An aircraft braking system includes a brake actuator, a primary hydraulic fluid supply circuit configured to supply pressurized hydraulic fluid to the brake actuator, and a secondary hydraulic fluid supply circuit including a piezoelectric pump configured to supply pressurized hydraulic fluid to the brake actuator.

    本申请涉及一种飞行器制动系统,该飞行器制动系统包括:制动致动器、构造成将加压液压流体供应到制动致动器的主液压流体供应回路、以及包括构造成将加压液压流体供应到制动致动器的压电泵的副液压流体供应回路。


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    Title :

    Aircraft braking system


    Additional title:

    飞行器制动系统


    Contributors:

    Publication date :

    2024-02-20


    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



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