DE69724526D1 - Verfahren zur Herstellung von doppelwandigen Turbinenteilen aus vorkonsolidierten Einheiten - Google Patents

Verfahren zur Herstellung von doppelwandigen Turbinenteilen aus vorkonsolidierten Einheiten

Info

Publication number
DE69724526D1
DE69724526D1 DE69724526T DE69724526T DE69724526D1 DE 69724526 D1 DE69724526 D1 DE 69724526D1 DE 69724526 T DE69724526 T DE 69724526T DE 69724526 T DE69724526 T DE 69724526T DE 69724526 D1 DE69724526 D1 DE 69724526D1
Authority
DE
Germany
Prior art keywords
double
production
turbine parts
walled turbine
consolidated
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.)
Expired - Lifetime
Application number
DE69724526T
Other languages
English (en)
Other versions
DE69724526T2 (de
Inventor
Ann Melinda Ritter
Melvin Robert Jackson
Nesim Abuaf
Robert Patrick Campbell
Ronald Scott Bunker
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
Application filed by General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE69724526D1 publication Critical patent/DE69724526D1/de
Publication of DE69724526T2 publication Critical patent/DE69724526T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21H—MAKING PARTICULAR METAL OBJECTS BY ROLLING, e.g. SCREWS, WHEELS, RINGS, BARRELS, BALLS
    • B21H1/00—Making articles shaped as bodies of revolution
    • B21H1/06—Making articles shaped as bodies of revolution rings of restricted axial length
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/13—Parts of turbine combustion chambers
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)
  • Powder Metallurgy (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
DE69724526T 1996-06-24 1997-06-24 Verfahren zur Herstellung von doppelwandigen Turbinenteilen aus vorkonsolidierten Einheiten Expired - Lifetime DE69724526T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/669,070 US5933699A (en) 1996-06-24 1996-06-24 Method of making double-walled turbine components from pre-consolidated assemblies
US669070 1996-06-24

Publications (2)

Publication Number Publication Date
DE69724526D1 true DE69724526D1 (de) 2003-10-09
DE69724526T2 DE69724526T2 (de) 2004-06-24

Family

ID=24684880

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69724526T Expired - Lifetime DE69724526T2 (de) 1996-06-24 1997-06-24 Verfahren zur Herstellung von doppelwandigen Turbinenteilen aus vorkonsolidierten Einheiten

Country Status (4)

Country Link
US (1) US5933699A (de)
EP (1) EP0816010B1 (de)
JP (1) JP3807521B2 (de)
DE (1) DE69724526T2 (de)

