DE60212295T2 - Verfahren und Vorrichtung zur Korrektur der Verwindung einer Schaufel - Google Patents

Verfahren und Vorrichtung zur Korrektur der Verwindung einer Schaufel Download PDF

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Publication number
DE60212295T2
DE60212295T2 DE60212295T DE60212295T DE60212295T2 DE 60212295 T2 DE60212295 T2 DE 60212295T2 DE 60212295 T DE60212295 T DE 60212295T DE 60212295 T DE60212295 T DE 60212295T DE 60212295 T2 DE60212295 T2 DE 60212295T2
Authority
DE
Germany
Prior art keywords
clamping device
carriage
claw
blade
airfoil component
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
DE60212295T
Other languages
German (de)
English (en)
Other versions
DE60212295D1 (de
Inventor
Lum Kok Wah
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.)
GE Aviation Service Operation LLP
Original Assignee
GE Aviation Service Operation LLP
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 GE Aviation Service Operation LLP filed Critical GE Aviation Service Operation LLP
Application granted granted Critical
Publication of DE60212295D1 publication Critical patent/DE60212295D1/de
Publication of DE60212295T2 publication Critical patent/DE60212295T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • B23P6/00—Restoring or reconditioning objects
    • B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
    • 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
    • F01D5/005—Repairing methods or devices
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/37—Impeller making apparatus
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49318—Repairing or disassembling
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49764—Method of mechanical manufacture with testing or indicating
    • Y10T29/49771—Quantitative measuring or gauging

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Straightening Metal Sheet-Like Bodies (AREA)
DE60212295T 2001-11-09 2002-10-30 Verfahren und Vorrichtung zur Korrektur der Verwindung einer Schaufel Expired - Lifetime DE60212295T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US38074 2001-11-09
US10/038,074 US6792655B2 (en) 2001-11-09 2001-11-09 Apparatus for correcting airfoil twist

Publications (2)

Publication Number Publication Date
DE60212295D1 DE60212295D1 (de) 2006-07-27
DE60212295T2 true DE60212295T2 (de) 2007-05-16

Family

ID=21897951

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60212295T Expired - Lifetime DE60212295T2 (de) 2001-11-09 2002-10-30 Verfahren und Vorrichtung zur Korrektur der Verwindung einer Schaufel

Country Status (5)

Country Link
US (1) US6792655B2 (enExample)
EP (1) EP1310632B1 (enExample)
JP (1) JP4197426B2 (enExample)
DE (1) DE60212295T2 (enExample)
SG (1) SG122769A1 (enExample)

