The invention discloses an airplane electro-hydrostatic brake control device and a dynamic control method, and relates to the technical field of brake control systems, the airplane electro-hydrostatic brake control device comprises a controller, a brushless direct current motor, a plunger pump, an energy accumulator, an electromagnetic valve, a safety valve and a hydraulic mechanism; an output shaft of the brushless direct current motor is coaxially connected with the plunger pump and drives the plunger pump to operate, the energy accumulator provides initial pressure for the plunger pump, and the plunger pump is communicated with the hydraulic mechanism through the safety valve and the electromagnetic valve. And the controller performs closed-loop control based on the internal temperature and pressure information of the hydraulic mechanism, the rotating speed information of the brushless direct current motor and the displacement information of the hydraulic mechanism so as to control the electromagnetic valve and the brushless direct current motor to cooperatively drive the hydraulic mechanism. It is guaranteed that the static brake system is switched on when the airplane needs static brake, it is guaranteed that the static brake is not switched on mistakenly when the static brake is not needed, and the safety of the airplane is effectively improved. The takeoff line brake pressure maintaining device is high in efficiency, high in frequency response and capable of maintaining takeoff line brake pressure. And the brake pressure can be quickly and accurately controlled.

    本发明公开了一种飞机电静液刹车控制装置及动态控制方法,涉及刹车控制系统技术领域,包括控制器、无刷直流电机、柱塞泵、储能器、电磁阀、安全阀和液压机构;无刷直流电机输出轴与柱塞泵同轴相连并驱动柱塞泵运转,储能器向柱塞泵提供初始压力,柱塞泵通过安全阀和电磁阀连通液压机构;控制器基于液压机构内部温压信息、无刷直流电机转速信息和液压机构的位移信息进行闭环控制,进而控制电磁阀和无刷直流电机配合驱动液压机构。本发明保证飞机需要静刹车时将静刹车系统接通,在不需要静刹车时,保证静刹车不会误接通,有效提高飞机的安全性。本发明效率高,频响高,可实现起飞线刹车压力保持。实现了对刹车压力的快速、精确控制。


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    Title :

    Aircraft electro-hydrostatic brake control device and dynamic control method


    Additional title:

    一种飞机电静液刹车控制装置及动态控制方法


    Contributors:
    LU JIULI (author) / QING LYUJUN (author)

    Publication date :

    2023-06-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF / B64C AEROPLANES , Flugzeuge



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