首页> 外国专利> Non-contact method for monitoring turbine blade particular individual steam or gas turbines in power system and system thereof

Non-contact method for monitoring turbine blade particular individual steam or gas turbines in power system and system thereof

机译:用于监视动力系统中的涡轮叶片特定的单个蒸汽或燃气涡轮机的非接触式方法及其系统

摘要

The method of contactless monitoring of turbines, particularly static and dynamic parameters of individual blades of steam or gas turbine power plants where turbine comprises one or more paddle wheels mounted on a common shaft . Turbines in operation senses the position of non-contact rotating blades during their passage in the vicinity of at least one sensor ( 2 , 3 , 4 ) , situated on the static part of the turbine impeller outside the periphery thereof , and at least one sensor ( 1 ) the reference marks on the rotating the turbine shaft , and also takes away the time of their passage in the corresponding sensor . The recorded data is digitized , processed and stored in binary form files as carrying time information with a resolution of 10 ns , information about the events of the time and pulse -shaped blade . The selected number of revolutions of the turbine is processed always contiguous block of data and performed the statistical analysis thereof , when time data generated by crossing blades around various sensors ( 2 , 3 , 4 ) are transformed into normalized vectors , describing the sequence of transitions of the blade around the downstream sensors , with the reference marks on the turbine shaft is calculated time difference with regard to the next reference mark , thus eliminating non-uniformity of rotation of the turbine shaft . Observed values are normalized according to the current speed and turbine circuit and performs the correction for the time lag , caused by a different blade shape pulses , the time difference of the blades is converted to instantaneous deviations from the mean position and analyzed .
机译:涡轮机的非接触式监视的方法,尤其是蒸汽或燃气涡轮机电厂的各个叶片的静态和动态参数,其中涡轮机包括一个或多个安装在同一轴上的桨轮。在运行中,涡轮机感测非接触旋转叶片在其通过期间在至少一个传感器(2、3、4)附近的位置,该传感器位于涡轮机叶轮的外围之外的静态部分上,并且至少一个传感器(1)旋转的涡轮轴上的参考标记,并占用了它们通过相应传感器的时间。记录的数据被数字化,处理并存储在二进制文件中,以承载具有10 ns分辨率的时间信息,有关时间事件的信息以及脉冲状的叶片。选定的涡轮机转数始终处理连续的数据块,并进行统计分析,然后将围绕各个传感器(2、3、4)的交叉叶片产生的时间数据转换成归一化矢量,描述过渡的顺序计算下游传感器周围叶片的角度,计算涡轮轴上的参考标记相对于下一个参考标记的时间差,从而消除涡轮轴旋转的不均匀性。根据当前速度和涡轮电路对观测值进行归一化,并对由不同叶片形状脉冲引起的时滞进行校正,将叶片的时间差转换为与平均位置的瞬时偏差并进行分析。

著录项

  • 公开/公告号SK288140B6

    专利类型

  • 公开/公告日2013-11-04

    原文格式PDF

  • 申请/专利权人 STARMAN STANISLAV;

    申请/专利号SK20100050028

  • 发明设计人 STARMAN STANISLAV;

    申请日2010-06-28

  • 分类号G01P3/68;G01H1/00;G05B23/00;

  • 国家 SK

  • 入库时间 2022-08-21 16:39:59

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