CN1987054A - 涡轮机叶片末端冷却 - Google Patents

涡轮机叶片末端冷却 Download PDF

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Publication number
CN1987054A
CN1987054A CNA2006101686678A CN200610168667A CN1987054A CN 1987054 A CN1987054 A CN 1987054A CN A2006101686678 A CNA2006101686678 A CN A2006101686678A CN 200610168667 A CN200610168667 A CN 200610168667A CN 1987054 A CN1987054 A CN 1987054A
Authority
CN
China
Prior art keywords
spanwise
stem portion
chamber
flow
blade
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.)
Pending
Application number
CNA2006101686678A
Other languages
English (en)
Chinese (zh)
Inventor
F·J·昆哈
J·E·阿尔伯特
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of CN1987054A publication Critical patent/CN1987054A/zh
Pending 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22C—FOUNDRY MOULDING
    • B22C9/00—Moulds or cores; Moulding processes
    • B22C9/10—Cores; Manufacture or installation of cores
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22C—FOUNDRY MOULDING
    • B22C9/00—Moulds or cores; Moulding processes
    • B22C9/10—Cores; Manufacture or installation of cores
    • B22C9/103—Multipart cores
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/186—Film cooling
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/20—Specially-shaped blade tips to seal space between tips and stator
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/21—Manufacture essentially without removing material by casting
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/202—Heat transfer, e.g. cooling by film cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CNA2006101686678A 2005-12-22 2006-12-22 涡轮机叶片末端冷却 Pending CN1987054A (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/317,394 US7413403B2 (en) 2005-12-22 2005-12-22 Turbine blade tip cooling
US11/317394 2005-12-22

Publications (1)

Publication Number Publication Date
CN1987054A true CN1987054A (zh) 2007-06-27

Family

ID=37888097

Family Applications (1)

Application Number Title Priority Date Filing Date
CNA2006101686678A Pending CN1987054A (zh) 2005-12-22 2006-12-22 涡轮机叶片末端冷却

Country Status (7)

Country Link
US (1) US7413403B2 (enExample)
EP (1) EP1801351B1 (enExample)
JP (1) JP2007170379A (enExample)
KR (1) KR20070066843A (enExample)
CN (1) CN1987054A (enExample)
SG (1) SG133467A1 (enExample)
TW (1) TW200724775A (enExample)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102458715A (zh) * 2009-04-20 2012-05-16 西门子公司 用于制造燃气轮机的涡轮动叶片的浇铸装置和涡轮动叶片
CN103485839A (zh) * 2012-06-08 2014-01-01 通用电气公司 涡轮发动机的气动组件
CN106660125A (zh) * 2014-05-30 2017-05-10 诺沃皮尼奥内股份有限公司 制造涡轮机构件的方法、涡轮机构件和涡轮机
CN111335960A (zh) * 2018-12-18 2020-06-26 通用电气公司 涡轮发动机翼型件及冷却方法
CN111677557A (zh) * 2020-06-08 2020-09-18 清华大学 涡轮导向叶片及具有其的涡轮机械

