JPS629157A - 衝突冷却装置 - Google Patents

衝突冷却装置

Info

Publication number
JPS629157A
JPS629157A JP10690486A JP10690486A JPS629157A JP S629157 A JPS629157 A JP S629157A JP 10690486 A JP10690486 A JP 10690486A JP 10690486 A JP10690486 A JP 10690486A JP S629157 A JPS629157 A JP S629157A
Authority
JP
Japan
Prior art keywords
impingement
cooling device
air
impingement cooling
combustor
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.)
Granted
Application number
JP10690486A
Other languages
English (en)
Japanese (ja)
Other versions
JPH0524337B2 (no
Inventor
レウィス・バークレイ・ディビス,ジュニア
ウォルター・ウォールズ・グッドウィン
チャールズ・イブン・ステバー
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.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=24950020&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=JPS629157(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by General Electric Co filed Critical General Electric Co
Publication of JPS629157A publication Critical patent/JPS629157A/ja
Publication of JPH0524337B2 publication Critical patent/JPH0524337B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08Cooling; Heating; Heat-insulation
    • F01D25/12Cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/201Heat transfer, e.g. cooling by impingement of a fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/202Heat transfer, e.g. cooling by film cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03044Impingement cooled combustion chamber walls or subassemblies

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Devices That Are Associated With Refrigeration Equipment (AREA)
  • Heat Treatments In General, Especially Conveying And Cooling (AREA)
JP10690486A 1985-05-14 1986-05-12 衝突冷却装置 Granted JPS629157A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US73401885A 1985-05-14 1985-05-14
US734018 1985-05-14

Publications (2)

Publication Number Publication Date
JPS629157A true JPS629157A (ja) 1987-01-17
JPH0524337B2 JPH0524337B2 (no) 1993-04-07

Family

ID=24950020

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10690486A Granted JPS629157A (ja) 1985-05-14 1986-05-12 衝突冷却装置

Country Status (6)

Country Link
EP (1) EP0203431B2 (no)
JP (1) JPS629157A (no)
AU (1) AU593551B2 (no)
CA (1) CA1263243A (no)
DE (1) DE3675690D1 (no)
NO (1) NO162887C (no)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0275819A (ja) * 1988-08-17 1990-03-15 Rolls Royce Plc ガスタービンエンジンの燃焼室
JP2002155759A (ja) * 2000-11-20 2002-05-31 General Electric Co <Ge> 衝突冷却遷移ダクトの側板冷却を強化する空力装置及び関連方法
JP2007292451A (ja) * 2006-04-24 2007-11-08 General Electric Co <Ge> ガスタービンエンジンの圧力損失を減少するシステム
JP2008267799A (ja) * 2007-04-17 2008-11-06 General Electric Co <Ge> 燃焼器圧力降下の低減を促進する方法及び装置
JP2011027403A (ja) * 2009-07-24 2011-02-10 General Electric Co <Ge> ガスタービン燃焼器のためのシステム及び方法
JP2011179812A (ja) * 2010-03-02 2011-09-15 General Electric Co <Ge> 燃焼器空気流スリーブ内の角度付き静翼
JP2011207755A (ja) * 2010-03-30 2011-10-20 General Electric Co <Ge> 流体被冷却改質器および改質器を冷却するための方法
JP2011220335A (ja) * 2010-04-08 2011-11-04 General Electric Co <Ge> 流れスリーブを有する燃焼器
JP2011226481A (ja) * 2010-04-19 2011-11-10 General Electric Co <Ge> トランジションダクト界面における燃焼器ライナ冷却及びその関連する方法
JP2013213492A (ja) * 2012-04-03 2013-10-17 General Electric Co <Ge> 移行ノズル燃焼システム
JP2013234833A (ja) * 2012-05-02 2013-11-21 General Electric Co <Ge> ガスタービン燃焼器のフロースリーブに配置される音響共鳴器

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5157188A (en) * 1985-03-19 1992-10-20 Phillips Petroleum Company Methane conversion
JPH0752014B2 (ja) * 1986-03-20 1995-06-05 株式会社日立製作所 ガスタ−ビン燃焼器
US4984429A (en) * 1986-11-25 1991-01-15 General Electric Company Impingement cooled liner for dry low NOx venturi combustor
CA1309873C (en) * 1987-04-01 1992-11-10 Graham P. Butt Gas turbine combustor transition duct forced convection cooling
DE4239856A1 (de) * 1992-11-27 1994-06-01 Asea Brown Boveri Gasturbinenbrennkammer
FR2714154B1 (fr) * 1993-12-22 1996-01-19 Snecma Chambre de combustion comportant une paroi munie d'une multiperforation.
DE19720786A1 (de) * 1997-05-17 1998-11-19 Abb Research Ltd Brennkammer
GB2328011A (en) * 1997-08-05 1999-02-10 Europ Gas Turbines Ltd Combustor for gas or liquid fuelled turbine
DE60137099D1 (de) * 2000-04-13 2009-02-05 Mitsubishi Heavy Ind Ltd Kühlstruktur für das Endstück einer Gasturbinenbrennkammer
DE10064264B4 (de) 2000-12-22 2017-03-23 General Electric Technology Gmbh Anordnung zur Kühlung eines Bauteils
US7010921B2 (en) * 2004-06-01 2006-03-14 General Electric Company Method and apparatus for cooling combustor liner and transition piece of a gas turbine
EP1650503A1 (en) * 2004-10-25 2006-04-26 Siemens Aktiengesellschaft Method for cooling a heat shield element and a heat shield element
WO2009103636A1 (de) * 2008-02-20 2009-08-27 Alstom Technology Ltd. Thermische maschine
EP2738469B1 (en) * 2012-11-30 2019-04-17 Ansaldo Energia IP UK Limited Combustor part of a gas turbine comprising a near wall cooling arrangement
US10415478B2 (en) 2015-01-20 2019-09-17 United Technologies Corporation Air mixing systems having mixing chambers for gas turbine engines
US10100738B2 (en) 2015-01-20 2018-10-16 United Technologies Corporation Overcooled air cooling system with annular mixing passage
EP3874129A4 (en) * 2018-11-02 2022-10-05 Chromalloy Gas Turbine LLC SYSTEM AND METHOD FOR SUPPLYING COMPRESSED AIR TO A GAS TURBINE COMBUSTOR

