CN103375187B - 过渡件、燃烧系统和形成一体式铸造过渡件的方法 - Google Patents

过渡件、燃烧系统和形成一体式铸造过渡件的方法 Download PDF

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Publication number
CN103375187B
CN103375187B CN201310145765.XA CN201310145765A CN103375187B CN 103375187 B CN103375187 B CN 103375187B CN 201310145765 A CN201310145765 A CN 201310145765A CN 103375187 B CN103375187 B CN 103375187B
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CN
China
Prior art keywords
transition piece
transition
ratio
thickness
combustion
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
CN201310145765.XA
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English (en)
Chinese (zh)
Other versions
CN103375187A (zh
Inventor
K.W.麦马罕
A.佩克
N.弗勒西斯
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 Company PLC
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
Publication of CN103375187A publication Critical patent/CN103375187A/zh
Application granted granted Critical
Publication of CN103375187B publication Critical patent/CN103375187B/zh
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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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/02Sand moulds or like moulds for shaped castings
    • B22C9/04Use of lost patterns
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • B22D19/0009Cylinders, pistons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • B22D19/04Casting in, on, or around objects which form part of the product for joining parts
    • B22D19/045Casting in, on, or around objects which form part of the product for joining parts for joining tubes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D21/00Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
    • B22D21/02Casting exceedingly oxidisable non-ferrous metals, e.g. in inert atmosphere
    • B22D21/025Casting heavy metals with high melting point, i.e. 1000 - 1600 degrees C, e.g. Co 1490 degrees C, Ni 1450 degrees C, Mn 1240 degrees C, Cu 1083 degrees C
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/13Parts of turbine combustion chambers
    • 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
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/21Manufacture essentially without removing material by casting
    • 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
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/21Manufacture essentially without removing material by casting
    • F05D2230/211Manufacture essentially without removing material by casting by precision casting, e.g. microfusing or investment casting
    • 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
    • F05D2230/00Manufacture
    • F05D2230/50Building or constructing in particular ways
    • F05D2230/53Building or constructing in particular ways by integrally manufacturing a component, e.g. by milling from a billet or one piece construction
    • 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
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • F05D2300/17Alloys
    • F05D2300/175Superalloys
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4998Combined manufacture including applying or shaping of fluent material
    • Y10T29/49988Metal casting

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Powder Metallurgy (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Paper (AREA)
CN201310145765.XA 2012-04-24 2013-04-24 过渡件、燃烧系统和形成一体式铸造过渡件的方法 Active CN103375187B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/454,785 US9109447B2 (en) 2012-04-24 2012-04-24 Combustion system including a transition piece and method of forming using a cast superalloy
US13/454785 2012-04-24
US13/454,785 2012-04-24

Publications (2)

Publication Number Publication Date
CN103375187A CN103375187A (zh) 2013-10-30
CN103375187B true CN103375187B (zh) 2016-11-23

Family

ID=48139842

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310145765.XA Active CN103375187B (zh) 2012-04-24 2013-04-24 过渡件、燃烧系统和形成一体式铸造过渡件的方法

Country Status (5)

Country Link
US (1) US9109447B2 (enExample)
EP (1) EP2657453B1 (enExample)
JP (1) JP6130714B2 (enExample)
CN (1) CN103375187B (enExample)
RU (1) RU2013118656A (enExample)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2915957A1 (en) * 2014-03-05 2015-09-09 Siemens Aktiengesellschaft Cast tubular duct for a gas turbine and manufacturing method thereof
US10830142B2 (en) * 2016-10-10 2020-11-10 General Electric Company Combustor aft frame cooling
CN107178792A (zh) * 2017-06-13 2017-09-19 东方电气集团东方汽轮机有限公司 一种燃气轮机及航空发动机燃烧器尾筒结构

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3527285A (en) 1967-11-07 1970-09-08 Gen Motors Corp Method and mold for casting thin wall cylinders
US3657882A (en) * 1970-11-13 1972-04-25 Westinghouse Electric Corp Combustion apparatus
US6416596B1 (en) 1974-07-17 2002-07-09 The General Electric Company Cast nickel-base alloy
US4236378A (en) 1978-03-01 1980-12-02 General Electric Company Sectoral combustor for burning low-BTU fuel gas
US4422288A (en) * 1981-03-02 1983-12-27 General Electric Company Aft mounting system for combustion transition duct members
US5335502A (en) 1992-09-09 1994-08-09 General Electric Company Arched combustor
US5414999A (en) 1993-11-05 1995-05-16 General Electric Company Integral aft frame mount for a gas turbine combustor transition piece
JP3756994B2 (ja) * 1995-07-11 2006-03-22 株式会社日立製作所 ガスタービン用燃焼器及びガスタービン並びにその部材
US5964091A (en) * 1995-07-11 1999-10-12 Hitachi, Ltd. Gas turbine combustor and gas turbine
JPH10226838A (ja) * 1997-02-19 1998-08-25 Hitachi Metals Ltd 燃焼器用鋳造部品およびその製造方法
JP4097233B2 (ja) * 1997-05-07 2008-06-11 株式会社東芝 X線管の収容容器およびその製造方法、並びにx線管装置
WO1999006771A1 (en) 1997-07-31 1999-02-11 Alliedsignal Inc. Rib turbulators for combustor external cooling
US6553767B2 (en) 2001-06-11 2003-04-29 General Electric Company Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form
US6851263B2 (en) 2002-10-29 2005-02-08 General Electric Company Liner for a gas turbine engine combustor having trapped vortex cavity
US6890148B2 (en) * 2003-08-28 2005-05-10 Siemens Westinghouse Power Corporation Transition duct cooling system
US7373772B2 (en) 2004-03-17 2008-05-20 General Electric Company Turbine combustor transition piece having dilution holes
US7082766B1 (en) * 2005-03-02 2006-08-01 General Electric Company One-piece can combustor
US7377117B2 (en) 2005-08-09 2008-05-27 Turbine Services, Ltd. Transition piece for gas turbine
US7540156B2 (en) 2005-11-21 2009-06-02 General Electric Company Combustion liner for gas turbine formed of cast nickel-based superalloy
US7631504B2 (en) * 2006-02-21 2009-12-15 General Electric Company Methods and apparatus for assembling gas turbine engines
US7908867B2 (en) * 2007-09-14 2011-03-22 Siemens Energy, Inc. Wavy CMC wall hybrid ceramic apparatus
US20090249791A1 (en) * 2008-04-08 2009-10-08 General Electric Company Transition piece impingement sleeve and method of assembly
US8549861B2 (en) 2009-01-07 2013-10-08 General Electric Company Method and apparatus to enhance transition duct cooling in a gas turbine engine
US8397511B2 (en) * 2009-05-19 2013-03-19 General Electric Company System and method for cooling a wall of a gas turbine combustor
US8226886B2 (en) * 2009-08-31 2012-07-24 General Electric Company Nickel-based superalloys and articles

Also Published As

Publication number Publication date
RU2013118656A (ru) 2014-10-27
JP2013227973A (ja) 2013-11-07
CN103375187A (zh) 2013-10-30
JP6130714B2 (ja) 2017-05-17
EP2657453A2 (en) 2013-10-30
US20130276451A1 (en) 2013-10-24
EP2657453A3 (en) 2018-03-28
US9109447B2 (en) 2015-08-18
EP2657453B1 (en) 2023-05-31

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Effective date of registration: 20240103

Address after: Swiss Baden

Patentee after: GENERAL ELECTRIC CO. LTD.

Address before: New York State, USA

Patentee before: General Electric Co.

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