A multi-rotor device having an angled rotor is disclosed. In various embodiments, a multi-rotor device as disclosed herein includes a fuselage and a plurality of rotors. At least some of the rotors are disposed on opposite sides of the fuselage and each oriented at a corresponding angle with respect to a substantially horizontal plane of the aircraft, said angle having a magnitude such that the plane of rotation of the rotors does not intersect at least a critical portion of the fuselage.
公开一种具有带角度旋翼的多旋翼器。在各种实施例中,如本文中所公开的多旋翼器包括机身以及多个旋翼。该旋翼中的至少一些设置在机身的相对侧上并且各自相对于飞行器的大致水平平面以对应角度取向,所述角度具有使得旋翼的旋转平面不与机身的至少一关键部分相交的量值。
Multi-rotor device with angular rotors
具有带角度旋翼的多旋翼器
2022-08-09
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |