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Microstructures Evolution of a Ni-Base Superalloy After Long-Term Aging at 750 °C

机译:750°C长期时效后的镍基高温合金的组织演变

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The microstructures evolution of a new type Ni-base superalloy used as a component of gas turbine engine has been investigated after long-term aging at 750°C for 2000h. The results indicate that TCP, a harmful phase greatly affects the mechanical properties of the alloy, is un-precipitated in the aging process. γ' phase is precipitated in two kinds of sizes during long-term aging. The shape of larger one is transit from spherical to cubic with prolonging of aging time. The M23C6carbide formed mainly by Cr, and other elements such as Al, Ti, Co and Mo is also precipitated in both γ matrix and grain boundaries, and the quantities of the carbide increase gradually with the increasing of aging time.
机译:在750°C长期老化2000h后,研究了用作燃气涡轮发动机部件的新型Ni基高温合金的组织演变。结果表明,TCP是一种有害相,会严重影响合金的机械性能,在时效过程中未析出。在长期老化过程中,γ'相以两种尺寸析出。较大的一个形状是从球形过渡到立方形,并随着时间的延长而延长。 M23C6碳化物主要由Cr和其他元素(如Al,Ti,Co和Mo)形成,也析出在γ基体和晶界中,并且碳化物的数量随着时效时间的增加而逐渐增加。

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