Patent ID: 9567076
Date: 2017-02-14
CPC Classifications: B29C,B29K,B64C

Claim:
1. A fuselage of an unmanned aerial vehicle, wherein 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 middle spacing plate is arranged in the receiving space and divides the receiving space into an upper cavity and a lower cavity; 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.