Families Citing this family (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7674093B2 (en) * 2006-12-19 2010-03-09 General Electric Company Cluster bridged casting core
US7866370B2 (en) * 2007-01-30 2011-01-11 United Technologies Corporation Blades, casting cores, and methods
US8177507B2 (en) * 2008-05-14 2012-05-15 United Technologies Corporation Triangular serpentine cooling channels
US8172533B2 (en) * 2008-05-14 2012-05-08 United Technologies Corporation Turbine blade internal cooling configuration
US8157527B2 (en) 2008-07-03 2012-04-17 United Technologies Corporation Airfoil with tapered radial cooling passage
US8572844B2 (en) 2008-08-29 2013-11-05 United Technologies Corporation Airfoil with leading edge cooling passage
US8303252B2 (en) 2008-10-16 2012-11-06 United Technologies Corporation Airfoil with cooling passage providing variable heat transfer rate
US8100165B2 (en) * 2008-11-17 2012-01-24 United Technologies Corporation Investment casting cores and methods
US8171978B2 (en) 2008-11-21 2012-05-08 United Technologies Corporation Castings, casting cores, and methods
US8113780B2 (en) * 2008-11-21 2012-02-14 United Technologies Corporation Castings, casting cores, and methods
US8109725B2 (en) 2008-12-15 2012-02-07 United Technologies Corporation Airfoil with wrapped leading edge cooling passage
GB2468669C (en) * 2009-03-17 2013-11-13 Rolls Royce Plc A flow discharge device
US20100239409A1 (en) * 2009-03-18 2010-09-23 General Electric Company Method of Using and Reconstructing a Film-Cooling Augmentation Device for a Turbine Airfoil
US8052378B2 (en) * 2009-03-18 2011-11-08 General Electric Company Film-cooling augmentation device and turbine airfoil incorporating the same
US8118553B2 (en) * 2009-03-20 2012-02-21 Siemens Energy, Inc. Turbine airfoil cooling system with dual serpentine cooling chambers
US8764379B2 (en) * 2010-02-25 2014-07-01 General Electric Company Turbine blade with shielded tip coolant supply passageway
US9212560B2 (en) † 2011-06-30 2015-12-15 United Technologies Corporation CMC blade with integral 3D woven platform
US8876484B2 (en) 2011-08-05 2014-11-04 Hamilton Sundstrand Corporation Turbine blade pocket pin stress relief
US9200523B2 (en) 2012-03-14 2015-12-01 Honeywell International Inc. Turbine blade tip cooling
US9429027B2 (en) 2012-04-05 2016-08-30 United Technologies Corporation Turbine airfoil tip shelf and squealer pocket cooling
US9279331B2 (en) * 2012-04-23 2016-03-08 United Technologies Corporation Gas turbine engine airfoil with dirt purge feature and core for making same
US10408066B2 (en) 2012-08-15 2019-09-10 United Technologies Corporation Suction side turbine blade tip cooling
US9115590B2 (en) 2012-09-26 2015-08-25 United Technologies Corporation Gas turbine engine airfoil cooling circuit
US9995148B2 (en) 2012-10-04 2018-06-12 General Electric Company Method and apparatus for cooling gas turbine and rotor blades
US8920123B2 (en) 2012-12-14 2014-12-30 Siemens Aktiengesellschaft Turbine blade with integrated serpentine and axial tip cooling circuits
US9932837B2 (en) * 2013-03-11 2018-04-03 United Technologies Corporation Low pressure loss cooled blade
US20160222794A1 (en) * 2013-09-09 2016-08-04 United Technologies Corporation Incidence tolerant engine component
US10041374B2 (en) * 2014-04-04 2018-08-07 United Technologies Corporation Gas turbine engine component with platform cooling circuit
FR3021697B1 (fr) * 2014-05-28 2021-09-17 Snecma Aube de turbine a refroidissement optimise
US9714583B2 (en) * 2014-08-21 2017-07-25 Honeywell International Inc. Fan containment cases for fan casings in gas turbine engines, fan blade containment systems, and methods for producing the same
US9835087B2 (en) 2014-09-03 2017-12-05 General Electric Company Turbine bucket
EP3271553A1 (en) 2015-03-17 2018-01-24 Siemens Energy, Inc. Turbine blade with a non-constraint flow turning guide structure
FR3034128B1 (fr) * 2015-03-23 2017-04-14 Snecma Noyau ceramique pour aube de turbine multi-cavites
FR3037829B1 (fr) * 2015-06-29 2017-07-21 Snecma Noyau pour le moulage d'une aube ayant des cavites superposees et comprenant un trou de depoussierage traversant une cavite de part en part
US10989056B2 (en) 2016-12-05 2021-04-27 Raytheon Technologies Corporation Integrated squealer pocket tip and tip shelf with hybrid and tip flag core
US10465529B2 (en) 2016-12-05 2019-11-05 United Technologies Corporation Leading edge hybrid cavities and cores for airfoils of gas turbine engine
US10563521B2 (en) 2016-12-05 2020-02-18 United Technologies Corporation Aft flowing serpentine cavities and cores for airfoils of gas turbine engines
US10815800B2 (en) 2016-12-05 2020-10-27 Raytheon Technologies Corporation Radially diffused tip flag
US20190003316A1 (en) * 2017-06-29 2019-01-03 United Technologies Corporation Helical skin cooling passages for turbine airfoils
US11021966B2 (en) * 2019-04-24 2021-06-01 Raytheon Technologies Corporation Vane core assemblies and methods
US12006836B2 (en) 2021-07-02 2024-06-11 Rtx Corporation Cooling arrangement for gas turbine engine component
US11913353B2 (en) 2021-08-06 2024-02-27 Rtx Corporation Airfoil tip arrangement for gas turbine engine

