Abstract

Automatic fiber placement (AFP) is a type of labor-saving automatic technology for forming composite materials that are widely used in aviation and other fields. In this process, concave surface delamination is a common defect, as existing research on the conditions for this defect to occur is insufficient. To predict the occurrence of this defect, the concept of allowable interlaminar normal stress is proposed to define its occurrence conditions, and based on this concept, probe tests are carried out using the principle of time–temperature equivalence. Through the laying speed/allowable normal stress curve measured in the probe experiment, the physical meaning of allowable normal stress is discussed. At the same time, the measured curve is quantitatively analyzed, combined with viscoelastic theory and the molecular diffusion reptation model, and the dominating effect in the formation of a metal/prepreg layer and prepreg/prepreg layer is determined. Finally, the experimental data are used to guide the parameter selection in an automatic placement engineering case and prove its correctness.

Highlights

  • Automatic fiber placement (AFP)(prepreg) technologyisisautomatically a production process resinimpregnated carbon fiber tape laid in onwhich a mold to make impregnated carbon fiber tape is automatically laid on a mold to make composite site parts

  • Before the equivalent laying speed/allowable normal stress curve can be measured under different experiment, the sample was compressed with the weight of this experiment for min to laying pressures

  • Tocharacterize characterizethe theconditions conditionsunder underwhich whichprepreg prepreglayer layerseparation separationoccurs occursduring during the forward thethe concept of allowable normal stress

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Summary

Introduction

Polymers 2021, Automatic fiber placement (AFP) technology is a production process in whic. Academic Editors: Jannick (AFP)(prepreg) technologyisisautomatically a production process resinimpregnated carbon fiber tape laid in onwhich a mold to make impregnated carbon fiber tape (prepreg) is automatically laid on a mold to make composite site parts. This process has been widely used in the aviation industry in the past 3 parts.

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