CPC B64C 5/02 (2013.01) [B64C 3/10 (2013.01); B64C 5/06 (2013.01); B64C 9/00 (2013.01); B64C 39/024 (2013.01); B64C 39/12 (2013.01); B64U 10/25 (2023.01); B64U 20/10 (2023.01)] | 20 Claims |
1. An aircraft apparatus, comprising:
a tubular fuselage boom having a proximal end and a distal end;
a wing coupled to the fuselage boom at a proximal end of the fuselage boom, wherein the wing comprises a port outboard wing section and a starboard outboard wing section;
a servo horn slidably coupled to a stabilizer to slidably receive and detachably couple a servo arm to the stabilizer;
wherein each of the port outboard wing section and the starboard outboard wing section comprise curved leading edges of varying radii; and
wherein each of the port outboard wing section and the starboard outboard wing section comprise curved trailing edges of varying radii.
|