| 摘要 |
FIELD: combined flying vehicles at high level of safety. SUBSTANCE: proposed flying vehicle has fuselage, landing gear, power plant, controls and wing with movable part which includes two double-blade rotors over wing tips and units for securing them relative to wing. These units blocks rotation of rotors in cruising mode and at parking. Vertical thrust propeller and solid-fuel landing decelerators are also provided. Rotors are provided with braking units for control of their twisting at unlocking in transient modes. EFFECT: reduced instability in transient modes; reduced landing speed; possibility of performing emergency vertical landing. 1 dwg |
