CN100406678C - 用于组装可转动机器的方法和设备 - Google Patents

用于组装可转动机器的方法和设备 Download PDF

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Publication number
CN100406678C
CN100406678C CNB2004100325283A CN200410032528A CN100406678C CN 100406678 C CN100406678 C CN 100406678C CN B2004100325283 A CNB2004100325283 A CN B2004100325283A CN 200410032528 A CN200410032528 A CN 200410032528A CN 100406678 C CN100406678 C CN 100406678C
Authority
CN
China
Prior art keywords
blade
rotor
geometric parameter
blades
computer system
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 - Fee Related
Application number
CNB2004100325283A
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English (en)
Chinese (zh)
Other versions
CN1536199A (zh
Inventor
T·R·亨宁
G·J·范德梅尔维
W·C·吕尔
D·E·莫尔曼
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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
Publication of CN1536199A publication Critical patent/CN1536199A/zh
Application granted granted Critical
Publication of CN100406678C publication Critical patent/CN100406678C/zh
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/027Arrangements for balancing
    • 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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • 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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/662Balancing of rotors
    • 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
    • F05D2230/60Assembly methods
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/50Vibration damping features
    • 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
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making
    • Y10T29/49321Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member

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)
CNB2004100325283A 2003-04-08 2004-04-08 用于组装可转动机器的方法和设备 Expired - Fee Related CN100406678C (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/409392 2003-04-08
US10/409,392 US6908285B2 (en) 2003-04-08 2003-04-08 Methods and apparatus for assembling rotatable machines

Publications (2)

Publication Number Publication Date
CN1536199A CN1536199A (zh) 2004-10-13
CN100406678C true CN100406678C (zh) 2008-07-30

Family

ID=32869193

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2004100325283A Expired - Fee Related CN100406678C (zh) 2003-04-08 2004-04-08 用于组装可转动机器的方法和设备

Country Status (4)

Country Link
US (1) US6908285B2 (enExample)
EP (1) EP1467063A1 (enExample)
JP (1) JP2004308660A (enExample)
CN (1) CN100406678C (enExample)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6898547B1 (en) 2000-09-11 2005-05-24 Axiam, Incorporated Rotor assembly system and method
GB0325215D0 (en) * 2003-10-29 2003-12-03 Rolls Royce Plc Design of vanes for exposure to vibratory loading
US8180596B2 (en) * 2004-07-13 2012-05-15 General Electric Company Methods and apparatus for assembling rotatable machines
US7090464B2 (en) * 2004-07-13 2006-08-15 General Electric Company Methods and apparatus for assembling rotatable machines
US7287958B2 (en) * 2005-01-10 2007-10-30 General Electric Company Methods and apparatus for assembling rotatable machines
US7572101B2 (en) * 2005-02-22 2009-08-11 General Electric Company Methods and apparatus for assembling rotatable machines
FR2886012B1 (fr) * 2005-05-23 2007-07-06 Snecma Moteurs Sa Procede de calibrage en masse de pieces destinees a etre montees en peripherie d'un rotor
GB0601837D0 (en) 2006-01-31 2006-03-08 Rolls Royce Plc An aerofoil assembly and a method of manufacturing an aerofoil assembly
US7497662B2 (en) * 2006-07-31 2009-03-03 General Electric Company Methods and systems for assembling rotatable machines
US7539594B2 (en) 2006-09-26 2009-05-26 Axiam, Incorporated Method and apparatus for geometric rotor stacking and balancing
US8142161B2 (en) * 2007-09-20 2012-03-27 General Electric Company Replaceable staking insert
US7792600B2 (en) * 2007-12-31 2010-09-07 General Electric Company System and a method for assembling a rotor stack
US9157723B2 (en) 2009-01-30 2015-10-13 Axiam, Inc. Absolute diameter measurement arm
US8219353B2 (en) 2009-01-30 2012-07-10 Axiam, Inc. Absolute diameter measurement arm
DE102009016123B4 (de) * 2009-04-03 2014-07-17 Schenck Rotec Gmbh Verfahren zum Zusammenbau und Bestimmen der Unwucht von Rotoren
US8069707B2 (en) * 2009-08-05 2011-12-06 General Electric Company Methods and apparatus for determining moment weight of rotating machine components
GB201009216D0 (en) * 2010-06-02 2010-07-21 Rolls Royce Plc Rotationally balancing a rotating part
US9404367B2 (en) * 2012-11-21 2016-08-02 Solar Turbines Incorporated Gas turbine engine compressor rotor assembly and balancing system
US10710705B2 (en) * 2017-06-28 2020-07-14 General Electric Company Open rotor and airfoil therefor
FR3073045B1 (fr) * 2017-10-26 2019-11-22 Safran Aircraft Engines Procede d'equilibrage d'un ensemble d'aubes
US10816429B2 (en) * 2018-12-07 2020-10-27 Raytheon Technologies Corporation Determining a moment weight of a component based on measured surface geometry/solid model of the component
CN113323920B (zh) * 2021-01-18 2023-05-09 中国民用航空飞行学院 一种发动机风扇叶片更换及风扇转子静态再平衡调整方法
FR3124216B1 (fr) * 2021-06-21 2023-10-20 Safran Aircraft Engines Procédé d’equilibrage d’aubes de soufflante avec usinage du bord de fuite

