4.7 Article

An improved 3D model of composite bolted joints with detailed thread structure and progressive damage analysis of realistic tightening process

Journal

COMPOSITE STRUCTURES
Volume 315, Issue -, Pages -

Publisher

ELSEVIER SCI LTD
DOI: 10.1016/j.compstruct.2023.117016

Keywords

Composite bolted joint; Progressive damage analysis; Initial assembly damage; Delamination damage; Tightening coefficient

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Bolted joint is a common connection method in composite structure assembling. The initial assembly state affects subsequent performance. An improved 3D model is proposed to simulate the assembly process of composite bolted joints, considering detailed thread structure and realistic tightening process. The relationship between tightening torque and bolt tension is analyzed, as well as the effect of friction coefficient on tightening coefficient. A fitting model and quantitative analysis method for nonlinear pressure distribution on the outer surface of composite laminates during assembly process are established. The effects of bolt tension and washer type on initial assembly damage are analyzed and experimentally verified.
Bolted joint is a common connection method in composite structure assembling. The initial assembly state has a significant influence on the subsequent performance. To realize the simulation of the assembly process of composite bolted joints, an improved 3D model is proposed. This model considers the detailed thread structure and can be used to simulate the realistic tightening process. The relationship between the tightening torque and bolt tension is analyzed and the effect of the friction coefficient on the value of the tightening coefficient is analyzed using this model. A new fitting model for the nonlinear pressure distribution state on the outer surface of the composite laminates during the assembly process is proposed. And a quantitative analysis and prediction method of the nonlinear pressure distribution state is established. Finally, the effects of bolt tension and washer type on initial assembly damage are analyzed and experimentally verified.

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