起落架
汽车工程
复合数
航空航天工程
工程类
计算机科学
结构工程
机械工程
海洋工程
算法
作者
Yen-Chu Liang,Pei-Chieh Chin,Yun-Ping Sun,Muh-Rong Wang
摘要
Unmanned aerial vehicles (UAVs) have become popular for military applications as well as for use in structural inspection, weather monitoring, and festival demonstrations. Suitable landing gears to ensure that the UAV can take off and land safely are important when the price of the cargo and UAV increase. A lightweight and high-strength landing gear is desirable to overcome accidents during service. Composite materials are a promising, excellent solution for this purpose. This study demonstrated the design, numerical analysis (Ansys), manufacture, and experimental verification (LabVIEW) of a composite landing gear for a UAV. In particular, landing gears with different carbon fiber-reinforced polymer (CFRP) composite fiber orientations were analyzed, manufactured, and experimentally verified in this study.
科研通智能强力驱动
Strongly Powered by AbleSci AI