US 12,420,923 B1
Rotary wing-fixed wing convertible morphing aircraft
Xiayang Zhang, Nanjing (CN); Chencheng Gao, Nanjing (CN); Wei Li, Nanjing (CN); Tingjie Mei, Nanjing (CN); and Bin Luo, Nanjing (CN)
Assigned to Nanjing University of Aeronautics and Astronautics, Nanjing (CN)
Filed by Nanjing University of Aeronautics and Astronautics, Nanjing (CN)
Filed on Dec. 27, 2024, as Appl. No. 19/003,015.
Claims priority of application No. 202411174029.1 (CN), filed on Aug. 23, 2024.
Int. Cl. B64C 29/02 (2006.01); B64C 11/30 (2006.01); B64C 11/48 (2006.01)
CPC B64C 29/02 (2013.01) [B64C 11/30 (2013.01); B64C 11/48 (2013.01)] 10 Claims
OG exemplary drawing
 
1. A rotary wing-fixed wing convertible morphing aircraft, comprising:
a fuselage, wherein a tail of the fuselage is provided with a tail-thrust propeller; and
at least two morphing wing structures arranged on the fuselage, wherein each of the at least two morphing wing structures comprises at least two morphing wings, and is rotatable around a central line of the fuselage; each of the at least two morphing wings has an adjustable tilting angle, and comprises a morphing wing body and at least one trailing edge flap which is located at a tail of the morphing wing body and is rotatable relative to the morphing wing body; and the rotary wing-fixed wing convertible morphing aircraft is in a fixed wing configuration layout, or a rotary wing configuration layout.