JPS5647601A - Vibration damping construction for turbine blade - Google Patents

Vibration damping construction for turbine blade

Info

Publication number
JPS5647601A
JPS5647601A JP12202979A JP12202979A JPS5647601A JP S5647601 A JPS5647601 A JP S5647601A JP 12202979 A JP12202979 A JP 12202979A JP 12202979 A JP12202979 A JP 12202979A JP S5647601 A JPS5647601 A JP S5647601A
Authority
JP
Japan
Prior art keywords
oscillation
blade
piece
turbine
damping
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
JP12202979A
Other languages
Japanese (ja)
Inventor
Hirotaka Azami
Takeru Hasegawa
Michio Kuroda
Kiyoshi Namura
Daizo Morimoto
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.)
Hitachi Ltd
Hitachi Kizai Inc
Original Assignee
Hitachi Ltd
Hitachi Kizai Inc
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 Hitachi Ltd, Hitachi Kizai Inc filed Critical Hitachi Ltd
Priority to JP12202979A priority Critical patent/JPS5647601A/en
Publication of JPS5647601A publication Critical patent/JPS5647601A/en
Pending legal-status Critical Current

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

PURPOSE: To absorb the energy of oscillation in a turbine blade and increase the effect of damping its oscillation for the turbine blade integrally constructed with a turbine disc, by longitudinally providing a hold and inserting an oscillation damping piece into the hole.
CONSTITUTION: A disc 1 and a blade 1 are formed as an integral unit, and a hole 3 is provided toward the center of the disc 1 from a tip end part of the blade 2. At both end parts of the hole 3 female screw threads tapped. At both end parts of a vibration damping piece 5 male screws are threaded, and an intermediate part of the piece is constructed by using a material easy to damp its oscillation. At a certain speed of rotation of a turbine, oscillating frequency of the blade 2 resonates and its stress of oscillation tends to raidly increase. At this time, the piece 5 is also oscillated in accordance with the oscillation of the blade 2, and the energy of oscillation of the blade 2 is absorbed by the oscillation of the piece 5 to obtain an effect of damping the oscillation.
COPYRIGHT: (C)1981,JPO&Japio
JP12202979A 1979-09-25 1979-09-25 Vibration damping construction for turbine blade Pending JPS5647601A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12202979A JPS5647601A (en) 1979-09-25 1979-09-25 Vibration damping construction for turbine blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12202979A JPS5647601A (en) 1979-09-25 1979-09-25 Vibration damping construction for turbine blade

Publications (1)

Publication Number Publication Date
JPS5647601A true JPS5647601A (en) 1981-04-30

Family

ID=14825821

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12202979A Pending JPS5647601A (en) 1979-09-25 1979-09-25 Vibration damping construction for turbine blade

Country Status (1)

Country Link
JP (1) JPS5647601A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130294913A1 (en) * 2012-05-04 2013-11-07 Christian X. Campbell Turbine blade with tuned damping structure
WO2014176228A1 (en) * 2013-04-23 2014-10-30 United Technologies Corporation Internally damped airfoiled component and method
CN104314619A (en) * 2014-08-15 2015-01-28 中国燃气涡轮研究院 Adjustment structure and method for inherent frequencies of blades of overall blade disk of turbine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130294913A1 (en) * 2012-05-04 2013-11-07 Christian X. Campbell Turbine blade with tuned damping structure
US9121288B2 (en) * 2012-05-04 2015-09-01 Siemens Energy, Inc. Turbine blade with tuned damping structure
WO2014176228A1 (en) * 2013-04-23 2014-10-30 United Technologies Corporation Internally damped airfoiled component and method
US10697303B2 (en) 2013-04-23 2020-06-30 United Technologies Corporation Internally damped airfoiled component and method
US11668197B2 (en) 2013-04-23 2023-06-06 Raytheon Technologies Corporation Internally damped airfoiled component
CN104314619A (en) * 2014-08-15 2015-01-28 中国燃气涡轮研究院 Adjustment structure and method for inherent frequencies of blades of overall blade disk of turbine

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