CN103228993B - 燃气轮机组件和为此的方法 - Google Patents

燃气轮机组件和为此的方法 Download PDF

Info

Publication number
CN103228993B
CN103228993B CN201180056506.9A CN201180056506A CN103228993B CN 103228993 B CN103228993 B CN 103228993B CN 201180056506 A CN201180056506 A CN 201180056506A CN 103228993 B CN103228993 B CN 103228993B
Authority
CN
China
Prior art keywords
sleeve
flange
air supply
supply pipe
gas
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
CN201180056506.9A
Other languages
English (en)
Chinese (zh)
Other versions
CN103228993A (zh
Inventor
A.贝彻
T.A.福克斯
D.W.加朗
T.格里布
J.克莱因菲尔德
T.克里格
S.A.拉米尔
D.M.里特兰德
M.泽霍斯特
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.)
Siemens Energy Global GmbH and Co KG
Original Assignee
Siemens Corp
Siemens Energy Inc
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 Siemens Corp, Siemens Energy Inc filed Critical Siemens Corp
Publication of CN103228993A publication Critical patent/CN103228993A/zh
Application granted granted Critical
Publication of CN103228993B publication Critical patent/CN103228993B/zh
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • 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
    • F05D2260/00—Function
    • F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
    • 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
    • F05D2260/00—Function
    • F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
    • F05D2260/941—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF] particularly aimed at mechanical or thermal stress reduction
    • 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
    • F23R2900/00005—Preventing fatigue failures or reducing mechanical stress in gas turbine components
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49229—Prime mover or fluid pump making

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)
CN201180056506.9A 2010-12-01 2011-11-30 燃气轮机组件和为此的方法 Active CN103228993B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/957,476 US20120137691A1 (en) 2010-12-01 2010-12-01 Gas turbine assembly and method therefor
US12/957,476 2010-12-01
PCT/EP2011/071340 WO2012072659A1 (en) 2010-12-01 2011-11-30 Gas turbine assembly and method therefor

Publications (2)

Publication Number Publication Date
CN103228993A CN103228993A (zh) 2013-07-31
CN103228993B true CN103228993B (zh) 2016-11-09

Family

ID=45092354

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201180056506.9A Active CN103228993B (zh) 2010-12-01 2011-11-30 燃气轮机组件和为此的方法

Country Status (5)

Country Link
US (1) US20120137691A1 (enExample)
EP (1) EP2622278B1 (enExample)
JP (1) JP5791731B2 (enExample)
CN (1) CN103228993B (enExample)
WO (1) WO2012072659A1 (enExample)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9032735B2 (en) * 2012-04-26 2015-05-19 General Electric Company Combustor and a method for assembling the combustor
US10533750B2 (en) 2014-09-05 2020-01-14 Siemens Aktiengesellschaft Cross ignition flame duct
WO2016064391A1 (en) 2014-10-23 2016-04-28 Siemens Energy, Inc. Flexible fuel combustion system for turbine engines
US11230976B2 (en) * 2017-07-14 2022-01-25 General Electric Company Integrated fuel nozzle connection

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS549310A (en) * 1977-05-11 1979-01-24 Lucas Industries Ltd Sealing arrangement for combustion assembled body
US4441323A (en) * 1981-04-16 1984-04-10 Rolls-Royce Limited Combustion equipment for a gas turbine engine including a fuel burner capable of accurate positioning and installation as a unit in a flame tube
WO2009039142A2 (en) * 2007-09-17 2009-03-26 Delavan Inc Flexure seal for fuel injection nozzle
CN101676632A (zh) * 2008-09-16 2010-03-24 通用电气公司 用于合成气燃料喷嘴的可重复使用的焊接接头
EP2189720A1 (de) * 2008-11-21 2010-05-26 Siemens Aktiengesellschaft Brenneranordnung

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04124522A (ja) * 1990-09-17 1992-04-24 Hitachi Ltd 燃焼装置の燃料供給方法、燃料供給系統および拡散燃料ノズル
JP2002350092A (ja) * 2001-05-28 2002-12-04 Kawasaki Heavy Ind Ltd 熱交換器とこれを用いたガスタービン装置
US7900456B2 (en) * 2006-05-19 2011-03-08 Delavan Inc Apparatus and method to compensate for differential thermal growth of injector components
FR2903172B1 (fr) * 2006-06-29 2008-10-17 Snecma Sa Agencement pour chambre de combustion de turbomachine ayant un defecteur a collerette
US8899010B2 (en) * 2010-11-17 2014-12-02 General Electric Company Pulse detonation combustor

