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

Translated title of the contribution: Hot extrusion forming numerical simulation and microstructure and properties of Maraging250 steel for aviation shaft forging

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

School of Materials Sience and Engineering

Research output: Contribution to journal › Article › peer-review

1 Scopus citations

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.

Translated title of the contribution	Hot extrusion forming numerical simulation and microstructure and properties of Maraging250 steel for aviation shaft forging
Original language	Chinese (Traditional)
Pages (from-to)	181-187
Number of pages	7
Journal	Cailiao Rechuli Xuebao/Transactions of Materials and Heat Treatment
Volume	42
Issue number	6
DOIs	https://doi.org/10.13289/j.issn.1009-6264.2021-0021
State	Published - 25 Jun 2021

Access to Document

10.13289/j.issn.1009-6264.2021-0021

Cite this

@article{320967049e7748629d04ec33ea888658,

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",

year = "2021",

month = jun,

day = "25",

doi = "10.13289/j.issn.1009-6264.2021-0021",

language = "繁体中文",

volume = "42",

pages = "181--187",

journal = "Cailiao Rechuli Xuebao/Transactions of Materials and Heat Treatment",

issn = "1009-6264",

publisher = "Chinese Mechanical Engineering Society",

number = "6",

}

TY - JOUR

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 - http://www.scopus.com/inward/record.url?scp=85110065641&partnerID=8YFLogxK

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

Abstract

Access to Document

Other files and links

Fingerprint

Cite this