High-temperature fretting wear behavior and microstructure stability of a laser-cladding Ti-Al-C-N composite coating meditated by variable cycle conditions
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引用次数: 0
Abstract
Ti-6Al-4 V titanium alloy is used for low-pressure compressor blades of aero-engine due to its high specific strength, excellent corrosion resistance and high-temperature stability. Low-pressure compressor blades are subject to fretting wear in service, which may lead to fracture failure of the blades. The preparation of wear-resistant coatings is currently an effective solution in solving the problem of fretting wear on Ti-6Al-4 V titanium alloy. However, the fretting wear resistance and microstructure stability of the coating under variable cycle fretting conditions require more attention. In this work, the fretting wear performance and microstructure stability of the Ti-Al-C-N composite coating under variable cycle fretting conditions are investigated. The results show that the parameters of variable cycle operating conditions have a notable effect on the coefficient of friction (COF). The variable frequency and variable temperature working conditions result in the alteration of the fretting operation mechanism. Whereas the variable stroke amplitude and the variable load conditions do not cause changes in the fretting operation mechanism, and both are in the gross slip region (GSR). The lowest wear rate occurs under variable stroke amplitude conditions. The wear rate is the maximum under the variable cycle temperature condition. According to the dissipated energy calculation, the difference between the two different stroke amplitudes is the biggest among all the conditions. EBSD and TEM analyses show that the subsurface of variable stroke amplitude worn scar has a more uniform strain distribution, and reveals a unique subsurface structure with a transformation from crystalline to amorphous, which contributes to improving the wear resistance. This work provides insights into coating microstructure stability and wear mechanisms under variable cycle conditions.
Ti-6Al-4 V 钛合金具有高比强度、优异的耐腐蚀性和高温稳定性,可用于航空发动机的低压压缩机叶片。低压压缩机叶片在使用过程中会受到摩擦磨损,可能导致叶片断裂失效。目前,制备耐磨涂层是解决 Ti-6Al-4 V 钛合金摩擦磨损问题的有效方法。然而,涂层在变循环烧蚀条件下的抗烧蚀磨损性和微观结构稳定性需要更多的关注。本文研究了变循环烧蚀条件下 Ti-Al-C-N 复合涂层的烧蚀磨损性能和微观结构稳定性。结果表明,变循环工作条件参数对摩擦系数(COF)有显著影响。变频和变温工作条件导致了摩擦运行机制的改变。而变冲程振幅和变载荷工况不会导致摩擦磨损机理发生变化,且都处于总滑移区(GSR)。在变行程振幅条件下,磨损率最低。在变循环温度条件下,磨损率最大。根据耗散能量计算,两种不同冲程振幅之间的差异是所有条件中最大的。EBSD 和 TEM 分析表明,变冲程振幅磨损疤痕的次表面应变分布更均匀,并显示出独特的次表面结构,即从晶体到非晶体的转变,这有助于提高耐磨性。这项工作有助于深入了解变循环条件下涂层微观结构的稳定性和磨损机制。
期刊介绍:
Tribology is the science of rubbing surfaces and contributes to every facet of our everyday life, from live cell friction to engine lubrication and seismology. As such tribology is truly multidisciplinary and this extraordinary breadth of scientific interest is reflected in the scope of Tribology International.
Tribology International seeks to publish original research papers of the highest scientific quality to provide an archival resource for scientists from all backgrounds. Written contributions are invited reporting experimental and modelling studies both in established areas of tribology and emerging fields. Scientific topics include the physics or chemistry of tribo-surfaces, bio-tribology, surface engineering and materials, contact mechanics, nano-tribology, lubricants and hydrodynamic lubrication.