SYSTEM FOR CONTROL OF FLYING VEHICLE BRAKING AT DECK LANDING Russian patent published in 1995 - IPC

FIELD: aeronautical engineering. SUBSTANCE: system is provided with braking mechanism of arresting hooks 43, cross-deck pendant 42, power cut-in unit 38, second electrohydraulic braking drive, two strain gauges 24 and 25, two amplifiers 26 and 27, adder 37 and three comparators 28-30. Throttle cock control device is made in form of delay unit 31, NOT gate 32, AND gate 33, electrohydraulic drive of throttle cock 34 and adder 35. Wheel braking control unit 12 consists of four adders 13-16, three AND gates 9-11, pulse generator 20, switch element 19, integrator 18, differentiating unit 17, signal shaper corresponding to speed of loose wheel 21 and two relay units 22 and 23, braking arrestment mechanism is made in form of two symmetrical arresting hooks 44 and 45 fastened by common axle, hydraulic cylinder 41 for extension of arresting hooks and oscillation damper 40. EFFECT: enhanced probability of deck landing of flying vehicle under adverse-weather conditions through bringing it to axis of landing area. 1 dwg