PPS复合材料在空空导弹导引部件承力结构件上的应用研究  

Application Research of PPS Composite Material on the Support Structure of Air-to-Air Missile Seeker

作　　者：陈世锋[1] 汤晓云 姚达斌[1] 曹旭东[1,3] Chen Shifeng;Tang Xiaoyun;Yao Dabin;Cao Xudong(China Airborne Missile Academy,Luoyang 471009,China;The First Military Representative Office of Air Force Equipment Department in Luoyang District,Luoyang 471009,China;Aviation Key Laboratory of Science and Technology on Airborne Guided Weapons,Luoyang 471009,China)

机构地区：[1]中国空空导弹研究院,河南洛阳471009 [2]空装驻洛阳地区第一军事代表室,河南洛阳471009 [3]航空制导武器航空科技重点实验室,河南洛阳471009

出　　处：《航空兵器》2020年第2期97-102,共6页Aero Weaponry

摘　　要：本文以空空导弹导引部件中的承力结构件放置舱骨架作为研究对象,改进放置舱骨架的结构设计,研究PPS复合材料注塑成型工艺,成型制造PPS-GF40材料的放置舱骨架,并在空空导弹导引部件的力学环境试验条件下进行试验验证。试验结果表明,在模拟真实负载装配的情况下,PPS-GF40放置舱骨架在力学试验完成后未发生影响功能的损伤与破坏。该结果为导引部件的轻量化设计提供新的方向,为PPS复合材料在空空导弹上的应用提供工程依据。In this paper,the support structure of air-to-air missile seeker is taken as the research object,the structural design of the frame is improved,the injection molding process of PPS composite material is studied,the frame of PPS-GF40 material is manufactured,and the test is carried out under the force environment test condition of the air-to-air missile seeker.The test results show that under the condition of simulating the real load assembly,PPS-GF40 electronic cabin frame has no damage to its function after the mechanical test.The results provide a new direction for the lightweight design of guidance components and engineering basis for the application of PPS composite material in air-to-air missiles.

关 键 词：空空导弹 导引部件 轻量化 PPS 复合材料 

分 类 号：TJ760.4[兵器科学与技术—武器系统与运用工程]