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镍基高温合金的热机械疲劳寿命预测模型研究

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针对发动机热端部件常用材料镍基高温合金GH4169进行了 200~450 ℃及400~650 ℃条件下的同相位热机械疲劳(TMF)试验,考虑TMF条件下多晶材料在弹性阶段产生的微观损伤应变能,提出一种适用于多晶材料的TMF寿命预测模型,并结合试验数据确定模型参数;采用GH4169、IN718、DD8三种高温合金对该模型的TMF寿命预测能力进行评估,结果表明,提出的寿命模型预测精度高于TMF寿命预测常用的Manson-Coffin模型和Ostergren模型.
Research on Thermo-mechanical Fatigue Life Prediction Model of Ni-base Superalloy
In phase TMF tests on nickel-based high-temperature alloy GH4169,a commonly used material for engine hot end components,under conditions of 200-450 ℃ and 400-650 ℃ is conduc-ted.Considering the micro damage strain energy of polycrystalline materials in the elastic stages under the condition of TMF,a TMF life prediction model suitable for polycrystalline materials was pro-posed,model parameters were determined by combining the TMF test data.Three superalloys,GH4169,IN718,DD8,were used to evaluate the TMF life prediction ability of this model.The pre-diction accuracy of the life model is higher than that of the Manson-Coffin model and Ostergen model commonly used for TMF life prediction.

nickel-base superalloythermo-mechanical fatigue(TMF)dmamage strain energylife prediction

崔海涛、钱春华

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南京航空航天大学能源与动力学院,南京,210016

镍基高温合金 热机械疲劳(TMF) 损伤应变能 寿命预测

国家自然科学基金

91860111

2024

中国机械工程
中国机械工程学会

中国机械工程

CSTPCD北大核心
影响因子:0.678
ISSN:1004-132X
年,卷(期):2024.35(1)
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