Patent ID: 8702031

Claim:
An aircraft ( 1 ) comprising: two fuselages ( 2 ) spaced apart from one another, each of which having a stabilizer ( 12 ) extending from an aft portion; a center wing ( 3 ) being the only structure connecting the two fuselages; wherein said center wing has a rotor ( 4 ) and at least one engine ( 6 ) attached to is such that said center wing, rotor, and at least one engine are placed near a longitudinal center of gravity of the aircraft; wherein said center wing contains split ailerons ( 7 ) that counter rotor torque by deflecting in opposite directions a down-wash created by said rotor; wherein said center wing, rotor, and at least one engine can be rotated in unison with respect to said two fuselages from a vertical flight position to a horizontal flight position and back while said ailerons counter the rotor torque; and an outboard fixed wing attached to an outboard portion of each fuselage.