JP6310680B2 - 付加製造法を用いたエフュージョンプレート - Google Patents

付加製造法を用いたエフュージョンプレート Download PDF

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Publication number
JP6310680B2
JP6310680B2 JP2013238395A JP2013238395A JP6310680B2 JP 6310680 B2 JP6310680 B2 JP 6310680B2 JP 2013238395 A JP2013238395 A JP 2013238395A JP 2013238395 A JP2013238395 A JP 2013238395A JP 6310680 B2 JP6310680 B2 JP 6310680B2
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Japan
Prior art keywords
effusion plate
channels
effusion
channel
plate
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.)
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Application number
JP2013238395A
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English (en)
Japanese (ja)
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JP2014141961A5 (enExample
JP2014141961A (ja
Inventor
トーマス・エドワード・ジョンソン
ダニエル・ジャーリット・ウェジェリフ
クリストファー・ポール・キーナー
ヒース・マイケル・オステビー
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General Electric Co
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General Electric Co
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Publication of JP2014141961A5 publication Critical patent/JP2014141961A5/ja
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Classifications

    • 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
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20Direct sintering or melting
    • B22F10/28Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/009Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine components other than turbine blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • 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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • 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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/10Sintering only
    • B22F3/1035Liquid phase sintering
    • 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
    • F23R2900/03041Effusion cooled combustion chamber walls or domes
    • 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
    • F23R2900/03042Film cooled combustion chamber walls or domes
    • 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
    • F23R2900/03045Convection cooled combustion chamber walls provided with turbolators or means for creating turbulences to increase 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
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/25Process efficiency
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Materials Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Powder Metallurgy (AREA)
JP2013238395A 2013-01-23 2013-11-19 付加製造法を用いたエフュージョンプレート Active JP6310680B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/748,568 2013-01-23
US13/748,568 US9309809B2 (en) 2013-01-23 2013-01-23 Effusion plate using additive manufacturing methods

Publications (3)

Publication Number Publication Date
JP2014141961A JP2014141961A (ja) 2014-08-07
JP2014141961A5 JP2014141961A5 (enExample) 2016-12-22
JP6310680B2 true JP6310680B2 (ja) 2018-04-11

Family

ID=51064359

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013238395A Active JP6310680B2 (ja) 2013-01-23 2013-11-19 付加製造法を用いたエフュージョンプレート

Country Status (3)

Country Link
US (1) US9309809B2 (enExample)
JP (1) JP6310680B2 (enExample)
DE (1) DE102013112939B4 (enExample)

