IT1031937B - Sistema di bilanciamento di turbomotore a gas evitante il successivo bilanciamento di parti sostitutte - Google Patents

Sistema di bilanciamento di turbomotore a gas evitante il successivo bilanciamento di parti sostitutte

Info

Publication number
IT1031937B
IT1031937B IT20509/75A IT2050975A IT1031937B IT 1031937 B IT1031937 B IT 1031937B IT 20509/75 A IT20509/75 A IT 20509/75A IT 2050975 A IT2050975 A IT 2050975A IT 1031937 B IT1031937 B IT 1031937B
Authority
IT
Italy
Prior art keywords
balancing
turbomotor
gas
replaced parts
avoiding subsequent
Prior art date
Application number
IT20509/75A
Other languages
English (en)
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Application granted granted Critical
Publication of IT1031937B publication Critical patent/IT1031937B/it

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
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
    • 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
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/32—Correcting- or balancing-weights or equivalent means for balancing rotating bodies, e.g. vehicle wheels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/32—Correcting- or balancing-weights or equivalent means for balancing rotating bodies, e.g. vehicle wheels
    • F16F15/322—Correcting- or balancing-weights or equivalent means for balancing rotating bodies, e.g. vehicle wheels the rotating body being a shaft
    • 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
    • G01M1/32—Compensating imbalance by adding material to the body to be tested, e.g. by correcting-weights
    • 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
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49229—Prime mover or fluid pump making
    • Y10T29/49231—I.C. [internal combustion] engine making
    • Y10T29/49233—Repairing, converting, servicing or salvaging
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT20509/75A 1974-02-25 1975-02-21 Sistema di bilanciamento di turbomotore a gas evitante il successivo bilanciamento di parti sostitutte IT1031937B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US445675A US3916495A (en) 1974-02-25 1974-02-25 Method and means for balancing a gas turbine engine

Publications (1)

Publication Number Publication Date
IT1031937B true IT1031937B (it) 1979-05-10

Family

ID=23769799

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20509/75A IT1031937B (it) 1974-02-25 1975-02-21 Sistema di bilanciamento di turbomotore a gas evitante il successivo bilanciamento di parti sostitutte

Country Status (7)

Country Link
US (1) US3916495A (it)
JP (1) JPS591337B2 (it)
BE (1) BE825926A (it)
DE (1) DE2507695C2 (it)
FR (1) FR2262197B1 (it)
GB (1) GB1491961A (it)
IT (1) IT1031937B (it)

