Ablation Mechanism of AlSiB-C/C Composites under an Oxy-Acetylene Torch

In order to improve the ablation resistance of C/C composites, an AlSiB alloy (mass ratio of Al/Si/B = 2:4:1) was used as a dissipative agent to fill the pores of a C/C composites matrix by reactive melt infiltration to prepare AlSiB-C/C composites. The microstructure evolution and ablation behavior...

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Main Authors: Qiuchen Han, Lei Chang, Zhaoqun Sun, Jiaqi Sun, Zengyan Wei, Pingping Wang, Ziyang Xiu, Huasong Gou, Pengchao Kang, Gaohui Wu
Format: Article
Language:English
Published: MDPI AG 2023-01-01
Series:Metals
Subjects:
Online Access:https://www.mdpi.com/2075-4701/13/1/160
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author Qiuchen Han
Lei Chang
Zhaoqun Sun
Jiaqi Sun
Zengyan Wei
Pingping Wang
Ziyang Xiu
Huasong Gou
Pengchao Kang
Gaohui Wu
author_facet Qiuchen Han
Lei Chang
Zhaoqun Sun
Jiaqi Sun
Zengyan Wei
Pingping Wang
Ziyang Xiu
Huasong Gou
Pengchao Kang
Gaohui Wu
author_sort Qiuchen Han
collection DOAJ
description In order to improve the ablation resistance of C/C composites, an AlSiB alloy (mass ratio of Al/Si/B = 2:4:1) was used as a dissipative agent to fill the pores of a C/C composites matrix by reactive melt infiltration to prepare AlSiB-C/C composites. The microstructure evolution and ablation behavior of the obtained AlSiB-C/C composites (mass ratio of Al/Si/B = 2:4:1) under oxy-acetylene flame were investigated by SEM after ablating for 25 s, 50 s, 100 s and 150 s. At the beginning of the ablation process, thermal chemical erosion played a leading part. By using the heat-absorption effect of sweating and the sealing protection effect of the oxide layer, AlSiB-C/C composites significantly reduced the ablation surface temperature, and the linear ablation rate was 4.04 μm/s. With the process of ablation, thermal mechanical erosion tended to dominate. The specimen surface could not form a continuous covering of oxide film to slow down the flame scour, resulting in non-uniform ablation and further expansion of the ablation pit. The self-transpiration cooling behavior and the self-sealing of the ablation products of the dissipative agent played an important role in reducing the extent of thermal chemical erosion and preventing matrix ablation.
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spelling doaj.art-d08125814ae34c3cb322f38a5e338cfd2023-11-30T23:31:33ZengMDPI AGMetals2075-47012023-01-0113116010.3390/met13010160Ablation Mechanism of AlSiB-C/C Composites under an Oxy-Acetylene TorchQiuchen Han0Lei Chang1Zhaoqun Sun2Jiaqi Sun3Zengyan Wei4Pingping Wang5Ziyang Xiu6Huasong Gou7Pengchao Kang8Gaohui Wu9School of Materials Science and Engineering, Harbin Institute of Technology, Harbin 150001, ChinaSchool of Materials Science and Engineering, Harbin Institute of Technology, Harbin 150001, ChinaLaboratory No. 8, Institute of Electronic System Engineering, Beijing 100854, ChinaSchool of Materials Science and Engineering, Harbin Institute of Technology, Harbin 150001, ChinaSchool of Materials Science and Engineering, Harbin Institute of Technology, Harbin 150001, ChinaSchool of Materials Science and Engineering, Harbin Institute of Technology, Harbin 150001, ChinaSchool of Materials Science and Engineering, Harbin Institute of Technology, Harbin 150001, ChinaSchool of Materials Science and Engineering, Harbin Institute of Technology, Harbin 150001, ChinaSchool of Materials Science and Engineering, Harbin Institute of Technology, Harbin 150001, ChinaSchool of Materials Science and Engineering, Harbin Institute of Technology, Harbin 150001, ChinaIn order to improve the ablation resistance of C/C composites, an AlSiB alloy (mass ratio of Al/Si/B = 2:4:1) was used as a dissipative agent to fill the pores of a C/C composites matrix by reactive melt infiltration to prepare AlSiB-C/C composites. The microstructure evolution and ablation behavior of the obtained AlSiB-C/C composites (mass ratio of Al/Si/B = 2:4:1) under oxy-acetylene flame were investigated by SEM after ablating for 25 s, 50 s, 100 s and 150 s. At the beginning of the ablation process, thermal chemical erosion played a leading part. By using the heat-absorption effect of sweating and the sealing protection effect of the oxide layer, AlSiB-C/C composites significantly reduced the ablation surface temperature, and the linear ablation rate was 4.04 μm/s. With the process of ablation, thermal mechanical erosion tended to dominate. The specimen surface could not form a continuous covering of oxide film to slow down the flame scour, resulting in non-uniform ablation and further expansion of the ablation pit. The self-transpiration cooling behavior and the self-sealing of the ablation products of the dissipative agent played an important role in reducing the extent of thermal chemical erosion and preventing matrix ablation.https://www.mdpi.com/2075-4701/13/1/160reactive melt infiltrationablation resistanceAlSiB-C/C compositesoxy-acetylene flameheat dissipation
spellingShingle Qiuchen Han
Lei Chang
Zhaoqun Sun
Jiaqi Sun
Zengyan Wei
Pingping Wang
Ziyang Xiu
Huasong Gou
Pengchao Kang
Gaohui Wu
Ablation Mechanism of AlSiB-C/C Composites under an Oxy-Acetylene Torch
Metals
reactive melt infiltration
ablation resistance
AlSiB-C/C composites
oxy-acetylene flame
heat dissipation
title Ablation Mechanism of AlSiB-C/C Composites under an Oxy-Acetylene Torch
title_full Ablation Mechanism of AlSiB-C/C Composites under an Oxy-Acetylene Torch
title_fullStr Ablation Mechanism of AlSiB-C/C Composites under an Oxy-Acetylene Torch
title_full_unstemmed Ablation Mechanism of AlSiB-C/C Composites under an Oxy-Acetylene Torch
title_short Ablation Mechanism of AlSiB-C/C Composites under an Oxy-Acetylene Torch
title_sort ablation mechanism of alsib c c composites under an oxy acetylene torch
topic reactive melt infiltration
ablation resistance
AlSiB-C/C composites
oxy-acetylene flame
heat dissipation
url https://www.mdpi.com/2075-4701/13/1/160
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