2H2-O2焰中的燒蝕行為。結(jié)果表明:無(wú)緯布、穿刺纖維束由CVI+PIC制備的碳基體填充而形成致密C/C區(qū)域,RMI生成的SiC主要位于網(wǎng)胎層中,其含量37.3wt%。復(fù)合材料表面因過(guò)量硅化而形成了SiC富集層。燒蝕距離20mm、O2:C2H2=2:1時(shí),燒蝕600s后材料X-Y、Z向線燒蝕率分別為:0.8×10-4 mm/s、3.6×10-4 mm/s,比PIP工藝制備C/C-SiC材料燒蝕率小一個(gè)數(shù)量級(jí)。燒蝕面SiC富集層保護(hù)及被動(dòng)氧化作用是材料具有優(yōu)異抗氧化燒蝕性能的主要原因。隨燒蝕距離由20mm向10mm減小,復(fù)合材料燒蝕率先緩慢變化后快速增大,燒蝕率快速增長(zhǎng)階段復(fù)合材料發(fā)生主動(dòng)氧化燒蝕。"/>

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RMI法制備穿刺C/C-SiC復(fù)合材料的微結(jié)構(gòu)及燒蝕性能研究
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西安航天復(fù)合材料研究所

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中圖分類號(hào):

TB332

基金項(xiàng)目:

國(guó)家自然科學(xué)基金(21676163)、中國(guó)航天青年拔尖人才項(xiàng)目(2019.1-2021.12)


Microstructure and ablation properties of the pierced C/C-SiC composites
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1.Xi’an Aerospace Composites Research Institute,Xi’an 710025;2.China

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    摘要:

    以無(wú)緯布/網(wǎng)胎0°/90°疊層穿刺預(yù)制體為增強(qiáng)體,采用化學(xué)氣相滲(Chemical vapor infiltration,CVI)、樹(shù)脂浸漬碳化(Polymer infiltration carbonization,PIC)與反應(yīng)熔滲(Reactive melt infiltration,RMI)復(fù)合工藝制備穿刺C/C-SiC復(fù)合材料,研究其微觀組織及在C2H2-O2焰中的燒蝕行為。結(jié)果表明:無(wú)緯布、穿刺纖維束由CVI+PIC制備的碳基體填充而形成致密C/C區(qū)域,RMI生成的SiC主要位于網(wǎng)胎層中,其含量37.3wt%。復(fù)合材料表面因過(guò)量硅化而形成了SiC富集層。燒蝕距離20mm、O2:C2H2=2:1時(shí),燒蝕600s后材料X-Y、Z向線燒蝕率分別為:0.8×10-4 mm/s、3.6×10-4 mm/s,比PIP工藝制備C/C-SiC材料燒蝕率小一個(gè)數(shù)量級(jí)。燒蝕面SiC富集層保護(hù)及被動(dòng)氧化作用是材料具有優(yōu)異抗氧化燒蝕性能的主要原因。隨燒蝕距離由20mm向10mm減小,復(fù)合材料燒蝕率先緩慢變化后快速增大,燒蝕率快速增長(zhǎng)階段復(fù)合材料發(fā)生主動(dòng)氧化燒蝕。

    Abstract:

    The C/C-SiC composites were prepared by chemical vapor infiltration (CVI) combined with polymer infiltration carbonization (PIC) and reactive melt infiltration (RMI) using pierced non-woven carbon fiber felt preform. The microstructure and ablation properties were investigated. The results presented that non-woven carbon fiber cloth and pierced carbon fiber bundle formed dense C/C microstructure after CVI and PIC processes. SiC matrix was mainly located in the felt after RMI process and the content was 37.3wt%. SiC-rich layer was formed on the surface of the composites. When the ablation distance is 20mm, the ablation rates on XY and Z directions of the composites are 0.8×10-4 mm/s and 3.6×10-4 mm/s, respectively. The excellent ablation performance could be owing to the passive oxidation of SiC-rich layer on the surface. With the ablation distance decreased from 20mm to 10mm, the ablation rate of the composites changed slowly and then increased rapidly, because of the active oxidation ablation of the composites.

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吳小軍,劉明強(qiáng),張兆甫,謝棟,郭春園. RMI法制備穿刺C/C-SiC復(fù)合材料的微結(jié)構(gòu)及燒蝕性能研究[J].稀有金屬材料與工程,2021,50(11):4023~4030.[WU Xiaojun, LIU Mingqing, ZHANG Zhaofu, XIE Dong, GUO Chunyuan. Microstructure and ablation properties of the pierced C/C-SiC composites[J]. Rare Metal Materials and Engineering,2021,50(11):4023~4030.]
DOI:10.12442/j. issn.1002-185X.20200877

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  • 收稿日期:2020-11-13
  • 最后修改日期:2020-12-14
  • 錄用日期:2020-12-23
  • 在線發(fā)布日期: 2021-11-30
  • 出版日期: 2021-11-24