FIELD: transport.
SUBSTANCE: invention relates to light transport aircraft, particularly, to no-run take-off and landing light aircraft. Proposed VTOL comprises take-off-and-sustainer engines, tailplane and tail landing gear arranged at fuselage rear. Tail landing gear allows vertical orientation of fuselage lengthwise axis on ground and is equipped with telescoping shock absorbers. Note here that tail landing gear represents telescopic rods, each hinged to fuselage by one end and to brace by opposite end. Brace incorporates mechanism to vary its length. When in flight, telescopic rods are arranged streamwise due to pulling braces in tailplane and, in landing, said rods are arranged to make trapezoid.
EFFECT: higher safety and payload factor.
1 dwg
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