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TURBOMACHINE COMPONENT DAMPING STRUCTURE AND METHOD OF DAMPING VIBRATION OF TURBOMACHINE COMPONENT

机译:涡轮机组件的阻尼结构和阻尼振动的方法

摘要

PROBLEM TO BE SOLVED: To provide a damping structure, in a turbomachine component, for damping vibration which causes fatigue to shorten the operational life of the turbomachine component.;SOLUTION: This turbomachine component 2 has a body 10 having surfaces 18 and 20, and a damping structure part 60 mounted to the surfaces 18 and 20 of the body 10. The damping structure part 60 is formed from a material having a temperature dependent damping characteristic. As the operation temperature and speed increase, the damping structure part 60 passes through the transition temperature, thus increasing its vibration damping level.;COPYRIGHT: (C)2010,JPO&INPIT
机译:解决的问题:在涡轮机部件中提供一种阻尼结构,用于阻尼会引起疲劳的振动,从而缩短涡轮机部件的使用寿命。解决方案:该涡轮机部件2的主体10具有表面18和20,并且阻尼结构部件60安装在主体10的表面18和20上。阻尼结构部件60由具有取决于温度的阻尼特性的材料形成。随着工作温度和速度的增加,阻尼结构部件60会通过转变温度,从而增加其振动阻尼水平。版权所有:(C)2010,JPO&INPIT

著录项

  • 公开/公告号JP2010031864A

    专利类型

  • 公开/公告日2010-02-12

    原文格式PDF

  • 申请/专利权人 GENERAL ELECTRIC CO GE;

    申请/专利号JP20090172613

  • 发明设计人 DELVAUX JOHN MCCONNELL;VEHR JAMES WILLIAM;

    申请日2009-07-24

  • 分类号F01D5/26;F01D5/16;F01D5/10;F01D25/06;

  • 国家 JP

  • 入库时间 2022-08-21 19:04:27

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