首页> 外文会议>14th ASTM International Symposium on Composite Materials: Testing and Design; Mar 11-12, 2002; Pittsburgh, PA >Fatigue Life of SCS-6/Timetal~(~R) 834 at Room Temperature and 600℃: Experiments and Modeling
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Fatigue Life of SCS-6/Timetal~(~R) 834 at Room Temperature and 600℃: Experiments and Modeling

机译:SCS-6 / Timetal〜(〜R)834在室温和600℃下的疲劳寿命:实验和建模

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摘要

Fatigue of the titanium matrix composite (TMC) SCS6/Timetal 834 has been investigated at room temperature and 600℃. Whereas the room temperature behavior is mainly influenced by fatigue crack formation and growth, this is not the case for fatigue at 600℃. The runout specimens did not show any crack, whereas runout specimens tested at room temperature showed multiple transverse cracks with a characteristic distance. The main reason for the lack of cracks was found to be the result of stress relaxation of the matrix. This effect is strong due to the fact that the first 10~5 cycles are performed at a low frequency (0.25 Hz). In the second part of this work attention is focused on modeling the most important damage mechanism under room temperature conditions. Initial computation of crack growth rates in TMC, assuming interfacial friction being the only stress transfer mechanism (i.e., bond strength is considered to be zero), proved to be unrealistically high. For that reason in the present work crack growth rates are calculated considering a fiber/matrix bond strength and friction in case the bond breaks. In this case three dimensional finite element models deliver more accurate crack growth rates.
机译:研究了钛基复合材料(TMC)SCS6 / Timetal 834在室温和600℃下的疲劳。室温下的行为主要受疲劳裂纹形成和扩展的影响,而600℃时的疲劳则不是这种情况。跳动试样未显示任何裂纹,而在室温下测试的跳动试样显示多个具有特征距离的横向裂纹。发现没有裂纹的主要原因是基体应力松弛的结果。由于前10到5个周期是在低频(0.25 Hz)下执行的,因此这种效果很强。在这项工作的第二部分中,注意力集中在对室温条件下最重要的损坏机理进行建模上。假设界面摩擦是唯一的应力传递机制(即粘结强度被认为是零),则TMC中裂纹扩展速率的初始计算被证明是不切实际的。因此,在目前的工作中,考虑到纤维/基体的粘结强度和在粘结破裂的情况下的摩擦力来计算裂纹扩展速率。在这种情况下,三维有限元模型可提供更准确的裂纹扩展速率。

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