树脂基复合材料

先进航空树脂基复合材料研究与应用进展

Development and application of advanced aeronautical polymer matrix composites

树脂基复合材料热固化过程微机控制系统

A PC control system for thermal curing of polymer matrix composites

本研究采用常压浸渍工艺制备了玻璃纤维增强光固化聚丙烯酸酯类树脂基复合材料（GL/EEPE和G（3D）/EEPE）。

In this paper , glass fiber reinforced visible light curable dimethacrylate resin composites were prepared through impregnation technique .

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。

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

光固化快速成型中SiC晶须增强树脂基复合材料的研究

Investigation on the SiC Whisker Reinforced Resin Matrix Composite in the UV Curing of Rapid Prototyping

用Weibull模数表征炭纤维增强树脂基复合材料的力学性能

Characterization of the mechanic properties of CFRP with Weibull distribution theory

ZnO晶须及其树脂基复合材料的研究进展

ZnO Whisker and Its Composites

炭黑/二氧化硅/环氧树脂基复合材料的PTC效应

PTC effect in carbon black / silica loaded epoxy resin

树脂基复合材料中石墨与MoS2的减摩作用机理

Antifriction Mechanism of Graphite and MoS_2 in Epoxy Composites

BMP系列热固性聚酰亚胺树脂基复合材料的应用进展

Application Progress of BMP Thermosetting Polyimide Resin Matrix Composites

炭纤维增强树脂基复合材料（CFRP）是炭纤维应用的主要形式。

Carbon fibers reinforced plastics composites ( CFRP ) is a main form of utilization of carbon fibers .

本文采用ENF试样研究了树脂基复合材料T300/5405单向板的Ⅱ型层间断裂韧性G（Ⅱc）。

The mode n interlaminar fracture toughness of T300 / 5405 composite laminates was investigated . The ENF specimen was used .

通过透射电镜测试观察分析了PI及SiC／PI树脂基复合材料的组织结构；

Have passed electric mirror of transmission test and observed and analyzed the institutional framework of PI and SiC / PI resin base composite ;

对单向及正交碳纤维增强树脂基复合材料（CFRP）在静态拉伸及动态拉-拉载荷作用下的电阻-应变特性进行了研究。

The characteristics of electric resistance-strain relationship of unidirectional and cross-ply CFRP laminates were studied under static and tensile-tensile dynamic loading .

利用红外分析仪测量了光谱吸收情况，分析了SiC／PI树脂基复合材料的微观化学结构；

Utilize the infrared analysis instrument to measure the spectrum to absorb the situation , has analyzed the micro chemical constitution of SiC / PI resin base composite ;

碳织物增强热塑性PEEK树脂基复合材料是一种适合空间环境的高性能复合材料，可以用于制作光学反射镜。

So , this composite is an excellent high performance composite , which was suitable for service in space environment .

航空发动机用PMR聚酰亚胺树脂基复合材料

High-temperature polyimide composites and its application in aeronautical engine

根据碳纤维的晶体学特点，提出了利用X射线衍射技术分析碳纤维/树脂基复合材料界面残余应力的新方法。

Based on the crystallography properties of carbon fiber , a method of determining the interfacial residual stress in carbon fiber reinforced epoxy composites by X ray diffraction technique was established in this paper .

应用动态差示扫描量热（DSC）方法对炭纤维增强树脂基复合材料（CFRP）压力容器树脂体系固化反应进行分析。

The non-isothermal differential scanning calorimetry ( DSC ) technique was used to study the cure kinetics of the resin system for the CFRP pressure vessel .

S-2玻纤增强树脂基复合材料弹托的试验研究

An experimental study sabots made of S-2 glassfibre reinforced composites

PEK-C对酚醛树脂基复合材料性能的影响

Influence of PEK-C resin on phenolic composite property

本文详细介绍了树脂基复合材料（FRP）的组成材料，探讨了用于混凝土结构增强和加固的树脂基复合材料的成型工艺。

This paper introduces the Components for Composite materials with polymer matrix in detail and Studies the process of Composite materials with polymer matrix used for reinforcing and Strengthening Concrete structures .

FRP（树脂基复合材料）拉挤工艺过程研究的一项重要任务就是确定合适的拉挤工艺参数，模具温度是拉挤工艺过程中的最重要的参数之一。

One of the important tasks in pultrusion of FRP ( Fiber Reinforce Plastic ) is the confirmation of appropriate process parameters , the die temperature is one of the most important parameters .

利用INSTRON实验机和落锤装置对圆筒形碳纤维增强环氧树脂基复合材料结构进行了静、动态压缩实验。

Cylinder structure of carbon fiber reinforced epoxy resin matrix composite material is compressed by INSTRON and drop weight experimental equipment .

根据玻璃纤维毡增强热塑性树脂基复合材料（GMT）制备新工艺特点，提出了稀相喷动流化床的操作方式。

Due to the characteristics of the new process for manufacturing glass mat reinforced thermoplastic ( GMT ) sheets , the way of dilute spout-fluid bed was proposed .

SiC（W芯）纤维/树脂基复合材料并具有明显的吸收电磁波的性能。

The SiC ( W core ) filament / resin composites also have the capability to absorb electromagnetic waves . The SiC ( W core ) filament composites are expected to be widely used in the fields of aviation and aerospace .

因为单向炭纤维增强树脂基复合材料（UD－CFRP）属于脆性材料，它的力学性能如层间剪切强度（ILSS）的大小依赖于UD－CFRP中随机分布的缺陷。

Because carbon fibers reinforced plastic ( CFRP ) composites belong to brittle materials their mechanic properties such as interlaminar shear strength ( ILSS ) depend on stochastic defects .

在此基础上，借助银浆导电胶，制成了中间充有PI与不同纳米SiC含量的SiC／PI树脂基复合材料薄膜的平行板式电容器。

On this basis , draw support from the conductive glue of silver thick liquid , fill on the condenser of parallel modes in Chinese operatic music of SiC / PI resin base composite membrane with PI and different nanometer SiC content while making .

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。

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 .

作为重要的先进航空航天结构材料，碳纤维增强树脂基复合材料（CFRP）的性能取决于增强碳纤维与树脂基体的性能以及两者之间的界面结合状况。

As an important advanced structural materials in the area of aerospace , the properties of carbon fiber reinforced polymer ( CFRP ) highly depend on the properties of the carbon fiber ( CF ) and the resin matrix , and the properties of interface .