Abstract
Interference fit connection technique can effectively improve the fatigue life of aircraft structure. Considering the engineering practice, in this paper, the pin treated as an elastic deformed body is introduced in the analysis of interference fit connection. In the theoretical derivation, we obtain the contact stress between the hole and pin, the interference fit size of the elastic limit, and also the relationship between the plastic zone radius and interference fit size. At the same time, the finite element model is established, and the numerical simulation is conducted. By comparing theoretical and finite element results, the theoretical formulas are verified, which can be used furtherly in quick engineering calculation.
Sign-in/Register to access full text options 
Free) 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
