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METHOD FOR MONITORING SHAFT TORSIONAL VIBRATION AND FATIGUE OF TURBINE GENERATOR

机译:汽轮发电机轴系扭振与疲劳监测方法

摘要

PURPOSE:To monitor exactly shaft torsional vibration and fatigue of a turbine generator, by adjusting a parameter of a mathematical model of a modal analyzing method by calculated modal damping, and deciding torsional vibration and stress of a shaft system. CONSTITUTION:By a damping operation part 8a of a signal processing part 8, torsional natural vibration of a shaft 4, modal damping, etc. are deciced from shaft torsional angle displacement from torsional angle detecting parts 5a, 5b. In accordance with decision of them, in a torsional vibration and stress calculating part 8b, a mathematical parameter by set modal analysis by electric torque and vapor pressure from detecting parts 6, 7 is adjusted, and a torsional vibration and stress state of each part of the shaft 4 is calculated. Subsequently, by a compare-operating part 8c, a calculation result of the calculating part 8b is compared with shaft torsional angle displacement, and in case when its error is large, the mathematical model parameter is readjusted, and it is repeated until the error becomes small. In this way, in accordance with a correct calculation result of the claculating part 8b, shaft torsional vibration and fatigue of a turbine generator is monitored exactly through a fatigue and life operating part 9.
机译:目的:通过计算模态阻尼来调整模态分析方法的数学模型参数,并确定轴系的扭转振动和应力,以精确监测涡轮发电机的轴扭转振动和疲劳。组成:通过信号处理部分8的阻尼操作部分8a,可从轴上的扭转角位移来减小轴4的扭转固有振动,模态阻尼等。根据它们的决定,在扭转振动和应力计算部8b中,通过基于来自检测部6、7的电动转矩和蒸气压进行的设定模态分析,调整数学参数,并且,对各部位的扭转振动和应力状态进行设定。计算出轴4。随后,通过比较操作部分8c,将计算部分8b的计算结果与轴扭转角位移进行比较,并且在其误差较大的情况下,重新调整数学模型参数,并重复进行直到误差变为小。以此方式,根据咬合部8b的正确计算结果,通过疲劳寿命操作部9精确地监视涡轮发电机的轴扭转振动和疲劳。

著录项

  • 公开/公告号JPH0326341B2

    专利类型

  • 公开/公告日1991-04-10

    原文格式PDF

  • 申请/专利权人 TOKYO SHIBAURA ELECTRIC CO;

    申请/专利号JP19820029611

  • 发明设计人 NAGATA AKINORI;

    申请日1982-02-25

  • 分类号G01M99/00;G01H1/10;G01N3/32;

  • 国家 JP

  • 入库时间 2022-08-22 06:05:17

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