Tension-compression fatigue of a SiC/SiC ceramic matrix composite at 1200 °C in air and in steam

被引:50
|
作者
Ruggles-Wrenn, M. B. [1 ]
Jones, T. P. [1 ]
机构
[1] USAF, Inst Technol, Dept Aeronaut & Astronaut, Wright Patterson AFB, OH 45433 USA
关键词
Ceramic matrix composites (CMCs); Fatigue; High-temperature properties; Mechanical properties; Fractography; CREEP-BEHAVIOR; HIGH-TEMPERATURE; OXIDATION; STABILITY; FAILURE; DAMAGE; SIBC;
D O I
10.1016/j.ijfatigue.2012.08.006
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Tension-compression fatigue behavior of a non-oxide ceramic composite with a multilayered matrix was investigated at 1200 degrees C in laboratory air and in steam. The composite was produced via chemical vapor infiltration (CVO. The composite had an oxidation inhibited matrix, which consisted of alternating layers of silicon carbide and boron carbide and was reinforced with laminated woven Hi-Nicalon (TM) fibers. Fiber preforms had pyrolytic carbon fiber coating with boron carbide overlay applied. Tension-compression fatigue behavior was studied for fatigue stresses ranging from 80 to 200 MPa at a frequency of 1.0 Hz. Presence of steam significantly degraded the fatigue performance. Specimens that achieved fatigue run-out were subjected to tensile tests to failure to characterize the retained tensile properties. The material retained 100% of its tensile strength. Composite microstructure, as well as damage and failure mechanisms were investigated. Published by Elsevier Ltd.
引用
收藏
页码:154 / 160
页数:7
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