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Influence of Heat Treatment on the Microstructures and Mechanical Properties of K465 Superalloy

机译:热处理对K465高温合金组织和力学性能的影响

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摘要

The microstructures and mechanical properties of superalloy K465 under different heat treatment, including as as-cast, solution treatment and aging, were investigated. The results showed that γ' precipitates in as-cast condition exhibited two kinds of morphologies of fine regular cuboidal shape at dendritic arm and coarse irregular form in interdendritic region. MC carbides decomposed into M_6C carbides partly after 1210℃/4h solution treatment. The high temperature stress-rupture life can be improved obviously with the increasing cooling rate. When cooling rate was lower than 70℃/min, the room temperature tensile elongation increased with cooling rate increasing. When cooling rate was higher than 90℃/min the room temperature tensile elongation decreased with cooling rate increasing. The proper cooling rate of 70℃/min~90℃/min is advantageous for the achievement of excellent comprehensive properties. When aging treatments continued the regularization of γ' resulted in the improvement of stress-rupture life and the reduction of tensile elongation. The mechanical property gap between the solution treatment and aging can be decreased with increasing cooling rate.
机译:研究了高温合金K465在铸态,固溶和时效等不同热处理条件下的组织和力学性能。结果表明,在铸态条件下,γ'析出物呈现出两种形态:树枝状臂的细规则长方体形和树枝状间区域的粗大不规则形。 1210℃/ 4h固溶处理后,MC碳化物部分分解为M_6C碳化物。随着冷却速度的增加,高温应力断裂寿命可以明显提高。当冷却速率低于70℃/ min时,室温拉伸伸长率随冷却速率的增加而增加。当冷却速率高于90℃/ min时,室温拉伸伸长率随冷却速率的增加而降低。 70℃/ min〜90℃/ min的适当冷却速度有利于获得优异的综合性能。当继续进行时效处理时,γ'的正则化导致应力断裂寿命的延长和拉伸伸长率的降低。随着冷却速率的增加,固溶处理和时效之间的机械性能差距可以减小。

著录项

  • 来源
    《Materials science forum》 |2016年第2016期|570-579|共10页
  • 作者单位

    Science and Technology on Advanced High Temperature Structural Materials Laboratory, Beijing Institute of Aeronautical Materials, Beijing 100095 China;

    Science and Technology on Advanced High Temperature Structural Materials Laboratory, Beijing Institute of Aeronautical Materials, Beijing 100095 China;

    Science and Technology on Advanced High Temperature Structural Materials Laboratory, Beijing Institute of Aeronautical Materials, Beijing 100095 China;

    Science and Technology on Advanced High Temperature Structural Materials Laboratory, Beijing Institute of Aeronautical Materials, Beijing 100095 China;

    Science and Technology on Advanced High Temperature Structural Materials Laboratory, Beijing Institute of Aeronautical Materials, Beijing 100095 China;

    Military Deputy of Air Force of the CPLA in Beijing, Beijing 100095 China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    K465 superalloy; Heat treatment; Microstructure; Mechanical property;

    机译:K465高温合金;热处理;微观结构机械性能;

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