FIELD: aviation.SUBSTANCE: invention relates to aircraft armament systems with forced catapult separation. Method of forced release - ejection of cargo consists in the fact that linear accelerations on body, front and rear rods of hydraulic pushers (7.1, 7.2) are measured, preset values of kinematic parameters of movement of load center of mass and around center of mass are calculated depending on flight mode, current values of kinematic parameters of cargo movement are calculated from measured overloads. Control signals of hydraulic distributors (5.1, 5.2) of front and rear hydraulic pushers are formed in two stages. At the first stage control signals are generated by difference of preset and current values of linear and angular accelerations, that is control of ejection is adaptive to external factors. At the second stage, in the remaining time before cargo separation, control signals are generated by difference of preset and current values of linear and angular velocities, that is control of catapulting is adaptive to internal factors.EFFECT: invention improves quality of cargo release, eliminates possibility of emergency situation.2 cl, 1 dwg


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    Title :

    Адаптивный способ и устройство принудительного сброса - катапультирования груза


    Publication date :

    2019-04-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT