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首页> 外文期刊>Journal of Materials Engineering and Performance >Solid Particle Erosion Behaviors of Carbon-Fiber Epoxy Composite and Pure Titanium
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Solid Particle Erosion Behaviors of Carbon-Fiber Epoxy Composite and Pure Titanium

机译:碳纤维环氧复合材料和纯钛的固体颗粒冲蚀行为

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摘要

Rotor blades of Bell CH-146 Griffon helicopter experience excessive solid particle erosion at low altitudes in desert environment. The rotor blade is made of an advanced light-weight composite which, however, has a low resistance to solid particle erosion. Coatings have been developed and applied to protect the composite blade. However, due to the influence of coating process on composite material, the compatibility between coating and composite base, and the challenges of repairing damaged coatings as well as the inconsistency between the old and new coatings, replaceable thin metal shielding is an alternative approach; and titanium, due to its high-specific strength and better formability, is an ideal candidate. This work investigates solid particle erosion behaviors of carbon-fiber epoxy composite and titanium in order to assess the feasibility of titanium as a viable candidate for erosion shielding. Experiment results showed that carbon-fiber epoxy composite showed a brittle erosion behavior, whereas titanium showed a ductile erosion mode. The erosion rate on composite was 1.5 times of that on titanium at impingement angle 15 degrees and increased to 5 times at impact angle 90 degrees.
机译:贝尔CH-146 Griffon直升机的旋翼在沙漠环境中的低海拔地区会遭受过多的固体颗粒侵蚀。转子叶片由先进的轻质复合材料制成,然而,它对固体颗粒侵蚀的抵抗力很低。已经开发出涂层并将其用于保护复合材料叶片。但是,由于涂层工艺对复合材料的影响,涂层与复合材料基体之间的相容性以及修复受损涂层的挑战以及新旧涂层之间的不一致,可替换的薄金属屏蔽层是替代方法;钛因其高比强度和更好的可成型性而成为理想的选择。这项工作研究了碳纤维环氧复合材料和钛的固体颗粒腐蚀行为,以评估钛作为防腐蚀屏蔽材料的可行性。实验结果表明,碳纤维环氧复合材料表现出脆性的腐蚀行为,而钛表现出韧性的腐蚀模式。撞击角为15度时,复合材料的腐蚀速率是钛的1.5倍,撞击角为90度时,腐蚀速率增加至5倍。

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