| Citation: | Li Zhaoyu, Li Xiaoqiang, Zhang Pengfei, et al. Research progress of blind cavity bolt tightening technology for aeroengine rotors[J]. Journal of Aerospace Power, 2026, 42（X）：20250177 doi: 10.13224/j.cnki.jasp.20250177
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The current research status of blind cavity bolt tightening technology for aircraft engine rotors was summarized. Guided by the technical requirements for tightening bolts in rotor blind cavities, three aspects were discussed: tightening process, tightening equipment, and tightening inspection. Firstly, focusing on the two stages of rotor rabbet fit and bolt connection, optimized processes such as rabbet press-fitting process, torque-rotation angle method, and multi-axis tightening method were summarized. Secondly, focusing on equipment configuration design and accuracy control methods, research results such as torque transmission methods of tightening equipment, mechanism deployment methods, overall configuration development, as well as bolt positioning and tightening accuracy control methods were summarized. Finally, focusing on bolt tightening inspection methods, current detection technologies for tightening torque, rotation angle, and pre-tightening force were summarized. The research results indicate that to fully overcome the limitations of the narrow space in rotor blind cavities and enhance rotor assembly quality, the blind cavity bolt tightening technology will develop towards an integrated process of press-fitting, tightening, and measurement, intelligent robotic tightening, and multi-modal fusion measurement.
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