纤维增强陶瓷基复合材料

碳纤维增强陶瓷基复合材料富碳界面

A Study of Carbon Fiber Reinforced Ceramic Composites with Rich-carbon Interphase

先驱体转化法制备连续纤维增强陶瓷基复合材料的研究

Research and Development of Continuous-Fiber-Reinforced Ceramic Matrix Composites Fabricated by Precursor-Infiltration-Pyrolysis

纤维增强陶瓷基复合材料的强化、韧化机制

Strength and Toughness of Fiber Reinforced Ceramic Matrix Composites

连续纤维增强陶瓷基复合材料界面研究进展

Progress of Continuous Fibers Reinforced Ceramic Matrix Composites Interfaces

活性填料在先驱体转化法纤维增强陶瓷基复合材料中的应用Ⅰ.复合材料的致密化模型

Application of active filler in preparation of fiber reinforced ceramic matrix composites by polymer-infiltration-pyrolysis ⅰ . densification models

由于纤维增强陶瓷基复合材料属于难加工材料，使得其加工特别是成形加工非常困难。

Because fiber reinforced ceramic matrix composite is considered to be difficult-to-machine material , its machining especially forming machining is very difficult .

研究了不同介质中单向短纤维增强玻璃陶瓷基复合材料的静疲劳行为。

The static fatigue behaviors of unidirectional short fiber reinforced glass ceramic matrix composites under different medium were investigated .

短碳化硅纤维增强玻璃陶瓷基复合材料的弯曲应力-挠度曲线、以及断裂行为具有与长纤维复合材料类似的特征，其断裂方式为非灾难性断裂。

The bending stress - flexibility , fracture behavior of short fibers composite are same as long fiber composite .

研究了单向短碳纤维增强玻璃陶瓷基复合材料的氧化行为.结果表明：短碳纤维复合材料氧化随时间的变化符合抛物线规律，基体对短纤维的包裹在一定程度上减缓了后期氧化速率；

The oxidation behavior of unidirectional chopped carbon fiber reinforced LAS ( Lithium Aluminosilicate ) glass ceramic matrix composite is studied .

单向短碳化硅纤维增强玻璃陶瓷基复合材料的主要增强机制为纤维脱粘、纤维滑移、纤维桥接、纤维断裂与纤维拔出。

It is considered that the main strengthen mechanism are un-bonded , slip , bridge , fracture and pull out of fiber .

采用料浆渗积-有机前躯体裂解工艺制备碳纤维增强碳化硅陶瓷基复合材料。

Three dimensional carbon fiber reinforced silicon carbide ceramic matrix Composites were fabricated by SiC slurry infiltration - precursor conversion in this paper .

非相变增韧陶瓷、相变增韧陶瓷、晶须（或纤维）增强陶瓷基复合材料的循环疲劳行为和疲劳裂纹扩展机理。

The main topics includes the fatigue behavior and fatigue mechanisms in non-transforming toughened ceramics , ZrO_2-toughened ceramics and whisker ( fiber ) - reinforced ceramic matrix composites ( CMC ) .

连续碳纤维增强碳化硅陶瓷基复合材料（C/SiC）是一种极具潜力的高温结构复合材料，在航空航天、能源及核技术等领域有着广阔的应用前景。

Continuous carbon fiber reinforced silicon carbide ceramic matrix composites ( C / SiC ) are considered as the most promising thermal structural candidate materials for aerospace , energy and nuclear technologies etc.

用化学气相渗透法制备了三维针刺碳纤维增强碳化硅陶瓷基复合材料，复合材料的平均密度为2.15g/cm3，气孔率为16.0%。

The ablation property of three dimensional needled carbon / silicon carbide composites with a density of 2.15 g / cm3 and a porosity of 16.0 % fabricated by the chemical vapor infiltration was studied using oxyacetylene ablation equipment .

采用先驱体转化法制备了2.5维石英纤维织物增强氮化物陶瓷基复合材料。

Using the polymeric precursor impregnation and pyrolysis method , 2.5-dimensional braided silica fiber-reinforced ni-tride-based composites ( 2.5D-SRNCs ) were prepared .