首页|Inconel 617合金热变形过程中几何必须位错的演变

Inconel 617合金热变形过程中几何必须位错的演变

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利用热模拟试验机对Inconel 617合金在温度1000~1200℃,应变速率0.001~1 s-1范围内进行热压缩试验.采用电子背散射衍射和透射电子显微镜技术研究了其热压缩过程中的微观组织演变和几何必须位错(GND)特征.结果表明,随着温度的升高和应变速率的降低,再结晶程度增大,GND密度降低,并且明显的绝热升温效应加速了再结晶的形核和长大.Inconel 617合金热变形过程中大量的位错墙相互缠结,GND首先在大角度晶界处塞积,然后形成亚晶界,最终演变为再结晶晶粒.
Evolution of Geometrically Necessary Dislocations in Inconel 617 Alloy during Hot Deformation
The hot compression test of Inconel 617 alloy was carried out at 1000 ℃-1200 ℃ and the strain rate of 0.001 s-1-1 s-1 by the thermal simulation testing machine.Electron backscatter diffraction and transmission electron microscopy techniques were used to investigate the microstructure evolution and the characteristics of geometrically necessary dislocations(GND)during hot compression.The results show that with the increase of temperature and the decrease of strain rate,the degree of recrystallization increases,the density of GND decreases,and the obvious adiabatic heating effect accelerates the nucleation and growth of recrystallization.During the thermal deformation of Inconel 617 alloy,a large number of dislocation walls are entangled with each other.GND first accumulates at the large angle grain boundary,then forms sub-grain boundary,and finally evolves into recrystallized grain.

Inconel 617 alloythermal deformationrecrystallizationgeometrically necessary dislocations(GND)

王炳正、王旭明、陈伟、杨武、汪彦江、贾智

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兰州兰石集团有限公司铸锻分公司,甘肃兰州 730000

兰州理工大学省部共建有色金属先进加工与再利用国家重点实验室,甘肃兰州 730050

Inconel 617合金 热变形 再结晶 几何必须位错(GND)

国家自然科学基金项目甘肃省杰出青年基金项目

5166503218JR3RA134

2024

热加工工艺
中国船舶重工集团公司热加工工艺研究所 中国造船工程学会船舶材料学术委员会

热加工工艺

CSTPCD北大核心
影响因子:0.55
ISSN:1001-3814
年,卷(期):2024.53(18)
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