Advanced Heliopol/Stratimat Composite Laminate Material Behavior under Cyclic Bending Loads

被引：0

作者：

Modrea, Arina ^{[1
]}

Teodorescu-Draghicescu, Horatiu ^{[2
]}

Szava, Joan ^{[2
]}

Szava, Renata ^{[2
]}

Galfi, Botond ^{[2
]}

机构：

[1] Petru Maior Univ, 1 Nicolae Iorga Str, Targu Mures 540088, Romania

[2] Transilvania Univ Brasov, 29 Eroilor Ave, Brasov 500036, Romania

来源：

10TH INTERNATIONAL CONFERENCE INTERDISCIPLINARITY IN ENGINEERING, INTER-ENG 2016 | 2017年 / 181卷

关键词：

Heliopol resin; Stratimat; Composite laminate; Three-point bend test; Cyclic bending load; NONWOVEN POLYESTER MAT; REINFORCED COMPOSITE; MECHANICAL-BEHAVIOR; CARBON; ELASTICITY; STRETCH; TESTS;

D O I：

10.1016/j.proeng.2017.02.426

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

Within this paper, the material behavior of an advanced composite laminate subjected to static cyclic bending loads have been experimentally determined on an LR5KP1us Lloyd Instruments materials testing machine. The composite laminate structure is formed of HELIOPOL 9431 ATYX_LSE resin reinforced with five layers STRATIMAT300 glass fibers of 300 g/m(2) specific weight. One composite specimen has been subjected to various deflection limits to determine its hysteresis behavior. The results show a maximum hysteresis towards 14 mm upper deflection limit. (C) 2017 The Authors. Published by Elsevier Ltd.

引用

页码：175 / 181

页数：7

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