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US4097194A (en) * 1976-03-22 1978-06-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Redundant disc
JPS5924242B2 (ja) * 1976-03-31 1984-06-08 株式会社東芝 タ−ビンロ−タ−構体
US4177692A (en) * 1977-11-25 1979-12-11 General Motors Corporation Shaft balancing
US4191485A (en) * 1978-10-30 1980-03-04 Carrier Corporation Apparatus for securing a wheel to a rotatable shaft of a turbo-machine
US4349291A (en) * 1978-10-27 1982-09-14 Carrier Corporation Apparatus for securing a wheel to a rotatable shaft of a turbomachine
FR2544387B1 (fr) * 1983-04-15 1985-06-14 Snecma Appareillage pour le transfert d'un module de turbine complet d'une machine d'equilibrage a un moteur et vice versa, et procede pour la mise en oeuvre dudit appareillage
JPS6185501A (ja) * 1984-10-03 1986-05-01 Ngk Insulators Ltd セラミツクスロ−タ−のバランス修正方法並びにそれに用いられる修正治具
JPS61217737A (ja) * 1985-03-23 1986-09-27 Ngk Insulators Ltd タ−ボチャ−ジャ−ロ−タの回転試験方法並びにそのための装置
DE3532929A1 (de) * 1985-09-14 1987-03-26 Mtu Muenchen Gmbh Einrichtung zur verbindung einander konzentrisch benachbarter rotorbauteile von maschinen, insbesondere stroemungsmaschinen
DE8701379U1 (it) * 1987-01-29 1988-06-01 Carl Schenck Ag, 6100 Darmstadt, De
US4784012A (en) * 1987-09-08 1988-11-15 United Technologies Corporation Rotor balance system
US4835827A (en) * 1987-09-08 1989-06-06 United Technologies Corporation Method of balancing a rotor
US4767272A (en) * 1987-10-14 1988-08-30 United Technologies Corporation Method for reducing blade tip variation of a bladed rotor
US4817455A (en) * 1987-10-15 1989-04-04 United Technologies Corporation Gas turbine engine balancing
JP2756117B2 (ja) * 1987-11-25 1998-05-25 株式会社日立製作所 ガスタービンロータ
US4879792A (en) * 1988-11-07 1989-11-14 Unitedtechnologies Corporation Method of balancing rotors
US5214585A (en) * 1989-06-30 1993-05-25 General Electric Company Balancing method and product
DE3924829A1 (de) * 1989-07-27 1991-02-07 Mtu Muenchen Gmbh Verdichter-oder turbinenlaeufer, insbesondere fuer gasturbinentriebwerke
FR2667365B1 (fr) * 1990-10-02 1993-01-08 Europ Propulsion Roue de turbine en materiau composite.
DE4120197A1 (de) * 1991-06-19 1992-12-24 Audi Ag Verfahren zum auswuchten zumindest zweier miteinander verbundener rotoren
GB2265964B (en) * 1992-04-07 1995-03-15 Rolls Royce Rotor balancing
WO1996018817A1 (en) * 1994-12-14 1996-06-20 The Ingersoll-Dresser Pump Company Impeller
US5628621A (en) * 1996-07-26 1997-05-13 General Electric Company Reinforced compressor rotor coupling
US5725353A (en) * 1996-12-04 1998-03-10 United Technologies Corporation Turbine engine rotor disk
JP3310907B2 (ja) * 1997-06-12 2002-08-05 三菱重工業株式会社 ガスタービンフランジ接合面のシール構造
DE19857554A1 (de) 1998-12-14 2000-06-15 Rolls Royce Deutschland Verbindungsanordnung zweier Laufscheiben einer Axial-Strömungsmaschine
US6572337B1 (en) * 1999-11-30 2003-06-03 General Electric Co. Turbine rotor torque transmission
SE520612C2 (sv) * 2000-05-09 2003-07-29 Turbec Ab En rotorenhet och en metod för dess balansering
US6595751B1 (en) * 2000-06-08 2003-07-22 The Boeing Company Composite rotor having recessed radial splines for high torque applications
GB0116479D0 (en) * 2001-07-06 2001-08-29 Rolls Royce Plc Coupling arrangement
JP4007062B2 (ja) * 2002-05-22 2007-11-14 株式会社日立製作所 ガスタービン及びガスタービン発電装置
GB0216355D0 (en) * 2002-07-13 2002-08-21 Rolls Royce Plc Anti-score plates
US6994519B2 (en) * 2003-05-20 2006-02-07 General Electric Company Apparatus and methods for coupling axially aligned turbine rotors
US7234916B2 (en) * 2004-09-16 2007-06-26 General Electric Company Method and apparatus for balancing gas turbine engines
US7448221B2 (en) * 2004-12-17 2008-11-11 United Technologies Corporation Turbine engine rotor stack
US7371042B2 (en) * 2004-12-21 2008-05-13 General Electric Company Method and apparatus for balancing gas turbine engines
US20070071545A1 (en) * 2005-08-26 2007-03-29 Honeywell International, Inc. Lubricated Hirth serration coupling
US7685876B2 (en) * 2006-12-20 2010-03-30 General Electric Company Methods and systems for balancing a rotatable member
FR2911959B1 (fr) * 2007-01-29 2009-04-24 Snecma Sa Procede d'equilibrage modulaire de rotor de turbomachine
US8051709B2 (en) * 2009-02-25 2011-11-08 General Electric Company Method and apparatus for pre-spinning rotor forgings
US8650885B2 (en) * 2009-12-22 2014-02-18 United Technologies Corporation Retaining member for use with gas turbine engine shaft and method of assembly
EP2397651A1 (en) 2010-06-17 2011-12-21 Siemens Aktiengesellschaft Balance correction weight providing constant mass
US9145771B2 (en) 2010-07-28 2015-09-29 United Technologies Corporation Rotor assembly disk spacer for a gas turbine engine
US20130323074A1 (en) * 2012-05-31 2013-12-05 Hamilton Sundstrand Corporation Friction welded turbine disk and shaft
US20140099210A1 (en) * 2012-10-09 2014-04-10 General Electric Company System for gas turbine rotor and section coupling
EP2789797B1 (en) * 2013-04-08 2018-08-08 Ansaldo Energia Switzerland AG Rotor
US9143022B2 (en) 2013-07-29 2015-09-22 General Electric Company System and method for rebalancing generator rotor in-situ
US9093886B2 (en) 2013-07-29 2015-07-28 General Electric Company System and method for rebalancing generator rotor in-situ
US9083220B2 (en) 2013-07-29 2015-07-14 General Electric Company Method for servicing generator rotor in-situ
US9334850B2 (en) 2013-09-05 2016-05-10 General Electric Company System and method for centering wye ring in-situ
US10107256B2 (en) 2013-09-05 2018-10-23 General Electric Company System for centering wye ring in-situ
EP3219911A1 (de) * 2016-03-17 2017-09-20 Siemens Aktiengesellschaft Rotor einer gasturbine mit verschraubten rotorscheiben
US10927709B2 (en) * 2018-06-05 2021-02-23 Raytheon Technologies Corporation Turbine bearing stack load bypass nut
EP3896252B1 (en) * 2020-04-16 2023-04-12 ANSALDO ENERGIA S.p.A. Method and assembly for controlling the positioning of at least one rotor disc about a tie-rod of a partially assembled rotor
EP4172469A1 (en) * 2020-09-03 2023-05-03 Siemens Energy Global GmbH & Co. KG Rotor assembly for a gas turbine
US11732585B2 (en) * 2021-01-28 2023-08-22 General Electric Company Trapped rotatable weights to improve rotor balance

