The invention discloses a multi-rotor-wing aircraft stander. The multi-rotor-wing aircraft stander comprises a machine body and a cantilever, and is characterized in that when the stander is horizontally arranged, the outer contour of the cross section of the cantilever is of a polygon with an angle facing upwards; a biosector of an upward-facing angle is perpendicular to the horizontal plane; in order to prevent the stander from cutting hands, the polygon is a round-angle polygon; the polygon is a regular polygon; the polygon is an odd-number polygon; the odd-number polygon is a triangle or a pentagon. The multi-rotor-wing aircraft stander has beneficial effect that the air resistance of an aircraft in the flying process can be reduced.
Multi-rotor-wing aircraft stander
2015-05-27
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
HYBRID-POWER SYSTEM FOR MULTI-ROTOR-WING AIRCRAFT AND MULTI-ROTOR-WING AIRCRAFT
European Patent Office | 2021
|HYBRID-POWER SYSTEM FOR MULTI-ROTOR-WING AIRCRAFT AND MULTI-ROTOR-WING AIRCRAFT
European Patent Office | 2021
|