Mechanical behavior of LSI based C/C-SiC composites subjected to flexural loadings

被引:46
|
作者
Li, Yang [1 ,2 ]
Xiao, Peng [1 ]
Shi, Yuan [3 ]
Almeida, Renato S. M. [4 ]
Zhou, Wei [1 ]
Li, Zhuan [1 ]
Luo, Heng [1 ]
Reichert, Florian [2 ]
Langhof, Nico [2 ]
Krenkel, Walter [2 ]
机构
[1] Cent S Univ, State Key Lab Powder Met, Changsha 410083, Peoples R China
[2] Univ Bayreuth, Ceram Mat Engn, D-95447 Bayreuth, Germany
[3] German Aerosp Ctr, Inst Struct & Design, D-70569 Stuttgart, Germany
[4] Univ Bremen, Adv Ceram, D-28359 Bremen, Germany
基金
中国国家自然科学基金;
关键词
c/c-sic; Flexural fatigue; Interfacial degradation; 3D reinforcement; CERAMIC-MATRIX COMPOSITES; THERMAL RESIDUAL-STRESS; FIBER-REINFORCED CARBON; FATIGUE BEHAVIOR; ROOM-TEMPERATURE; TENSILE FATIGUE; CARBON/CARBON COMPOSITES; STRENGTH EVOLUTION; BRAKE COMPOSITES; MICROSTRUCTURE;
D O I
10.1016/j.compositesa.2017.01.024
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In general, flexural loads result in more complicated and uneven stress distributions in specimens, compared to axial loading. This study reports the influence of flexural fatigue loads including different stress levels and cycles on the mechanical behavior of a 3D C/C-SiC composite. The cyclic tensile loads in the lower part of the specimens result in strength enhancement after short fatigue duration with the expense of decreased flexural modulus due to the fatigue damage such as cracking and interfacial degradation. Whereas the upper part of the post-fatigue specimens, which is almost free of fatigue damage under compressive stress, can still properly deflect the cracks and result in quasi-plastic failures like virgin specimens. Most notably, specimens will suffer strength decline rapidly, after 50,000 cycles with maximum stress of 95 MPa for instance, because of considerable stress concentrations and wear of fibers at 90 fiber bundles in the lower part. (C) 2017 Elsevier Ltd. All rights reserved.
引用
收藏
页码:315 / 324
页数:10
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