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59231102A (ja) * 1983-06-15 1984-12-25 Toshiba Corp ガスタ−ビンの翼
JPH06102963B2 (ja) * 1983-12-22 1994-12-14 株式会社東芝 ガスタ−ビン空冷翼
US4767268A (en) * 1987-08-06 1988-08-30 United Technologies Corporation Triple pass cooled airfoil
US4753575A (en) * 1987-08-06 1988-06-28 United Technologies Corporation Airfoil with nested cooling channels
JPH06137102A (ja) * 1992-10-26 1994-05-17 Mitsubishi Heavy Ind Ltd ガスタービン中空動翼
DE69328439T2 (de) * 1992-11-24 2000-12-14 United Technologies Corp., Hartford Kühlbare schaufelsstruktur
US5403159A (en) * 1992-11-30 1995-04-04 United Technoligies Corporation Coolable airfoil structure
US5603606A (en) * 1994-11-14 1997-02-18 Solar Turbines Incorporated Turbine cooling system
EP0954679B1 (en) * 1996-06-28 2003-01-22 United Technologies Corporation Coolable airfoil for a gas turbine engine
US5931638A (en) * 1997-08-07 1999-08-03 United Technologies Corporation Turbomachinery airfoil with optimized heat transfer
US5902093A (en) * 1997-08-22 1999-05-11 General Electric Company Crack arresting rotor blade
JPH11241602A (ja) * 1998-02-26 1999-09-07 Toshiba Corp ガスタービン翼
US6168381B1 (en) * 1999-06-29 2001-01-02 General Electric Company Airfoil isolated leading edge cooling
US6595748B2 (en) * 2001-08-02 2003-07-22 General Electric Company Trichannel airfoil leading edge cooling
US6637500B2 (en) * 2001-10-24 2003-10-28 United Technologies Corporation Cores for use in precision investment casting
US6974308B2 (en) * 2001-11-14 2005-12-13 Honeywell International, Inc. High effectiveness cooled turbine vane or blade
US7059834B2 (en) * 2003-01-24 2006-06-13 United Technologies Corporation Turbine blade
US6824359B2 (en) * 2003-01-31 2004-11-30 United Technologies Corporation Turbine blade
US7104757B2 (en) * 2003-07-29 2006-09-12 Siemens Aktiengesellschaft Cooled turbine blade
US7632071B2 (en) * 2005-12-15 2009-12-15 United Technologies Corporation Cooled turbine blade

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102458715A (zh) * 2009-04-20 2012-05-16 西门子公司 用于制造燃气轮机的涡轮动叶片的浇铸装置和涡轮动叶片
CN103485839A (zh) * 2012-06-08 2014-01-01 通用电气公司 涡轮发动机的气动组件
CN106660125A (zh) * 2014-05-30 2017-05-10 诺沃皮尼奥内股份有限公司 制造涡轮机构件的方法、涡轮机构件和涡轮机
CN111335960A (zh) * 2018-12-18 2020-06-26 通用电气公司 涡轮发动机翼型件及冷却方法
CN111335960B (zh) * 2018-12-18 2023-06-06 通用电气公司 涡轮发动机翼型件及冷却方法
CN111677557A (zh) * 2020-06-08 2020-09-18 清华大学 涡轮导向叶片及具有其的涡轮机械

Also Published As

Publication number Publication date
EP1801351A2 (en) 2007-06-27
US20070147997A1 (en) 2007-06-28
TW200724775A (en) 2007-07-01
JP2007170379A (ja) 2007-07-05
SG133467A1 (en) 2007-07-30
EP1801351A3 (en) 2010-11-24
KR20070066843A (ko) 2007-06-27
EP1801351B1 (en) 2016-03-02
US7413403B2 (en) 2008-08-19

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Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication