resin matrix composite

Discussion on Out put/ Input Effectiveness for Advanced Defense Research Review of the DARPA Affordable Resin Matrix Composite Program

国防预研投入产出效益探讨美国国防预研计划局支付得起的树脂基复合材料计划进展述评

The 3-5 μ m non-porous composite microspheres of zirconia and urea-formaldehyde ( UF) resin were used as matrix of HPLAC stationary phase. The diameter and construction of the composite microspheres were judged by scanning electron microscope.

以3－5μm的非多孔二氧化锆与脲醛树脂（UTR）复合物微球用作高效液相亲和色谱固定相的基体，并用扫描电子显微镜检验该基体的结构和粒径。

When the content of 3wt% silane-treated barium glass filler reached 40wt%, simultaneously added 3wt% nano-sized silic into resin matrix, the experimental composite obtained optimal mechanical properties and suitable viscosity. 5.

当3wt%硅烷偶联剂处理后的钡玻璃填料在树脂体系中含量达到40wt%，同时加入3wt%的二氧化硅纳米填料，可以获得较佳的复合树脂力学性能和适合的树脂体系粘度。

This paper describes the goads of the DARPA affordable resin matrix composite program, reviews the developing status and technology maturity levels of the projects under the program.

本文介绍美国国防预研计划局（DARPA）支付得起的树脂基复合材料计划的目标，评述该计划的项目进展状况和各项目技术成熟水平。

The curing process of thermosetting resin matrix composite materials involves complex mechanical, thermal and chemical reactions.

树脂基复合材料的热固化成型是一个力 、 热与化学反应相互耦合的过程.

The manufacturability, microhardness, tensile-strength of SiC whisker/ Resin Matrix Composite was investigated.

考察了SiC晶须树脂基复合材料的工艺性，硬度，拉伸强度等性能。

Upper limit working temperature of resin matrix composite

树脂基复合材料的上限工作温度

The design of structure and laminating, the choice of matrix resin and forming process as well as its performance test for a composite tail boom of an unmanned air vehicle are introduced in this paper.

本文介绍了复合材料管件（无人机尾撑杆）的结构与铺层设计、基体树脂选择和成型工艺以及性能测试等内容。

This sensor is embedded in a resin matrix composite lath to detect the change of lath's curvature.

将此传感器埋入树脂基复合材料板内部，测量板的弯曲变形。