摘要
本文介绍了以Kevlar纤维和聚酰亚胺树脂为原料制备航空发动机用耐高低温、耐油、耐磨、高强度纤维 -树脂复合材料的方法。
The fibre-resins composite backup plate of the aeroengine was prepared with Kevlar fibres and polyimdie resins. The composite has the excellent heat-cold resistant,oil-proof,wear resistant and high strength.
出处
《化学工程师》
CAS
2004年第7期13-14,共2页
Chemical Engineer
基金
国防科工委攻关项目 ( 93 0 13 )
