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

Claim 4:
5. 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 being joined with a trailing edge curved line, the trailing edge curved line tangentially joins the inner section straight trailing edge and the tiplet section straight trailing edge, whereby the inner section straight trailing edge before the inner section trailing edge cutout point, the trailing edge curved line, and the tiplet section straight trailing edge after the tiplet section trailing edge cutout point being the trailing edge of the aircraft wing with tiplet.