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Publication number Priority date Publication date Assignee Title
JP4028442B2 (ja) 2002-06-26 2007-12-26 株式会社東芝 ガスタービン翼の変形修正装置及び方法
US6969821B2 (en) * 2003-06-30 2005-11-29 General Electric Company Airfoil qualification system and method
EP1510283B1 (en) * 2003-08-27 2007-10-17 ALSTOM Technology Ltd Automated adaptive machining of obstructed passages
US7328496B2 (en) * 2003-10-31 2008-02-12 General Electric Company Apparatus for rebuilding gas turbine engine blades
US7334331B2 (en) * 2003-12-18 2008-02-26 General Electric Company Methods and apparatus for machining components
US7204677B2 (en) * 2005-06-30 2007-04-17 General Electric Company Countering laser shock peening induced blade twist
US7217102B2 (en) * 2005-06-30 2007-05-15 General Electric Campany Countering laser shock peening induced airfoil twist using shot peening
US7536783B2 (en) * 2005-10-13 2009-05-26 Siemens Energy, Inc. Turbine vane airfoil reconfiguration method
US7503113B2 (en) * 2005-10-13 2009-03-17 Siemens Energy, Inc. Turbine vane airfoil reconfiguration system
US7762004B2 (en) * 2007-01-31 2010-07-27 General Electric Company Inspection tool for measuring bucket Z notch position
US8186056B2 (en) * 2007-06-28 2012-05-29 Siemens Energy, Inc. Turbine vane restoration system
SG155788A1 (en) * 2008-03-18 2009-10-29 Turbine Overhaul Services Pte Methods and apparatuses for correcting twist angle in a gas turbine engine blade
US8127581B2 (en) 2008-04-15 2012-03-06 United Technologies Corporation Turbine blade twist angle correction tooling
US8122601B2 (en) * 2008-04-15 2012-02-28 United Technologies Corporation Methods for correcting twist angle in a gas turbine engine blade
US7970555B2 (en) * 2008-04-15 2011-06-28 United Technologies Corporation Method for developing a repair process to correct a deformed gas turbine engine component
SG159412A1 (en) * 2008-08-25 2010-03-30 Pratt & Whitney Services Pte L Fixture for compressor stator chord restoration repair
GB201117183D0 (en) * 2011-10-06 2011-11-16 Rolls Royce Plc Method and equipment for shaping a cast component
US9567860B2 (en) 2012-11-27 2017-02-14 General Electric Company Fixture for an airfoil shroud and method for modifying an airfoil shroud
US9151587B2 (en) 2013-11-11 2015-10-06 General Electric Company Bucket tip shroud measurement fixture and method of measuring bucket tip shroud orientation
US9611753B2 (en) 2014-04-29 2017-04-04 General Electric Company Apparatus and method for inspecting a turbine blade tip shroud
CN104057243A (zh) * 2014-06-18 2014-09-24 安徽虎博机电科技有限公司 转盘式扣件自动清理修复上油装置
US9542739B1 (en) 2015-08-12 2017-01-10 General Electric Company Virtual turbomachine blade contact gap inspection
US10013752B2 (en) * 2016-11-18 2018-07-03 General Electric Company Virtual blade inspection
US10711611B2 (en) 2018-03-22 2020-07-14 Raytheon Technologies Corporation Fan blade repair fixture and method of repair
CN110253208A (zh) * 2019-07-17 2019-09-20 大连亚明汽车部件股份有限公司 铝合金压铸件整形系统
CN113460327A (zh) * 2021-07-27 2021-10-01 成都飞机工业（集团）有限责任公司 一种用于翼面类飞机型架的气动支撑装置及支撑方法
CN115069824B (zh) * 2022-06-30 2025-02-14 武昌船舶重工集团有限公司 一种锥板扭曲变形的校正装置及方法
CN116493445B (zh) * 2023-06-30 2023-09-29 海目星激光科技集团股份有限公司 热压整形设备

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1578991A (enExample) * 1968-05-22 1969-08-22
US4146967A (en) 1977-08-15 1979-04-03 The Boeing Company Rotor blade inspection fixture
GB2080156B (en) * 1980-07-25 1984-01-04 Ufimsk Aviatsion Inst Turbine blade making method and blade twisting devices
DE3274629D1 (en) * 1981-01-12 1987-01-22 Refurbished Turbine Components Turbine blade repair
US4908782A (en) 1983-05-19 1990-03-13 Compressor Components Textron Inc. Airfoil inspection method
JPS6064737A (ja) * 1983-09-21 1985-04-13 Hitachi Ltd 羽根ねじり成形加工機
US4805351A (en) * 1988-02-08 1989-02-21 Avco Corporation Blade airfoil holding system
US5581882A (en) * 1994-06-07 1996-12-10 Rolls-Royce Plc Method of manufacturing an article by superplastic forming and diffusion bonding
FR2724127B1 (fr) * 1994-09-07 1996-12-20 Snecma Procede de fabrication d'une aube creuse de turbomachine
FR2752539B1 (fr) * 1996-08-22 1998-09-18 Snecma Procede de fabrication d'une aube creuse de turbomachine et equipement de vrillage evolutif a chaud utilise
US6209216B1 (en) 1999-08-16 2001-04-03 General Electric Company Methods and apparatus for measuring airfoil coordinates

Also Published As

Publication number Publication date
SG122769A1 (en) 2006-06-29
DE60212295D1 (de) 2006-07-27
EP1310632B1 (en) 2006-06-14
EP1310632A1 (en) 2003-05-14
JP4197426B2 (ja) 2008-12-17
JP2003184572A (ja) 2003-07-03
US20030088958A1 (en) 2003-05-15
US6792655B2 (en) 2004-09-21

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