DE2503513C2 - Schwingungsdämpfungseinrichtung für eine Turbomaschine - Google Patents

Schwingungsdämpfungseinrichtung für eine Turbomaschine

Info

Publication number
DE2503513C2
DE2503513C2 DE2503513A DE2503513A DE2503513C2 DE 2503513 C2 DE2503513 C2 DE 2503513C2 DE 2503513 A DE2503513 A DE 2503513A DE 2503513 A DE2503513 A DE 2503513A DE 2503513 C2 DE2503513 C2 DE 2503513C2
Authority
DE
Germany
Prior art keywords
damping device
vibration damping
core element
turbine disk
platform
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
Application number
DE2503513A
Other languages
German (de)
English (en)
Other versions
DE2503513A1 (de
Inventor
Richard Loveland Ohio Beal
John Donald West Chester Ohio Hennessey
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
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 DE2503513A1 publication Critical patent/DE2503513A1/de
Application granted granted Critical
Publication of DE2503513C2 publication Critical patent/DE2503513C2/de
Expired 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
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • 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
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/24—Blade-to-blade connections, e.g. for damping vibrations using wire or the like
    • 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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
    • F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
    • F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
    • 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
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/50—Vibration damping features

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)
DE2503513A 1974-05-28 1975-01-29 Schwingungsdämpfungseinrichtung für eine Turbomaschine Expired DE2503513C2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US473680A US3881844A (en) 1974-05-28 1974-05-28 Blade platform vibration dampers

Publications (2)

Publication Number Publication Date
DE2503513A1 DE2503513A1 (de) 1975-12-11
DE2503513C2 true DE2503513C2 (de) 1983-09-22

Family

ID=23880555

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2503513A Expired DE2503513C2 (de) 1974-05-28 1975-01-29 Schwingungsdämpfungseinrichtung für eine Turbomaschine

Country Status (7)

