FUSELAGE POSITIONING MECHANISM (VERSIONS), AIRCRAFT AND AIRCRAFT BALANCING METHOD (VERSIONS) Russian patent published in 2019 - IPC B64C3/38 B64C1/26 

FIELD: aviation.

SUBSTANCE: aircraft comprises fuselage having lengthwise axis, wing assembly and fuselage positioning mechanism operably connecting fuselage with wing assembly. Versions of the fuselage positioning mechanism are configured to move the fuselage relative to the wing assembly in a longitudinal direction parallel to the longitudinal axis between the maximum front fuselage position and the maximum rear fuselage position. Versions of balancing method characterize aircraft preparation processes using fuselage to flight positioning mechanism. Position of the center of gravity of the aircraft relative to the center of the lifting force is determined. Fuselage can be moved relative to wing assembly with shift of center of gravity in permissible range of distances from center of lift for balancing of aircraft to flight. Fuselage positioning mechanism can be automated to allow fuselage position adjustment during aircraft flight.

EFFECT: group of inventions is aimed at increasing the aircraft effective use capabilities.

15 cl, 16 dwg