Fatigue behavior of an advanced SiC/SiC ceramic composite with a self-healing matrix at 1300°C in air and in steam

被引:53
作者
Ruggles-Wrenn, M. B. [1 ]
Lee, M. D. [1 ]
机构
[1] US Air Force, Inst Technol, Dept Aeronaut & Astronaut, Wright Patterson AFB, OH 45433 USA
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 2016年 / 677卷
关键词
Ceramic-matrix composites (CMCs); Fatigue; High-temperature properties; Mechanical properties; Fractography; CREEP-BEHAVIOR; HI-NICALON(TM)/SIC-B4C COMPOSITE; NOTCH SENSITIVITY; SIC FIBERS; DEGREES-C; OXIDATION; TEMPERATURE; MECHANISMS; STABILITY; TENSION;
D O I
10.1016/j.msea.2016.09.076
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The fatigue behavior of a non-oxide ceramic composite with a multilayered matrix was investigated at 1300 degrees C in laboratory air and in steam environment. The composite was produced via chemical vapor infiltration (CVI). 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-NicalonTM fibers. Fiber preforms had pyrolytic carbon fiber coating with boron carbon overlay applied. Tensile stress-strain behavior and tensile properties were evaluated at 1300 degrees C. Tension-tension fatigue behavior was studied for fatigue stresses ranging from 70 to 160 MPa in air and in steam. The fatigue limit (based on a run-out condition of 2 x 10(5) cycles) was between 80 and 100 MPa. Presence of steam had little influence on fatigue performance. The retained properties of all specimens that achieved fatigue run-out were characterized. Composite microstructure, as well as damage and failure mechanisms were investigated. Published by Elsevier B.V.
引用
收藏
页码:438 / 445
页数:8
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