首页> 外文会议>ASME Turbomachinery Technical Conference and Exposition >FRETTING FATIGUE AND WEAR OF TI-6AL-4V WITH HVOF SPRAYED STELLITE COATING ON CONTACT SURFACES OF SHROUDS AND STUBS OF TURBINE BLADES
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FRETTING FATIGUE AND WEAR OF TI-6AL-4V WITH HVOF SPRAYED STELLITE COATING ON CONTACT SURFACES OF SHROUDS AND STUBS OF TURBINE BLADES

机译:用HVOF喷涂毛线涂层疲劳和磨损Ti-6AL-4V的磨损和涡轮叶片的带罩和短截线

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High velocity oxygen fuel (HVOF) sprayed stellite coating is often adopted on contact surfaces of the shrouds and stubs of titanium turbine blades, in order to increase fretting fatigue strength and reduce fretting wear. To confirm the effectiveness of the sprayed stellite coating, we conducted friction-type fretting tests originally developed to simulate the load condition of shrouds and stubs, vibratory force was carried only by friction force. We also investigated the fretting fatigue mechanism of coated materials by observing non-propagating cracks in the tested specimens and analyzed crack propagation behavior at the interface using fracture mechanics. The fretting fatigue tests confirmed that the sprayed stellite coating could double the fretting fatigue strength of Ti-6Al-4V. The fretting fatigue mechanism of Ti-6Al-4V with a sprayed stellite coating was revealed as follows: Final fracture was led by a newly initiated micro-crack at the interface as cracks initiated on the coating surface did not continuously propagate into the substrate but mainly propagated along the interface. The micro-crack propagation at the substrate depends on the length of interface crack. The longer interface crack delays micro-crack propagation to the substrate because the lines of force are less concentrated at the crack tip. Hence, the interface crack makes the fretting fatigue strength of coated Ti-6Al-4V higher than that of uncoated specimens. This finding was supported by the cross-sectional observations of non-propagating cracks in the tested specimens, and by FE analysis which revealed that ΔK of the substrate crack initiated at the interface decreases with an increase in delaminated crack length. Ti-6Al-4V with a sprayed stellite coating offers better wear resistance than uncoated Ti-6Al-4V because the coating's friction coefficient is lower than that of Ti-6Al-4V, although the wear rates of coated and uncoated materials against the consumption energy per cycle were almost the same.
机译:高速氧气燃料(HVOF)喷涂的粗涂层通常采用钛涡轮叶片的护罩和短截线的接触表面上采用,以提高疲劳疲劳强度并减少微动磨损。为了确认喷涂的脱衣涂层的有效性,我们进行了摩擦型微动试验,最初开发出用于模拟护罩和短截线的负载条件,振动力仅通过摩擦力携带。我们还通过观察试样中的非繁殖裂缝并在界面中分析使用骨折力学来分析裂纹传播行为的涂覆材料的微动疲劳机理。微动疲劳试验证实,喷涂的恒星涂层可以使Ti-6Al-4V的微动疲劳强度增加。 Ti-6Al-4V与喷涂的星形涂层的微裂疲劳机理如下:最终裂缝通过在界面上的裂缝在界面上进行的新引发的微裂纹引起,因为在涂层表面上没有连续地传播到基材中但主要是沿接口传播。基板上的微裂纹传播取决于界面裂纹的长度。较长的界面裂缝延迟到基板上的微裂纹传播,因为力线浓缩在裂缝尖端处。因此,界面裂缝使得涂覆的Ti-6Al-4V高于比未涂层标本高的疲劳强度。该发现得到了测试样品中的非传播裂缝的横截面观察,以及通过Fe分析,显示在界面处引发的基板裂纹的ΔK随着分层裂缝长度的增加而降低。带喷涂的星形涂层的Ti-6Al-4V提供比未涂层的Ti-6AL-4V更好的耐磨性,因为涂层的摩擦系数低于Ti-6Al-4V,尽管涂层和未涂覆材料的磨损率抵抗消费能量每个周期几乎是一样的。

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