整体高温辅助激光定向能量沉积TiAl4822合金开裂抑制机理及组织性能研究OA
Suppression of cracking and microstructure-property investigation of TiAl4822 alloy by laser directed energy deposition with integral high-temperature assistance
激光定向能量沉积(laser directed energy deposition,LDED)凭借高效率与工艺柔性,正成为解决室温高脆性和高活性的TiAl4822(Ti-48Al-2Cr-2Nb)合金传统工艺难加工、难制备大型复杂构件问题的关键途径,以充分发挥其航空发动机等高温轻质部件的理想材料潜力.然而,LDED过程中快速熔融-凝固循环会产生极大的温度梯度和残余应力,从而导致构件开裂,但目前尚无成熟手段能够完全抑制裂纹产生.本工作利用整体高温辅助LDED制备出 30 mm×25 mm×6 mm致密无裂纹的TiAl4822合金薄壁构件,并对其宏观形貌、微观组织、孔隙率及显微硬度进行研究.研究结果表明:在常温条件下,LDED制备的TiAl4822合金薄壁样件易发生以解理为主的脆性断裂,显微组织以细小等轴晶为主;引入 800℃整体高温辅助后,沉积层晶粒定向生长为自下而上倾斜的柱状晶,孔隙率从 0.05%降至 0.008%,孔径分布更均匀,表面未见宏观裂纹;与此同时,显微硬度由常温样件的 390.46HV0.2 降至354.94HV0.2,这主要归因于在高温辅助条件下晶粒长大、晶界减少及析出相中γ相的含量相对增加.因此,整体高温辅助不仅有效抑制裂纹与大尺寸孔隙的产生,还优化微观组织均匀性,为TiAl4822合金的高致密、高性能制备提供新途径.
The TiAl4822(Ti-48Al-2Cr-2Nb)alloy,renowned for its exceptional high-temperature mechanical properties and low density,stands out as a highly promising candidate for critical aerospace components.However,its high chemical reactivity and inherent room-temperature brittleness pose significant challenges to the conventional manufacturing of large and complex geometries.Laser directed energy deposition(LDED),characterized by its high fabrication efficiency and remarkable process flexibility,has emerged as a crucial approach for preparing TiAl4822 alloy components.Nevertheless,the rapid melting-solidification cycle during LDED induces a substantial temperature gradient and residual stress,which results in component cracking.Currently,there is no well-established method to completely prevent crack formation.In this study,a dense and crack-free thin-walled TiAl4822 alloy component with dimensions of 30 mm×25 mm×6 mm is successfully fabricated using the whole high-temperature-assisted LDED technique.An investigation is conducted on their macro-morphology,microstructure,porosity,and microhardness.The results reveal that the thin-walled TiAl4822 alloy specimen prepared by LDED at room temperature is prone to brittle fracture primarily through cleavage,and its microstructure mainly comprises fine equiaxed grains.After implementing whole high-temperature assistance at an integral temperature of 800℃,the grains in the deposited layer transform from bottom to top into inclined columnar grains.The porosity is significantly reduced from 0.05%to 0.008%,accompanied by a more uniform pore-size distribution,and no macroscopic cracks are observed on the surface.Concurrently,the microhardness decreases from 390.46HV0.2 to 354.94HV0.2,which can be attributed to grain coarsening,a decrease in grain-boundary density,and precipitate evolution under high-temperature conditions.Overall,the integral high-temperature-assisted LDED effectively inhibits crack initiation and the formation of large pores while homogenizing the microstructure,providing a novel pathway for high-density,high-performance TiAl4822 preparing.
牛方勇;祝明春;成浩然;于学鑫;高佳丽
大连理工大学 高性能精密制造全国重点实验室,辽宁 大连 116024||精密/特种加工及微制造技术教育部重点实验室(B类),辽宁 大连 116024大连理工大学 高性能精密制造全国重点实验室,辽宁 大连 116024||精密/特种加工及微制造技术教育部重点实验室(B类),辽宁 大连 116024大连理工大学 高性能精密制造全国重点实验室,辽宁 大连 116024||精密/特种加工及微制造技术教育部重点实验室(B类),辽宁 大连 116024大连理工大学 高性能精密制造全国重点实验室,辽宁 大连 116024||精密/特种加工及微制造技术教育部重点实验室(B类),辽宁 大连 116024上海理工大学 机械工程学院,上海 200093
航空航天
激光定向能量沉积TiAl4822合金裂纹显微组织显微硬度
laser directed energy depositionTiAl4822 alloycrackmicrostructuremicrohardness
《航空材料学报》 2026 (1)
51-59,9
国家自然科学基金项目(52375312)大连理工大学精密/特种加工及微制造技术教育部重点实验室(B类)开放课题基金资助项目(B202305)
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