Crack propagation and residual stress in laminated Si3N4/BN composite structures

被引:16
|
作者
Krstic, Zoran [1 ]
Krstic, Vladimir D. [1 ]
机构
[1] Queens Univ, Dept Mat & Mech, Kingston, ON K7L 3N6, Canada
关键词
Composites; Residual stress; Crack propagation; Thermal expansion; Interfaces; INDENTATION;
D O I
10.1016/j.jeurceramsoc.2011.03.009
中图分类号
TQ174 [陶瓷工业]; TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The level of residual stress and crack propagation in a new generation of laminates, based on silicon nitride (Si3N4) layer and a mixture of boron nitride (BN) and alumina (Al2O3) interlayer, was presented. The structure consists of alternated concentric rings of Si3N4 separated by the weak BN interlayer possessing no planes of easy crack propagation and fracture resistance much larger than that of any classical planar laminates. The results on direction of crack propagation and residual stress in relation to inter-layer composition, the number of layers, and their thickness are investigated and reported. The effect of residual stress on crack propagation was studied by using Vicksrs intentation. The highest compressive residual stress of similar to 170 MPa was found in samples with five layers possessing an average layer thickness of similar to 310 x 10(-6) m. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1841 / 1847
页数:7
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