首页> 外国专利> Stage-by-stage Measurement, Regulation and Distribution Method for Dynamic Characteristics of Multi-Stage Components of Large-Scale High-Speed Rotary Equipment Based on Multi-Biased Error Synchronous Compensation

Stage-by-stage Measurement, Regulation and Distribution Method for Dynamic Characteristics of Multi-Stage Components of Large-Scale High-Speed Rotary Equipment Based on Multi-Biased Error Synchronous Compensation

机译:基于多偏差误差同步补偿的大型高速旋转设备多阶段部件动力特性的逐级测量,调节和分配方法

摘要

The present invention provides a stage-by-stage measurement, regulation and distribution method for dynamic characteristics of multi-stage components of large-scale high-speed rotary equipment based on multi-biased error synchronous compensation and belongs to the technical field of mechanical assembly. Firstly, a single-stage rotor five-parameter circular contour measurement model is established, and the five-parameter circular contour measurement model is simplified by using a distance from an ith sampling point of an ellipse to a geometry center to obtain a simplified five-parameter circular contour measurement model. Then, actually measured circular contour data is taken into the simplified five-parameter circular contour measurement model to determine a relationship between dynamic response parameters after rotor assembly and eccentricity errors as well as the amount of unbalance of all stages of rotors. Finally, a rotor speed is set according to the relationship between the dynamic response parameters after rotor assembly and the eccentricity errors as well as the amount of unbalance of all stages of rotors to obtain a critical speed parameter objective function. The high-speed response critical speed parameters for n rotors assembly are optimized by adjusting assembly phases of all stages of rotors, so that a high-speed response to a multi-stage rotor of an aero-engine can be optimized.
机译:本发明提供了一种基于多偏置误差同步补偿的大型高速旋转设备多级部件动态特性的逐级测量,调节和分配方法,属于机械装配技术领域。首先,建立单级转子五参数圆形轮廓测量模型,并通过使用椭圆的第i个采样点到几何中心的距离来简化五参数圆形轮廓测量模型,从而获得简化的五参数圆形轮廓测量模型。然后,将实际测得的圆形轮廓数据输入到简化的五参数圆形轮廓测量模型中,以确定转子装配后的动态响应参数与偏心误差以及转子各级不平衡量之间的关系。最后,根据转子组装后的动态响应参数与偏心误差以及转子各级不平衡量之间的关系来设置转子速度,以获得临界速度参数目标函数。通过调节转子的所有级的组装相位来优化用于n个转子组件的高速响应临界速度参数,从而可以优化对航空发动机的多级转子的高速响应。

著录项

  • 公开/公告号US2020217738A1

    专利类型

  • 公开/公告日2020-07-09

    原文格式PDF

  • 申请/专利权人 HARBIN INSTITUTE OF TECHNOLOGY;

    申请/专利号US201916374926

  • 发明设计人 YONGMENG LIU;JIUBIN TAN;CHUANZHI SUN;

    申请日2019-04-04

  • 分类号G01M1/16;B64F5/60;G06F17/50;

  • 国家 US

  • 入库时间 2022-08-21 11:20:22

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