CA2710019A1 - Rotor assembly system and method - Google Patents

Rotor assembly system and method Download PDF

Info

Publication number
CA2710019A1
CA2710019A1 CA2710019A CA2710019A CA2710019A1 CA 2710019 A1 CA2710019 A1 CA 2710019A1 CA 2710019 A CA2710019 A CA 2710019A CA 2710019 A CA2710019 A CA 2710019A CA 2710019 A1 CA2710019 A1 CA 2710019A1
Authority
CA
Canada
Prior art keywords
rotor
assembling
stack
data
disks
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.)
Abandoned
Application number
CA2710019A
Other languages
English (en)
French (fr)
Inventor
Karl Lee Borneman
Craig Ronald Ziegler
Jeffrey John Eschenbach
Gregory Patrick Foley
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 Co
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of CA2710019A1 publication Critical patent/CA2710019A1/en
Abandoned 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/027—Arrangements for balancing
    • 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
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/60—Mounting; Assembling; Disassembling
    • F04D29/64—Mounting; Assembling; Disassembling of axial pumps
    • F04D29/644—Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/662—Balancing of rotors
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00—Testing static or dynamic balance of machines or structures
    • G01M1/14—Determining imbalance
    • G01M1/16—Determining imbalance by oscillating or rotating the body to be tested
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00—Testing static or dynamic balance of machines or structures
    • G01M1/30—Compensating imbalance
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2230/00—Manufacture
    • F05B2230/60—Assembly methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/40—Use of a multiplicity of similar components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/96—Preventing, counteracting or reducing vibration or noise
    • 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
    • F05D2230/60—Assembly 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
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Manufacture Of Motors, Generators (AREA)
CA2710019A 2007-12-31 2008-12-18 Rotor assembly system and method Abandoned CA2710019A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US11/968,098 2007-12-31
US11/968,098 US7792600B2 (en) 2007-12-31 2007-12-31 System and a method for assembling a rotor stack
PCT/US2008/087466 WO2009088696A2 (en) 2007-12-31 2008-12-18 Rotor assembly system and method

Publications (1)

Publication Number Publication Date
CA2710019A1 true CA2710019A1 (en) 2009-07-16

Family

ID=40738876

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2710019A Abandoned CA2710019A1 (en) 2007-12-31 2008-12-18 Rotor assembly system and method

Country Status (6)

Country Link
US (1) US7792600B2 (https=)
JP (1) JP2011508153A (https=)
CA (1) CA2710019A1 (https=)
DE (1) DE112008003453T5 (https=)
GB (1) GB2468440B (https=)
WO (1) WO2009088696A2 (https=)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108694294A (zh) * 2018-06-20 2018-10-23 西安交通大学 一种航空发动机高压转子装配偏心量预测方法

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8321118B2 (en) * 2008-12-23 2012-11-27 Honeywell International Inc. Operations support systems and methods with power assurance
US9996634B2 (en) * 2010-12-15 2018-06-12 Autodesk, Inc. Computer-aided design and manufacturing system and method for composite part manufacturing method and system
US8959785B2 (en) 2010-12-30 2015-02-24 General Electric Company Apparatus and method for measuring runout
FR2979682B1 (fr) * 2011-09-06 2013-09-13 Valeo Systemes Thermiques Procede d'assemblage d'un groupe moto-ventilateur et dispositif de controle d'assemblage correspondant
US9334739B2 (en) * 2013-08-08 2016-05-10 Solar Turbines Incorporated Gas turbine engine rotor assembly optimization
EP3140513B1 (en) * 2014-05-09 2019-04-24 Ansaldo Energia S.p.A. Method and auxiliary apparatus for balancing a rotor of a gas turbine
US9261382B2 (en) 2014-05-22 2016-02-16 General Electric Company System and method for mechanical runout measurement
US9932832B2 (en) 2014-05-29 2018-04-03 Pratt & Whitney Canada Corp. Method of balancing a spool of a gas turbine engine
CN104376157B (zh) * 2014-11-03 2017-09-19 哈尔滨汽轮机厂有限责任公司 大型汽轮发电机组轴系动静态特性分析计算系统
GB2541701A (en) * 2015-08-27 2017-03-01 Rolls Royce Plc A method of assembling a rotor stack
CN107688675A (zh) * 2016-08-03 2018-02-13 北京机电工程研究所 用于提取机械产品点的同心度误差的方法
IT201600123382A1 (it) * 2016-12-05 2018-06-05 Ansaldo Energia Spa Metodo e dispositivo per controllare il posizionamento di almeno un disco rotorico attorno ad un tirante di un rotore di una turbina a gas
US10627208B2 (en) * 2017-05-05 2020-04-21 General Electric Company Low resistance surface contact topography mapping

