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首页> 外文期刊>Journal of Alloys and Compounds: An Interdisciplinary Journal of Materials Science and Solid-state Chemistry and Physics >Influence of type and morphology of carbides on stress-rupture behavior of a cast cobalt-base superalloy
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Influence of type and morphology of carbides on stress-rupture behavior of a cast cobalt-base superalloy

机译:碳化物类型和形态对铸钴基超合金的应力破裂行为的影响

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AbstractThe relationships between the type and morphology of carbides and stress-rupture property have been studied in a cast cobalt-base superalloy. Different types and morphologies of carbides are achieved by varying the heat treatment conditions. After heat treatment at 1240?°C/4?h, the primary M7C3decomposes into M23C6, and the formed M23C6and primary MC partially dissolve into the matrix. After heat treatment at 1280?°C/4?h, the primary M7C3melts, resulting in the formation of a highly developed lamellar structure of M23C6, and the primary MC mostly dissolves into the matrix. The heat treatment at 1100?°C/300?h gives rise to the carbide transformation of M7C3→ M23C6and a profusion of secondary M23C6carbide around M23C6and MC. The samples in stress-rupture test at 980?°C for 83?MPa manifest the following rupture life: 1280?°C sample > 1240?°C sample?>?as-cast sample > 1100?°C sample. The longer rupture life of the samples of 1240?°C and 1280?°C is derived from the stable microstructure, dispersed MC carbide morphology and the supersaturated matrix. The shortest rupture life of the 1100?°C sample is mainly attributed to the overaging. Additionally, the carbide transformations of M7C3→ M23C6, MC → M23C6, M23C6→ M6C take place in the as-cast sample during creep exposure.Graphical abstractDisplay OmittedHighlights?The rupture life is following: 1280?°C sample > 1240?°C sample?>?as-cast sample > 1100?°C sample.?The stable microstructure, dispersed MC carbide morphology and the supersaturated matrix are beneficial to rupture life.?The carbide transformations of M7C3→ M23C6, MC → M23C6, M23C6→ M6C occur in as-cast alloy during stress-rupture.
机译:<![CDATA [ 抽象 在铸造钴基础中研究了碳化物和碳化物类型和形态之间的关系与压力破裂性能之间的关系超合金。通过改变热处理条件来实现碳化物的不同类型和形态。在1240℃/ 4℃下热处理后,主要M 7 C 3 分解为M 23 C 6 ,以及形成的M 23 C 6 和主MC部分溶解到矩阵中。在1280℃/ 4℃下热处理后,主要M 7 C 3 熔体,导致以M 23 C 6 ,主MC主要溶解到基质中。 1100?°C / 300?H的热处理引发了M 7 C 3 < / ce:inf>→m 23 c 6 和次级m 23 C 6 碳化物在m 23 C 6 和MC。 ?在980℃下83兆帕的应力 - 断裂试验°的样品清单以下断裂寿命:1280℃样品> 1240℃的样品>铸态样品> 1100℃样品????。的1240样品℃,1280较长断裂寿命?℃下从稳定微结构衍生的,分散的MC碳化物的形态和过饱和基质。 1100?°C样本的最短破裂寿命主要归因于过度融合。此外,M的碳化物转变 7 C 3 →M 23 C 6 ,MC→M 23 C 6 ,M 23 C 6 < / CE:INF>→M 6 C在蠕变曝光期间在AS-CAST样品中进行。 图形抽象 显示中省略 亮点 破裂寿命如下:1280?°C样本> 1240℃的样品>铸态样品> 1100℃样品 稳定的微观结构,分散的mc碳化物形态和超饱和基质有利于破裂的寿命。 碳化物M的变换< CE:INF LOC =“POST”> 7 C 3 →M 23 C 6 ,MC→M 23 C 6 中,M 23 C 6 →M < CE:INF LOC =“POST”> 6 C在压力破裂期间在铸造合金中发生。

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