Abstract：The relation between the tightening torque and preload of the fastener used in a certain aviation application was analyzed. Taking MJ8 multiplied by 1 size titanium fastener as the research object, this article focused on the influence and corresponding change law of different head-type fastener and tightening times when the titanium alloy fastener is under actual installation environment of aviation and aerospace model. The following results are acquired: The preload of the bolt reached 5%–35%Fmax (Fmax means the required minimum tension load of the bolt), with all other elements, such as thread accuracy level and the property level, etc, stayed the same except the head-type, for the headtype fastener with larger loading area on the bolt head, the generated end face friction torque is larger, and the required tightening torque is also larger to reach the same preload. The needed install moment and torsion modulus are all increased in the same bolt stress level with the addition of the install times.
高学敏，程全士，米保卫，冯德荣，袁浩. 基于TC4紧固件在不同头型下扭矩与预紧力关系研究[J]. 航空制造技术, 2020, 63(17): 92-97.
GAO Xuemin,CHENG Quanshi，MI Baowei,FENG Derong,YUAN Hao. Research on Torsion-Tension Relationship of TC4 Material Fastener With Different Head-Type. Aeronautical Manufacturing Technology, 2020, 63(17): 92-97.
2020, 
