首页 | 本学科首页   官方微博 | 高级检索  
     检索      

飞机前起落架防摆抗断研究
引用本文:贾朝升,沙伯南.飞机前起落架防摆抗断研究[J].航空学报,1989,10(10):495-500.
作者姓名:贾朝升  沙伯南
作者单位:西北工业大学 (贾朝升),西北工业大学(沙伯南)
摘    要: 本文将试验,计算与外场实测相结合,论证了歼六飞机前起落架损伤折断的主要原因是前轮摆振,采取简单、合理、易行的措施,解决歼六飞机前起落架防摆抗断问题,取得显著效果。

关 键 词:起落架  摆振  阻尼  应力  
收稿时间:1988-05-26;

THE ANTI-SHIMMY AND BREAK-PROOF STUDY OF NOSE LANDING GEAR
Northwestern Polytechnical University Jia Chaosheng and Sha Bonan.THE ANTI-SHIMMY AND BREAK-PROOF STUDY OF NOSE LANDING GEAR[J].Acta Aeronautica et Astronautica Sinica,1989,10(10):495-500.
Authors:Northwestern Polytechnical University Jia Chaosheng and Sha Bonan
Institution:Northwestern Polytechnical University Jia Chaosheng and Sha Bonan
Abstract:By considering the results from experiments and calculations, it has been proved that the main reason of damage of nose landing gear of an aircraft is due to shimmy. By using an easy, simple and reasonable method, the anti-shimmy and break-proof problem of nose landing gear has been solved and a satisfying result has been obtained.
Keywords:laoding gear  shimmy  damping  strees    
本文献已被 CNKI 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号