Bolted rabbet joint structure is commonly used in aero-engine, and bolt pre-tightening force is usually dispersed after assembled under the current process technology, which can aggravate the unsteadiness of mechanical properties. This paper analyzes the Von Mises equivalent stress of the joint interface and stiffness of the bolted rabbet joint structure with FEA software ANSYS Workbench. Five levels of bolt pre-tightening force dispersion were set up by engineering experience, then a group of pre-tightening forces were randomly generated for each of the dispersion level to simulate the pre-tightening force in engineering condition. The stress distribution of joint interface, the axial stiffness, the radial stiffness and the torsional stiffness were calculated, and related mathematical relation curves were plotted. Finally, the influence rules of bolt pre-tightening force dispersion on the bolted rabbet joint structure were summarized which can provide a theoretical reference for the control of bolt pre-tightening force dispersion.
作者简介: 陈飞宇:硕士研究生,主要研究方向为航空发动机装配连接工艺。
引用本文:
陈飞宇,李小强,董红瑞,平宇,李东升. 不同预紧力分散度条件下螺栓止口连接组件有限元分析[J]. 航空制造技术, 2018, 61(20): 63-68.
CHEN Feiyu, LI Xiaoqiang, DONG Hongrui, PING Yu, LI Dongsheng. Finite Element Analysis of Bolted Rabbet Joint Structure Under Dispersed Pre-Tightening Force. Aeronautical Manufacturing Technology, 2018, 61(20): 63-68.