Coaxial double-propeller unmanned aerial vehicle, unmanned aerial vehicle set and motor
Coaxial double-propeller unmanned aerial vehicle, unmanned aerial vehicle set and motor
- Neue Suche nach: ZHI LUODAN
- Neue Suche nach: ZHI LUODAN
A coaxial double-paddle unmanned aerial vehicle comprises a vehicle body (10), vehicle arms (20) and a power mechanism (30), the vehicle arms (20) are mechanically coupled with the vehicle body (10), the power mechanism (30) is installed on the vehicle arms (20) and comprises a driving assembly (31), a first paddle assembly (32) and a second paddle assembly (33), and the driving assembly (31) comprises a first installation position (31a) and a second installation position (31b) which are vertically arranged in the vertical direction of the vehicle body. The first paddle assembly (32) is installed at a first installation position (31a) of the driving assembly, the second paddle assembly (33) is installed at a second installation position (31b) of the driving assembly, and fool-proof structures are arranged between the second paddle assembly (33) and the first paddle assembly (32), between the driving assembly (31) and the first paddle assembly (31a) and/or between the driving assembly (31) and the second paddle assembly (33). The first blade assembly (32) can only be installed at the first installation position (31a), and the second blade assembly (33) can only be installed at the second installation position (31b).
一种共轴双桨无人机，包括机身(10)、机臂(20)和动力机构(30)，机臂(20)与机身(10)机械耦合，动力机构(30)安装于机臂(20)，动力机构(30)包括驱动组件(31)、第一桨叶组件(32)和第二桨叶组件(33)，驱动组件(31)包括沿机身垂直方向上下设置的第一安装位(31a)和第二安装位(31b)，第一桨叶组件(32)安装于驱动组件的第一安装位(31a)，第二桨叶组件(33)安装于驱动组件的第二安装位(31b)，第二桨叶组件(33)与第一桨叶组件(32)，驱动组件(31)与第一桨叶组件(31a)之间和/或驱动组件(31)与第二桨叶组件(33)之间设有防呆结构，使得第一桨叶组件(32)只能安装于第一安装位(31a)，第二桨叶组件(33)只能安装于第二安装位(31b)。
Dokumentinformationen
Coaxial double-propeller unmanned aerial vehicle, unmanned aerial vehicle set and motor
共轴双桨无人机、无人机套装及电机
2024-03-05
Patent
Elektronische Ressource
Chinesisch
| IPC: | B64U |
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