4.7 Article

Rapid spark plasma sintering to produce dense UHTCs reinforced with undamaged carbon fibres

期刊

MATERIALS & DESIGN
卷 130, 期 -, 页码 1-7

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.matdes.2017.05.029

关键词

Aerospace; Ceramic matrix composites; Spark plasma sintering; Eutectic temperature; ZrB2; C

资金

  1. EPSRC [EP/K008749/1]
  2. EPSRC [EP/K008749/1, EP/K008749/2] Funding Source: UKRI
  3. Engineering and Physical Sciences Research Council [EP/K008749/1, EP/K008749/2] Funding Source: researchfish

向作者/读者索取更多资源

Short fibre reinforced ceramic composites, based on ZrB2 with a carbon fibre content of 45 vol%, were produced by ball-milling and rapid Spark Plasma Sintering (SPS) at 1800- 2300 degrees C by varying the holding times. Careful control of the sintering parameters, such as the heating rate, dwell temperature and holding time are required to produce a fully dense matrix and avoid fibre degradation. The sintered materials were characterized in terms of relative density, morphology of the fibres and microstructural features of the matrix. The final residual porosity ranged from 16 to 3 vol%. The carbon fibres maintained their original morphology and the matrix consisted of ZrB2, SiC and ZrC phases. In spite of the good adhesion between the fibre surface and the matrix promoted by SPS processing, extensive fibre pull-out was observed in the fracture surfaces of all of the composites sintered at or below 1900 degrees C.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.7
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据