EP1136653A3 - Beschaufelung mit Dämpfungselementen - Google Patents

Beschaufelung mit Dämpfungselementen Download PDF

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Publication number
EP1136653A3
EP1136653A3 EP01105747A EP01105747A EP1136653A3 EP 1136653 A3 EP1136653 A3 EP 1136653A3 EP 01105747 A EP01105747 A EP 01105747A EP 01105747 A EP01105747 A EP 01105747A EP 1136653 A3 EP1136653 A3 EP 1136653A3
Authority
EP
European Patent Office
Prior art keywords
blading
area
rotor
blades
bucket
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.)
Withdrawn
Application number
EP01105747A
Other languages
English (en)
French (fr)
Other versions
EP1136653A2 (de
Inventor
Jaroslaw Dr. Szwedowicz
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 Technology GmbH
Original Assignee
Alstom Schweiz AG
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 Alstom Schweiz AG filed Critical Alstom Schweiz AG
Publication of EP1136653A2 publication Critical patent/EP1136653A2/de
Publication of EP1136653A3 publication Critical patent/EP1136653A3/de
Withdrawn legal-status Critical Current

Links

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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/04Antivibration arrangements
    • F01D25/06Antivibration arrangements for preventing blade vibration
    • 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
    • F01D5/12Blades
    • F01D5/22Blade-to-blade connections, e.g. for damping vibrations
    • 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
    • F05D2250/00Geometry
    • F05D2250/70Shape
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Die vorliegende Erfindung betrifft eine Beschaufelung mit Dämpfungselementen, die einen Rotor (5) sowie am Umfang des Rotors eingefügte Schaufeln (6) mit Schaufelplattform (7), Schaufelhals (14) und Schaufelfuß (8) umfasst. Zwischen jeweils benachbarten Schaufeln (6) ist ein Dämpfungselement (9) angeordnet, das bei einer Rotation des Rotors (5) über Reibschluss mit zumindest einem ersten Bereich (1, 2) einer ersten und einem zweiten Bereich (3) einer zweiten der jeweils benachbarten Schaufeln (6) in Verbindung steht. Die Beschaufelung zeichnet sich dadurch aus, dass das Dämpfungselement (9) so ausgestaltet und zwischen der ersten und der zweiten Schaufel angeordnet ist, dass der erste Bereich (1, 2) und der zweite Bereich (3) an in radialer Richtung deutlich voneinander beabstandeten Positionen liegen.
Mit dieser Beschaufelung wird eine effiziente Schwingungsdämpfung auch bei geringen Relativbewegungen zwischen benachbarten Schaufeln erreicht.
EP01105747A 2000-03-22 2001-03-08 Beschaufelung mit Dämpfungselementen Withdrawn EP1136653A3 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10014198 2000-03-22
DE10014198A DE10014198A1 (de) 2000-03-22 2000-03-22 Beschaufelung mit Dämpfungselementen

Publications (2)

Publication Number Publication Date
EP1136653A2 EP1136653A2 (de) 2001-09-26
EP1136653A3 true EP1136653A3 (de) 2003-10-15

Family

ID=7635892

Family Applications (1)

Application Number Title Priority Date Filing Date
EP01105747A Withdrawn EP1136653A3 (de) 2000-03-22 2001-03-08 Beschaufelung mit Dämpfungselementen

Country Status (3)

