CN104812994B - 形成具有在叶尖附近带薄壁部分的主壁的长燃气轮机轮叶的方法 - Google Patents

形成具有在叶尖附近带薄壁部分的主壁的长燃气轮机轮叶的方法 Download PDF

Info

Publication number
CN104812994B
CN104812994B CN201380059286.4A CN201380059286A CN104812994B CN 104812994 B CN104812994 B CN 104812994B CN 201380059286 A CN201380059286 A CN 201380059286A CN 104812994 B CN104812994 B CN 104812994B
Authority
CN
China
Prior art keywords
casting
thickness
wall
main wall
outer radial
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
CN201380059286.4A
Other languages
English (en)
Chinese (zh)
Other versions
CN104812994A (zh
Inventor
C.X.坎贝尔
D.托梅迪斯
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.)
Siemens Energy Inc
Original Assignee
Siemens Energy Inc
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 Siemens Energy Inc filed Critical Siemens Energy Inc
Publication of CN104812994A publication Critical patent/CN104812994A/zh
Application granted granted Critical
Publication of CN104812994B publication Critical patent/CN104812994B/zh
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/147Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D46/00Controlling, supervising, not restricted to casting covered by a single main group, e.g. for safety reasons
    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • 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
    • F05D2230/10Manufacture by removing material
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Analysing Materials By The Use Of Radiation (AREA)
CN201380059286.4A 2012-11-13 2013-11-12 形成具有在叶尖附近带薄壁部分的主壁的长燃气轮机轮叶的方法 Active CN104812994B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/675,345 2012-11-13
US13/675,345 US8720526B1 (en) 2012-11-13 2012-11-13 Process for forming a long gas turbine engine blade having a main wall with a thin portion near a tip
PCT/US2013/069671 WO2014078305A1 (en) 2012-11-13 2013-11-12 Process for forming a long gas turbine engine blade having a main wall with a thin portion near a tip

Publications (2)

Publication Number Publication Date
CN104812994A CN104812994A (zh) 2015-07-29
CN104812994B true CN104812994B (zh) 2018-01-26

Family

ID=49759538

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201380059286.4A Active CN104812994B (zh) 2012-11-13 2013-11-12 形成具有在叶尖附近带薄壁部分的主壁的长燃气轮机轮叶的方法

Country Status (8)

Country Link
US (1) US8720526B1 (enExample)
EP (1) EP2920425B1 (enExample)
JP (1) JP5973081B2 (enExample)
CN (1) CN104812994B (enExample)
IN (1) IN2015DN03335A (enExample)
RU (1) RU2015117767A (enExample)
SA (1) SA515360421B1 (enExample)
WO (1) WO2014078305A1 (enExample)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10260352B2 (en) 2013-08-01 2019-04-16 Siemens Energy, Inc. Gas turbine blade with corrugated tip wall
CN107109948B (zh) 2015-01-13 2020-10-27 通用电气公司 具有熔合架构的复合材料翼型件
US10101577B2 (en) * 2015-04-13 2018-10-16 Siemens Energy, Inc. System to prognose gas turbine remaining useful life
EP3433040B1 (en) 2016-04-27 2023-01-25 Siemens Energy, Inc. Gas turbine blade with corrugated tip wall and manufacturing method thereof
EP3551852B1 (en) 2017-01-13 2021-10-27 Siemens Energy Global GmbH & Co. KG Adaptive machining of cooled turbine airfoil
EP3511522A1 (en) * 2018-01-11 2019-07-17 Siemens Aktiengesellschaft Gas turbine blade and method for producing such blade
FR3103126B1 (fr) * 2019-11-20 2022-03-25 Safran Aircraft Engines Dispositif et procédé améliorés d’usinage de pièce aéronautique
FR3143679A1 (fr) * 2022-12-16 2024-06-21 Safran Aircraft Engines Système propulsif aéronautique
FR3143685A1 (fr) * 2022-12-16 2024-06-21 Safran Aircraft Engines Systeme propulsif aeronautique

Family Cites Families (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB627295A (en) * 1946-04-10 1949-08-05 Adrian Albert Lombard Improvements in or relating to the manufacture of guide vanes for axial-flow turbines and compressors
US3935766A (en) 1973-10-09 1976-02-03 Masters Christopher F Method and apparatus for machining cylindrical tubes
GB8508391D0 (en) * 1985-03-30 1985-05-09 Ae Plc Measurement of engineering components
US4959523A (en) 1988-11-18 1990-09-25 Hydro-Quebec Method and apparatus for automatically sensing the configuration of a surface area and effecting a work function thereon
US5446673A (en) 1993-03-30 1995-08-29 General Electric Company System and method for finish machining an in-process part having an inaccessible interior cavity
EP0894558A1 (de) * 1997-07-29 1999-02-03 Siemens Aktiengesellschaft Turbinenschaufel sowie Verfahren zur Herstellung einer Turbinenschaufel
US6850874B1 (en) 1998-04-17 2005-02-01 United Technologies Corporation Method and apparatus for predicting a characteristic of a product attribute formed by a machining process using a model of the process
EP1057565B1 (en) * 1999-06-02 2006-03-29 General Electric Company Post-cast EDM method for reducing the thickness of a turbine nozzle wall
DE10001516B4 (de) 2000-01-15 2014-05-08 Alstom Technology Ltd. Zerstörungsfreies Verfahren zur Bestimmung der Schichtdicke einer metallischen Schutzschicht auf einem metallischen Grundmaterial
US6376801B1 (en) 2000-10-12 2002-04-23 General Electric Company Gas turbine component refurbishment apparatus and repair method
US6968290B2 (en) 2001-03-27 2005-11-22 General Electric Company Electrochemical machining tool assembly and method of monitoring electrochemical machining
GB0114503D0 (en) * 2001-06-14 2001-08-08 Rolls Royce Plc Air cooled aerofoil
US7204019B2 (en) 2001-08-23 2007-04-17 United Technologies Corporation Method for repairing an apertured gas turbine component
US6701615B2 (en) 2002-03-08 2004-03-09 General Electric Company Inspection and sorting system and method for part repair
JP2003344026A (ja) * 2002-05-27 2003-12-03 Mitsubishi Heavy Ind Ltd 中空翼検査方法、及び中空翼検査用コンピュータプログラム
DE10255346A1 (de) * 2002-11-28 2004-06-09 Alstom Technology Ltd Verfahren zum Herstellen einer Turbinenschaufel
US6969821B2 (en) * 2003-06-30 2005-11-29 General Electric Company Airfoil qualification system and method
US20050091848A1 (en) * 2003-11-03 2005-05-05 Nenov Krassimir P. Turbine blade and a method of manufacturing and repairing a turbine blade
US7010982B2 (en) 2004-04-30 2006-03-14 General Electric Company Method of ultrasonically inspecting airfoils
DE502004004360D1 (de) * 2004-05-03 2007-08-30 Siemens Ag Verfahren zum Herstellen eines hohlgegossenen Bauteils mit Innenbeschichtung
DE102005025338B4 (de) 2005-05-31 2019-03-14 Siemens Aktiengesellschaft 08.Verfahren zur Bearbeitung eines Werkstückes
US7272529B2 (en) 2005-07-08 2007-09-18 Honeywell International, Inc. Dual wall turbine blade ultrasonic wall thickness measurement technique
US7306026B2 (en) 2005-09-01 2007-12-11 United Technologies Corporation Cooled turbine airfoils and methods of manufacture
GB0518153D0 (en) 2005-09-07 2005-10-12 Rolls Royce Plc Apparatus for measuring wall thicknesses of objects
US8244025B2 (en) 2006-03-20 2012-08-14 Siemens Energy, Inc. Method of coalescing information about inspected objects
US8477154B2 (en) 2006-03-20 2013-07-02 Siemens Energy, Inc. Method and system for interactive virtual inspection of modeled objects
DE102006043339B4 (de) 2006-09-15 2010-11-11 Siemens Ag Verfahren und Vorrichtung zur Bestimmung von Bauteilwandstärken mittels Thermographie
DE102006050440A1 (de) * 2006-10-26 2008-04-30 Mtu Aero Engines Gmbh Verfahren zum Herstellen einer Leichtbau-Turbinenschaufel
US8087447B2 (en) 2006-10-30 2012-01-03 United Technologies Corporation Method for checking wall thickness of hollow core airfoil
CN102016234B (zh) * 2008-03-28 2015-05-20 阿尔斯通技术有限公司 燃气轮机的导向叶片
US9177371B2 (en) 2008-06-09 2015-11-03 Siemens Energy, Inc. Non-destructive examination data visualization and analysis
US8500411B2 (en) 2010-06-07 2013-08-06 Siemens Energy, Inc. Turbine airfoil with outer wall thickness indicators
EP2469099B1 (de) * 2010-12-23 2017-08-02 Grundfos Management A/S Laufrad für eine Pump- sowie Kernanordnung und Verfahren zum Gießen eines Laufrades einer Pumpe

