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Fatigue and creep fracture properties of plane-woven SiC/SiC composites at room temperature and 1473K

机译:平面编织SiC / SiC复合材料在室温和1473K下的疲劳和蠕变断裂特性

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摘要

Fatigue tests of plane-woven SiC/SiC composites, which had carbon layer as the interphase on the surface of the fiber, were carried out at room temperature in air and at 1 473K in vacuum and also creep tests at 1 473K in vacuum. At room temperature, the S-N relation was almost flat and the level was slightly lower than the static strength, showing the fracture mechanism was similar to that of static fracture. On the other hand, at 1473K, fracture behavior was mainly caused by time-dependent creep mechanism. The fracture surface showed that debonding occurred between matrix and carbon interphase in the case of static tests at room temperature. On the other hand, in the cases of static, creep and creep fatigue tests at 1473K, debonding occurred between fiber and carbon interphase because of creep deformation of fiber. Delamination was also dominant for all cases. The length of delamination and debonding was longer in creep fatigue test at 1473K than in fatigue test at room temperature and creep test at 1473K because of reduction in sliding resistance of interface caused by cyclic loading. Thus, stress concentration caused by breakage of fiber and matrix was weaker in creep fatigue test than in creep test. The relation between the test time and the creep strain in creep tests could be evaluated quantitatively using the stress power law.
机译:在室温,空气中,真空度为1473K的条件下,进行了在纤维表面具有碳层作为相界面的平面编织SiC / SiC复合材料的疲劳试验,并在真空度为1473K的条件下进行了疲劳试验。在室温下,S-N关系几乎是平坦的,且水平略低于静态强度,表明断裂机理与静态断裂相似。另一方面,在1473K时,断裂行为主要是由时间相关的蠕变机制引起的。断裂表面表明,在室温下进行静态测试的情况下,基体与碳相之间会发生剥离。另一方面,在1473K的静态,蠕变和蠕变疲劳测试中,由于纤维的蠕变变形,在纤维和碳中间相之间发生了脱胶。在所有情况下,分层也是主要因素。在1473K的蠕变疲劳试验中,与在室温下的疲劳试验和在1473K的蠕变试验中相比,脱层和剥离的长度更长,这是由于循环载荷引起的界面滑动阻力的降低。因此,由纤维和基体断裂引起的应力集中在蠕变疲劳试验中比在蠕变试验中弱。蠕变试验中试验时间与蠕变应变之间的关系可以使用应力幂定律进行定量评估。

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