Country Link
US (1) US6450769B2 (de)
EP (1) EP1136653A3 (de)
DE (1) DE10014198A1 (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1180196B1 (de) * 1999-05-14 2005-02-16 Siemens Aktiengesellschaft Strömungsmaschine mit einem dichtsystem für einen rotor
US6851932B2 (en) * 2003-05-13 2005-02-08 General Electric Company Vibration damper assembly for the buckets of a turbine
US7367123B2 (en) * 2005-05-12 2008-05-06 General Electric Company Coated bucket damper pin and related method
US7270517B2 (en) * 2005-10-06 2007-09-18 Siemens Power Generation, Inc. Turbine blade with vibration damper
DE102006041322A1 (de) * 2006-09-01 2008-04-24 Rolls-Royce Deutschland Ltd & Co Kg Dämpfungs- und Dichtungssystem für Turbinenschaufeln
GB0814018D0 (en) * 2008-08-01 2008-09-10 Rolls Royce Plc Vibration damper
US8137072B2 (en) * 2008-10-31 2012-03-20 Solar Turbines Inc. Turbine blade including a seal pocket
US8393869B2 (en) 2008-12-19 2013-03-12 Solar Turbines Inc. Turbine blade assembly including a damper
US8834123B2 (en) * 2009-12-29 2014-09-16 Rolls-Royce Corporation Turbomachinery component
FR2962481B1 (fr) * 2010-07-12 2012-08-31 Snecma Propulsion Solide Amortisseur de vibrations a bras de levier pour aube d'un rotor de moteur a turbine a gaz
US8876478B2 (en) 2010-11-17 2014-11-04 General Electric Company Turbine blade combined damper and sealing pin and related method
US8915718B2 (en) * 2012-04-24 2014-12-23 United Technologies Corporation Airfoil including damper member
US9140132B2 (en) 2012-05-31 2015-09-22 Solar Turbines Incorporated Turbine blade support
DE102012106789B4 (de) * 2012-07-26 2022-10-27 Ihi Charging Systems International Gmbh Verstellbarer Leitapparat für eine Turbine, Turbine für einen Abgasturbolader und Abgasturbolader
US9309782B2 (en) 2012-09-14 2016-04-12 General Electric Company Flat bottom damper pin for turbine blades
US9353629B2 (en) 2012-11-30 2016-05-31 Solar Turbines Incorporated Turbine blade apparatus
US10584597B2 (en) 2015-09-03 2020-03-10 General Electric Company Variable cross-section damper pin for a turbine blade
US10385701B2 (en) 2015-09-03 2019-08-20 General Electric Company 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
DE102016205997A1 (de) * 2016-04-11 2017-10-12 MTU Aero Engines AG Leitschaufelsegment
US10662784B2 (en) 2016-11-28 2020-05-26 Raytheon Technologies Corporation Damper with varying thickness for a blade
US10731479B2 (en) * 2017-01-03 2020-08-04 Raytheon Technologies Corporation Blade platform with damper restraint
US10677073B2 (en) 2017-01-03 2020-06-09 Raytheon Technologies Corporation Blade platform with damper restraint
EP3438410B1 (de) 2017-08-01 2021-09-29 General Electric Company Dichtungssystem für eine rotationsmaschine
GB2573520A (en) * 2018-05-08 2019-11-13 Rolls Royce Plc A damper
DE102018221533A1 (de) 2018-12-12 2020-06-18 MTU Aero Engines AG Turbomaschinen Schaufelanordnung
FR3096734B1 (fr) * 2019-05-29 2021-12-31 Safran Aircraft Engines Ensemble pour turbomachine

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3666376A (en) * 1971-01-05 1972-05-30 United Aircraft Corp Turbine blade damper
US4182598A (en) * 1977-08-29 1980-01-08 United Technologies Corporation Turbine blade damper
SU1127979A1 (ru) * 1983-02-23 1984-12-07 Предприятие П/Я Р-6837 Рабочее колесо турбомашины
EP0509838A1 (de) * 1991-04-19 1992-10-21 General Electric Company Vibrationsdämpfung von Gasturbinenschaufeln

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4872812A (en) * 1987-08-05 1989-10-10 General Electric Company Turbine blade plateform sealing and vibration damping apparatus
US4872810A (en) * 1988-12-14 1989-10-10 United Technologies Corporation Turbine rotor retention system
US4936749A (en) * 1988-12-21 1990-06-26 General Electric Company Blade-to-blade vibration damper
US5478207A (en) * 1994-09-19 1995-12-26 General Electric Company Stable blade vibration damper for gas turbine engine
US6042336A (en) * 1998-11-25 2000-03-28 United Technologies Corporation Offset center of gravity radial damper

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3666376A (en) * 1971-01-05 1972-05-30 United Aircraft Corp Turbine blade damper
US4182598A (en) * 1977-08-29 1980-01-08 United Technologies Corporation Turbine blade damper
SU1127979A1 (ru) * 1983-02-23 1984-12-07 Предприятие П/Я Р-6837 Рабочее колесо турбомашины
EP0509838A1 (de) * 1991-04-19 1992-10-21 General Electric Company Vibrationsdämpfung von Gasturbinenschaufeln

Also Published As

Publication number Publication date
US20010024614A1 (en) 2001-09-27
DE10014198A1 (de) 2001-09-27
US6450769B2 (en) 2002-09-17
EP1136653A2 (de) 2001-09-26

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