冷却速率对Ti55531钛合金组织和性能的影响
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1.江西景航航空锻铸有限公司;2.中国航发北京航空材料研究院 先进钛合金航空科技重点实验室

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TG146.2

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Effect of cooling rate on microstructure and properties of Ti55531 titanium alloy
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1.Jiangxi Jinghang Aviation Forging Casting Co,Ltd;2.Key Laboratory of Advanced Titanium Alloys,AECC Beijing Institute of Aeronautical Materials

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    摘要:

    研究了β退火冷却时冷却速率对Ti55531钛合金显微组织、室温拉伸性能、断裂韧度和冲击功的影响。结果表明, Ti55531钛合金以不同的冷却速率炉冷后,显微组织均由平直晶界α相(αGB)、残余β相以及其上分布的尺寸不一的晶内片层状α相(αWM)组成,随着冷却速率的提高,晶内片层状α相的厚度则逐渐减小,晶界α相的变化不是很明显;Ti55531钛合金β退火冷却时析出的片层状α相厚度与其力学性能有着直接的关系,随着片层状α相厚度的减小,其抗拉强度和屈服强度逐渐增加,延伸率和断面收缩率逐渐减小,断裂韧度和冲击功均呈现逐渐减小的趋势。

    Abstract:

    Influences of cooling rate on the microstructures, room temperature tensile properties, fracture toughness and impact properties of Ti55531 titanium alloy during β annealing were analyzed. The result shows that, Ti55531 titanium alloy after furnace cooling with different cooling rates, its microstructures are composed of straight grain boundary α phase (αGB), residual β phase and intragranular lamellar α phase (αWM). As the cooling rate is increased, the thickness of intragranular lamellar α phase decreases gradually, and the change of grain boundary α phase is not obvious. There has a direct relationship between the thickness of lamellar α phase precipitated during β annealing cooling and mechanical properties of Ti55531 titanium alloy. With the decrease of the thickness of lamellar α phase, the tensile strength and yield strength increase gradually, the elongation and reduction of area decrease gradually, and the fracture toughness and impact energy decrease gradually.

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历史
  • 收稿日期:2023-09-19
  • 最后修改日期:2023-09-28
  • 录用日期:2023-10-13
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