DE60031027D1 - Selbstsichernder Schwingungsdämpfer für Turbinenschaufeln - Google Patents

Selbstsichernder Schwingungsdämpfer für Turbinenschaufeln

Info

Publication number
DE60031027D1
DE60031027D1 DE60031027T DE60031027T DE60031027D1 DE 60031027 D1 DE60031027 D1 DE 60031027D1 DE 60031027 T DE60031027 T DE 60031027T DE 60031027 T DE60031027 T DE 60031027T DE 60031027 D1 DE60031027 D1 DE 60031027D1
Authority
DE
Germany
Prior art keywords
self
vibration damper
turbine blades
locking vibration
locking
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 - Lifetime
Application number
DE60031027T
Other languages
English (en)
Other versions
DE60031027T2 (de
Inventor
Philip Francis Stec
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
Application granted granted Critical
Publication of DE60031027D1 publication Critical patent/DE60031027D1/de
Publication of DE60031027T2 publication Critical patent/DE60031027T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
DE60031027T 1999-04-01 2000-02-24 Selbstsichernder Schwingungsdämpfer für Turbinenschaufeln Expired - Lifetime DE60031027T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/283,429 US6171058B1 (en) 1999-04-01 1999-04-01 Self retaining blade damper
US283429 1999-04-01

Publications (2)

Publication Number Publication Date
DE60031027D1 true DE60031027D1 (de) 2006-11-16
DE60031027T2 DE60031027T2 (de) 2007-05-16

Family

ID=23086018

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60031027T Expired - Lifetime DE60031027T2 (de) 1999-04-01 2000-02-24 Selbstsichernder Schwingungsdämpfer für Turbinenschaufeln

Country Status (4)

Country Link
US (1) US6171058B1 (de)
EP (1) EP1041248B1 (de)
JP (1) JP4460103B2 (de)
DE (1) DE60031027T2 (de)

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US6471484B1 (en) 2001-04-27 2002-10-29 General Electric Company Methods and apparatus for damping rotor assembly vibrations
US6796408B2 (en) * 2002-09-13 2004-09-28 The Boeing Company Method for vibration damping using superelastic alloys
US6776583B1 (en) * 2003-02-27 2004-08-17 General Electric Company Turbine bucket damper pin
JP2005233141A (ja) 2004-02-23 2005-09-02 Mitsubishi Heavy Ind Ltd 動翼およびその動翼を用いたガスタービン
US7066714B2 (en) * 2004-03-26 2006-06-27 United Technologies Corporation High speed rotor assembly shroud
US7121802B2 (en) * 2004-07-13 2006-10-17 General Electric Company Selectively thinned turbine blade
US7097429B2 (en) * 2004-07-13 2006-08-29 General Electric Company Skirted turbine blade
FR2874402B1 (fr) * 2004-08-23 2006-09-29 Snecma Moteurs Sa Aube de rotor d'un compresseur ou d'une turbine a gaz
US7121800B2 (en) * 2004-09-13 2006-10-17 United Technologies Corporation Turbine blade nested seal damper assembly
US7467924B2 (en) * 2005-08-16 2008-12-23 United Technologies Corporation Turbine blade including revised platform
US7244101B2 (en) * 2005-10-04 2007-07-17 General Electric Company Dust resistant platform blade
US7322797B2 (en) * 2005-12-08 2008-01-29 General Electric Company Damper cooled turbine blade
EP1820872B1 (de) * 2006-01-10 2011-03-02 Siemens Aktiengesellschaft Verfahren zur Vorbereitung von Turbinenschaufeln mit einer Abdeckleiste mit Steckverbindung für eine anschließende Behandlung, sowie Turbinenschaufel dafür
US7731482B2 (en) * 2006-06-13 2010-06-08 General Electric Company Bucket vibration damper system
US8884182B2 (en) * 2006-12-11 2014-11-11 General Electric Company Method of modifying the end wall contour in a turbine using laser consolidation and the turbines derived therefrom
GB2446812A (en) * 2007-02-21 2008-08-27 Rolls Royce Plc Damping member positioned between blades of an aerofoil assembly
US20090096174A1 (en) * 2007-02-28 2009-04-16 United Technologies Corporation Blade outer air seal for a gas turbine engine
US8011892B2 (en) * 2007-06-28 2011-09-06 United Technologies Corporation Turbine blade nested seal and damper assembly
US8182208B2 (en) * 2007-07-10 2012-05-22 United Technologies Corp. Gas turbine systems involving feather seals
US8435008B2 (en) * 2008-10-17 2013-05-07 United Technologies Corporation Turbine blade including mistake proof feature
US8672626B2 (en) 2010-04-21 2014-03-18 United Technologies Corporation Engine assembled seal
FR2970033B1 (fr) * 2011-01-04 2015-10-16 Turbomeca Procede d'amortissement de pale de turbine a gaz et amortisseur de vibration de mise en oeuvre
US10287897B2 (en) * 2011-09-08 2019-05-14 General Electric Company Turbine rotor blade assembly and method of assembling same
US9587495B2 (en) 2012-06-29 2017-03-07 United Technologies Corporation Mistake proof damper pocket seals
BR112015000081A2 (pt) 2012-06-30 2017-06-27 Gen Electric estrutura de vedação de pá de turbina.
US9309782B2 (en) 2012-09-14 2016-04-12 General Electric Company Flat bottom damper pin for turbine blades
US10247023B2 (en) 2012-09-28 2019-04-02 United Technologies Corporation Seal damper with improved retention
US10641109B2 (en) * 2013-03-13 2020-05-05 United Technologies Corporation Mass offset for damping performance
EP2971555B1 (de) * 2013-03-13 2021-04-28 Raytheon Technologies Corporation Rotoranordnung mit dämpferdichtung zwischen den schaufeln
US10036260B2 (en) 2013-03-13 2018-07-31 United Technologies Corporation Damper mass distribution to prevent damper rotation
EP3044420A2 (de) 2013-09-11 2016-07-20 General Electric Company Schichtarchitektur für eine integrierte plattform und dämpferrückhaltefunktionen in cmc-turbinenschaufeln
EP3047107B1 (de) 2013-09-17 2022-02-23 Raytheon Technologies Corporation Plattformdichtungskühlung für gasturbinentriebwerkskomponenten
EP2881544A1 (de) * 2013-12-09 2015-06-10 Siemens Aktiengesellschaft Schaufelprofil für eine Gasturbine und zugehörige Anordnung
US9856737B2 (en) * 2014-03-27 2018-01-02 United Technologies Corporation Blades and blade dampers for gas turbine engines
US10689988B2 (en) 2014-06-12 2020-06-23 Raytheon Technologies Corporation Disk lug impingement for gas turbine engine airfoil
US9822644B2 (en) * 2015-02-27 2017-11-21 Pratt & Whitney Canada Corp. Rotor blade vibration damper
US9810075B2 (en) 2015-03-20 2017-11-07 United Technologies Corporation Faceted turbine blade damper-seal
US9920637B2 (en) 2015-04-07 2018-03-20 United Technologies Corporation Gas turbine engine damping device
US10196915B2 (en) * 2015-06-01 2019-02-05 United Technologies Corporation Trailing edge platform seals
US11092018B2 (en) 2015-08-07 2021-08-17 Transportation Ip Holdings, Llc Underplatform damping members and methods for turbocharger assemblies
US10472975B2 (en) 2015-09-03 2019-11-12 General Electric Company Damper pin having elongated bodies for damping adjacent turbine blades
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
US10443408B2 (en) 2015-09-03 2019-10-15 General Electric Company Damper pin for a turbine blade
US10100648B2 (en) 2015-12-07 2018-10-16 United Technologies Corporation Damper seal installation features
ES2891084T3 (es) * 2016-04-27 2022-01-26 MTU Aero Engines AG Conjunto de paletas de turbomaquinaria
US10662784B2 (en) 2016-11-28 2020-05-26 Raytheon Technologies Corporation Damper with varying thickness for a blade
US10677073B2 (en) 2017-01-03 2020-06-09 Raytheon Technologies Corporation Blade platform with damper restraint
US10648347B2 (en) * 2017-01-03 2020-05-12 General Electric Company Damping inserts and methods for shrouded turbine blades
US10731479B2 (en) * 2017-01-03 2020-08-04 Raytheon Technologies Corporation Blade platform with damper restraint
US10519785B2 (en) 2017-02-14 2019-12-31 General Electric Company Turbine blades having damper pin slot features and methods of fabricating the same
EP3438410B1 (de) 2017-08-01 2021-09-29 General Electric Company Dichtungssystem für eine rotationsmaschine
US10975714B2 (en) * 2018-11-22 2021-04-13 Pratt & Whitney Canada Corp. Rotor assembly with blade sealing tab
US11242756B2 (en) 2020-05-04 2022-02-08 General Electric Company Damping coating with a constraint layer
US11085303B1 (en) 2020-06-16 2021-08-10 General Electric Company Pressurized damping fluid injection for damping turbine blade vibration
US11143036B1 (en) 2020-08-20 2021-10-12 General Electric Company Turbine blade with friction and impact vibration damping elements

