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Experiments on Residual Compressive Strength After Fatigue of Carbon Fiber Fabric Composites of Spacecraft in Hydrothermal Environment

机译:水热环境航天器碳纤维织物复合材料疲劳疲劳之后的实验

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In order to study the effect of hydrothermal environment on the fatigue properties of carbon fiber fabric composites, the experiments on fatigue and residual compressive strength with the center-hole laminates were carried out. For the experiments on fatigue in hydrothermal environment, an environmental chamber used for hydrothermal environment was designed, and the FLUENT was used to simulate the field of temperature in the environmental chamber, it proved that the design met the test requirements. In accordance with ASTM standard, the fatigue test fixture and compression test fixture were designed and produced. Then the tension-compression fatigue tests were carried out in conditions of standard environment(temperature of 23+2 °C, relative humidity of 50+/-5%RH)and hydrothermal environment(temperature of 70 +2°C, relative humidity of 85+/-5%RH). After that, the residual compressive strength tests were carried out, respectively. The residual compressive strength after fatigue in condition of standard environment was set as a reference value, compared with the value in condition of hydrothermal environment, calculating the difference between them. According to the result of residual compressive strength tests, it shows that the residual compressive strength after fatigue in condition of hydrothermal environment was decreased by 13.5%,so the hydrothermal environment has little effect on the residual compressive strength of carbon fiber fabric composites laminates after fatigue under load spectrum in this research.
机译:为了研究水热环境对碳纤维织物复合材料的疲劳性能的影响,进行了与中心孔层压板的疲劳和剩余抗压强度的实验。对于水热环境疲劳的实验,设计了一种用于水热环境的环境室,流畅的用于模拟环境室中的温度领域,证明了该设计达到了测试要求。根据ASTM标准,设计并制造了疲劳试验夹具和压缩试验夹具。然后在标准环境(温度为23 + 2℃,相对湿度的50 +/- 5%RH)和水热环境(温度为70 + 2°C,相对湿度的温度下进行张力 - 压缩疲劳试验85 +/- 5%RH)。之后,分别进行残留的抗压强度试验。标准环境条件下疲劳后的残留抗压强度被设定为参考值,与水热环境条件的值相比,计算它们之间的差异。根据残留抗压强度试验的结果,它表明,水热环境条件下疲劳后的残留抗压强度降低了13.5%,因此水热环境对疲劳后碳纤维织物复合材料的残留抗压强度几乎没有影响在该研究中的负载谱下。

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