Influence of a hydrogen/oxygen flame on the fire-behaviour and the tensile properties of hybrid Carbon Glass fibers reinforced PEEK composite laminates

被引:0
|
作者
Vieille, B. [1 ]
Davin, T. [1 ]
Barbe, F. [1 ]
Sarazin, J. [2 ]
Bourbigot, S. [2 ,3 ]
机构
[1] Normandie Univ, UNIROUEN Normandie, INSA Rouen, CNRS,Grp Phys Mat, F-76800 St Etienne Du Rouvray, France
[2] Univ Lille, CNRS, ENSCL, UMR 8207,UMET,Unite Mat & Transformat, F-5900 Lille, France
[3] Inst Univ France, Paris, France
关键词
Hydrogen flame; Thermoplastic; Pyrolysis; Post-fire behaviour; Mechanical testing; HEAT-TRANSFER; PRESSURE-VESSELS; STORAGE; CYLINDERS; TESTS;
D O I
10.1016/j.ijhydene.2024.09.288
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
This study investigates the residual tensile behaviour of hybrid Carbon Glass fibers reinforced thermoplastic PEEK laminates after they were exposed for 5 min to a hydrogen/oxygen flame. This flame results in a severe thermal aggression characterized by a wall temperature ranging from 900 to 1270 degrees C and with different heat fluxes (from 200 to 800 kW/m(2)). The thermally-induced damages were examined by means of microscopic observations and micro CT analyses. The results show that the mass loss linearly depends on the measured heat flux for a 5 min exposure. Depending on the fire testing conditions, the mechanical properties in tension (stiffness and strength) are totally degraded after exposure to the highest heat fluxes (600 and 800 kW/m(2)) but the retention of the tensile properties is moderate (about -35 to -60% decrease in strength and stiffness, respectively) after exposure to a 200 kW/m(2) heat flux. The residual tensile properties of CG/PEEK laminates follow master curves representing the correlations between the mass loss and the changes in the tensile properties regardless the heat flux. These master curves provide a relevant design rule for composite parts to be used under critical service conditions (H-2/O-2 flame exposure).
引用
收藏
页码:1226 / 1236
页数:11
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