US Patent 11332239 Fixed-wing VTOL aerial vehicle

A long-distance drone is disclosed having a canard wing configuration with a cabin attached to a left main wing and a right main wing. There is a left forewing and a right forewing connected together to form a single-piece forewing. There is a left linear support connecting the left forewing to the left main wing, and a right linear support connecting the right forewing to the right main wing. A plurality of propellers is disposed on the left and the right linear supports.