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS549310A (en) * 1977-05-11 1979-01-24 Lucas Industries Ltd Sealing arrangement for combustion assembled body
US4441323A (en) * 1981-04-16 1984-04-10 Rolls-Royce Limited Combustion equipment for a gas turbine engine including a fuel burner capable of accurate positioning and installation as a unit in a flame tube
WO2009039142A2 (en) * 2007-09-17 2009-03-26 Delavan Inc Flexure seal for fuel injection nozzle
CN101676632A (zh) * 2008-09-16 2010-03-24 通用电气公司 用于合成气燃料喷嘴的可重复使用的焊接接头
EP2189720A1 (de) * 2008-11-21 2010-05-26 Siemens Aktiengesellschaft Brenneranordnung

Also Published As

Publication number Publication date
CN103228993A (zh) 2013-07-31
US20120137691A1 (en) 2012-06-07
JP5791731B2 (ja) 2015-10-07
EP2622278A1 (en) 2013-08-07
WO2012072659A1 (en) 2012-06-07
EP2622278B1 (en) 2019-05-08
JP2013544345A (ja) 2013-12-12

Similar Documents

Publication Publication Date Title
CN103017199B (zh) 燃烧器以及用于向燃烧器供给燃料的方法
CN102818288B (zh) 在燃烧衬套上的集成式迟稀薄喷射和迟稀薄喷射套管组件
JP5451344B2 (ja) 燃料ノズルの取り外し可能なバーナチューブ
JP4380855B2 (ja) トラップ渦空洞を有するガスタービンエンジン燃焼器のライナ用の冷却ナゲット
CN103201563B (zh) 脉冲爆震燃烧器
US9423134B2 (en) Bundled tube fuel injector with a multi-configuration tube tip
US9267689B2 (en) Combustor apparatus in a gas turbine engine
JP5451314B2 (ja) ガスタービンエンジンで使用する燃料ノズル組立体及びその組立法。
CN103228993B (zh) 燃气轮机组件和为此的方法
CN107191970A (zh) 燃气涡轮流套管安装
JP2018112386A (ja) ラジアル燃料インジェクタ用のエアシールドを有する燃焼器アセンブリ
JP2010071641A (ja) 燃料ノズルチップ組立体
US9500370B2 (en) Apparatus for mixing fuel in a gas turbine nozzle
CN105209723B (zh) 用于燃气涡轮发动机的中框架壳体的热屏蔽歧管系统
JP6106507B2 (ja) 燃焼器及び燃焼器の組立方法
JP2011085383A (ja) 高強度クロスオーバマニホルド及び接合方法
JP2018048630A (ja) ガスタービンエンジンの流体導管用取り付けアセンブリ
CN107152699B (zh) 套筒组件及其制造方法
US10634344B2 (en) Fuel nozzle assembly with fuel purge
US9488105B2 (en) Gas turbine assembly and method therefor
TWI588418B (zh) 燃燒器、燃氣渦輪機
US7703286B2 (en) Internal fuel manifold and fuel fairing interface
CN110366661A (zh) 用于燃烧器的端盖组件
Barker Apparatus for mixing fuel in a gas turbine nozzle

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
ASS Succession or assignment of patent right

Free format text: FORMER OWNER: SIEMENS ENERGY INC.

Effective date: 20131218

C41 Transfer of patent application or patent right or utility model
TA01 Transfer of patent application right

Effective date of registration: 20131218

Address after: Munich, Germany

Applicant after: SIEMENS AG

Address before: Munich, Germany

Applicant before: Siemens AG

Applicant before: SIEMENS ENERGY, Inc.

C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20220215

Address after: Munich, Germany

Patentee after: Siemens energy Global Ltd.

Address before: Munich, Germany

Patentee before: SIEMENS AG

CP03 Change of name, title or address
CP03 Change of name, title or address

Address after: Munich, Germany

Patentee after: Siemens Energy International

Country or region after: Germany

Address before: Munich, Germany

Patentee before: Siemens energy Global Ltd.

Country or region before: Germany