摘要
本文研究的课题所选用的是四轴飞行器,其螺旋桨与电机直接相连而且是在同一水平高度上对称分布,且螺旋桨的形状尺寸完全一样,螺旋桨支架端的电机为整个飞行器提供稳定运行的能量。相邻的螺旋桨旋转方向采用反向结构,这种结构设计能均衡飞行器运行时产生的力矩,避免出现旋翼在空中打转的情况。
In this paper, a four-axis aircraft was selected. The propeller was directly connected to the motor and sym- metrically distributed at the same level. The shape and size of the propeller were exactly the same. The motor at the propeller support provided the stable operation energy for the whole aircraft. The reverse direction was applied to the rotation direction of adjacent propellers. This kind of structure design could balance the torque produced by the aircraft when it was running, avoid the rotator rotating in the air.
作者
张涛然
ZHANG Taoran(Institute of Mobile Communication,Chongqing University of Posts and Telecommunications,Chongqing 401520)
出处
《河南科技》
2018年第26期122-123,共2页
Henan Science and Technology
基金
重庆市高等教育教学改革研究项目(183002)
关键词
多旋翼飞行器
旋翼
应急装置
飞行控制
multi rotor aircraft
rotor
emergency device
flight control