FIELD: aircraft engineering.
SUBSTANCE: proposed device comprises landing strip elevated section. Landing strip section is laid on overpass with boards. Said overpass is equipped with electrically driven winch and transducers for control over aircraft run speed. Aircraft stopped at overpass, said transducers actuated extending brake thrusts and extending barriers. Said overpass is overlapped by six extending brake thrusts and two extending barriers. Stopped aircraft is locked and towed by electrically driven winch to runway.
EFFECT: smooth and safe deceleration.
10 cl, 29 dwg
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