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首页> 外文期刊>Applied Composite Materials >Notch Sensitivity of Fatigue Behavior of a Hi-Nicalon™/SiC-B4C Composite at 1,200 °C in Air and in Steam
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Notch Sensitivity of Fatigue Behavior of a Hi-Nicalon™/SiC-B4C Composite at 1,200 °C in Air and in Steam

机译:Hi-Nicalon™/ SiC-B4C复合材料在空气和蒸汽中在1,200°C时的疲劳行为的缺口敏感性

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The effect of holes on the fatigue life of a non-oxide ceramic composite processed via chemical vapor infiltration (CVI) was examined at 1,200 °C in laboratory air and in steam. The effect of holes on tensile strength at 1,200 °C was also evaluated. The composite comprised laminated woven Hi-Nicalon™ fibers in an oxidation inhibited matrix, which consisted of alternating layers of silicon carbide and boron carbide. Fiber preforms had pyrolytic carbon fiber coating with boron carbon overlay applied. Unnotched specimens and specimens with a center hole having a radius to width ratio of 0.24 were tested in tension-tension fatigue at 0.1 Hz and at 1.0 Hz. The fatigue stresses ranged from 100 to 140 MPa in air and in steam. Fatigue run-out was defined as 105 cycles at 0.1 Hz and as 2 × 105 cycles at 1.0 Hz. The net-section strength was less than the unnotched ultimate tensile strength. Comparison of notched and unnotched data also revealed that the fatigue performance was notch insensitive in both air and steam environments. Composite microstructure, as well as damage and failure mechanisms were investigated.
机译:在1,200°C的实验室空气和蒸汽中检查了孔对通过化学气相渗透(CVI)处理的非氧化物陶瓷复合材料的疲劳寿命的影响。还评估了孔对1,200°C拉伸强度的影响。该复合材料包括处于氧化抑制基质中的层压机织Hi-Nicalon™纤维,该纤维由碳化硅和碳化硼的交替层组成。纤维预成型件具有热解碳纤维涂层,并涂有硼碳涂层。在0.1Hz和1.0Hz的拉伸-拉伸疲劳试验中,对未开槽的试样和半径与宽度之比为0.24的中心孔试样进行了测试。空气和蒸汽中的疲劳应力范围为100至140 MPa。疲劳跳动定义为0.1 Hz下的105个周期和1.0 Hz下的2××105个周期。净截面强度小于无缺口的极限抗拉强度。缺口和未缺口数据的比较还表明,疲劳性能在空气和蒸汽环境下均不敏感。研究了复合材料的微观结构,以及破坏和破坏机理。

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