航空轴锻件用Maraging250钢热挤压成形数值模拟及组织性能

Chun Xu Wang; Li Mei Shang; Shun Han; Yong Li; Dong Liu; Jian Guo Wang; Chao Yang

doi:10.13289/j.issn.1009-6264.2021-0021

航空轴锻件用Maraging250钢热挤压成形数值模拟及组织性能

Chun Xu Wang
, Li Mei Shang
, Shun Han
, Yong Li
, Dong Liu
, Jian Guo Wang
, Chao Yang

材料学院

China Iron and Steel Research Institute Group
Northwestern Polytechnical University Xian
AECC Commercial Aircraft Engine Co., Ltd.

科研成果: 期刊稿件 › 文章 › 同行评审

1 引用（Scopus）

摘要

DEFORM-2D software was used to simulate the hot extrusion process of maraging250 steel for aviation shaft forgings, the distribution of temperature field, equivalent strain field and stress field during the extrusion were analyzed, and microstructure and mechanical properties of the forgings after extrusion were analyzed. The results show that after hot extrusion forming, the temperature of the forgings along the radial direction to the outer surface increases, the equivalent strain of the forgings is 1.0-1.5, and the temperature is between 1135-1174℃, which shows the temperature distribution and strain distribution of the forgings are uniform. The microstructure and mechanical properties of the forgings have good uniformity, and the average grain size is 41.42-61.07 μm.

投稿的翻译标题	Hot extrusion forming numerical simulation and microstructure and properties of Maraging250 steel for aviation shaft forging
源语言	繁体中文
页（从-至）	181-187
页数	7
期刊	Cailiao Rechuli Xuebao/Transactions of Materials and Heat Treatment
卷	42
期	6
DOI	https://doi.org/10.13289/j.issn.1009-6264.2021-0021
出版状态	已出版 - 25 6月 2021

关键词

Equivalent strain
Hot extrusion
Maraging250 steel
Microstructure
Numerical simulation
Temperature

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10.13289/j.issn.1009-6264.2021-0021

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引用此

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title = "航空轴锻件用Maraging250钢热挤压成形数值模拟及组织性能",

abstract = "DEFORM-2D software was used to simulate the hot extrusion process of maraging250 steel for aviation shaft forgings, the distribution of temperature field, equivalent strain field and stress field during the extrusion were analyzed, and microstructure and mechanical properties of the forgings after extrusion were analyzed. The results show that after hot extrusion forming, the temperature of the forgings along the radial direction to the outer surface increases, the equivalent strain of the forgings is 1.0-1.5, and the temperature is between 1135-1174℃, which shows the temperature distribution and strain distribution of the forgings are uniform. The microstructure and mechanical properties of the forgings have good uniformity, and the average grain size is 41.42-61.07 μm.",

keywords = "Equivalent strain, Hot extrusion, Maraging250 steel, Microstructure, Numerical simulation, Temperature",

author = "Wang, \{Chun Xu\} and Shang, \{Li Mei\} and Shun Han and Yong Li and Dong Liu and Wang, \{Jian Guo\} and Chao Yang",

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T1 - 航空轴锻件用Maraging250钢热挤压成形数值模拟及组织性能

AU - Wang, Chun Xu

AU - Shang, Li Mei

AU - Han, Shun

AU - Li, Yong

AU - Liu, Dong

AU - Wang, Jian Guo

AU - Yang, Chao

PY - 2021/6/25

Y1 - 2021/6/25

N2 - DEFORM-2D software was used to simulate the hot extrusion process of maraging250 steel for aviation shaft forgings, the distribution of temperature field, equivalent strain field and stress field during the extrusion were analyzed, and microstructure and mechanical properties of the forgings after extrusion were analyzed. The results show that after hot extrusion forming, the temperature of the forgings along the radial direction to the outer surface increases, the equivalent strain of the forgings is 1.0-1.5, and the temperature is between 1135-1174℃, which shows the temperature distribution and strain distribution of the forgings are uniform. The microstructure and mechanical properties of the forgings have good uniformity, and the average grain size is 41.42-61.07 μm.

AB - DEFORM-2D software was used to simulate the hot extrusion process of maraging250 steel for aviation shaft forgings, the distribution of temperature field, equivalent strain field and stress field during the extrusion were analyzed, and microstructure and mechanical properties of the forgings after extrusion were analyzed. The results show that after hot extrusion forming, the temperature of the forgings along the radial direction to the outer surface increases, the equivalent strain of the forgings is 1.0-1.5, and the temperature is between 1135-1174℃, which shows the temperature distribution and strain distribution of the forgings are uniform. The microstructure and mechanical properties of the forgings have good uniformity, and the average grain size is 41.42-61.07 μm.

KW - Equivalent strain

KW - Hot extrusion

KW - Maraging250 steel

KW - Microstructure

KW - Numerical simulation

KW - Temperature

UR - https://www.scopus.com/pages/publications/85110065641

U2 - 10.13289/j.issn.1009-6264.2021-0021

DO - 10.13289/j.issn.1009-6264.2021-0021

M3 - 文章

AN - SCOPUS:85110065641

SN - 1009-6264

VL - 42

SP - 181

EP - 187

JO - Cailiao Rechuli Xuebao/Transactions of Materials and Heat Treatment

JF - Cailiao Rechuli Xuebao/Transactions of Materials and Heat Treatment

IS - 6

ER -

航空轴锻件用Maraging250钢热挤压成形数值模拟及组织性能

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