Free wing multirotor transitional S/VTOL aircraft

An aircraft comprising:

• an airframe comprising two or more spars positioned fore and aft on the airframe and extending laterally;
• free wings having control surfaces are positioned on the spars such that they rotate about the spar on a spar-centered axis of rotation;
• at least three rotatably from horizontal to vertical thrust producing rotors located at outermost ends of each one of the spars;
• wherein the free wings are mechanically coupled front-to-back and side-to-side with each other such that a rotation induced in one free wing affects all free wings, and a center of mass of each free wing is located at a distance aft of the spar-centered axis of rotation, and
• the free wings rotate about their respective spar without physical or mechanical coupling to a fuselage and the rotatably thrust producing rotors.

An aircraft comprising:

• a fuselage comprising a vertical stabilizer, two sides, a floor, and at least two spars coupled thereto and extending laterally therefrom;
• four rotatably from horizontal to vertical thrust producing rotors with one positioned on each spar;
• free wings having control surfaces positioned on each spar having a spar-centered center of rotation, coupled front-to-back and side-to-side with one another and without physical or mechanical coupling to and between the fuselage and the rotatably thrust producing rotors;
• wherein a center of mass of each free wing is located aft of the spar-centered center of rotation of the free wing, and each of the four rotatably thrust producing rotors is located outside of each free wing.