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5455778A (en) * 1987-05-29 1995-10-03 Ide; Russell D. Bearing design analysis apparatus and method
US6230501B1 (en) * 1994-04-14 2001-05-15 Promxd Technology, Inc. Ergonomic systems and methods providing intelligent adaptive surfaces and temperature control
JPH11247605A (ja) * 1997-12-26 1999-09-14 United Technol Corp <Utc> タ―ボマシ―ンコンポ―ネントの振動緩衝方法及び装置
US6148494A (en) * 1999-04-08 2000-11-21 General Electric Company Floating fastener tolerance method
US6625507B1 (en) * 2000-02-23 2003-09-23 United Technologies Corporation Method and system for designing a low pressure turbine shaft
US6341419B1 (en) * 2000-02-29 2002-01-29 General Electric Company Loop stacked rotor assembly
US6898547B1 (en) * 2000-09-11 2005-05-24 Axiam, Incorporated Rotor assembly system and method
US20030074244A1 (en) * 2001-04-11 2003-04-17 Braxton Charles R. Distributed energy technology assurance
US20040263099A1 (en) * 2002-07-31 2004-12-30 Maslov Boris A Electric propulsion system
US6908285B2 (en) * 2003-04-08 2005-06-21 General Electric Company Methods and apparatus for assembling rotatable machines
US7021892B2 (en) * 2003-11-19 2006-04-04 Massachusetts Institute Of Technology Method for assembling gas turbine engine components
US7321809B2 (en) * 2003-12-30 2008-01-22 The Boeing Company Methods and systems for analyzing engine unbalance conditions
US7725299B2 (en) * 2004-03-01 2010-05-25 Purdue Research Foundation Multi-tier and multi-domain distributed rapid product configuration and design system
WO2006083320A2 (en) * 2004-07-09 2006-08-10 Board Of Trustees Of Michigan State University Ultra micro gas turbine
US20060089737A1 (en) * 2004-10-08 2006-04-27 General Electric Company Methods and systems for integrating design software modules
US7287958B2 (en) * 2005-01-10 2007-10-30 General Electric Company Methods and apparatus for assembling rotatable machines
JP2007198265A (ja) * 2006-01-26 2007-08-09 Kawasaki Heavy Ind Ltd タービン動翼の配列方法
US7953586B2 (en) * 2006-07-21 2011-05-31 Halliburton Energy Services, Inc. Method and system for designing bottom hole assembly configuration
US7539594B2 (en) * 2006-09-26 2009-05-26 Axiam, Incorporated Method and apparatus for geometric rotor stacking and balancing

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108694294A (zh) * 2018-06-20 2018-10-23 西安交通大学 一种航空发动机高压转子装配偏心量预测方法

Also Published As

Publication number Publication date
US20090171491A1 (en) 2009-07-02
GB2468440A (en) 2010-09-08
DE112008003453T5 (de) 2010-11-04
GB201010160D0 (en) 2010-07-21
US7792600B2 (en) 2010-09-07
WO2009088696A8 (en) 2010-08-12
GB2468440B (en) 2012-06-13
JP2011508153A (ja) 2011-03-10
WO2009088696A2 (en) 2009-07-16
WO2009088696A3 (en) 2009-09-03

Similar Documents

Publication Publication Date Title
CA2710019A1 (en) Rotor assembly system and method
US7912587B2 (en) Method of balancing a gas turbine engine rotor
US9206692B2 (en) Gas turbine rotor assembly balancing method
CN111241609B (zh) 一种航空发动机转静子装配叶尖间隙的预测方法
CN204804885U (zh) 燃气涡轮发动机压缩机转子组件及燃气涡轮发动机
US11499428B2 (en) Rotor balancing method and apparatus
EP1936114A2 (en) Methods and systems for balancing a rotatable member
JP2011508153A5 (https=)
US11698320B2 (en) Rotor balancing method and apparatus
US9932832B2 (en) Method of balancing a spool of a gas turbine engine
EP3663516A1 (en) Component inspection using measured and theoretical moment weights
Lubell et al. Identification and correction of rotor instability in an oil-free gas turbine
CN118190375A (zh) 一种缩比航空发动机双转子模拟试验台设计方法
Gardner Energy efficient engine: High pressure turbine uncooled rig technology report
CN114136266A (zh) 一种双转子航空发动机同轴度检测方法
CN115199352B (zh) 基于发动机振动识别发动机转子的不平衡的方法
US20240230448A1 (en) Computationally balancing a rotating structure
CN115854967B (zh) 一种航空发动机转子装配质量的评价控制方法
CN117993125B (zh) 一种航空发动机滚动轴承剥落故障演化的宏观动力学模型
CN117021017B (zh) 一种基于双目标优化的高压压气机转子装配方法及系统
Srinivasan et al. Aerodynamically excited vibrations of a part-span shrouded fan
Snellgrove et al. Experimental performance evaluation of a supersonic turbine for rocket engine applications

Legal Events

Date Code Title Description
EEER Examination request

Effective date: 20131017

FZDE Discontinued

Effective date: 20141218