PBO基质平流层飞艇蒙皮材料的制备研究  

Fabrication and Investigation of Envelope Materials for Stratospheric Aircraft with PBO Fabric as Load-carriers

作　　者：曹旭[1] 高诚贤[2] 

机构地区：[1]北京空间机电研究所,北京100076 [2]中国纺织科学研究院,北京100025

出　　处：《高科技纤维与应用》2009年第4期37-42,共6页Hi-Tech Fiber and Application

摘　　要：以聚对苯撑苯并二恶唑(PBO)平纹织物为承重层、聚氟乙烯(PVF)薄膜为阻氦/耐候层,采用层压复合工艺制备了无镀铝聚酯薄膜和含镀铝聚酯薄膜两种平流层飞艇蒙皮材料试样。对试样进行性能测试,结果表明两种材料均满足面密度<230g/m2、氦气渗透率<0.5L/(m2·24h·0.1MPa)的要求,无铝蒙皮材料的抗拉强度>1000N/cm,强度性能也满足要求。Two types of stratospheric aircraft envelope materials made of AL-PET membrane and non-AL membrane with Poly（p-phenylene-2,6-benzobisoxazole） （PBO） fabric as load carders, PVF film as weatherproofed/gastight layer were fabricated by a laminating process. The test result shows that the weight of the two envelope materials is lower than 230 g/m^2 and the helium transmission is less than 0.5 L/（m^2·24 h·0.1 MPa）. Only mechanical properties of the envelope without Al-membrane was tested, and the result indicates that its tensile breaking strength can meet the requirement of strengths higher than 1 000 N/cm.

关 键 词：平流层飞艇 蒙皮材料 PBO织物 层压复合 

分 类 号：V259[一般工业技术—材料科学与工程]