激光粉末床熔融成形TA15合金薄壁结构拉伸性能研究OA
Study on Tensile Properties of TA15 Alloy Thin-walled Structure Fabricated by Laser Powder Bed Fusion
激光粉末床熔融(LPBF)技术在制造复杂薄壁部件方面具有显著优势,在航空航天和生物医疗等领域具有广阔应用前景.本文通过LPBF技术打印了 1~4mm厚TA15合金薄壁结构,综合评估了厚度对显微组织、室温及高温(500 ℃)拉伸性能的影响.结果表明,随着厚度的增加,合金初生β晶粒尺寸降低,α板条宽度略有增加;不同厚度薄壁试样的室温及高温抗拉强度(UTS)和屈服强度(YS)基本相当,但几何尺度和β晶粒尺寸的影响使得合金的总伸长率随厚度增加显著提升,4 mm厚试样的伸长率比1 mm厚试样高出28.5%(室温)和162%(500 ℃);随薄壁试样厚度减小,断口韧窝数量减少,解理平面面积增加,断裂机制从正断向剪切型断裂转变;同时,高温下合金的应变硬化率高于室温,这主要归因于高温下合金基面和锥面滑移的临界分切应力降低促进位错缠结,进而提升应变硬化能力.本文揭示了薄壁结构的微观组织及拉伸性能随厚度演变的规律,为航空航天领域高性能薄壁构件的设计与制造提供了理论支持和技术指导.
Laser powder bed melting(LPBF)technology offers significant advantages in manufacturing complex thin-walled components and has broad application prospects in fields such as aerospace and biomedicine.In this study,TA15 alloy thin-walled structures with thicknesses ranging from 1 mm to 4 mm were fabricated using LPBF technology.The effects of building thickness on the microstructure,as well as the room-temperature and high-temperature(500 ℃)tensile properties were comprehensively evaluated.The results indicate that as the building thickness increases,the grain size of the primary β phase decreases,while the width of the α laths slightly increases.The ultimate tensile strength(UTS)and yield strength(YS)of thin-walled samples with different thicknesses show minimal differences at both room temperature and high temperature.However,the influence of geometric scale and βgrain size leads to a significant improvement in the total elongation with increasing thickness.Specifically,the elongation of the 4 mm thick specimen is 28.5%(room temperature)and 162%(500 ℃)higher than that of the 1 mm-thick sample.As the thickness of the thin-walled samples decreases,the number of dimples on the fracture surface reduces,while the area of cleavage planes increases,indicating a transition in the fracture mechanism from normal fracture to shear fracture.Meanwhile,the strain hardening rate of the alloy at high temperatures is higher than that at room temperature.This is mainly attributed to the reduction of the critical resolved shear stress(CRSS)of the basal and pyramidal slip systems at high temperature,which promotes dislocation entanglement and thereby enhances the strain hardening capacity.This paper reveals the evolution law of the microstructure and tensile properties of thin-walled structures with thickness,providing theoretical support and technical guidance for the design and manufacture of high-performance thin-walled components in the aerospace field.
王海韬;王源晨;陈玮;万宏远;张智博;宋竹满;张广平
中国科学院金属研究所高性能均质合金国家工程研究中心,辽宁沈阳 110016||中国科学技术大学,辽宁沈阳 110016中国科学院金属研究所高性能均质合金国家工程研究中心,辽宁沈阳 110016中国航空制造技术研究院高能束流加工技术重点实验室,北京 100024||中国航空制造技术研究院增材制造航空科技重点实验室,北京 100024中国航空制造技术研究院高能束流加工技术重点实验室,北京 100024||中国航空制造技术研究院增材制造航空科技重点实验室,北京 100024中国航空制造技术研究院高能束流加工技术重点实验室,北京 100024||中国航空制造技术研究院增材制造航空科技重点实验室,北京 100024中国科学院金属研究所高性能均质合金国家工程研究中心,辽宁沈阳 110016中国科学院金属研究所高性能均质合金国家工程研究中心,辽宁沈阳 110016
航空航天
激光粉末床熔融TA15薄壁拉伸性能高温
laser powder bed fusionTA15thin-walltensile propertieshigh temperature
《航空科学技术》 2026 (5)
23-35,13
航空科学基金(20230042092003)国家重点研发计划(2022YFB4601000) Aeronautical Science Foundation of China(20230042092003)National Key R&D Program of China(2022YFB4601000)
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