Due to the low density and excellent mechanical proper-ties,high performance fiber reinforced materials have aconsiderable application in the area of high technologyand dally usage.In this paper,the Ultra-high Molecu-...Due to the low density and excellent mechanical proper-ties,high performance fiber reinforced materials have aconsiderable application in the area of high technologyand dally usage.In this paper,the Ultra-high Molecu-lar Weight Polyethylene(UHMWPE)fiber reinforcedPE tape prepared with the method of powder impregnat-ion was studied.The effect of impregnate length and thetensile force of the yarn on the fiber content as well as on the strength and modulus of the tape were discussed.Calculation shows that the strength and the modulus ofthe ULMWPE fiber can keep about 85% after it undergothe process.展开更多
介绍了热障涂层(TBC)的主要材料和制备工艺,分析了TBC在国内外航空发动机中的典型应用实例。目前工程应用的TBC多为由金属底层和陶瓷面层组成的双层结构,金属底层采用MCr Al Y包覆型涂层或Pt-Al(或Al)渗层,陶瓷面层采用YSZ涂层。美国的...介绍了热障涂层(TBC)的主要材料和制备工艺,分析了TBC在国内外航空发动机中的典型应用实例。目前工程应用的TBC多为由金属底层和陶瓷面层组成的双层结构,金属底层采用MCr Al Y包覆型涂层或Pt-Al(或Al)渗层,陶瓷面层采用YSZ涂层。美国的航空发动机中,体积较大的静子零件多采用VPS MCr Al Y底层+APS YSZ面层的TBC,体积较小的转动零件主要采用Pt-Al渗层(或EB-PVD MCr Al Y)+EB-PVD YSZ面层的TBC。我国的航空发动机中,燃烧室浮动瓦片和高压涡轮导叶等零件采用了TBC,其主要技术难点在于涂层的厚度均匀性控制、表面粗糙度控制以及涂层对气膜孔影响的控制等方面。展开更多
文摘Due to the low density and excellent mechanical proper-ties,high performance fiber reinforced materials have aconsiderable application in the area of high technologyand dally usage.In this paper,the Ultra-high Molecu-lar Weight Polyethylene(UHMWPE)fiber reinforcedPE tape prepared with the method of powder impregnat-ion was studied.The effect of impregnate length and thetensile force of the yarn on the fiber content as well as on the strength and modulus of the tape were discussed.Calculation shows that the strength and the modulus ofthe ULMWPE fiber can keep about 85% after it undergothe process.
文摘介绍了热障涂层(TBC)的主要材料和制备工艺,分析了TBC在国内外航空发动机中的典型应用实例。目前工程应用的TBC多为由金属底层和陶瓷面层组成的双层结构,金属底层采用MCr Al Y包覆型涂层或Pt-Al(或Al)渗层,陶瓷面层采用YSZ涂层。美国的航空发动机中,体积较大的静子零件多采用VPS MCr Al Y底层+APS YSZ面层的TBC,体积较小的转动零件主要采用Pt-Al渗层(或EB-PVD MCr Al Y)+EB-PVD YSZ面层的TBC。我国的航空发动机中,燃烧室浮动瓦片和高压涡轮导叶等零件采用了TBC,其主要技术难点在于涂层的厚度均匀性控制、表面粗糙度控制以及涂层对气膜孔影响的控制等方面。