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5098105U (no) * 1974-01-12 1975-08-15
JPS5443123A (en) * 1977-09-12 1979-04-05 Furukawa Electric Co Ltd:The High tensile electric condictive copper alloy
JPS58197402A (ja) * 1982-05-14 1983-11-17 Hitachi Ltd ガスタ−ビン翼

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2873944A (en) * 1952-09-10 1959-02-17 Gen Motors Corp Turbine blade cooling
GB849255A (en) * 1956-11-01 1960-09-21 Josef Cermak Method of and arrangements for cooling the walls of combustion spaces and other spaces subject to high thermal stresses
GB1070480A (en) * 1966-02-01 1967-06-01 Rolls Royce Aerofoil shaped blade for a fluid flow machine such as a gas turbine engine
US3652181A (en) * 1970-11-23 1972-03-28 Carl F Wilhelm Jr Cooling sleeve for gas turbine combustor transition member
US3806276A (en) * 1972-08-30 1974-04-23 Gen Motors Corp Cooled turbine blade
FR2221020A5 (no) * 1973-03-09 1974-10-04 Gen Electric
CH584833A5 (no) * 1975-05-16 1977-02-15 Bbc Brown Boveri & Cie
CH633347A5 (de) * 1978-08-03 1982-11-30 Bbc Brown Boveri & Cie Gasturbine.
US4526226A (en) * 1981-08-31 1985-07-02 General Electric Company Multiple-impingement cooled structure
CA1193551A (en) * 1981-12-31 1985-09-17 Paul C. Holden Shell-spar cooled airfoil having variable coolant passageway area

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5098105U (no) * 1974-01-12 1975-08-15
JPS5443123A (en) * 1977-09-12 1979-04-05 Furukawa Electric Co Ltd:The High tensile electric condictive copper alloy
JPS58197402A (ja) * 1982-05-14 1983-11-17 Hitachi Ltd ガスタ−ビン翼

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0275819A (ja) * 1988-08-17 1990-03-15 Rolls Royce Plc ガスタービンエンジンの燃焼室
JP2002155759A (ja) * 2000-11-20 2002-05-31 General Electric Co <Ge> 衝突冷却遷移ダクトの側板冷却を強化する空力装置及び関連方法
JP2007292451A (ja) * 2006-04-24 2007-11-08 General Electric Co <Ge> ガスタービンエンジンの圧力損失を減少するシステム
JP2008267799A (ja) * 2007-04-17 2008-11-06 General Electric Co <Ge> 燃焼器圧力降下の低減を促進する方法及び装置
JP2011027403A (ja) * 2009-07-24 2011-02-10 General Electric Co <Ge> ガスタービン燃焼器のためのシステム及び方法
JP2011179812A (ja) * 2010-03-02 2011-09-15 General Electric Co <Ge> 燃焼器空気流スリーブ内の角度付き静翼
JP2011207755A (ja) * 2010-03-30 2011-10-20 General Electric Co <Ge> 流体被冷却改質器および改質器を冷却するための方法
JP2011220335A (ja) * 2010-04-08 2011-11-04 General Electric Co <Ge> 流れスリーブを有する燃焼器
JP2011226481A (ja) * 2010-04-19 2011-11-10 General Electric Co <Ge> トランジションダクト界面における燃焼器ライナ冷却及びその関連する方法
JP2013213492A (ja) * 2012-04-03 2013-10-17 General Electric Co <Ge> 移行ノズル燃焼システム
JP2013234833A (ja) * 2012-05-02 2013-11-21 General Electric Co <Ge> ガスタービン燃焼器のフロースリーブに配置される音響共鳴器

Also Published As

Publication number Publication date
NO861900L (no) 1986-11-17
EP0203431B1 (en) 1990-11-22
AU593551B2 (en) 1990-02-15
CA1263243A (en) 1989-11-28
JPH0524337B2 (no) 1993-04-07
DE3675690D1 (de) 1991-01-03
EP0203431A1 (en) 1986-12-03
NO162887C (no) 1990-02-28
NO162887B (no) 1989-11-20
AU5735386A (en) 1986-11-20
EP0203431B2 (en) 1996-05-22

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