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GB879444A (en) * 1958-09-05 1961-10-11 Gen Electric Improvements in two-tier turbine and compressor blades
US4101245A (en) * 1976-12-27 1978-07-18 United Technologies Corporation Interblade damper and seal for turbomachinery rotor
US4455122A (en) * 1981-12-14 1984-06-19 United Technologies Corporation Blade to blade vibration damper
US4568247A (en) * 1984-03-29 1986-02-04 United Technologies Corporation Balanced blade vibration damper
GB2194000A (en) * 1986-08-13 1988-02-24 Rolls Royce Plc Turbine rotor assembly with seal plates
GB2228541B (en) * 1989-02-23 1993-04-14 Rolls Royce Plc Device for damping vibrations in turbomachinery blades
US5281097A (en) * 1992-11-20 1994-01-25 General Electric Company Thermal control damper for turbine rotors
US5460489A (en) * 1994-04-12 1995-10-24 United Technologies Corporation Turbine blade damper and seal
US5478207A (en) * 1994-09-19 1995-12-26 General Electric Company Stable blade vibration damper for gas turbine engine
GB9609721D0 (en) * 1996-05-09 1996-07-10 Rolls Royce Plc Vibration damping
US5827047A (en) * 1996-06-27 1998-10-27 United Technologies Corporation Turbine blade damper and seal
US5785499A (en) * 1996-12-24 1998-07-28 United Technologies Corporation Turbine blade damper and seal
US5803710A (en) * 1996-12-24 1998-09-08 United Technologies Corporation Turbine engine rotor blade platform sealing and vibration damping device
US5924699A (en) * 1996-12-24 1999-07-20 United Technologies Corporation Turbine blade platform seal

Also Published As

Publication number Publication date
US6171058B1 (en) 2001-01-09
JP2000291407A (ja) 2000-10-17
EP1041248A3 (de) 2002-07-03
DE60031027T2 (de) 2007-05-16
JP4460103B2 (ja) 2010-05-12
EP1041248A2 (de) 2000-10-04
EP1041248B1 (de) 2006-10-04

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Legal Events

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