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。
Aircraft braking system
飞行器制动系统
2024-02-20
Patent
Electronic Resource
Chinese
IPC: | B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF |
Aircraft braking control system, undercarriage, aircraft and aircraft braking method
European Patent Office | 2022
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