FIELD: transport.
SUBSTANCE: invention relates to aircraft landing systems. Proposed device comprises landing strip elevated section. Said elevated section is laid on ramp with sides equipped with motor-driven winch. Two parallel outer curbs are secured on both side of ramp lengthwise axis and diverge to different sides to close at runway end side edges. Curb upper section is composed of inclined tip-up sides. Aircraft speed sensors are arranged between parallel inner curbs. Two extending braking swing gates are activated behind aircraft rear wheel at aircraft stoppage. Swing gates slide in track skids via ramp side openings and are locked between inner and outer curbs to rest thereon, on tracks and brake thrusts secured at the ramp.
EFFECT: safe emergent deceleration of aircraft.
20 dwg
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