを備えるガスタービン
US20240003543A1 (en) * 2022-06-29 2024-01-04 General Electric Company Acoustic liner for a gas turbine engine
CN120418590A (zh) * 2023-02-22 2025-08-01 三菱重工业株式会社 燃烧器用筒体、燃烧器及燃气轮机
GB2632877A (en) * 2023-08-14 2025-02-26 Siemens Energy Global Gmbh & Co Kg Combustor with resonator for gas turbine engine
CN119042669A (zh) * 2024-07-29 2024-11-29 北京航空航天大学 燃烧室及燃烧室中吸声结构的参数确定方法、装置和设备

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050034918A1 (en) * 2003-08-15 2005-02-17 Siemens Westinghouse Power Corporation High frequency dynamics resonator assembly
JP2009097841A (ja) * 2007-10-19 2009-05-07 Mitsubishi Heavy Ind Ltd ガスタービン
US20110220433A1 (en) * 2009-02-27 2011-09-15 Mitsubishi Heavy Industries, Ltd. Combustor and gas turbine having the same
US20150020498A1 (en) * 2013-07-19 2015-01-22 Reinhard Schilp Cooling cover for gas turbine damping resonator
US20150059345A1 (en) * 2012-03-21 2015-03-05 Alstom Technology Ltd Simultaneous broadband damping at multiple locations in a combustion chamber

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10243884A1 (de) 2002-09-21 2004-04-01 Mann + Hummel Gmbh Resonatorschalldämpfer
JP2008121961A (ja) 2006-11-10 2008-05-29 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器用の音響ライナー
US8789372B2 (en) * 2009-07-08 2014-07-29 General Electric Company Injector with integrated resonator
US8413443B2 (en) * 2009-12-15 2013-04-09 Siemens Energy, Inc. Flow control through a resonator system of gas turbine combustor
EP2385303A1 (en) * 2010-05-03 2011-11-09 Alstom Technology Ltd Combustion Device for a Gas Turbine
EP2690365B1 (en) 2011-03-22 2015-12-30 Mitsubishi Heavy Industries, Ltd. Acoustic damper, combustor, and gas turbine
US9163837B2 (en) * 2013-02-27 2015-10-20 Siemens Aktiengesellschaft Flow conditioner in a combustor of a gas turbine engine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050034918A1 (en) * 2003-08-15 2005-02-17 Siemens Westinghouse Power Corporation High frequency dynamics resonator assembly
JP2009097841A (ja) * 2007-10-19 2009-05-07 Mitsubishi Heavy Ind Ltd ガスタービン
US20110220433A1 (en) * 2009-02-27 2011-09-15 Mitsubishi Heavy Industries, Ltd. Combustor and gas turbine having the same
US20150059345A1 (en) * 2012-03-21 2015-03-05 Alstom Technology Ltd Simultaneous broadband damping at multiple locations in a combustion chamber
US20150020498A1 (en) * 2013-07-19 2015-01-22 Reinhard Schilp Cooling cover for gas turbine damping resonator

Also Published As

Publication number Publication date
CN107407484A (zh) 2017-11-28
US20180180288A1 (en) 2018-06-28
WO2017006971A1 (ja) 2017-01-12
US10712004B2 (en) 2020-07-14
JP2017020682A (ja) 2017-01-26
JP6579834B2 (ja) 2019-09-25
CN107407484B (zh) 2019-12-03
KR20180008687A (ko) 2018-01-24
DE112016002108T5 (de) 2018-03-08
KR102055493B1 (ko) 2019-12-12

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Owner name: MITSUBISHI POWER, LTD., YOKOHAMA-SHI, JP

Free format text: FORMER OWNER: MITSUBISHI HITACHI POWER SYSTEMS, LTD., YOKOHAMA-SHI, KANAGAWA-KEN, JP

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Representative=s name: HENKEL & PARTNER MBB PATENTANWALTSKANZLEI, REC, DE

R020 Patent grant now final