Patent ID: 11873086
Assignee: nan
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 0:
1. A variable-sweep wing aerial vehicle adapted for airplane horizontal flight and VTOL flight comprising:
a longitudinal extended fuselage;
a pair of swiveling canards extended transverse from opposed sides of the fuselage;
a vertical stabilizer extended vertical from the fuselage;
a rear ducted fan secured to the fuselage;
a variable-sweep wing secured to the fuselage, said variable-sweep wing comprising:
a port side wing structure, said port side wing structure comprising:
a port side upper wing;
a port side lower wing; and
a port side pylon joined to the distal tip of said port side upper wing and said port side lower wing; and

a starboard side wing structure, said starboard side wing structure comprising:
a starboard side upper wing;
a starboard side lower wing; and
a starboard side pylon joined to the distal tip of said starboard side upper wing and said starboard side lower wing;

a plurality of ducted fans secured on the upper surface along the span of said port side upper wing;
a plurality of ducted fans secured on the upper surface along the span of said port side lower wing;
a plurality of ducted fans secured on the upper surface along the span of said starboard side upper wing;
a plurality of ducted fans secured on the upper surface along the span of said starboard side lower wing;
a blown flap secured to the trailing edge of said port side upper wing;
a blown flap secured to the trailing edge of said port side lower wing;
a blown flap secured to the trailing edge of said starboard side upper wing; and
a blown flap secured to the trailing edge of said starboard side lower wing.