航空航天
变形
外倾角(空气动力学)
航空航天工程
机身
执行机构
空气动力学
翼
飞行操纵面
有效载荷(计算)
微型飞行器
工程类
智能材料
结构工程
汽车工程
计算机科学
材料科学
电气工程
网络数据包
纳米技术
计算机视觉
计算机网络
作者
Javier Crespo Moreno,Rafael Bardera Mora,Ángel Antonio Rodríguez Sevillano,Álvaro Cobo-González
标识
DOI:10.1016/j.compstruct.2023.116794
摘要
The purpose of this paper is to show the advantages of using a smart composite in a micro air vehicle (MAV) equipped with morphing wing technology. A Macro Fiber Composite (MFC) actuator is attached to the wing's bottom surface to modify the wing camber during the mission. This material allows the MAV to be optimized according to each flight, thus making it more versatile and attractive to the market. The elongation of the lower surface when a positive voltage is applied to the actuator is translated to an increment in camber, which results in an increment in the maximum lift coefficient, thus enabling the vehicle to fly slower to adapt to any payload. Besides, a reduction in camber results in an increase in aerodynamic efficiency, which improves range and endurance. Several tests of the MAV at prototype level have been carried out at INTA, so as to demonstrate the feasibility of implementing MFC actuators to control and manoeuvre these vehicles. The use of this material in aerospace industry opens up various fields of research in aerospace engineering, such as new features in flight mechanics and aerodynamic performance and new strategies in the design of flight stability and control laws.
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