Country Link
US (1) US3881844A (enFirst)
JP (1) JPS5855360B2 (enFirst)
CA (1) CA1013259A (enFirst)
DE (1) DE2503513C2 (enFirst)
FR (1) FR2275641A1 (enFirst)
GB (1) GB1491557A (enFirst)
IT (1) IT1031364B (enFirst)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1114301A (en) * 1979-06-27 1981-12-15 Ivor J. Roberts Locking device for blade mounting
FR2474095B1 (fr) * 1980-01-17 1986-02-28 Rolls Royce Dispositif amortisseur de vibrations pour aubes mobiles de moteur a turbine a gaz
US4347040A (en) * 1980-10-02 1982-08-31 United Technologies Corporation Blade to blade vibration damper
USRE32339E (en) * 1980-10-02 1987-01-27 United Technologies Corporation Blade to blade vibration damper
GB2119026B (en) * 1981-03-25 1984-06-20 Rolls Royce Aerofoil blade mounting
US4355957A (en) * 1981-06-18 1982-10-26 United Technologies Corporation Blade damper
US4482297A (en) * 1981-11-16 1984-11-13 Terry Corporation Bladed rotor assembly
GB2122691B (en) * 1982-06-17 1985-05-01 Rolls Royce Mounting of aerofoil blades
US4767247A (en) * 1987-02-24 1988-08-30 Westinghouse Electric Corp. Apparatus and method for preventing relative blade motion in steam turbine
GB2236809B (en) * 1989-09-22 1994-03-16 Rolls Royce Plc Improvements in or relating to gas turbine engines
FR2674569A1 (fr) * 1991-03-27 1992-10-02 Snecma Disque ailete monobloc avec amortissement des vibrations pour turbomachine.
FR2716931B1 (fr) * 1994-03-03 1996-04-05 Snecma Système d'équilibrage et d'amortissement d'un dique de turbomachine.
DE4436729A1 (de) * 1994-10-14 1996-04-18 Abb Management Ag Beschaufelter Rotor
JPH10325302A (ja) * 1997-05-26 1998-12-08 Ishikawajima Harima Heavy Ind Co Ltd 動翼の制振構造
US6494679B1 (en) * 1999-08-05 2002-12-17 General Electric Company Apparatus and method for rotor damping
US6482533B2 (en) * 2001-03-05 2002-11-19 The Boeing Company Article having imbedded cavity
US6901821B2 (en) * 2001-11-20 2005-06-07 United Technologies Corporation Stator damper anti-rotation assembly
US6736602B2 (en) * 2002-07-31 2004-05-18 United Technologies Corporation Hollow fan hub under blade bumper
EP1703080A1 (de) * 2005-03-03 2006-09-20 ALSTOM Technology Ltd Rotierende Maschine
US8177502B2 (en) * 2008-11-25 2012-05-15 General Electric Company Vane with reduced stress
US20100126018A1 (en) * 2008-11-25 2010-05-27 General Electric Company Method of manufacturing a vane with reduced stress
JP5743072B2 (ja) * 2011-03-25 2015-07-01 三菱日立パワーシステムズ株式会社 タービン動翼の固定構造及びタービン動翼の脱着方法
JP5579112B2 (ja) * 2011-03-28 2014-08-27 三菱重工業株式会社 タービン動翼の固定構造及び翼根バネの脱着方法
EP2573327A1 (en) * 2011-09-20 2013-03-27 Siemens Aktiengesellschaft Damping wire, corresponding rotor blade stage, steam turbine and producing method
RU2526129C2 (ru) * 2012-09-10 2014-08-20 Открытое акционерное общество "Омское моторостроительное конструкторское бюро" (ОАО ОМБК) Рабочее колесо осевой турбомашины гтд
EP2806106A1 (de) 2013-05-23 2014-11-26 MTU Aero Engines GmbH Turbomaschinenschaufel mit einem Impulskörper
US9765625B2 (en) * 2013-05-23 2017-09-19 MTU Aero Engines AG Turbomachine blade
US20170067349A1 (en) * 2015-09-03 2017-03-09 General Electric Company Damper pin for a turbine blade
US10584597B2 (en) 2015-09-03 2020-03-10 General Electric Company Variable cross-section damper pin for a turbine blade
US10472975B2 (en) 2015-09-03 2019-11-12 General Electric Company Damper pin having elongated bodies for damping adjacent turbine blades
US10443408B2 (en) * 2015-09-03 2019-10-15 General Electric Company Damper pin for a turbine blade
US10385701B2 (en) 2015-09-03 2019-08-20 General Electric Company Damper pin for a turbine blade
DE102016205997A1 (de) * 2016-04-11 2017-10-12 MTU Aero Engines AG Leitschaufelsegment
US11208903B1 (en) 2020-11-20 2021-12-28 Solar Turbines Incorporated Stiffness coupling and vibration damping for turbine blade shroud
US11976565B2 (en) * 2022-07-27 2024-05-07 Ge Infrastructure Technology Llc Nested damper pin and vibration dampening system for turbine nozzle or blade
US12371998B2 (en) 2023-06-29 2025-07-29 Ge Infrastructure Technology Llc Nested damper pin and vibration dampening system for turbine nozzle or blade

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1856786A (en) * 1931-10-16 1932-05-03 Gen Electric Bucket wheel and like rotating member
US2840299A (en) * 1952-09-22 1958-06-24 Thompson Prod Inc Axial flow compressor rotor
US2873088A (en) * 1953-05-21 1959-02-10 Gen Electric Lightweight rotor construction

Also Published As

Publication number Publication date
GB1491557A (en) 1977-11-09
IT1031364B (it) 1979-04-30
CA1013259A (en) 1977-07-05
JPS5855360B2 (ja) 1983-12-09
DE2503513A1 (de) 1975-12-11
JPS50153305A (enFirst) 1975-12-10
FR2275641B1 (enFirst) 1980-01-25
US3881844A (en) 1975-05-06
FR2275641A1 (fr) 1976-01-16

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Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee