无人机倾斜式双旋翼气动特征分析  

Analysis of Aerodynamic Characteristics of Tilt Twin Rotor of UAV

作　　者：刘荣豪 李哲伦 李广伟 Liu Ronghao;Li Zhelun;Li Guangwei(Department of UAV,Automation Research Institute Co.,Ltd.of China South Industries Group Corporation,Mianyang 621000,China;Research and Development Department,No.208 Research Institute of China Ordnance Industries,Beijing 102202,China;PLA Presentation Office in Guangyuan District,PLA Representation Bureau of Army Equipment Department in Chongqing,guangyuan 628017,China)

机构地区：[1]中国兵器装备集团自动化研究所有限公司无人机事业部,四川绵阳621000 [2]中国兵器工业第二〇八研究所科研发展部,北京102202 [3]陆军装备部驻重庆地区军事代表局驻广元地区军事代表室,四川广元628017

出　　处：《兵工自动化》2025年第4期101-103,共3页Ordnance Industry Automation

摘　　要：为提升多旋翼无人机抗风性能,对倾斜式双旋翼的气动特性进行分析。通过分析桨盘倾角对同轴非共轴形式布局的影响,螺旋桨与电机座之间采用一定安装角倾斜安装,以增大偏航控制力矩,倾斜式的桨盘设计使每个旋翼具备多个旋转自由度,能够有效地纠正姿态,提高无人机的稳态性能。对不同倾角的双旋翼进行了试验和计算流体力学(computational fluid dynamics,CFD)数值模拟。结果表明:该研究能为倾斜式多旋翼无人机提供设计支撑。In order to improve the anti-wind performance of multi-rotor UAV,the aerodynamic characteristics of tilt-rotor were analyzed.By analyzing the influence of the rotor disk inclination angle on the coaxial and non-coaxial configuration of the UAV,a certain installation angle is adopted between the propeller and the motor base to increase the yaw control moment,and the inclined rotor disk design enables each rotor to have multiple rotational degrees of freedom,which can effectively correct the attitude and improve the steady-state performance of the UAV.Experiments and computational fluid dynamics(CFD)numerical simulations were carried out on twin rotors with different pitch angles.The results show that the research can provide design support for the tilting multi-rotor UAV.

关 键 词：旋翼无人机 共轴 旋翼倾角 气动性能 

分 类 号：V279[航空宇航科学与技术—飞行器设计]