一种具有可旋转副翼的直升机模型的设计  

作　　者：王雄志 王静怡 刘馨雨 王琛 刘书辉 景想云[1] 

机构地区：[1]湖北汽车工业学院机械学院,湖北十堰442002

出　　处：《科技创新导报》2020年第6期96-97,99,共3页Science and Technology Innovation Herald

基　　金：《2019年大学生创新创业项目》(项目编号:DC2019024)

摘　　要：直升机作为20世纪航空技术极具特色的创造之一,极大地拓展了飞行器的应用范围。但是,其缺点在于增加的副翼与主旋翼的推进方向始终保持一致,使直升机飞行姿态的调控受到限制,抗风能力较差,于是我们进行了创新。本文介绍了一种具有可旋转副翼的直升机的设计,我们通过步进电机与齿轮传动系统,为副翼增加了可以改变推进角度的功能,能更加自由地修正机身姿态,提升了直升机的抗风能力,具有重大的现实意义和理论创新。As one of the most characteristic creations of aviation technology in the 20th century,helicopter has greatly expanded the application range of aircraft.However,the disadvantage is that the added aileron and the main rotor always keep the same propulsion direction,which limits the control of the helicopter’s flight attitude and has poor wind resistance,so we made innovations.This paper introduces the design of a helicopter with a rotatable aileron.Through the step motor and gear transmission system,we add the function that can change the propulsion angle to the aileron,which can modify the fuselage attitude more freely and improve the wind resistance of the helicopter.It has great practical significance and theoretical innovation.

关 键 词：可旋转副翼 抗风直升机 副翼倾转 SOLIDWORKS 

分 类 号：V249[航空宇航科学与技术—飞行器设计]