Influence of position error of bolt hole on assembly mechanical characteristics of short precision bolted connection structure

被引:0
|
作者
Jiao J. [1 ,2 ]
Mo R. [1 ,2 ]
Xu G. [3 ]
Fu X. [3 ]
Sun H. [1 ,2 ]
Chang Z. [1 ,2 ]
机构
[1] Key Laboratory of High Performance Manufacturing for Aeroengine, Ministry of Industry and Information Technology, Northwestern Polytechnical University, Xi'an
[2] Institute for Aero-engine Smart Assembly of Shaanxi Province, Northwestern Polytechnical University, Xi'an
[3] Sichuan Gas Turbine Establishment, Aero Engine Corporation of China, Mianyang
来源
关键词
Assembly process; Connection stiffness; Mechanical property; Positioning error; Short precision bolted connection;
D O I
10.13224/j.cnki.jasp.2021.05.005
中图分类号
学科分类号
摘要
In order to study the influence of position error of bolt hole on assembly mechanical characteristics, the error model and finite element model considering the position error were built, and the influences of position error on the connection stiffness and stress of bolt hole edge of single short precision bolted connection structure were studied. Computing model and finite model of position error of short precision bolt group were established, and the effects of assembly phases of two parts and assembly position of the 1st bolt on connection stiffness of short precision bolt group were analyzed. It was concluded that position error had a small influence on axial stiffness, and a significant effect on tangential stiffness. The projection of position error in the direction of tangential load was a major influencing factor to the tangential stiffness, and the stress of bolt hole edge reached the maximum at the position of 180°. By computing and comparing standard deviation of the projection and length of position error, three better assembly plans of bolts were obtained. © 2021, Editorial Department of Journal of Aerospace Power. All right reserved.
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页码:935 / 947
页数:12
相关论文
共 18 条
  • [1] (2010)
  • [2] LI Xiaoqiang, MENG Qingkuo, DU Yifan, Et al., Influence of tightening strategy on pre-tightening force of aero-engine sigle-bolt connection, Journal of Mechanical Engineering, 56, 13, pp. 231-241, (2020)
  • [3] CHEN Yingtao, AI Yanting, ZHANG Yunda, Simulation analysis on the effect of bolt connection preload on static characteristics of turbine disk, Gas Turbine Experiment and Research, 32, 1, pp. 26-29, (2019)
  • [4] HUANG Weiqiang, Study on pre tightening force for connecting bolts of aeroengine low pressure rotor, (2018)
  • [5] YANG Guoqing, WANG Fei, HONG Jun, Et al., Theoretical analysis for bolted member stiffness, Journal of Xi'an Jiaotong University, 46, 7, pp. 50-56, (2012)
  • [6] HUANG Xin, Research on stiffness of bolted joints considering joint surfaces contact, (2016)
  • [7] ZHANG Yongjie, SUN Qin, Sheared bolt joint stiffness analysis with pre-tightened force, Structure and Environment Engineering, 34, 4, pp. 22-25, (2007)
  • [8] YAO Xingyu, WANG Jianjun, Effects of load and structure parameters of aero-engine bolted joints on joint stiffness, Journal of Propulsion Technology, 38, 2, pp. 424-433, (2017)
  • [9] GUO Wenxin, YAO Yuhui, LI Yun, Et al., The influence of bolt joint characteristics on bending stiffness of rotor joint surface, Noise and Vibration Control, 38, 1, pp. 52-57, (2018)
  • [10] ZHAO Dan, Study on the influence of bolted joint on the dynamic characteristic of rotor structure, (2013)