半转翼飞行器升力机理研究  

A Study of the Lift Mechanism of a Half-rotor Aircraft

作　　者：王翔民 钱爱文 许发 王卓霖 WANG Xiangmin;QIAN Aiwen;XU Fa;WANG Zhuolin(School of Mechanical and Automotive Engineering,Bengbu University,Bengbu 233030,China)

机构地区：[1]蚌埠学院机械与车辆工程学院,安徽蚌埠233030

出　　处：《机械工程与自动化》2025年第1期10-12,共3页Mechanical Engineering & Automation

基　　金：安徽省创新训练项目(S202111305031)。

摘　　要：为解决现有扑翼飞行器非定常运动难以理论化、尺寸无法大型化等问题,基于半转机构设计半转翼飞行器;半转翼飞行器试验模型采用连续转动的半转叶片来模拟昆虫翅膀的上下摆动,通过研究半转叶片的连续转动机理,得到升力的理论计算方法,为后续半转翼飞行器升力测试装置的设计以及试验模型的升力测试奠定了基础。In order to solve the problems of non-constant motion of the existing flapping wing vehicle,which is difficult to be theorized,and the size can not be large-scale,we design the semi-rotor vehicle based on the half-rotor mechanism,and the semi-rotor vehicle test model simulates the up and down swing of the insect wings with the continuously rotating half-rotor blade,and we get the theoretical calculation method of the lift by studying the continuous rotation mechanism of the half-rotor blade,which lays the foundation for the design of the subsequent semi-rotor vehicle lift test device as well as the lift test of the experimental model.It lays the foundation for the design of the lift test device of the half-rotor aircraft and the lift test of the model.

关 键 词：半转翼飞行器 性能参数 升力 

分 类 号：TH113.2[机械工程—机械设计及理论] V275[航空宇航科学与技术—飞行器设计]