Wenmin Chu1,2, Kuai Zhou3,4, Tengzhou Xu3,4

  • 1School of Aeronautical Engineering, Nanjing University of Industry Technology, No.1, North Yangshan Road, Qixia District, Nanjing, 210023, China. chuwenmin@live.com.

Scientific reports
|October 23, 2025
PubMed
概括

本研究介绍了一种合规的直升机环形部件组装方法,使用自适应式插入速度来最大限度地减少热传导和变形. 这种新的方法显著减少了组装接触力和插入时间,提高了制造效率.

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