期刊文献+

飞机桨叶胶接强度试验与分析 被引量:3

Experiment and analysis of joint strength on wing of aircraft
在线阅读 下载PDF
导出
摘要 针对飞机桨叶与防除冰装置的胶接强度开展研究。设计1套能用于测量拉伸剪切力和180°剥离力的测量装置,参照国家标准采用牌号为EA9309和J-200-1A的胶黏剂制备,刚性胶接材料为2A12铝合金,挠性材料为双向碳纤维布的试验试件,最后利用该装置对试验试件胶接强度进行测量试验。结果表明:上述胶黏剂的拉伸剪切强度分别为14.5 MPa和7.7 MPa,180°剥离强度分别为4.58kN/m和4.61kN/m。 The research of the joint strength of adhesives between the wing of aircraft and posed. A simple measuring equipment, which can be used to measure the tensile shear strsigned. According to national standards, EA9303 and J-200-1A adhesives were used to manufact2A12 aluminum alloy and carbon fiber bidirectional fabric were selected as materials of rigid and Finally, the equipment was used to carry out the joint strength of the specimens. The results demonstrated that the tensile shear strengths of the adhesives were 14. 5 MPa and 7 7 MPa respectively. The peel strengths were 4.58 kN/m and 4.61 kN/m in the direction of 180° respectively.
作者 杨毅青 王熙 何舜朗 YANGYiqing;WANGX i;HEShunlang(School of Mechanical Engineering and Automation , Beihang University , Beijing 100191, China)
出处 《中国科技论文》 北大核心 2017年第22期2555-2559,共5页 China Sciencepaper
基金 XX科研计划资助项目(XXXX0110009)
关键词 拉伸装置 桨叶胶接 剥离强度 剪切强度 tension device glued blade peel strength shear strength
  • 相关文献

参考文献7

二级参考文献39

共引文献160

同被引文献39

引证文献3

二级引证文献10

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部