AIRCRAFT Russian patent published in 2006 - IPC B64C39/04 

FIELD: aircraft manufacture.

SUBSTANCE: proposed aircraft has fuselage with tail unit in form of stabilizer with elevator and two end fins with rudder, wing, engine and landing gear. Aircraft is also provided with additional fuselages which are located in parallel and symmetrically relative to longitudinal axis; these fuselages are secured on upper surface of root section of each wing outer panel connected by means of coupling members with main fuselage. Secured to lower surface of tail section along longitudinal axis of main fuselage is fin with rudder and rear support. Cavity of each additional fuselage is communicated with cavity of main fuselage by means of passage of coupling members. Leading and trailing edges of wing outer panels and stabilizer are made in form of conchoid curve. Stabilizer is connected with tail section of each fuselage. Coupling members are made in form of flanges and adapter.

EFFECT: extended capabilities.

5 dwg