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以W丝作为成孔剂,采用孔隙预置技术制备了发汗多孔C/SiC复合材料,对其孔隙结构进行表征,研究了材料的力学性能和渗透行为.结果表明:采用孔隙预置技术能够有效的控制多孔C/SiC材料开孔率和孔隙结构,其孔隙主要由W丝去除后形成的直通孔组成,开孔率决定于W丝的体积含量,所制备的材料具有良好的力学性能和渗透性能.其弯曲强度达到358 MPa、弯曲模量达到124 GPa,断裂韧性达到16.7 MPa·m1/2,空隙率为23.5%,渗透率为1.02×10-3mm2,材料表现为韧性断裂模式,其孔隙的存在并没有对材料的力学性能产生明显的影响.

参考文献

[1] Mayor W O H .TEKAN-research on cryogenic rocket engines at DLR lampold-shausdn AIAA 2000-3219[R].,2001.
[2] Erhan Serbest;Haidn O J;Hald H .Effusion cooling of throat regionin rocket engines applying fibre reinforced ceramics AIAA 2001-3410[R].,2001.
[3] Frohlke K;Haidn O J;Serbest E .New experimental results on transpiration cooling for H2/O2 rocket combustion chambers.AIAA 1998-3443[R].,1998.
[4] Serbest E;Haidn O;Hald H et al.Effusion cooling in rocket combustors applying fiber reinforced ceramics.AIAA 1999-2911[R].,1999.
[5] Wults H G .Joining fastening and sealling of CMC structures AIAA 1999-3552[R].,1999.
[6] Haidn O;Greuel D;Herbertz A .Transpiration cooling applied to C/SiC liners of cryogenic liquid rocket engines.AIAA2004-3682[R].,2004.
[7] Frohlke K;Haberzettl A;Haidn O J et al.First host fire testcampaign at the French/German research facility P8 AIAA 1997-2929[R].,1997.
[8] Calabro M;Perie J B;Prodhomme M T .Innovative upper stage propulsion concepts for futrue launchers IAA 2001-3692[R].,2001.
[9] Bear J.Dynamics of Fluids in Porous Media[M].American Elsevier Publishing Comp INC,1972
[10] 宋麦丽,王涛,闫联生,邹武,余惠琴,刘毅佳.高性能C/SiC复合材料的快速制备[J].新型炭材料,2001(02):57-60.
[11] Collins R E.Flow of Fluids Though Porous Materials[M].New York:Reinhold,1961
[12] Dullien F A L.Porous Media Fluid Transport and Pore Structure[M].San Diego:academic Press,1992
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