Aircraft with its fuselage suspended under the wing

An aircraft with which a marker aircraft is linked, determined by a longitudinal direction X oriented positively toward the front of the plane, a vertical direction Z perpendicular to direction X and oriented positively toward the bottom of the aircraft and a lateral direction Y perpendicular to the plane defined by the directions X and Z and oriented positively toward the right of the aircraft displays conventionally a fuselage, a wing affixed to the fuselage in an upper part and in a central part of the fuselage along the longitudinal axis X, a set of airfoils situated behind the wing and propulsion engines mounted on the wing, characterized in that the wing, the set of airfoils and the propulsion engines are part of a structural unit, said air propulsion unit being independent of the fuselage;

• the aero-propulsive unit is connected to the fuselage by a connection system permitting the controlled modification in flight of the position of the air propulsion unit relative to the fuselage in the three directions X, Y and Z of the reference aircraft and in rotation about the three directions X, Y and Z.