首页|激光增材制造近β钛合金显微组织与力学性能研究

激光增材制造近β钛合金显微组织与力学性能研究

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研究了激光沉积打印Ti55511钛合金的显微组织和室温拉伸性能,表征了打印态、热处理态Ti55511合金的晶粒形态及晶体学织构,分析了不同退火热处理温度对激光增材制造钛合金强塑性的影响.结果表明,原始打印态Ti55511钛合金由粗大的β晶粒组成,并且β晶粒以柱状晶和等轴晶两种类型的晶粒交替生长,呈现竹节状形态.在打印态Ti55511组织中,β基体析出的α片层提供了大量的界面,有效阻碍了位错运动,使合金具有高强度和低塑性.580 ℃退火热处理后,合金的屈服强度、抗拉强度变化不明显,伸长率有一定的提升.进一步提高退火温度至620 ℃后,合金的屈服强度、抗拉强度降低,但强度值依然大于1 000 MPa,同时伸长率大幅提升.因此,可通过退火热处理调控α晶粒的尺寸和体积分数,以提高合金的强塑性匹配.当应力平行于Z方向时,样品的屈服强度、抗拉强度略低于垂直于Z方向的,而伸长率显著高于应力垂直于Z方向的.
Study on Microstructure and Mechanical Properties of Laser Metal Deposition Near β Titanium Alloy
The microstructure and tensile properties at room temperature of the laser additive manufacturing Ti55511 titanium al-loy are studied,the grain morphologies and crystallographic texture of the as-deposited and heat treated Ti55511 titanium alloy are characterized,and the effects of different annealing temperatures on plasticity of the laser additive manufactured Ti55511 ti-tanium alloy are analyzed.The results indicate that the as-deposited Ti55511 titanium alloy consists of coarse β grains,and theβ grains grow alternately in the form of columnar and equiaxed grains,presenting a bamboo-like morphology.In the as-deposi-ted Ti55511 titanium alloy,the α lamellae precipitated from the β matrix provides a large number of interfaces,effectively hin-dering the movement of dislocations,and allows the alloy having high strength and low plasticity.The yield strength and tensile strength of the alloy annealed at 580 ℃ does not show significant changes,and the elongation increases to a certain extent.When the annealing temperature increases to 620℃,the yield strength and tensile strength of the alloy reduce,still greater than 1 000 MPa,and the elongation significantly increases.Therefore,the size and volume fraction of the α grains can be regu-lated through the annealing heat treatment to improve the strength and toughness balance of the alloy.When the stress is parallel to the Z deposition direction,the yield strength and tensile strength of the specimen are slightly lower than those of the specimen whose stress is perpendicular to the Z deposition direction,and the elongation is significantly higher than that of the specimen whose stress is perpendicular to the Z deposition direction.

Ti55511 titanium alloyadditive manufacturingmicrostructuremechanical property

李海涛、齐敏、陈冬梅、黄森森、王倩、马英杰、雷家峰

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中航工业沈阳飞机设计研究所,辽宁沈阳 110035

中国科学院金属研究所,辽宁沈阳 110016

Ti55511钛合金 增材制造 显微组织 力学性能

国家重点研发计划

2021YFC2801801

2024

材料开发与应用
洛阳船舶材料研究所 中国造船工程学会船舶材料学术委员会

材料开发与应用

CSTPCD
影响因子:0.342
ISSN:1003-1545
年,卷(期):2024.39(1)
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