发明名称 Architecture of an aircraft braking system
摘要 The structure has a power module (7) for sending phase currents to electromechanical actuators (3) such that the actuators exert braking efforts. A control module (8) controls the power module in response to a braking command such that the appropriate phase currents are sent to the actuators to increase the desired braking efforts. A power supply box (20) comprises a high-voltage converter (21) generating high voltages for providing high power to the power module. The box comprises a low-voltage converter (22) generating low voltages for supplying low voltages to the control module.
申请公布号 EP2508399(B1) 申请公布日期 2016.08.24
申请号 EP20120163043 申请日期 2012.04.03
申请人 MESSIER-BUGATTI-DOWTY 发明人 THIBAULT, JULIEN;MUDRY, STÉPHANE;ONFROY, DOMINIQUE
分类号 B60T8/17;B60T8/32 主分类号 B60T8/17
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