JP2000161005A - タ―ビンロ―タのブレ―ドに付随して起こる半径方向の振動を減衰するダンパ - Google Patents

タ―ビンロ―タのブレ―ドに付随して起こる半径方向の振動を減衰するダンパ

Info

Publication number
JP2000161005A
JP2000161005A JP11334256A JP33425699A JP2000161005A JP 2000161005 A JP2000161005 A JP 2000161005A JP 11334256 A JP11334256 A JP 11334256A JP 33425699 A JP33425699 A JP 33425699A JP 2000161005 A JP2000161005 A JP 2000161005A
Authority
JP
Japan
Prior art keywords
damper
blades
blade
platform
disk
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.)
Pending
Application number
JP11334256A
Other languages
English (en)
Japanese (ja)
Other versions
JP2000161005A5 (enExample
Inventor
Charles A Bulgrin
エー ベルグリン チャールズ
John O Struthers
オー ストラサーズ ジョン
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of JP2000161005A publication Critical patent/JP2000161005A/ja
Publication of JP2000161005A5 publication Critical patent/JP2000161005A5/ja
Pending 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
    • F01D5/26—Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
    • 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
    • F16F15/10—Suppression of vibrations in rotating systems by making use of members moving with the system
    • 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
    • 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)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
JP11334256A 1998-11-25 1999-11-25 タ―ビンロ―タのブレ―ドに付随して起こる半径方向の振動を減衰するダンパ Pending JP2000161005A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/199,615 US6042336A (en) 1998-11-25 1998-11-25 Offset center of gravity radial damper
US09/199615 1998-11-25

Publications (2)

Publication Number Publication Date
JP2000161005A true JP2000161005A (ja) 2000-06-13
JP2000161005A5 JP2000161005A5 (enExample) 2007-01-18

Family

ID=22738302

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11334256A Pending JP2000161005A (ja) 1998-11-25 1999-11-25 タ―ビンロ―タのブレ―ドに付随して起こる半径方向の振動を減衰するダンパ

Country Status (5)

Country Link
US (1) US6042336A (enExample)
EP (1) EP1004749B1 (enExample)
JP (1) JP2000161005A (enExample)
KR (1) KR100584798B1 (enExample)
DE (1) DE69919491T2 (enExample)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101994526A (zh) * 2009-08-03 2011-03-30 通用电气公司 用于周向燕尾形转子叶片附接系统的锁定隔离件组件
JP2013139777A (ja) * 2012-01-05 2013-07-18 General Electric Co <Ge> タービンロータリムシールの軸方向保持組立体
JP2013537953A (ja) * 2010-09-24 2013-10-07 シーメンス アクティエンゲゼルシャフト ブレード配列、及び当該ブレード配列を具備するガスタービン
WO2022201926A1 (ja) 2021-03-24 2022-09-29 三菱重工航空エンジン株式会社 タービン動翼及びタービン

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2372875A1 (en) * 1999-05-14 2000-11-23 Siemens Aktiengesellschaft Turbomachine with a sealing system for a rotor
DE10014198A1 (de) * 2000-03-22 2001-09-27 Alstom Power Nv Beschaufelung mit Dämpfungselementen
FR2896289B1 (fr) * 2006-01-13 2008-03-28 Snecma Sa Masselotte d'equilibrage, disque de rotor en etant equipe, rotor et moteur d'aeronef les comportant
US7806410B2 (en) 2007-02-20 2010-10-05 United Technologies Corporation Damping device for a stationary labyrinth seal
GB0814018D0 (en) * 2008-08-01 2008-09-10 Rolls Royce Plc Vibration damper
US8137067B2 (en) * 2008-11-05 2012-03-20 General Electric Company Turbine with interrupted purge flow
US8215915B2 (en) * 2009-05-15 2012-07-10 Siemens Energy, Inc. Blade closing key system for a turbine engine
US8745990B2 (en) * 2009-07-27 2014-06-10 Rolls-Royce Corporation Gas turbine engine with integrated electric starter/generator
US8834123B2 (en) * 2009-12-29 2014-09-16 Rolls-Royce Corporation Turbomachinery component
US9920625B2 (en) 2011-01-13 2018-03-20 Siemens Energy, Inc. Turbine blade with laterally biased airfoil and platform centers of mass
US10641109B2 (en) * 2013-03-13 2020-05-05 United Technologies Corporation Mass offset for damping performance
KR102000350B1 (ko) 2017-09-28 2019-07-15 두산중공업 주식회사 압축기 블레이드, 압축기 블레이드용 압축기 블레이드 댐퍼, 압축기 블레이드를 포함하는 압축기 및 이를 포함하는 가스 터빈

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1074594B (de) * 1961-02-23 1960-02-04 D Napier &. Son Limited, London Befestigung hohler tragflugelprofilierter Axialturbmen oder Axialverdichter Schaufeln
US3666376A (en) * 1971-01-05 1972-05-30 United Aircraft Corp Turbine blade damper
BE791375A (fr) * 1971-12-02 1973-03-01 Gen Electric Deflecteur et amortisseur pour ailettes de turbomachines
US3841792A (en) * 1973-03-09 1974-10-15 Westinghouse Electric Corp Turbomachine blade lock and seal device
US4101245A (en) * 1976-12-27 1978-07-18 United Technologies Corporation Interblade damper and seal for turbomachinery rotor
US4182598A (en) * 1977-08-29 1980-01-08 United Technologies Corporation Turbine blade damper
US4347040A (en) * 1980-10-02 1982-08-31 United Technologies Corporation Blade to blade vibration damper
GB2228541B (en) * 1989-02-23 1993-04-14 Rolls Royce Plc Device for damping vibrations in turbomachinery blades
FR2665726B1 (fr) * 1990-08-08 1993-07-02 Snecma Soufflante de turbomachine a amortisseur dynamique a cames.
US5201849A (en) * 1990-12-10 1993-04-13 General Electric Company Turbine rotor seal body
US5820346A (en) * 1996-12-17 1998-10-13 General Electric Company Blade damper for a turbine engine

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101994526A (zh) * 2009-08-03 2011-03-30 通用电气公司 用于周向燕尾形转子叶片附接系统的锁定隔离件组件
JP2013537953A (ja) * 2010-09-24 2013-10-07 シーメンス アクティエンゲゼルシャフト ブレード配列、及び当該ブレード配列を具備するガスタービン
US9341067B2 (en) 2010-09-24 2016-05-17 Siemens Aktiengesellschaft Blade arrangement and associated gas turbine
JP2013139777A (ja) * 2012-01-05 2013-07-18 General Electric Co <Ge> タービンロータリムシールの軸方向保持組立体
WO2022201926A1 (ja) 2021-03-24 2022-09-29 三菱重工航空エンジン株式会社 タービン動翼及びタービン
EP4317652A4 (en) * 2021-03-24 2024-10-23 Mitsubishi Heavy Industries Aero Engines, Ltd. Turbine rotor blade and turbine
US12163443B2 (en) 2021-03-24 2024-12-10 Mitsubishi Heavy Industries Aero Engines, Ltd. Turbine rotor blade and turbine
JP7599361B2 (ja) 2021-03-24 2024-12-13 三菱重工航空エンジン株式会社 タービン動翼及びタービン

Also Published As

Publication number Publication date
EP1004749B1 (en) 2004-08-18
US6042336A (en) 2000-03-28
KR20000047689A (ko) 2000-07-25
EP1004749A2 (en) 2000-05-31
KR100584798B1 (ko) 2006-06-02
DE69919491D1 (de) 2004-09-23
DE69919491T2 (de) 2004-12-23
EP1004749A3 (en) 2002-04-03

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