宇航材料工艺
宇航材料工藝
우항재료공예
AEROSPACE MATERIALS & TECHNOLOGY
2010年
1期
49-52
,共4页
李卫东%曹海琳%刘毅佳%陈国荣%史鹏飞
李衛東%曹海琳%劉毅佳%陳國榮%史鵬飛
리위동%조해림%류의가%진국영%사붕비
混杂纤维%复合材料%混杂效应%热性能%烧蚀
混雜纖維%複閤材料%混雜效應%熱性能%燒蝕
혼잡섬유%복합재료%혼잡효응%열성능%소식
Hybrid fiber%Composites%Hybrid effect%Thermal property%Ablation
制备了碳纤维/玄武岩纤维(CF/BF)增强酚醛树脂复合材料,研究了复合材料层合板不同胶合量对其层间剪切强度、热传导和耐烧蚀性能的影响.结果表明:CF/BF复合材料,在胶的体积分数为35%时,复合材料经纬向层间剪切强度达到最大值21和20 MPa;在胶的体积分数为39.5%处,热导率和线烧蚀率出现最低值0.366 W/(m·K)和87 μm/s.CF/BF混杂纤维复合材料性能符合混杂纤维复合材料性能混杂效应规律.
製備瞭碳纖維/玄武巖纖維(CF/BF)增彊酚醛樹脂複閤材料,研究瞭複閤材料層閤闆不同膠閤量對其層間剪切彊度、熱傳導和耐燒蝕性能的影響.結果錶明:CF/BF複閤材料,在膠的體積分數為35%時,複閤材料經緯嚮層間剪切彊度達到最大值21和20 MPa;在膠的體積分數為39.5%處,熱導率和線燒蝕率齣現最低值0.366 W/(m·K)和87 μm/s.CF/BF混雜纖維複閤材料性能符閤混雜纖維複閤材料性能混雜效應規律.
제비료탄섬유/현무암섬유(CF/BF)증강분철수지복합재료,연구료복합재료층합판불동효합량대기층간전절강도、열전도화내소식성능적영향.결과표명:CF/BF복합재료,재효적체적분수위35%시,복합재료경위향층간전절강도체도최대치21화20 MPa;재효적체적분수위39.5%처,열도솔화선소식솔출현최저치0.366 W/(m·K)화87 μm/s.CF/BF혼잡섬유복합재료성능부합혼잡섬유복합재료성능혼잡효응규률.
Carbon fiber (CF)/basah fiber (BF) hybrid fibers plain fabric reinforced phenolic resin composite was synthesized. The composite laminates were tested and the interlaminate shear strength, thermal properties and abla-tion behaviors were studied by adjusting its resin content. The testing results indicated that the CF/BF hybrid fiber re-inforced composites combined the advantages of both carbon fiber and basalt fiber. When resin content is 35%, the composite performance reach extreme value:warp and weft interlayer shear strength are 21 MPa and 20 MPa. When resin content is 39.5%,thermal conductivity and linear ablation rate are 0.366 W/(m·K) and 87 μm/s respectively. The properties of new composites has complied with the rules of hybrid effect.