[1]崔紅,閆聯(lián)生,劉勇瓊,等.摻雜改性C/C復(fù)合材料研究進(jìn)展[J].中國(guó)材料進(jìn)展,2011,(11):013-17.
CUI Hong,YAN Liansheng,LIU Yongqiong,et al. Advances on Ceramic Hybird Modified Carbon/Carbon Composites[J].MATERIALS CHINA,2011,(11):013-17.
點(diǎn)擊復(fù)制
摻雜改性C/C復(fù)合材料研究進(jìn)展(
)
中國(guó)材料進(jìn)展[ISSN:1674-3962/CN:61-1473/TG]
- 卷:
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- 期數(shù):
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2011年第11期
- 頁(yè)碼:
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013-17
- 欄目:
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特約研究論文
- 出版日期:
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2011-11-25
文章信息/Info
- Title:
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Advances on Ceramic Hybird Modified Carbon/Carbon Composites
- 作者:
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崔紅; 閆聯(lián)生; 劉勇瓊; 張強(qiáng); 孟祥利
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(西安航天復(fù)合材料研究所，陜西 西安 710025)
- Author(s):
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CUI Hong; YAN Liansheng; LIU Yongqiong; ZHANG Qiang; MENG Xiangli
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(Xi an Aerospace Composite Material Institute, Xian 710025，China)
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- 關(guān)鍵詞:
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; 高溫材料; C/C復(fù)合材料; 摻雜改性; 抗氧化
- 文獻(xiàn)標(biāo)志碼:
-
A
- 摘要:
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陶瓷摻雜改性碳/碳（C/C）復(fù)合材料在保持C/C復(fù)合材料原有優(yōu)異高溫力學(xué)性能及尺寸穩(wěn)定性等特性的前提下，顯著提高了C/C復(fù)合材料的高溫抗氧化、抗燒蝕性能，且其具有可設(shè)計(jì)性和良好的抗熱震性能等優(yōu)勢(shì)，是新型高超聲速飛行器和新一代高性能發(fā)動(dòng)機(jī)熱防護(hù)部件的理想候選材料。綜述了國(guó)內(nèi)外在SiC陶瓷摻雜改性C/C復(fù)合材料，ZrC，ZrB2超高溫陶瓷摻雜改性C/C復(fù)合材料以及TaC，HfC超高溫陶瓷摻雜改性C/C復(fù)合材料等方面的最新研究進(jìn)展和應(yīng)用情況，并分析了陶瓷摻雜改性C/C復(fù)合材料目前研究及應(yīng)用中存在的主要問題和今后潛在的研究發(fā)展方向。
- Abstract:
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Being the ideal candidate material for thermal protection parts in supersonic flight and the high performance rocket engine, carbon/carbon composites modified by ceramic hybrid have good oxidation and ablation resistance, designability, good thermal shock resistance as well as the inherent unique comprehensive properties, such as excellent mechanical properties and dimensional stability at high temperature. The present status of research and application of carbon/carbon composites modified by the SiC ceramics and ZrC, ZrB2, TaC, HfC ultrahigh temperature ceramics were summarized. The existing problems and the potential development direction on the investigation of the ceramic hybrid modification C/C composites were also proposed.
更新日期/Last Update:
2011-12-06