Patent ID: 11891171
Assignee: nan
Field: Transport (Mechanical engineering)
Classification: CPC B  Y | IPC B

Claim 3:
4. The aircraft wing with tiplet of claim 1, wherein the inner section straight trailing edge and the tiplet section straight trailing edge are respectively cut out before the intersect point at an inner section trailing edge cutout point and at a tiplet section trailing edge cutout point, the inner section trailing edge cutout point and the tiplet section trailing edge cutout point are joined with a transition section trailing edge straight line, whereby the inner section chord at the inner section trailing edge cutout point, the tiplet section chord at the tiplet section trailing edge cutout point, the aircraft wing with tiplet straight leading edge between the inner section chord at the inner section trailing edge cutout point and the tiplet section chord at the tiplet section trailing edge cutout point together with the transition section trailing edge straight line form a transition section of aircraft wing with tiplet, thus the inner section chord at the inner section trailing edge cutout point being a transition section root chord, the tiplet section chord at the tiplet section trailing edge cutout point being a transition section tip chord.