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US7186084B2 (en) * 2003-11-19 2007-03-06 General Electric Company Hot gas path component with mesh and dimpled cooling
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DE102006027506B4 (de) * 2006-06-14 2010-06-10 Mtu Aero Engines Gmbh Gasturbinengehäuse und Verfahren zur Herstellung eines Gasturbinengehäuses
KR100730599B1 (ko) * 2007-01-04 2007-06-20 주식회사 성일에스아이엠 인너라이너 내체 제작방법
US20100011770A1 (en) * 2008-07-21 2010-01-21 Ronald James Chila Gas Turbine Premixer with Cratered Fuel Injection Sites
US8549861B2 (en) * 2009-01-07 2013-10-08 General Electric Company Method and apparatus to enhance transition duct cooling in a gas turbine engine
JP5260402B2 (ja) * 2009-04-30 2013-08-14 三菱重工業株式会社 板状体の製造方法、板状体、ガスタービン燃焼器およびガスタービン
EP2309099B1 (de) * 2009-09-30 2015-04-29 Siemens Aktiengesellschaft Verbindungskanal
JP5578864B2 (ja) 2010-01-20 2014-08-27 三菱重工業株式会社 流路付き壁部材の補修方法
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US8784044B2 (en) 2011-08-31 2014-07-22 Pratt & Whitney Canada Corp. Turbine shroud segment
US9028744B2 (en) 2011-08-31 2015-05-12 Pratt & Whitney Canada Corp. Manufacturing of turbine shroud segment with internal cooling passages
US8784037B2 (en) 2011-08-31 2014-07-22 Pratt & Whitney Canada Corp. Turbine shroud segment with integrated impingement plate
US9079245B2 (en) 2011-08-31 2015-07-14 Pratt & Whitney Canada Corp. Turbine shroud segment with inter-segment overlap
US8784041B2 (en) 2011-08-31 2014-07-22 Pratt & Whitney Canada Corp. Turbine shroud segment with integrated seal
CN102489639B (zh) * 2011-12-27 2013-03-06 张家港海陆环形锻件有限公司 一种高合金钢大型环件细晶轧制成形方法
US9243506B2 (en) * 2012-01-03 2016-01-26 General Electric Company Methods and systems for cooling a transition nozzle
CN103028682B (zh) * 2012-11-29 2015-02-04 一重集团大连设计研究院有限公司 一种筒节轧制防跑偏工艺方法
CN103100619B (zh) * 2012-12-12 2014-12-17 贵州航宇科技发展股份有限公司 双相不锈钢复杂异形截面环形件的辗轧成形方法
CN103143885B (zh) * 2013-02-07 2016-04-20 沈阳黎明航空发动机(集团)有限责任公司 一种对开式薄壁零件的加工方法
US9080447B2 (en) * 2013-03-21 2015-07-14 General Electric Company Transition duct with divided upstream and downstream portions
CN103639655B (zh) * 2013-11-28 2016-08-17 江西洪都航空工业集团有限责任公司 一种大曲率全型面薄壁件的制造工艺
EP3018415B1 (de) * 2014-11-07 2020-01-01 United Technologies Corporation Kühlung eines brennkammerverdünnungslochs
CN106607666B (zh) * 2015-10-27 2018-08-03 哈尔滨建成集团有限公司 一种偏心弧形板的加工方法
US10036283B2 (en) 2015-11-24 2018-07-31 General Electric Company System and method for diffuser AFT plate assembly
US10041365B2 (en) 2015-11-24 2018-08-07 General Electric Company System of supporting turbine diffuser
US10287920B2 (en) 2015-11-24 2019-05-14 General Electric Company System of supporting turbine diffuser
US10041377B2 (en) * 2015-11-24 2018-08-07 General Electric Company System and method for turbine diffuser
US10036267B2 (en) 2015-11-24 2018-07-31 General Electric Company System of supporting turbine diffuser outlet
RU2706211C2 (ru) * 2016-01-25 2019-11-14 Ансалдо Энерджиа Свитзерлэнд Аг Охлаждаемая стенка компонента турбины и способ охлаждения этой стенки
CN105710607B (zh) * 2016-02-02 2018-07-03 哈电集团（秦皇岛）重型装备有限公司 一种核电蒸汽发生器锥形筒节的制造方法
DE102017108368A1 (de) * 2016-05-11 2017-11-16 General Electric Company System und Verfahren für eine Diffusorrückplattenanordnung
US11274569B2 (en) 2017-12-13 2022-03-15 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10533454B2 (en) 2017-12-13 2020-01-14 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10570773B2 (en) 2017-12-13 2020-02-25 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10502093B2 (en) * 2017-12-13 2019-12-10 Pratt & Whitney Canada Corp. Turbine shroud cooling
CN108672622B (zh) * 2018-04-02 2019-12-03 张家港中环海陆高端装备股份有限公司 高筒形薄壁纯钛环件稳定轧制工艺
CN108580768B (zh) * 2018-04-10 2019-12-03 张家港中环海陆高端装备股份有限公司 海洋工程用纯钛护套锻件的制造工艺
CN109351835B (zh) * 2018-11-13 2020-12-25 航天特种材料及工艺技术研究所 带环向加强筋曲母线薄壁壳体的整体旋压成形方法
CN109551184A (zh) * 2018-12-25 2019-04-02 厦门航天思尔特机器人系统股份公司 一种铝模板生产工艺
CN109807558B (zh) * 2019-01-28 2021-09-07 东北大学 一种钛合金的丝材电弧增材制造方法
US11365645B2 (en) 2020-10-07 2022-06-21 Pratt & Whitney Canada Corp. Turbine shroud cooling

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Also Published As

Publication number Publication date
US5933699A (en) 1999-08-03
EP0816010A3 (de) 1998-12-23
DE69724526T2 (de) 2004-06-24
EP0816010B1 (de) 2003-09-03
JP3807521B2 (ja) 2006-08-09
JPH1076335A (ja) 1998-03-24
EP0816010A2 (de) 1998-01-07

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN