欢迎登录材料期刊网

材料期刊网

高级检索

对含乙烯基陶瓷前驱体PSN1的固化工艺及其经准陶瓷化后所得材料的性能进行了研究.采用TGA、DMA对准陶瓷基体的热性能进行了表征.结果表明:其分解温度及800℃残重率随准陶瓷化温度升高而升高,N2气氛下分别达到580℃和87%,空气气氛中分解温度高于550℃,残重率达95%以上,Tg也随准陶瓷化温度上升而升高,420℃准陶瓷化基体在400℃以下没有明显的玻璃化转变.运用网络矢量分析仪测定了介电常数随温度和频率的变化情况,结果表明准陶瓷基体介电常数小于3,并且随温度和频率变化不大.准陶瓷基体吸水率较低,最低达到0.03%.初步研究表明PSN1准陶瓷基体具有良好的热、介电稳定性,吸水率低,有望用作耐高温透波复合材料基体.

参考文献

[1] Anthony Kelly;Carl Zweben.Comprehensive Composite Materials[M].Elsevier Ltd,2000:279-315.
[2] Zuo Hongjun;Chen Jiansheng;Fan Lin et al.Synthesis and characterization of melt-processable polyimides derived from 1,4-bis(4-amino-2-trifluoromethyiphenoxy) benzene[J].Journal of Applied Polymer Science,2008,107:755-765.
[3] Tang, HY;Li, WW;Fan, XH;Chen, XF;Shen, ZH;Zhou, QF .Synthesis, preparation and properties of novel high-performance allyl-maleimide resins[J].Polymer,2009(6):1414-1422.
[4] Zhang, BF;Wang, ZG;Zhang, X .Synthesis and properties of a series of cyanate resins based on phenolphthalein and its derivatives[J].Polymer,2009(3):817-824.
[5] Paquette,David G .Method of making a radar transparent window material operable above 2000℃[P].US Patent 5627542,1997-05-06.
[6] Place Jr,Thomas M .Low loss radar window for reentry vehicle[P].US Patent 4786548,1988-11-22.
[7] 胡连成;黎义;于翘.俄罗斯航天透波材料现状考察[J].宇航材料工艺,1994(01):48-50.
[8] Narayanan J;Aldinger F .Fabrication and characterization of fully dense Si-C-N ceramics from a poly (ureamethylvinyi) silazane precursor[J].Journal of the European Ceramic Society,2009,29:163-173.
[9] Li Y;Riedel R .Thermal crogs-linking and pyrolytic conversion of poly (ureamethylvinyl) silazanes to silicon-based ceramies[J].Applied Organometallic Chemistry,2001,15:820-832.
[10] G.Motz D.Suttor .Structural characterisation of silicon carbonitride ceramics derived from polymeric precursors[J].Journal of the European Ceramic Society,2000(2):215-225.
[11] Zhang Zongbo;Luo Yongming;Xu Caihong.Study on new high-temperature resistant silicon-containing polymer for composite radomes[A].黑龙江哈尔滨,2009:9-11.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%