Numerical Simulation on Residual Stress of SiC Fiber Reinforced Titanium Matrix Composite

doi:10.11901/1005.3093.2015.312

Chinese Journal of Materials Research

2016, Vol. 30

Issue (5): 355-364 DOI: 10.11901/1005.3093.2015.312

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Numerical Simulation on Residual Stress of SiC Fiber Reinforced Titanium Matrix Composite

ZHANG Zhichao¹, WANG Yumin^2,^*(

), LI Yufang¹, BAI Chunguang²

1.College of Material Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
2. Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China

Cite this article:

ZHANG Zhichao, WANG Yumin, LI Yufang, BAI Chunguang. Numerical Simulation on Residual Stress of SiC Fiber Reinforced Titanium Matrix Composite. Chinese Journal of Materials Research, 2016, 30(5): 355-364.

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Abstract

FEM calculation for the preparation process of SiC fiber and SiC/Ti-6Al-4V composite was carried out to investigate the effect of different processing parameters on the residual stress of the SiC fiber as well as the densification behavior and residual stress of the composite. The results show that, for the fabrication process of fibers, the axial thermal stress of the WC layer decreases with the decrease of deposition temperature and thickness of C layer. For the densification of composites, HIP temperature and sheath thickness have greater impact on the density, but HIP time and fiber volume fraction have smaller impact; with the increasing HIP temperature and decreasing sheath thickness, the density of the composite could be enhanced; the radial residual stress on the matrix greatly increases with the increase of HIP temperature and fiber volume fraction and decrease of sheath thickness appropriately; the hoop residual stress on the matrix greatly decreases with the increase of HIP temperature and sheath thickness, while decrease of HIP time appropriately. Finally the following processing parameters were recommended for preparation of SiC/Ti-6Al-4V composite with good quality: HIP temperature 950-960℃, HIP time 9 h and sheath thickness 70-80 mm and fiber volume fraction 45%-50%. FEM calculation results show some differences with those measured in the experiment for the residual stress of the composite, but with similar variation tendency.

Key words: titanium matrix composite SiC fiber densification residual stress finite element simulation

Received: 28 May 2015

ZTFLH:

TB331

About author: *To whom correspondence should be addressed, Tel: (024)23971962, E-mail: yuminwang@imr.ac.cn

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	Zhichao ZHANG
	Yumin WANG
	Yufang LI
	Chunguang BAI

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https://www.cjmr.org/EN/10.11901/1005.3093.2015.312 OR https://www.cjmr.org/EN/Y2016/V30/I5/355

Fig.1 Axisymmetric finite element model of SiC fiber

Table 1 Material property parameters

Fig.2 Temperature load

Fig.3 Finite element model for hot isostatic pressing

Fig.4 HIP parameters of composite

Fig.5 Deformation of HIP model

Table 2 Material properties of SiC fiber

Table 3 Material properties of Ti-6Al-4V matrix and capsule

Table 4 Average axial thermal stress of WC layer for orthogonal experiment

Fig.6 Effect of SiC fiber parameters on WC layer axial thermal stress (a) deposition temperature; (b) WC layer thickness; (c) SiC layer thickness; (d) C layer thickness

Table 5 Density orthogonal experiment table

Fig.7 Effect of HIP parameters on densification (a) temperature; (b) time; (c) thickness; (d) fiber volume fraction

Fig.8 Residual stress distribution curve of on path E (a) radial; (b) hoop

Table 6 F-point radial residual stress orthogonal experiment table

Fig.9 Effect of HIP parameters on radial residual stress: (a) temperature; (b) time; (c) thickness; (d) fiber volume fraction

Table 7 F-point hoop residual stress orthogonal experiment table

Fig.10 Effect of HIP parameters on hoop residual stress (a) temperature; (b) time; (c) thickness; (d) fiber volume fraction

Fig.11 Axial stress distribution curve along radial direction on the middle surface of symmetric model with different aspect ratio

Fig.12 SiC residual stress distribution curve along radial direction measureed by Laser Raman

Fig.13 Residual stress distribution of SiC fiber (a) nmiddle, (b) end

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