Amphibious Cargo Carrying UAV
An amphibious cargo carrying unmanned aerial vehicle (UAV) having a fuselage, two wings and two frames, in which a cargo hold is arranged at the lower end of the fuselage, the cargo hold is provided with a cargo chamber for cargo carrying, and the cargo hold can touch the water surface at the same time. When taking off or landing on the water surface, the hollow structure of the cargo chamber can provide additional buoyancy. The two wings are symmetrically arranged on both sides of the fuselage, the two frames are correspondingly arranged on the two wings, and the buoyancy parts can be detachably arranged on the two frames to provide buoyancy.
1 . An amphibious cargo carrying UAV (unmanned aerial vehicle), which is characterized by comprising:
a fuselage ( 1 ), a cargo hold ( 11 ) is arranged at the lower end of the fuselage ( 1 ), the cargo hold ( 11 ) is provided with a cargo chamber, and the cargo hold ( 11 ) can touch the water surface to provide buoyancy for the fuselage ( 1 );
two wings ( 2 ), which are symmetrically arranged on both sides of the fuselage ( 1 );
two frames ( 3 ), which are correspondingly arranged on the two wings, and can be detachably arranged with buoyancy parts ( 4 ).
2 . The amphibious cargo carrying UAV according to claim 1 , which is characterized in that the frame ( 3 ) has a first end ( 31 ) and a second end ( 32 ), the buoyancy parts ( 4 ) include a first buoyancy part ( 41 ) and a second buoyancy part ( 42 ), and the first buoyancy part ( 41 ) is arranged at the first end ( 31 ) of the frame ( 3 ), and the second buoyancy part ( 42 ) is arranged at the second end ( 32 ) of the frame ( 3 ).
3 . The amphibious cargo carrying UAV according to claim 2 , which is characterized in that the first end ( 31 ) of the frame ( 3 ) is provided with a landing gear ( 5 ), and the first buoyancy part ( 41 ) is arranged on the landing gear ( 5 ).
4 . The amphibious cargo carrying UAV according to claim 3 , which is characterized in that the first buoyancy part ( 41 ) is provided with a first socket, and the landing gear ( 5 ) is inserted into the first socket.
5 . The amphibious cargo carrying UAV according to claim 2 , which is characterized in that the second end ( 32 ) of the frame ( 3 ) is provided with a vertical tail ( 6 ), and the second buoyancy part ( 42 ) is arranged on the vertical tail ( 6 ).
6 . The amphibious cargo carrying UAV according to claim 5 , which is characterized in that the second buoyancy part ( 42 ) is provided with a second socket, and the vertical tail ( 6 ) is inserted into the second socket.
7 . The amphibious cargo carrying UAV according to claim 2 , which is characterized in that the first buoyancy part ( 41 ) and the second buoyancy part ( 42 ) are of hollow structure.
8 . The amphibious cargo carrying UAV according to claim 1 , which is characterized in that a buckle is arranged on the cargo hold ( 11 ), and the cargo hold ( 11 ) connects to the fuselage ( 1 ) through the detachable buckle.
9 . The amphibious cargo carrying UAV according to claim 1 , which is characterized in that a plurality of rotors ( 7 ) are arranged on the fuselage ( 1 ).
10 . The amphibious cargo carrying UAV according to claim 1 , which is characterized in that a speed sensor is arranged on the fuselage ( 1 ).