Abstract

Interference-fit is attracting increasing attention in the aerospace field because of its excellent enhancement of the sealing and fatigue life of carbon fiber reinforced plastic (CFRP). However, it also induces imbalanced pre-tightening forces on the interface, and affects its mechanical behavior. A series of experiments were conducted to assess the imbalanced pre-tightening force of CFRP interference bolted joints and its effects. High-precision washer force sensors were used to measure the pre-tightening force between upper and lower surfaces at various interference-fit and torque. Strain gauges were used to estimate the varying effect on the imbalanced pre-tightening force during tensile tests. The effects of varying interference-fit and torque on pre-loaded transfer, surface strain distribution, tensile strength, and damage mode were identified. The results show that the synergy of interference-fit and torque induces an imbalanced pre-tightening force, which, in turn, changes the stress-strain evolution of the surface, and a special “transition regime” was identified in the evolution curves. Compared with clearance-fit, the ultimate strength and optimal torque of interference-fit joints could be significantly enhanced. In addition, the damage originates from fiber/matrix slipping to the upper surface with a low pre-tightening force and the formation of stack buckling, which then causes delamination fracture.

Highlights

  • In the field of mechanical engineering, interference fit and bolt pre-tightening force are widely used to improve the performance of structure-connecting.[1,2,3] Because of the development of the aviation engineering technology, in aircrafts of the new types, interference fit is gradually applied to composites connecting structures

  • The transfer of the pre-tightening force has been measured at various tightening torque values, at a carbon fiber reinforced plastic (CFRP) interference-fit bolted joint

  • (3) Tightening torque and interference fit can improve the mechanical properties of CFRP bolted joints

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Summary

Introduction

In the field of mechanical engineering, interference fit and bolt pre-tightening force (caused by tightening torque) are widely used to improve the performance of structure-connecting.[1,2,3] Because of the development of the aviation engineering technology, in aircrafts of the new types, interference fit is gradually applied to composites connecting structures. Advances in Mechanical Engineering composites bolted joints.[4,5,6] because of the low interlaminar strength and weak properties of composite, it was concluded that the pre-tightening force should be restrained along the thickness direction.[7,8] In addition, the interference fit can micro-damage the connection hole,[9,10,11] which causes premature failure

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