FIELD: aviation.
SUBSTANCE: if the aircraft has insufficient path length to ensure braking of the aircraft during take-off and landing, the ends of the adjustable braking cable of the brake device of the fuselage rear part as well as the left and right wings of the aircraft are simultaneously fixed to the surface of the aircraft motion by dowel piles at angles of 20-10° to the surface of the aircraft motion using dowel guns that are controlled from the cockpit, the aircraft is braked at the length of the permissible braking distance. The aircraft is equipped with dowel guns installed in the rear part of the fuselage, as well as under the left and right wings of the aircraft, with the ability to rotate from the starting position from the internal cavities to the working position at angles of 20-10° to the surface of the aircraft, and having dowel piles, cables equipped with motion engagement stops, braking devices.
EFFECT: increased safety in the aircraft motion during take-off and landing.
2 cl, 1 dwg
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Authors
Dates
2017-06-14—Published
2016-07-08—Filed