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铸造镍基高温合金K417G中高温拉伸断裂机理研究

鲍俊 玄伟东 樊志明 曹后帆 李寒松 王保军 任忠鸣

铸造2024,Vol.73Issue(4):476-480,5.
铸造2024,Vol.73Issue(4):476-480,5.

铸造镍基高温合金K417G中高温拉伸断裂机理研究

Study on Tensile Fracture Mechanism of Cast Nickel-Based Superalloy K417G at Medium-High Temperature

鲍俊 1玄伟东 2樊志明 2曹后帆 2李寒松 1王保军 2任忠鸣2

作者信息

  • 1. 中国航发商用航空发动机有限责任公司,上海 200241
  • 2. 上海大学省部共建高品质特殊钢冶金与制备国家重点实验室,上海 200444
  • 折叠

摘要

Abstract

The fracture mechanism of the K417G high-temperature alloy under tensile conditions at 700℃and 950℃after hot isostatic pressing heat treatment was studied.Tensile tests at elevated temperatures were conducted using a universal testing machine,and observations of microstructures,fracture surfaces,and longitudinal sections were carried out through scanning electron microscopy.The results reveal that the dendritic morphology of the samples after heat treatment is pronounced,with a high degree of cuboidal γ'phase on the dendrite branches,measuring 0.4-0.5 μm and arranged in an orderly fashion.Petal-shaped γ'phase with sizes ranging from 1.5-2.6 μm precipitates between the dendrites.Comparing the tensile properties of samples at 950℃to those at 700℃,the tensile strength decreases by 46.3%,while the elongation increases by 200%.This indicates a reduction in high-temperature tensile strength and an increase in plasticity.During moderate-temperature tensile testing,elongated carbides between the dendrites serve as the primary crack initiation and propagation paths.In contrast,during high-temperature tensile testing,carbides at grain boundaries and eutectic constituents act as crack initiation sources,with cracks propagating along grain boundaries,forming a transgranular fracture morphology.

关键词

高温合金/K417G/热等静压热处理/高温拉伸/断裂机理

Key words

superalloy/K417G/hot isostatic pressing heat treatment/high-temperature tensile/fracture mechanism

分类

矿业与冶金

引用本文复制引用

鲍俊,玄伟东,樊志明,曹后帆,李寒松,王保军,任忠鸣..铸造镍基高温合金K417G中高温拉伸断裂机理研究[J].铸造,2024,73(4):476-480,5.

基金项目

国家自然科学基金(52274386,92060104) (52274386,92060104)

上海市经信委工业强基项目(GYQJ-2022-2-02) (GYQJ-2022-2-02)

航空科学基金重点项目(2022Z0470S6001) (2022Z0470S6001)

上海市商用飞机发动机联合创新项目(No.AR966). (No.AR966)

铸造

OACSTPCD

1001-4977

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