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Aero engine rotor assembling method and device based on concentricity and verticality measurement

机译:基于同心度和垂直度测量的航空发动机转子组装方法及装置

摘要

An aero engine rotor assembling method and device based on concentricity and verticality measurement belongs to mechanical assembly technology. The present invention effectively solves the problem of poor coaxality after the aero engine rotor is assembled and has the characteristics of high coaxality after the rotor is assembled, reduced vibration, mounting easiness, high flexibility and improved engine performance. The measurement and device is: determining rotary reference; determining the angular positioning of a rotary table; extracting the radial error of the radial mounting plane and the inclination error of the axial mounting plane of the rotor based on the four-probe measuring device to obtain the influencing weight of this rotor to the assembled rotor on coaxality; measuring respectively all the rotors to obtain the influencing weight of each rotor to the assembled rotor on coaxality; vector optimizing the weight of each rotor to obtain the assembling angle of each rotor.
机译:基于同心度和垂直度测量的航空发动机转子组装方法及装置属于机械组装技术。本发明有效地解决了航空发动机转子组装后同轴度差的问题,具有转子组装后同轴度高,振动小,安装简便,柔性高,发动机性能提高的特点。该测量和装置为:确定旋转参考;确定转台的角度定位;基于四探针测量装置,提取径向安装面的径向误差和转子轴向安装面的倾斜误差,得出该转子对同轴转子的影响重量。分别测量所有转子,以获得每个转子对同轴度的影响重量;向量优化每个转子的重量以获得每个转子的装配角度。

著录项

  • 公开/公告号US9709392B2

    专利类型

  • 公开/公告日2017-07-18

    原文格式PDF

  • 申请/专利权人 HARBIN INSTITUTE OF TECHNOLOGY;

    申请/专利号US201415118312

  • 发明设计人 LEI WANG;BO ZHAO;JIUBIN TAN;CHUANZHI SUN;

    申请日2014-12-26

  • 分类号G01B7/30;G01B21/24;G01M15/02;G01B21/02;G01B9/02;F01D5/02;F01D5/30;

  • 国家 US

  • 入库时间 2022-08-21 13:45:50

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