In-plane and out-of-plane deformations in automated fiber placement employing micromechanics method

被引:5
|
作者
Kheradpisheh, Meisam [1 ]
Hojjati, Mehdi [1 ]
机构
[1] Concordia Univ, Dept Mech Ind & Aerosp Engn, Montreal H3G 1M8, PQ, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
In-plane and out-of-plane configurations; Micro-mechanic approach; Viscoelastic uncured matrix; Automated fiber placement; WRINKLE FORMATION; PREPREG TACK; TOW; TEMPERATURE;
D O I
10.1016/j.compositesa.2023.107543
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
An experimental and theoretical investigation is performed on the in-plane and out-of-plane configurations of the thermoset tow prepregs in the automated fiber placement (AFP) process. Both in-plane and out-of-plane deformations, also known as waviness and wrinkle defects, respectively, are created mainly due to steering during the AFP process. This paper aims to present a viscoelastic micro-mechanics approach to capture the behavior of planar and non-planar deformations in order to predict these defects during the process and, more importantly, determine the conditions under which either in-plane or out-of-plane deformations occur. In this regard, a fiber-buckling model is employed to describe the deformation behavior of the fibers embedded in a viscoelastic uncured thermoset matrix. In this approach, fiber is considered as an elastic material embedded in an uncured viscoelastic matrix. The stickiness of the matrix in out-of-plane and in-plane directions is measured by different relaxation test methods using a rheometer equipment. On the basis of the obtained solutions, critical radii for in-plane and out-of-plane deformations are derived. The wavelength changes of out-of-plane buckling in the width direction of a steered tow are calculated and compared with the experimental results. In addition, we show the separation between the threshold of critical loading and critical radius for both in-plane and out-of-plane buckling in a steered tow. Finally, the values of the relaxation modulus that lead to a mixed mode in planar buckling are obtained, and also the effect of these values on the deformation behavior of in-plane buckling are discussed.
引用
收藏
页数:10
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