首页> 外国专利> TURBINE BLADE MAXIMUM RESPONSE PREDICTION METHOD, TURBINE BLADE MAXIMUM RESPONSE PREDICTION SYSTEM AND CONTROL PROGRAM, AND TURBINE EQUIPPED WITH TURBINE BLADE MAXIMUM RESPONSE PREDICTION SYSTEM

TURBINE BLADE MAXIMUM RESPONSE PREDICTION METHOD, TURBINE BLADE MAXIMUM RESPONSE PREDICTION SYSTEM AND CONTROL PROGRAM, AND TURBINE EQUIPPED WITH TURBINE BLADE MAXIMUM RESPONSE PREDICTION SYSTEM

机译:涡轮叶片最大响应预测方法,涡轮叶片最大响应预测系统和控制程序以及配备有涡轮叶片最大响应预测系统的涡轮

摘要

A turbine blade maximum vibration response prediction method for predicting a maximum vibration response acting on a plurality of turbine moving blades provided along the circumferential direction of a turbine rotor includes the steps of: gaining, before turbine operation start, prior response data that is distribution data on vibration response of all the turbine moving blades for each turbine operating condition; gaining, by using the prior response data, operation response data that is distribution data on the vibration response of all the turbine moving blades during the operation of the turbine; and predicting, from the operation response data, the turbine moving blade of all the turbine moving blades on which the maximum vibration response is acting, and the magnitude of the maximum vibration response.
机译:用于预测作用在沿着涡轮转子的周向设置的多个涡轮动叶片上的最大振动响应的涡轮叶片最大振动响应预测方法包括以下步骤:在涡轮操作开始之前获得作为分布数据的先验响应数据。在每个涡轮机运行条件下所有涡轮机动叶片的振动响应;通过使用先验响应数据,获得运行响应数据,该运行响应数据是有关涡轮机运行期间所有涡轮机动叶片的振动响应的分布数据;根据操作响应数据,预测最大振动响应所作用的所有涡轮动叶片中的涡轮动叶片以及最大振动响应的大小。

著录项

  • 公开/公告号US2018347394A1

    专利类型

  • 公开/公告日2018-12-06

    原文格式PDF

  • 申请/专利权人 MITSUBISHI HITACHI POWER SYSTEMS LTD.;

    申请/专利号US201815993640

  • 发明设计人 TOMOMI TANAKA;

    申请日2018-05-31

  • 分类号F01D21/14;F01D21/00;G05B19/042;

  • 国家 US

  • 入库时间 2022-08-21 12:04:09

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