Wing structure of fixed-wing vertical take-off and landing electric aircraft and aircraft

The utility model discloses a wing structure of a fixed wing vertical take-off and landing electric aircraft, which comprises a skin, a plurality of wing rib plates, tubular beams and support rods, through holes with the same number are formed in the wing rib plates, the tubular beams penetrate through the through holes to support the wing rib plates, the skin covers and wraps the wing rib plates,and the tubular beams are connected with the tubular beams through the through holes. Reinforcing sheets are arranged on two of the plurality of wing rib plates, the supporting rod is fixedly connected with the reinforcing sheets through metal joints, and motor mounting seats are arranged at two ends of the supporting rod and used for mounting driving motors; the aircraft has the advantages of simplifying the aircraft wing structure, reducing the self-weight of the aircraft and improving the mounting efficiency of the driving motor. 本实用新型公开了一种固定翼垂直起降电动飞机的机翼结构，所述蒙皮、多个翼肋肋板、管梁和撑杆，多个所述翼肋肋板上设置有数量相同的通孔，所述管梁穿过通孔支撑翼肋肋板，所述蒙皮覆