Research on the tightening force consistency of aero-engine rotor flange bolt connection
Purpose This paper presents a torque-angle control method aimed at enhancing the consistency of tightening force in bolt connection for aero-engine rotor flanges and a spectral confocal displacement sensor test system has been developed to achieve high-resolution measurement of bolt tightening force. Design/methodology/approach The mechanism of tightening force in a single bolt is explained through tightening experiments. An experiment on bolt tightening under varying lubrication conditions demonstrates the effectiveness of the torque-angle method in achieving consistent tightening force for a single bolt. A spectral confocal displacement sensor test system has been developed to achieve high-resolution measurement of the preload of a group of 48 bolts. Findings It was determined that the mean deviation of tightening force using the torque-angle control method under fully lubricated conditions was only 0.257 kN. The tightening force of the multiple bolts remains consistently has good consistency using the torque-angle control method and spectral confocal displacement sensor test system. Research limitations/implications The paper focuses on the measurement analysis and the subsequent need to optimize the process method. Originality/value This paper presents a torque-angle control method and a spectral confocal displacement sensor test method to regulate and measure the tightening force of multiple bolts.
Authors
- Bing Zhao (ORCID: https://orcid.org/0000-0002-5560-6750)
- Shoutian Ren (ORCID: https://orcid.org/0000-0002-6679-622X)
- Dongbo Wu
- Heng Li (ORCID: https://orcid.org/0000-0002-3187-9041)
- Weijin Ouyang
Institutions
- Qinghai University (CN)
- Tsinghua University (CN)
Publication Details
- Journal
- Robotic Intelligence and Automation
- Published
- 2025-03-08
- DOI
- https://doi.org/10.1108/ria-06-2024-0136
- Primary Topic
- Engineering Structural Analysis Methods
- Type
- article
- Field-Weighted Citation Impact
- 0.00