Co-rotating vertical take-off and landing membrane wing aircraft

The utility model discloses a co-rotating vertical take-off and landing film wing aircraft which comprises an aircraft body, at least two rows of power wing spars are rotationally connected to the aircraft body, and propellers are installed on each row of power wing spars. Membrane wings rotationally connected with the fuselage are arranged between the adjacent power wing spars; folding angle adjusting mechanisms are arranged in the middles of the membrane wings; and the fuselage is provided with a linkage operation device which enables the membrane wings and the power wing spars to synchronously rotate relative to the fuselage. The co-rotating vertical take-off and landing membrane-wing aircraft provided by the utility model has the advantages that the operation of switching between a take-off and landing state and a flying state is simple, the speed range is large, and the energy consumption is low. 本实用新型公开了一种共转垂直起降膜翼飞机，包括机身，所述机身上转动连接有至少两排动力翼梁，各排动力翼梁上安装有螺旋桨；相邻动力翼梁之间设有与机身转动连接的膜翼；膜翼中部设有折叠角度调节机构；机身上设有使膜翼与动力翼梁相