首页|期刊导航|航空科学技术|时效处理对保留有Laves相的激光立体成形GH4169合金强化相析出与力学性能的影响

时效处理对保留有Laves相的激光立体成形GH4169合金强化相析出与力学性能的影响OA

Effect of Aging Treatment on the Precipitation Behavior of Strengthening Phase and Mechanical Properties of Laser Solid Formed GH4169 Alloy with Reserved Laves Phase

中文摘要英文摘要

颗粒状Laves相对激光立体成形GH4169合金的力学性能有利.然而,Laves相的保留会占据部分GH4169合金的主要强化元素Nb,影响到后续时效过程中γ"相的析出和长大.目前,尚未有研究针对含有颗粒状Laves相的激光立体成形GH4169合金组织的时效处理工艺开展优化研究.本文采用了两种不同的短时固溶热处理工艺以获得具有不同特征参数的Laves相,并围绕这两种固溶热处理组织开展了时效工艺优化的探索研究.研究结果表明,固溶温度对晶粒和Laves相的演变有显著影响.在1020 ℃下保温30 min,粗大的柱状晶粒和大尺寸长条状Laves相颗粒仍旧存在于组织中.当固溶温度提高到1050 ℃时,保温30 min后的组织中便以等轴晶和颗粒状Laves相为主要特征.然而,Laves相的变化并未对γ"相的析出和长大产生明显影响,这两种固溶热处理态组织中的γ"相具有相似的粗化速率.室温拉伸性能测试结果表明,含有Laves相的激光立体成形GH4169合金组织的最佳时效处理工艺仍是720 ℃保温8h,以50 ℃/h炉冷至620 ℃,再保温8 h,最后空冷.此时合金的屈服强度、抗拉强度和延伸率分别为1067.0 MPa±18.2 MPa,1240.3 MPa±21.0 MPa和11.4%±0.6%.颗粒状Laves相的脱黏是试样断裂的主要原因.进一步测试了优化后组织在650 ℃不同应力条件下的高温蠕变性能.随着外加应力的升高,合金的蠕变寿命逐渐降低.高温蠕变过程中激光立体成形GH4169合金组织发生了动态再结晶和晶粒长大现象,这两个过程均受外加应力的影响,较低的外加应力水平会带来较高的蠕变寿命,从而使得更多的再结晶晶粒生成,并有更多的时间长大.试样在不同条件下的蠕变断裂机制均是沿晶断裂.研究成果加深了对含颗粒状Laves相激光立体成形GH4169合金的组织调控和蠕变行为的理解和认识,有助于促进激光立体成形技术在航空发动机关键材料成形中的应用.

Granular Laves phase is beneficial for the mechanical properties of laser solid formed GH4169 superalloy.Nevertheless,the retention of Laves phase occupies a portion of the principal strengthening element Nb,influencing the precipitation and growth of γ"strengthening phase during subsequent aging process.Up to now,no research has been conducted to optimize the aging treatment process for the LSF GH4169 microstructure with reserved granular Laves phases.In this paper,two distinct short-time solution heat treatment processes were employed to obtain Laves phases with diverse characteristics,and an exploratory research on the optimization of aging process was carried out.The results indicated that the solution heat treatment temperature had a significant influence on the evolution of the grain and the Laves phase.After holding at 1020 ℃ for 30 min,coarse columnar grains and large-sized and irregular Laves phase particles still persisted in the microstructure.When the solution heat treatment temperature was elevated to 1050 ℃ and held for 30 min,the microstructure was mainly characterized by equiaxed grains and granular Laves phases.However,the variation of the Laves phase did not have a pronounced effect on the precipitation and growth of the γ"phase,and the γ"phases in the two solution heat treated microstructures had a similar coarsening rate.The room temperature tensile result demonstrated that the optimal aging treatment process for the LSF GH4169 microstructure with reserved Laves phase remained as follows:holding at 720 ℃ for 8 h,furnace cooling at 50 ℃/h to 620 ℃,holding for 8 hours,and finally air cooling.At this point,the yield strength,tensile strength,and elongation of the alloy were 1067.0 MPa±18.2 MPa,1240.3 MPa±21.0 MPa,and 11.4%±0.6%,respectively.The debonding of the granular Laves phase was the primary cause of the sample fracture.The high-temperature creep properties of the optimized microstructure under different stress conditions at 650 ℃ were further tested.With the increase in the applied stress,the creep life of the alloy gradually decreases.During the high-temperature creep process,dynamic recrystallization and grain growth phenomena occurred in the LSF GH4169 microstructure,and both processes were affected by the applied stress.A lower applied stress level resulted in a higher creep life,enabling the generation of more recrystallized grains and allowing for more time for growth.The creep fracture mechanism of the samples under different conditions was intergranular fracture.The findings deepen the understanding of the microstructure evolutions and creep behaviors of laser solid formed GH4169 alloy with granular Laves particles,which is conducive to promoting the application of additive manufacturing in the formation of key structural parts for aero engines.

祁嘉伟;隋尚;徐春杰;齐郁馨;王一丰;张忠明

西安理工大学,陕西西安 710048西安理工大学,陕西西安 710048西安理工大学,陕西西安 710048西安理工大学,陕西西安 710048西安理工大学,陕西西安 710048西安理工大学,陕西西安 710048

航空航天

激光立体成形GH4169合金时效处理Laves相力学性能

laser solid formingGH4169 alloyaging treatmentLaves phasemechanical properties

《航空科学技术》 2026 (4)

11-23,13

国家自然科学基金(52305419)航空科学基金(2022Z0490T6001)陕西省秦创原高层次创新创业人才项目(QCYRCXM-2022-323) National Natural Science Foundation of China(52305419)Aeronautical Science Foundation of China(2022Z0490T6001)Qin Chuangyuan High-Level Innovation and Entrepreneurship Talent Project(QCYRCXM-2022-323)

10.19452/j.issn1007-5453.2026.04.002

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