Thermal deformation mechanism of TC11/TC17 linear friction welded joint during isothermal compression

2021 ◽  
pp. 111319
Author(s):  
P.K. Zhao ◽  
C. Wei ◽  
X.D. Xiao ◽  
Q.L. Chu ◽  
J.P. Niu ◽  
...  
2015 ◽  
Vol 8 (6) ◽  
pp. 30-32
Author(s):  
S. K. Kiseleva ◽  
◽  
A. Y. Medvedev ◽  
V. M. Bychkov ◽  
B. O. Bolshakov ◽  
...  

2015 ◽  
Vol 2015.23 (0) ◽  
pp. 109-110
Author(s):  
Yu HARUBEPPU ◽  
Hisashi TANIE ◽  
Koji SASAKI ◽  
Nobuhiko CHIWATA ◽  
Hiroyuki TESHIMA

2019 ◽  
Vol 6 (8) ◽  
pp. 0865i5
Author(s):  
Jingbo Wang ◽  
Qiuping Wang ◽  
Lu Li ◽  
Rongfeng Zhou ◽  
Yongkun Li ◽  
...  

2021 ◽  
Vol 19 (1) ◽  
pp. 091
Author(s):  
Vladimir A. Skripnyak ◽  
Kristina Iokhim ◽  
Evgeniya Skripnyak ◽  
Vladimir V. Skripnyak

The article presents the results of the analysis of the plastic flow of titanium alloys in the process of the Linear Friction Welding (LFW). LFW is a high-tech process for joining critical structural elements of aerospace engineering from light and high-temperature alloys. Experimental studies of LFW modes of such alloys are expensive and technically difficult. Numerical simulation was carried out for understanding the physics of the LFW process and the formation laws of a strong welded joint of titanium alloys. Simulation by the SPH method was performed using the LS DYNA software package (ANSYS WB 15.2) and the developed module for the constitutive equation. The new coupled thermomechanical 3D model of LFW process for joining structural elements from alpha and alpha + beta titanium alloys was proposed. It was shown that the formation of a welded joint occurs in a complex and unsteady stress-strain state. In the near-surface layers of the bodies being welded, titanium alloys can be deformed in the mode of severe plastic deformation. A deviation of the symmetry plane of the plastic deformation zone from the initial position of the contact plane of the bodies being welded occurs during a process of LFW. Extrusion of material from the welded joint zone in the transverse direction with respect to the movement of bodies is caused by a pressure gradient and a decrease in the alloy flow stress due to heating. The hcp-bcc phase transition of titanium alloys upon heating in the LFW process necessitates an increase in the cyclic loading time to obtain a welded joint.


2010 ◽  
Vol 97-101 ◽  
pp. 3895-3898 ◽  
Author(s):  
Li Jun Tan ◽  
Ze Kun Yao ◽  
Chun Qin ◽  
Hong Zhen Guo ◽  
Shi Qiong Li

Dissimilar joining of Ti-22Al-25Nb alloy and an α+β titanium alloy TC11 were carried out using electron beam process and linear friction process, respectively. The microstructure and tensile properties of the joints were investigated. The results show that both EBW and LFW could be adopted to the dissimilar joining of Ti-22Al-25Nb/TC11. The EB welded joint exhibits higher strength than that of the LF welded joint, due to the precipitation of O phase in the fusion zone of the former one. These results can be expected to be of great technical interest as basic data for the use of EBW or LFW in aerospace industry.


Materials ◽  
2021 ◽  
Vol 14 (1) ◽  
pp. 194
Author(s):  
Yongfei Wang ◽  
Shengdun Zhao ◽  
Yi Guo ◽  
Kuanxin Liu ◽  
Shunqi Zheng

Al-Mg-Si based alloys are popular alloys used in the automotive industry. However, limited studies have been performed to investigate the microstructure, deformation characteristics, and deformation mechanism for the semi-solid 6063 alloys. In this study, the cold radial forging method and semi-solid isothermal treatment (SSIT) are proposed in the semi-solid isothermal compression (SSIC) process to fabricate high-quality semi-solid 6063 billets. The effects of deformation temperature, strain rate, and strain on the microstructure, deformation characteristics, and deformation mechanism of the SSIC of cold radial forged 6063 alloys were investigated experimentally. Constitutive equations were established based on the measured data in experiments to predict the flow stress. Results show that an average grain size in the range from 59.22 to 73.02 μm and an average shape factor in the range from 071 to 078 can be obtained in the microstructure after the cold radial forged 6063 alloys were treated with SSIT process. Four stages (i.e., sharp increase, decrease, steady state, and slow increase) were observed in the true stress- true strain curve. The correlation coefficient of the constitutive equation was obtained as 0.9796 while the average relative error was 5.01%. The deformation mechanism for SSIC of cold radial forged aluminum alloy 6063 mainly included four modes: The liquid phase flow, grain slide or grain rotation along with the liquid film, slide among solid grains, and the plastic deformation of solid grains.


2014 ◽  
Vol 4 (3) ◽  
pp. 186-189
Author(s):  
S. K. Kiseleva ◽  
Vas. V. Astanin ◽  
L. Y. Gareeva ◽  
M. V. Karavaeva ◽  
V. M. Bychkov ◽  
...  

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