公开(公告)号：US20140100719A1

公开(公告)日：2014-04-10

申请号：US14045510

申请日：2013-10-03

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Julien THIBAULT

IPC: B64C25/46

CPC classification number: B64C25/46 ,  B60T8/1703

Abstract: The invention relates to a braking system architecture for an aircraft having wheels 1 braked by means of respective brakes 2, each brake having a plurality of electromechanical actuators 3a, 3b, the braking system having controllers 8a, 8b for distributing electric power Ps to the actuators 3a, 3b in response to a braking setpoint, each controller 8a, 8b being associated with some of the actuators of any given brake. According to the invention, each controller 8a, 8b has an input Ev for receiving information about the rotary speed of the wheel 1 braked by the actuators associated with said controller, the controller including processor means 13 for modulating the power transmitted to the actuators as a function of the speed of rotation of the wheel in order to provide anti-skid protection.

Abstract translation: 本发明涉及一种用于飞行器的制动系统结构，其具有通过相应的制动器2制动的车轮1，每个制动器具有多个机电致动器3a，3b，该制动系统具有用于将电力Ps分配给致动器的控制器8a，8b 3a，3b响应于制动设定点，每个控制器8a，8b与任何给定制动器的一些致动器相关联。 根据本发明，每个控制器8a，8b具有用于接收关于由与所述控制器相关联的致动器制动的车轮1的转速的信息的输入Ev，所述控制器包括处理器装置13，用于将传递到致动器的功率调制为 功能的轮子旋转速度，以提供防滑保护。