航天制造技术
航天製造技術
항천제조기술
HANGTIAN ZHIXAO JI SHU
2013年
5期
53-55
,共3页
刘梦媛%蔡良元%陈梦怡
劉夢媛%蔡良元%陳夢怡
류몽원%채량원%진몽이
蜂窝夹层结构%滚筒剥离强度%NH-1-2.75-72 Nomex蜂窝
蜂窩夾層結構%滾筒剝離彊度%NH-1-2.75-72 Nomex蜂窩
봉와협층결구%곤통박리강도%NH-1-2.75-72 Nomex봉와
honeycomb sandwich structure%cylinder peel strength%NH-1-2.75-72 Nomex honeycomb
研究了以 Nomex 蜂窝、铝蜂窝为芯层材料，SW-280A/3218中温固化环氧树脂玻璃布预浸料为蒙皮材料，FM 73M和SY-24C-300胶膜为蒙皮和蜂窝的胶接材料的蜂窝夹层结构的滚筒剥离强度。蜂窝夹层结构平板采用热压罐成型工艺方法和烘箱成型工艺方法一次共固化工艺，测试了蜂窝夹层结构平板的滚筒剥离强度。蜂窝夹层结构材料已应用于大型平板天线罩的制造。
研究瞭以 Nomex 蜂窩、鋁蜂窩為芯層材料，SW-280A/3218中溫固化環氧樹脂玻璃佈預浸料為矇皮材料，FM 73M和SY-24C-300膠膜為矇皮和蜂窩的膠接材料的蜂窩夾層結構的滾筒剝離彊度。蜂窩夾層結構平闆採用熱壓罐成型工藝方法和烘箱成型工藝方法一次共固化工藝，測試瞭蜂窩夾層結構平闆的滾筒剝離彊度。蜂窩夾層結構材料已應用于大型平闆天線罩的製造。
연구료이 Nomex 봉와、려봉와위심층재료，SW-280A/3218중온고화배양수지파리포예침료위몽피재료，FM 73M화SY-24C-300효막위몽피화봉와적효접재료적봉와협층결구적곤통박리강도。봉와협층결구평판채용열압관성형공예방법화홍상성형공예방법일차공고화공예，측시료봉와협층결구평판적곤통박리강도。봉와협층결구재료이응용우대형평판천선조적제조。
The cylinder peel strength of honeycomb sandwich structure were studied in this paper. NH-1-2.75-72 Nomex aluminium honeycomb used as sandwich material, SW-280A/3218 glass fabric reinforced epoxy resin solidified at 130℃FMw e7r3eMseal encdteSdYf-o2r4Csk-i3n.00 adhesive film for bonding skin and honeycomb. By applying one step autocalve and one step oven cure cycle,The honeycomb sandwich structure were produced. The cylinder peel strength were tested. The material of honeycomb sandwich structure has been used in manufacturing large-scale flat radome.
