成型压力对自粘性预浸料复合材料性能的影响  

THE INFLUENCE OF CURE PRESSURE ON PROPERTIES OF COMPOSITE MADE FROM SELF-STICKY PREPREGS

作　　者：赵鹏飞[1] 赵景丽[1] 何颖[1] 

机构地区：[1]西北工业大学第365研究所,西安710072

出　　处：《玻璃钢／复合材料》2010年第4期65-67,52,共4页Fiber Reinforced Plastics/Composites

摘　　要：本文通过试验比较了ACG公司以MTM-28为树脂基体的几种预浸料经热压罐固化成型与烘箱真空固化成型层压板或蜂窝夹层结构面板试样的力学性能,验证了该类预浸料适用于两种固化工艺条件的规范是适当的。This article compares the mechanical properties of composite laminates and panels of honeycomb sandwich structure made from ACG＇s MTM-28 matrix prepregs.The composites of the samples are cured in autoclave or in oven with vacuum system.The results show that these kinds of prepregs are available to autoclave and vacuum-bag techniques,as introduced in ACG＇s specifications.

关 键 词：无人机飞机机体 复合材料 预浸料 压力 力学性能 

分 类 号：TB332[一般工业技术—材料科学与工程]