Abstract
Press forming of thermoplastic unidirectional (UD) carbon fiber reinforced laminates is an attractive production method in the aerospace industry for cost-effective manufacturing of high-performance parts. The possible formation of wrinkling defects in the formed parts has led to the development of predictive, finite element based, process simulation tools. The material behavior during the forming process is described based on the governing deformation mechanisms, being intra-ply shear, inter-ply and tool-ply slippage and bending. Intra-ply shear is especially important when forming parts having double curvature. The intra-ply shear behavior of fabric-based composite materials is often characterized using the bias extension method but has not successfully been applied to thermoplastic UD tapes yet. This work describes the application of bias extension experiments on cross-ply UD laminates at forming conditions to characterize the intra-ply shear material behavior. The test procedure was designed to prevent deconsolidation and improve load introduction, promoting specimen integrity and reduce shear buckling during testing. Preliminary results show that the material exhibits rate-dependent behavior. A video extensometer was used to measure the shear deformation in the center of the specimen. Additionally, a deformation analysis was performed using a grid of lines on the specimen, where the theoretical areas of constant shear according to a pin-jointed net can be recognized but are not fully uniform. In particular, shear banding parallel to the fiber direction is observed on the outer ply at a length scale below the grid size used for the deformation analysis suggesting a yield point and softening behavior on the meso scale which is not directly evident from the macroscopic response.
Highlights
Fiber reinforced composite materials are applied in the aerospace industry to enable lightweight, high performance aerostructures that help reduce fuel consumption and CO2 emissions
This paper describes the preliminary results of the bias extension method applied to thermoplastic UD material
Preliminary results are presented for the characterization response of the material along with multiple ways of data analysis
Summary
Fiber reinforced composite materials are applied in the aerospace industry to enable lightweight, high performance aerostructures that help reduce fuel consumption and CO2 emissions. Press forming is a manufacturing technique for small to medium sized thermoplastic composite components in high volumes. In this process, a pre-consolidated blank is heated above the melting temperature of the polymer, quickly transferred to a press, shaped using a set of molds and solidified at the mold temperature whereafter the new part is released. Continuum based simulations typically model each ply in a laminate individually and distinguish the mechanisms of in-plane shear, bending, ply-ply friction and tool-ply friction. The current research addresses the accurate measurement and modelling of the intra-ply (in-plane) shear mechanism for thermoplastic UD tape materials. A variety of characterization methods have been developed to measure intra-ply shear on thermoplastic UD material; an overview is provided by Haanappel and Akkerman [2]. This paper describes the preliminary results of the bias extension method applied to thermoplastic UD material
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