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(P10-P0123)Study on mechanical properties and microstructure of HfMoNbTaTi refractory high-entropy alloy

机译:(P10-P0123)HFMONBTATI耐火材料高熵合金的力学性能和微观结构的研究

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Efficiency improving and emission reducing in turbine engines has become astrong driving force in aerospace industry. One of a feasible way is to elevate their operationtemperature. Although gas turbine engines are usually made of nickel-based alloys, it stillshows a limitation at a higher working temperature due to their melting point (1455 °C forpure nickel). Refractory high-entropy alloys (RHEAs), which generally consist of high meltingpoint elements, have attracted much attention in this field on account of its excellentperformance at elevated temperature. In this study, a new equimolar RHEA of HfMoNbTaTi withboth high melting point and high mechanical properties is fabricated and investigated.
机译:涡轮发动机的效率改善和排放减少,成为航空航天工业的Astrong推动力。一种可行的方式是提升他们的操作。虽然燃气轮机发动机通常由镍基合金制成,但是由于它们的熔点(1455°C注入镍),它仍然显示在更高的工作温度下的限制。通常由高熔点元素组成的耐火高熵合金(RHEAS),由于其在升高温度下的优异性,因此在该领域引起了很多关注。在该研究中,制造并研究了高熔点和高机械性能的HFMONBTATI的新Equmolar rhea。

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