中国航发北京航空材料研究院,北京,100095
纸质出版:2018
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黄浩,王敏涓,李虎,李四青,张书铭,李臻熙,黄旭,解川. 连续SiC纤维增强钛基复合材料研制[J]. 航空制造技术, 2018, 61(14): 26-36.
HUANG Hao, WANG Minjuan, LI Hu, LI Siqing, ZHANG Shuming, LI Zhenxi, HUANG Xu, XIE Chuan. Preparation of SiC Fibers Reinforced Titanium Matrix Composites. Aeronautical Manufacturing Technology, 2018, 61(14): 26-36.
黄浩,王敏涓,李虎,李四青,张书铭,李臻熙,黄旭,解川. 连续SiC纤维增强钛基复合材料研制[J]. 航空制造技术, 2018, 61(14): 26-36. DOI: 10.16080/j.issn1671-833x.2018.14.026.
HUANG Hao, WANG Minjuan, LI Hu, LI Siqing, ZHANG Shuming, LI Zhenxi, HUANG Xu, XIE Chuan. Preparation of SiC Fibers Reinforced Titanium Matrix Composites. Aeronautical Manufacturing Technology, 2018, 61(14): 26-36. DOI: 10.16080/j.issn1671-833x.2018.14.026.
钛基复合材料由于在中高温环境下具有很高的比强度、比模量以及良好的抗疲劳和抗蠕变特性,受到研究者的广泛关注。回顾了国内外该材料的发展历程,详细介绍了连续SiC 纤维增强钛基复合材料的研制过程,包括SiC 纤维制备、涂层制备、复合材料成型及构件制备等工艺过程。概述了研究团队近年来在连续SiC 纤维增强钛基复合材料研究领域开展的工作及取得的进展,包括成功研制了高性能连续SiC 纤维并实现小批量试制,设计了适用于不同增强基体合金的界面涂层,研究表明研制的C 涂层可使复合材料经1100℃处理后界面涂层保存较好;实现了20~50μm 性能优异的钛合金、铝合金、高温镍合金先驱丝的沉积;完成了Ф600mm×160mm 尺寸的复合材料环形件及Ф50mm×300mm 转动轴部件的试制。最后对该材料未来的发展趋势进行了展望。
Due to the high specific strength and modulus
as well as excellent anti-fatigue and creep resistance properties in the high temperature
continuous SiC fibers reinforced titanium matrix composite (SiCf/Ti) has attracted extensive attention. In the paper
we overviewed the manufacture techniques in the fabrication processing of SiCf/Ti composites
including the SiC fiber and coating deposition technique
hot isostatic press (HIP) consolidation technique and component manufacturing. Besides
our study and progress carried out in this area in recent years were summarized. We successfully can make a small bath trial for SiC fiber and also prepare SiCf/Ti composite with brilliant property. In addition
the interfacial reaction investigation in different matrix system consists of Ti alloy
Ti-Al
Al alloy have been performed. The experiments showed that the interface of SiCf/Ti composites can be retained intact with the help of protective coating (C coating) under heat treatment at 1100 ℃ /10h. Moreover
SiC fiber precursor wires of titanium alloy
aluminum alloy
and nickel-based super alloy have been explored through physical vapor deposition technique (PVD)
respectively. The most important is that we had a successful tempt to fabricate ring-like component with the size of Ф600mm×160mm at 1∶1 ratio and roll shaft with the size of Ф50mm×300mm were fabricated successfully.
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