Cure-dependent microstructures and their effect on elastic properties of interlayer toughened thermoset composites
Source abstract
Abstract
Abstract To shorten the cure cycle for thermoset prepreg composites, we can either increase the heating rate or the curing temperature. However, this raises the question whether modifying the cure cycle affects the laminate microstructure and physical and mechanical properties. Current state-of-the-art aerospace prepreg composites incorporate thermoplastic particles into the interlayer to increase delamination and impact resistance, which creates a more complicated composition and laminate microstructure. This research investigates the effect of curing conditions on the microstructure and elastic properties of an interlayer toughened prepreg system, Toray's T800SC/3900-2B. Laminates were processed to the same degree of cure using cure cycles with different heating rates. Optical microscopy showed that microstructural characteristics such as the interlayer thickness, particle shape, particle volume fraction and inter-particle distance are dependent on curing conditions. It was found that the glass transition temperature of the toughening particle, the resin viscosity and the elastic deformation of the fibre bed are important for the cure-dependent microstructural evolution at the pre-gelation stage. The out-of-plane lamina shear modulus ( G 13 ) dependence on temperature of fully cured laminates was measured with Dynamic Mechanical Analysis (DMA). The lamina G 13 decreases with increasing cure cycle heating rate at 150–200 °C, where toughening particles are rubbery and the matrix is glassy. A micromechanical model demonstrates that the reduction of lamina G 13 at higher heating rates results from a decrease in the interlayer shear modulus. Interlayer microstructural features such as particle volume fraction, particle aspect ratio and inter-particle contact contribute to the cure path dependence of the interlayer shear modulus. This study provides insight into the fundamental processing behavior of interlayer toughened prepregs and the influence on elastic properties.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Epoxy Resin Curing Processes · Mechanical Behavior of Composites · Fiber-reinforced polymer composites
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (28)
Show source-provided references
1. Effects of cure pressure on resin flow, voids, and mechanical properties10.1177/002199838702100502 ↗
2. Effects of cure cycles on void content and mechanical properties of composite laminates10.1016/j.compstruct.2005.02.001 ↗
3. Cure cycle design to suppress moisture-driven bubble growth in polymer composites10.1177/0021998317734393 ↗
4. The voids formation mechanisms and their effects on the mechanical properties of flax fiber reinforced epoxy composites10.1016/j.compositesa.2015.01.029 ↗
5. Effect of curing overheating on interlaminar shear strength and its modelling in thick FRP laminates10.1007/s00170-016-8613-5 ↗
6. A new methodology to evaluate the influence of curing overheating on the mechanical properties of thick FRP laminates10.1016/j.compositesb.2016.10.064 ↗
7. Development of TORAYCA prepreg P2302 carbon fiber reinforced plastic for aircraft primary structural materials10.1163/156855196X00301 ↗
8. Rapid Out-of-Autoclave Composite Manufacturing for Aerospace-Grade Prepregs
9. Curing rate effects on the toughness of epoxy polymers10.1016/j.polymer.2018.11.008 ↗
10. Cure path dependency of mode i fracture toughness in thermoplastic particle interleaf toughened prepreg laminates10.1016/j.compositesa.2016.04.016 ↗
11. Mechanisms generating residual stresses and distortion during manufacture of polymer-matrix composite structures10.1016/j.compositesa.2005.05.019 ↗
12. Experimental and numerical study of the effect of cure cycle, tool surface, geometry, and lay-up on the dimensional fidelity of autoclave-processed composite parts10.1016/S1359-835X(01)00123-3 ↗
13. A review on process-induced distortions of carbon fiber reinforced thermosets for large-scale production10.1007/s11740-017-0772-1 ↗
14. Shear-lag analysis of the effect of thickness on spring-in of curved composites10.1177/0021998306068072 ↗
15. Process-induced strain and distortion in curved composites. Part I: development of fiber-optic strain monitoring technique and analytical methods10.1016/j.compositesa.2017.09.020 ↗
16. Experimental and numerical investigation of effects of cure cycle on process-induced-distortions of carbon fibre reinforced composites
17. Modeling the influence of interleaf layers in composite materials on elastic properties, thermal expansion, and chemical shrinkage10.1177/0021998319830165 ↗
18. Toray Composite Materials America Inc
19. Mode I and Mode II delamination growth of interlayer toughened carbon/epoxy (T800H/3900-2) composite system
20. Dykeman · 2008
21. Mode II delamination and damage resistance of carbon/epoxy composite laminates interleaved with thermoplastic particles10.1177/0021998306063356 ↗
22. Engineering thermoplastics: acrylics, polycarbonates, polyurethanes, polyacetals, polyesters, and polyamides10.1016/B978-0-8155-2027-6.10007-8 ↗
23. A novel method to measure laminate shear modulus development of interlayer toughened composite laminates during the curing process
24. Cure shrinkage monitoring and process analysis of CFRP laminates with interlaminar-resin layers10.6089/jscm.41.168 ↗
25. Fatigue life prediction for transverse crack initiation of CFRP cross-ply and quasi-isotropic laminates10.3390/ma11071182 ↗
26. Mesoscopic fracture mechanism of mode II delamination fatigue crack propagation in interlayer-toughened CFRP10.1299/jsmea.40.423 ↗
27. Examination of quantitative infrared stress measurement of CFRP laminates and its application to non-destructive evaluation
28. Analysis of properties of fiber composites with anisotropic constituents10.1115/1.3424603 ↗