Also Published As

Publication number Publication date
RU2015117767A (ru) 2017-01-10
SA515360421B1 (ar) 2016-12-18
US8720526B1 (en) 2014-05-13
EP2920425B1 (en) 2016-11-02
EP2920425A1 (en) 2015-09-23
IN2015DN03335A (enExample) 2015-10-23
CN104812994A (zh) 2015-07-29
US20140130999A1 (en) 2014-05-15
WO2014078305A1 (en) 2014-05-22
JP2015536404A (ja) 2015-12-21
JP5973081B2 (ja) 2016-08-23

Similar Documents

Publication Publication Date Title
CN104812994B (zh) 形成具有在叶尖附近带薄壁部分的主壁的长燃气轮机轮叶的方法
JP5596163B2 (ja) 閉塞孔を検出するための表面分析、および装置
JP6736477B2 (ja) タービン部品に歪みセンサーを製造するための方法、タービン部品上に歪みセンサを製造し利用する方法、及び、歪みセンサを含むタービン部品
CN113441725B (zh) 利用增材制造的涡轮机叶片的修复方法
US20050091848A1 (en) Turbine blade and a method of manufacturing and repairing a turbine blade
EP3255517B1 (en) A method of manufacturing and inspecting gas washed components in a gas turbine engine
US10487665B2 (en) Acoustic breakthrough detection
US20170368647A1 (en) Methods for repairing film holes in a surface
JP2016020689A (ja) タービン部品に歪みセンサーを製作するための方法
CN113153442B (zh) 通过增材方式制造的具有一体式冲击套筒的涡轮转子叶片
CN102893122A (zh) 用于检测封闭的孔的表面分析和用于再打开的方法
JP2002256812A5 (enExample)
US20170350683A1 (en) Method of manufacturing and inspecting gas washed components in a gas turbine engine
JP7516399B2 (ja) Tbcシート破砕の程度の制御
US10792771B2 (en) Method of making integrally bladed rotor
JP2024170511A (ja) ブレード、加工システム及び加工方法
KR20120098632A (ko) 레이저 삼각 측정을 이용한 층 두께의 측정 방법 및 장치
CN111936723B (zh) 具有一个或多个内部腔体的涡轮叶片的失谐
EP3808941A1 (en) Angled tip rods in a casting core for a turbine blade
JP6586242B2 (ja) タービンブレードのベース本体を製造するための方法
US12371999B2 (en) Damping system for an integrally bladed rotor
EP4166760B1 (en) Angled tip rods used to cast holes in tips of blade cores of airfoils
JP7759337B2 (ja) ガスタービンエンジンの回転部構成部材およびその製造方法
CN102451884A (zh) 具有可变销的芯模和生产芯体的方法
FR3057187A1 (fr) Procede de determination du retrait d'un noyau de fonderie lors d'un traitement thermique du noyau

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
EXSB Decision made by sipo to initiate substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: Florida, USA

Patentee after: Siemens energy USA

Address before: Florida, USA

Patentee before: SIEMENS ENERGY, Inc.