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4732532A (en) * 1979-06-16 1988-03-22 Rolls-Royce Plc Arrangement for minimizing buzz saw noise in bladed rotors
US4767272A (en) * 1987-10-14 1988-08-30 United Technologies Corporation Method for reducing blade tip variation of a bladed rotor
GB2245661A (en) * 1990-07-03 1992-01-08 Rolls Royce Plc Turbine balancing system
EP0962660A1 (en) * 1998-06-05 1999-12-08 MAGNETI MARELLI CLIMATIZZAZIONE S.p.A. A method for assembling an electric fan

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2140816A1 (de) * 1971-08-14 1973-03-01 Motoren Turbinen Union Rotor fuer stroemungsmaschinen
US3888601A (en) 1974-05-23 1975-06-10 Gen Electric Turbomachine with balancing means
US4213736A (en) 1978-06-05 1980-07-22 Innerspace Corporation Turbomachinery and method of operation
JPS5525555A (en) 1978-08-12 1980-02-23 Hitachi Ltd Impeller
US4602412A (en) * 1982-12-02 1986-07-29 Westinghouse Electric Corp. Method for assembling in a circular array turbine blades each with an integral shroud
US4971641A (en) * 1988-11-14 1990-11-20 General Electric Company Method of making counterrotating aircraft propeller blades
US6290466B1 (en) 1999-09-17 2001-09-18 General Electric Company Composite blade root attachment
FR2842571B1 (fr) 2002-07-17 2004-10-15 Snecma Moteurs Procede de repartition d'aubes de rotor de turbomachine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4732532A (en) * 1979-06-16 1988-03-22 Rolls-Royce Plc Arrangement for minimizing buzz saw noise in bladed rotors
US4767272A (en) * 1987-10-14 1988-08-30 United Technologies Corporation Method for reducing blade tip variation of a bladed rotor
GB2245661A (en) * 1990-07-03 1992-01-08 Rolls Royce Plc Turbine balancing system
EP0962660A1 (en) * 1998-06-05 1999-12-08 MAGNETI MARELLI CLIMATIZZAZIONE S.p.A. A method for assembling an electric fan

Also Published As

Publication number Publication date
US20040202544A1 (en) 2004-10-14
EP1467063A1 (en) 2004-10-13
JP2004308660A (ja) 2004-11-04
CN1536199A (zh) 2004-10-13
US6908285B2 (en) 2005-06-21

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C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20080730

Termination date: 20100408