Patent ID: 11401029

Abstract:
An aircraft impeller (001) and an aircraft, relating to the field of aircraft drive components, the aircraft impeller (001) including a frame body (100) and a rotating wheel part (200); the frame body (100) includes a mounting groove (130), the rotating wheel part (200) being fixedly arranged in the mounting groove (130); the mounting groove (130) has an axial centre line (105); the mounting groove (130) also has an open face and a bottom face (131) arranged opposite to one another; the rotating wheel part (200) includes at least one vane (210) distributed around the axial centre line (105), the vane (210) including a windward face (211); at the connecting point of the windward face (211) and the open face, the angle of the tangent plane of the windward face (211) and the open face is an acute angle.