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2971974A4 (en) * 2013-03-14 2016-04-13 United Technologies Corp ADDITIVELY MANUFACTURED PANEL OF A GAS TURBINE CHAMBER
US9322555B2 (en) * 2013-07-01 2016-04-26 General Electric Company Cap assembly for a bundled tube fuel injector
EP2823952A1 (de) * 2013-07-09 2015-01-14 Siemens Aktiengesellschaft Anpassungsverfahren und Herstellverfahren für mittels SLM gefertigte Bauteile
US20160199913A1 (en) * 2013-09-04 2016-07-14 Bae Systems Plc Conduit system
US20150285502A1 (en) * 2014-04-08 2015-10-08 General Electric Company Fuel nozzle shroud and method of manufacturing the shroud
US9650958B2 (en) * 2014-07-17 2017-05-16 General Electric Company Combustor cap with cooling passage
US10578305B2 (en) * 2014-11-03 2020-03-03 Siemens Aktiengesellschaft Bruner assembly
EP3053674B1 (en) * 2015-02-03 2020-04-01 Ansaldo Energia IP UK Limited Method for manufacturing a combustor front panel and a combustor front panel
US20160230993A1 (en) * 2015-02-10 2016-08-11 United Technologies Corporation Combustor liner effusion cooling holes
US10094240B2 (en) 2015-02-12 2018-10-09 United Technologies Corporation Anti-deflection feature for additively manufactured thin metal parts and method of additively manufacturing thin metal parts
US10480787B2 (en) 2015-03-26 2019-11-19 United Technologies Corporation Combustor wall cooling channel formed by additive manufacturing
US20170138595A1 (en) * 2015-11-18 2017-05-18 General Electric Company Combustor Wall Channel Cooling System
JP2017106414A (ja) * 2015-12-11 2017-06-15 株式会社東芝 ノズルダイヤフラム、タービンおよびノズルダイヤフラムの製造方法
US10557464B2 (en) 2015-12-23 2020-02-11 Emerson Climate Technologies, Inc. Lattice-cored additive manufactured compressor components with fluid delivery features
US10634143B2 (en) 2015-12-23 2020-04-28 Emerson Climate Technologies, Inc. Thermal and sound optimized lattice-cored additive manufactured compressor components
US10982672B2 (en) 2015-12-23 2021-04-20 Emerson Climate Technologies, Inc. High-strength light-weight lattice-cored additive manufactured compressor components
EP3239613A1 (en) * 2016-04-29 2017-11-01 Siemens Aktiengesellschaft Burner component, burner, and methods of manufacturing or operating of these for dual fuel operation
US10221769B2 (en) 2016-12-02 2019-03-05 General Electric Company System and apparatus for gas turbine combustor inner cap and extended resonating tubes
US10220474B2 (en) 2016-12-02 2019-03-05 General Electricd Company Method and apparatus for gas turbine combustor inner cap and high frequency acoustic dampers
US10228138B2 (en) 2016-12-02 2019-03-12 General Electric Company System and apparatus for gas turbine combustor inner cap and resonating tubes
US10247296B2 (en) 2016-12-12 2019-04-02 General Electric Company Additively manufactured gearbox with integral heat exchanger
US10739001B2 (en) 2017-02-14 2020-08-11 Raytheon Technologies Corporation Combustor liner panel shell interface for a gas turbine engine combustor
US10830434B2 (en) 2017-02-23 2020-11-10 Raytheon Technologies Corporation Combustor liner panel end rail with curved interface passage for a gas turbine engine combustor
US10823411B2 (en) * 2017-02-23 2020-11-03 Raytheon Technologies Corporation Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustor
US10941937B2 (en) 2017-03-20 2021-03-09 Raytheon Technologies Corporation Combustor liner with gasket for gas turbine engine
US10718222B2 (en) 2017-03-27 2020-07-21 General Electric Company Diffuser-deswirler for a gas turbine engine
US11079111B2 (en) 2019-04-29 2021-08-03 Solar Turbines Incorporated Air tube
US11774093B2 (en) * 2020-04-08 2023-10-03 General Electric Company Burner cooling structures
US11454395B2 (en) * 2020-04-24 2022-09-27 Collins Engine Nozzles, Inc. Thermal resistant air caps
US11486578B2 (en) 2020-05-26 2022-11-01 Raytheon Technologies Corporation Multi-walled structure for a gas turbine engine
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US12065936B2 (en) 2020-09-18 2024-08-20 Ge Avio S.R.L. Probe placement within a duct of a gas turbine engine
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
CN113028449B (zh) * 2021-02-26 2023-03-17 中国空气动力研究与发展中心设备设计与测试技术研究所 一种燃气发生器流线型燃料分流盘
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4684323A (en) * 1985-12-23 1987-08-04 United Technologies Corporation Film cooling passages with curved corners
CA2288557C (en) 1998-11-12 2007-02-06 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor cooling structure
US6351947B1 (en) * 2000-04-04 2002-03-05 Abb Alstom Power (Schweiz) Combustion chamber for a gas turbine
JP3997986B2 (ja) * 2003-12-19 2007-10-24 株式会社Ihi 冷却タービン部品、及び冷却タービン翼
US20050156361A1 (en) * 2004-01-21 2005-07-21 United Technologies Corporation Methods for producing complex ceramic articles
DE102004032093B4 (de) * 2004-07-01 2007-05-16 Cl Schutzrechtsverwaltungs Gmbh Durch einen selektiven Lasersintervorgang (SLS) hergestelltes Bauteil
US7464554B2 (en) * 2004-09-09 2008-12-16 United Technologies Corporation Gas turbine combustor heat shield panel or exhaust panel including a cooling device
EP1686240A1 (de) * 2005-01-27 2006-08-02 Siemens Aktiengesellschaft Bauteil mit Abflachung in einem Loch
US7658590B1 (en) * 2005-09-30 2010-02-09 Florida Turbine Technologies, Inc. Turbine airfoil with micro-tubes embedded with a TBC
EP1975372A1 (en) * 2007-03-28 2008-10-01 Siemens Aktiengesellschaft Eccentric chamfer at inlet of branches in a flow channel
US20080271457A1 (en) * 2007-05-01 2008-11-06 General Electric Company Cooling Holes For Gas Turbine Combustor Having A Non-Uniform Diameter Therethrough
US7789626B1 (en) * 2007-05-31 2010-09-07 Florida Turbine Technologies, Inc. Turbine blade with showerhead film cooling holes
US20100263384A1 (en) * 2009-04-17 2010-10-21 Ronald James Chila Combustor cap with shaped effusion cooling holes
US8495881B2 (en) * 2009-06-02 2013-07-30 General Electric Company System and method for thermal control in a cap of a gas turbine combustor
GB0912715D0 (en) * 2009-07-22 2009-08-26 Rolls Royce Plc Cooling arrangement
US9334741B2 (en) 2010-04-22 2016-05-10 Siemens Energy, Inc. Discreetly defined porous wall structure for transpirational cooling
JP2012063094A (ja) * 2010-09-16 2012-03-29 Hitachi Ltd バーナ及び燃焼器
JP2014105886A (ja) * 2012-11-26 2014-06-09 Hitachi Ltd 燃焼器
DE102013214487A1 (de) * 2013-07-24 2015-01-29 Rolls-Royce Deutschland Ltd & Co Kg Brennkammerschindel einer Gasturbine

Also Published As

Publication number Publication date
US9309809B2 (en) 2016-04-12
DE102013112939B4 (de) 2025-10-02
DE102013112939A1 (de) 2014-07-24
JP2014141961A (ja) 2014-08-07
US20140202163A1 (en) 2014-07-24

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