Patent ID: 11964753
Assignee: DORONI AEROSPACE INC.
Field: Transport (Mechanical engineering)
Classification: CPC B  Y | IPC B

Claim 0:
1. A VTOL aircraft capable of horizontal wing-supported flight, comprising:
a) a fuselage having forward, central, and aft portions;
b) a first pair of airfoils joined to the forward portion of the fuselage;
c) a second pair of airfoils joined to the aft portion of the fuselage;
d) a cockpit integral to the central portion of the fuselage; and
e) at least one vertical thruster fixedly embedded within each one of the airfoils;, wherein, during horizontal flight, laminar flow across the upper surfaces of the airfoils is directed into the vertical thrusters, and laminar flow across the lower surfaces of the airfoils is directed across the exits of the vertical thrusters.