上海航天
上海航天
상해항천
AEROSPACE SHANGHAI
2012年
2期
31-35,54
,共6页
固体火箭发动机%衬层%成型工艺%界面粘接
固體火箭髮動機%襯層%成型工藝%界麵粘接
고체화전발동궤%츤층%성형공예%계면점접
Solid rocket motor%Liner%Forming technology%Bonding property
综述了固体火箭发动机衬层粘接技术。介绍了衬层材料选择原则,分析了刷涂、喷涂、抛涂、离心和拉涂等成型工艺,讨论了界面粘接及其影响因素与改善途径,给出了前人的研究方法,阐述了衬层关键技术的发展趋势。
綜述瞭固體火箭髮動機襯層粘接技術。介紹瞭襯層材料選擇原則,分析瞭刷塗、噴塗、拋塗、離心和拉塗等成型工藝,討論瞭界麵粘接及其影響因素與改善途徑,給齣瞭前人的研究方法,闡述瞭襯層關鍵技術的髮展趨勢。
종술료고체화전발동궤츤층점접기술。개소료츤층재료선택원칙,분석료쇄도、분도、포도、리심화랍도등성형공예,토론료계면점접급기영향인소여개선도경,급출료전인적연구방법,천술료츤층관건기술적발전추세。
The liner bonding technology of solid rocket motor was summarized in this paper.The design of liner formula was introduced.The forming technologies such as brush coating,spray coating,cast coating,centrifugal coating and pull coating were analyzed.The characterization of liner bonded interface and influencing factors of bonding property as well as the improving strategies were discussed.The study methods of the formers were given out.The developing trends of liner were also briefly introduced.
