The present disclosure provides a fuselage of an unmanned aerial vehicle. The fuselage comprises an upper plate, a lower plate opposite to the upper plate, a connecting plate, and a middle spacing plate; the connecting plate is connected between the upper plate and the lower plate; the upper plate, the lower plate, and the connecting plate are enclosed to define a receiving space; the upper plate, the lower plate, the connecting plate, and the middle spacing plate are integrally formed; the upper cavity is located between the middle spacing plate and the upper plate, and the lower cavity is located between the middle spacing plate and the lower plate; and a first mounting opening is defined in the upper plate allowing a component to enter the upper cavity, and a second mounting opening is defined in the lower plate allowing a component to enter the lower cavity. The present disclosure further provides a method for manufacturing the fuselage of the unmanned aerial vehicle and the unmanned aerial vehicle. The present disclosure can reduce the weight of the unmanned aerial vehicle, improve the flying performance of the unmanned aerial vehicle, and facilitate the maintenance and replacement of the components of the unmanned aerial vehicle.
UNMANNED AERIAL VEHICLE, UNMANNED AERIAL VEHICLE BODY, AND MANUFACTURING METHOD THEREFOR
UNBEMANNTES LUFTFAHRZEUG, GEHÄUSE FÜR DAS UNBEMANNTE LUFTFAHRZEUG UND HERSTELLUNGSVERFAHREN DAFÜR
VÉHICULE AÉRIEN SANS PILOTE, CORPS DE VÉHICULE AÉRIEN SANS PILOTE ET SON PROCÉDÉ DE FABRICATION
2016-04-13
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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