Family Cites Families (7)

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Publication number Priority date Publication date Assignee Title
US1776125A (en) * 1928-09-17 1930-09-16 Gen Electric Method of and means for balancing rotors
US2798383A (en) * 1955-05-25 1957-07-09 Gen Motors Corp Rotor balancing bolt lock
DE1128706B (de) * 1957-05-01 1962-04-26 Avco Mfg Corp Gasturbinenanlage mit einer sich durch die Verdichterantriebs-turbine erstreckenden Antriebswelle der Nutzleistungsturbine
US3097824A (en) * 1958-11-26 1963-07-16 Bendix Corp Turbine, wheel containment
US3304053A (en) * 1965-04-12 1967-02-14 United Aircraft Corp Balancing weights for a multistage fluid motor
US3736811A (en) * 1971-08-19 1973-06-05 Gen Electric Balance weight attachment for turbine wheels
US3761205A (en) * 1972-03-20 1973-09-25 Avco Corp Easily maintainable gas turbine engine

Also Published As

Publication number Publication date
FR2262197B1 (it) 1981-12-11
JPS591337B2 (ja) 1984-01-11
DE2507695A1 (de) 1975-08-28
US3916495A (en) 1975-11-04
DE2507695C2 (de) 1986-07-03
FR2262197A1 (it) 1975-09-19
BE825926A (fr) 1975-06-16
GB1491961A (en) 1977-11-16
JPS50124008A (it) 1975-09-29

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Legal Events

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TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19940224