A Review of Aeroengines’ Bolt Preload Formation Mechanism and Control Technology

Author:

Li Zhaoyu1,Li Xiaoqiang1,Han Yujie1,Zhang Pengfei1,Zhang Zongjiang1,Zhang Mingming1,Zhao Gang1

Affiliation:

1. School of Mechanical Engineering and Automation, Beihang University, Beijing 100191, China

Abstract

The bolt connection structure is widely used in the connection of aeroengine parts, and its connection quality is very important, as it can directly affect the geometric and dynamic performance of the aeroengine. Taking the bolt preload as the entry point, the research status of bolted aeroengine connections in recent years is summarized based on the bolt preload formation mechanism and control technology in this review. For the research of the preload formation mechanism, single and multiple bolts of aeroengine bolt arrays are analyzed. According to the characteristics of aeroengine bolt connections, the research of aeroengine bolt preload control technology is divided into two parts: bolt tightening technology, and bolt tightening equipment. Finally, based on the summarization of the research, the future research prospects are evaluated and discussed.

Funder

Major National Science and Technology Projects

Publisher

MDPI AG

Subject

Aerospace Engineering

Reference104 articles.

1. Liu, Y., Liang, C., and Shi, L. (2021). General Design of Aviation Gas Turbine, Science Press.

2. Yan, Q. (2019). Research on Assembly Tightness Detection Method for Aeroengine Bolt-Jointed Rotor, Chang’an University.

3. Modeling and application test of contact stiffness of bolt connection structure of disk and drum;Zhao;J. Aeronaut. Dyn.,2022

4. Influence of position error of bolt hole on assembly mechanical characteristic of short precision bolted connection structure;Jiao;J. Aeronaut. Dyn.,2021

5. Nonlinear stiffness mechanism analysis and numerical simulation of rabbet-bolted connection structure;Li;J. Aeronaut. Dyn.,2021

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