Abstract

Aerospace-grade composite parts can be manufactured using Vacuum Bag Only prepregs through an accurate process design. Quality in the desired part can be realized by following process modeling, process optimization, and validation, which strongly depend on a primary and systematic material characterization methodology of the prepreg system and material constitutive behavior. The present study introduces a systematic characterization approach of a Vacuum Bag Only prepreg by covering the relevant material properties in an integrated manner with the process mechanisms of fluid flow, consolidation, and heat transfer. The characterization recipe is practiced under the categories of (i) resin system, (ii) fiber architecture, and (iii) thermal behavior. First, empirical models are successively developed for the cure-kinetics, glass transition temperature, and viscosity for the resin system. Then, the fiber architecture of the uncured prepreg system is identified with X-ray tomography to obtain the air permeability. Finally, the thermal characteristics of the prepreg and its constituents are experimentally characterized by adopting a novel specimen preparation technique for the specific heat capacity and thermal conductivity. Thus, this systematic approach is designed to provide the material data to process modeling with the motivation of a robust and integrated Vacuum Bag Only process design.

Highlights

  • Publisher’s Note: MDPI stays neutralCarbon fiber-reinforced laminated composite materials have drawn significant attention from the aerospace industry in recent decades due to their high rigidity, high strength/weight ratio, and relatively high endurance to environmental factors

  • The degree of cure values of the resin system for different conditions could be obtained with Equation (4), and it was utilized to set the baseline to find out the isotherm values as in Equation (4), which contributes to determining the experimental cure rate of the reactions provided in Equation (5)

  • To present the fitting quality of the developed cure kinetics model, the predicted and experimental degrees of cure were compared for both dynamic and isothermal conditions in Figure 3, respectively. These results present that the cure kinetics model precisely predicts the curing evolution of the resin system for both dynamic and isothermal conditions

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Summary

A Systematic Characterization Approach for Vacuum Bag Only

Arikan 1,2 , Fatih Eroglu 1,2 , Volkan Eskizeybek 3 , Emine Feyza Sukur 1,4 , Mehmet Yildiz 1,2 and Hatice S. Characterization Approach for Vacuum Bag Only Prepregs towards an Accurate Process Design.

Introduction
Materials
Methodology
Cure Kinetics
Glass Transition Temperature
Viscosity
Fiber Architecture
Micro-CT Analysis
Fiber Volume Fraction Measurements
Numerical Permeability Characterization
Thermal Behavior
Specific Heat Capacity
Thermal Conductivity
Findings
Conclusions
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