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Erosive wear analysis of propeller blade coated with tungsten carbide cobalt by high-velocity oxy-fuel spray method

机译:高速氧燃料喷涂法涂有碳化钨钴碳化钨螺旋桨叶片的腐蚀磨损分析

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摘要

In the present study, the erosive wear of boat propeller blades with tungsten carbide cobalt (WC-Co) coatings by high-velocity oxy-fuel (HVOF) under different erosive wear conditions were investigated and compared with the wear of uncoated one. The (WC-Co) coating was deposited on Al7034 T6 composite reinforced with (Al_(2)O_(3)) and (SiC) particle in different weight percentages. Micro hardness test was employed to determine the hardness of the composite substrate. Eroded surface of the substrate was examined through scanning electron microscope (SEM). Finite element modelling was used to analyse the fracture surface of the propeller blade. Impact analysis was used to determine the stresses induced and deformation evolution under various impact condition. It is shown that crack was initiated from the surface of the blade and finally damages the blade at velocity 500 m/s under cyclic loading. This damage causes the improper functioning of the propeller blade and induced aerodynamic forces to increase the vibrational amplitude of the rotor blade. Results show that (WC-Co) coated propeller blade predominant over the life of the uncoated blade.
机译:在本研究中,通过在不同腐蚀磨损条件下采用高速氧燃料(HVOF)与碳化钨钴(WC-CO)涂层的船螺旋桨叶片的腐蚀磨损,并与未涂覆的磨损进行比较。用(Al_(2)O_(3))和(SiC)颗粒以不同的重量百分比沉积(WC-CO)涂层沉积在Al7034 T6复合物上。使用微硬度试验来确定复合衬底的硬度。通过扫描电子显微镜(SEM)检查基板的腐蚀表面。有限元建模用于分析螺旋桨叶片的断裂表面。采用影响分析来确定各种冲击条件下诱导和变形演化的应力。结果表明,从叶片的表面引发裂缝,最后在环状载荷下损坏速度为500m / s的叶片。这种损坏导致螺旋桨叶片的功能不当,并且诱导的空气动力力以增加转子叶片的振动幅度。结果表明,(WC-CO)涂覆的螺旋桨叶片在未涂层刀片的寿命上主要。

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