About the influence of stamping on thermoplastic-based composites for aeronautical applications

被引：74

作者：

Vieille, B. ^{[1
]}

Albouy, W. ^{[1
]}

Chevalier, L. ^{[1
]}

Taleb, L. ^{[1
]}

机构：

[1] INSA Rouen, CNRS, UMR 6634, Grp Phys Mat, F-76801 St Etienne, France

来源：

COMPOSITES PART B-ENGINEERING | 2013年 / 45卷 / 01期

关键词：

Thermoplastic resin; Environmental degradation; Mechanical testing; Forming; AXIS FATIGUE BEHAVIOR; FIBER REINFORCED PPS; ENVIRONMENTAL-CONDITIONS; POLY(PHENYLENE SULFIDE); MECHANICAL-PROPERTIES; FORMING TEMPERATURES; MATRIX COMPOSITES; WOVEN COMPOSITE; DURABILITY; STRENGTH;

D O I：

10.1016/j.compositesb.2012.07.047

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

An experimental study has been conducted to investigate changes in the mechanical behavior of carbon woven ply PPS laminates, obtained from thermo-compression, for aeronautics purposes. The influence of stamping on mechanical properties (tensile, compressive, in-plane shear, inter-laminar shear) of PPS-based laminates under severe environmental conditions (120 degrees C/hygrothermally aged) has been quantified, as well as for structural testing conditions (bolted joint). From the meso-structure observations, two important phenomena, re-compaction of fiber network and migration of resin melt, can be associated with the re-consolidation process of C/PPS laminates during stamping. This second thermo-compression improves the impregnation of fiber bundles by the PPS matrix and the interlaminar adhesion, which can be correlated with higher mechanical properties of PPS-based laminates under severe conditions. (c) 2012 Elsevier Ltd. All rights reserved.

引用

页码：821 / 834

页数：14

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