公开(公告)号：US08688341B2

公开(公告)日：2014-04-01

申请号：US13583814

申请日：2011-03-11

Applicant: Julien Thibault ,  Emmanuel Colin ,  Stephane Mudry

Inventor： Julien Thibault ,  Emmanuel Colin ,  Stephane Mudry

IPC: G06G7/00

CPC classification number: B60T8/1703

Abstract: A braking system for an aircraft with electric brakes comprising plural electromechanical actuators (2). The system comprises a braking control unit (20) delivering a normal braking setpoint (21) for one or more controllers (10) of the actuators, and selection logic (15) for causing the braking system to operate in a plurality of modes. The system includes: a normal braking mode where the control unit generates a normal braking setpoint (21) for the controller(s); an ultimate braking mode, having priority over the normal braking mode, being responsive to a parking control member, and controlling actuators to respond to the actuation of the parking control member; and a parking braking mode, applied in response to the parking control member and only if the aircraft is stationary, in which the actuators are controlled to apply a force in response to the parking control member being actuated and are then blocked in position.

Abstract translation: 一种具有电动制动器的飞机的制动系统，包括多个机电致动器（2）。 该系统包括为致动器的一个或多个控制器（10）提供正常制动设定点（21）的制动控制单元（20），以及用于使制动系统以多种模式操作的选择逻辑（15）。 该系统包括：正常制动模式，其中控制单元产生用于控制器的正常制动设定值（21）; 优先于正常制动模式的极限制动模式，响应于停车控制构件，并且控制致动器以响应停车控制构件的致动; 以及驻车制动模式，其响应于停车控制构件而应用，并且仅当飞行器处于静止状态时，其中致动器被控制以响应于停车控制构件被致动而施加力并且然后被阻挡就位。

公开(公告)号：US20130006447A1

公开(公告)日：2013-01-03

申请号：US13583814

申请日：2011-03-11

Applicant: Julien Thibault ,  Emmanuel Colin ,  Stephane Mudry

Inventor： Julien Thibault ,  Emmanuel Colin ,  Stephane Mudry

IPC: B64C19/00

CPC classification number: B60T8/1703

Abstract: A braking system for an aircraft with electric brakes comprising plural electromechanical actuators (2). The system comprises a braking control unit (20) delivering a normal braking setpoint (21) for one or more controllers (10) of the actuators, and selection means (15) for causing the braking system to operate in a plurality of modes. The system includes: a normal braking mode where the control unit generates a normal braking setpoint (21) for the controller(s); an ultimate braking mode, having priority over the normal braking mode, being responsive to a parking control member, and controlling actuators to respond to the actuation of the parking control member; and a parking braking mode, applied in response to the parking control member and only if the aircraft is stationary, in which the actuators are controlled to apply a force in response to the parking control member being actuated and are then blocked in position.

Abstract translation: 一种具有电动制动器的飞机的制动系统，包括多个机电致动器（2）。 该系统包括为致动器的一个或多个控制器（10）提供正常制动设定点（21）的制动控制单元（20），以及用于使制动系统以多种模式操作的选择装置（15）。 该系统包括：正常制动模式，其中控制单元产生用于控制器的正常制动设定值（21）; 优先于正常制动模式的极限制动模式，响应于停车控制构件，并且控制致动器以响应停车控制构件的致动; 以及驻车制动模式，其响应于停车控制构件而应用，并且仅当飞行器处于静止状态时，其中致动器被控制以响应于停车控制构件被致动而施加力并且然后被阻挡就位。

公开(公告)号：US20110079471A1

公开(公告)日：2011-04-07

申请号：US12996280

申请日：2009-06-03

Applicant: Emmanuel Colin ,  Julien Thibault ,  Stephane Mudry

Inventor： Emmanuel Colin ,  Julien Thibault ,  Stephane Mudry

IPC: B64C25/44 ,  G06F19/00 ,  B60T8/17 ,  B64C25/42

CPC classification number: B64C25/42 ,  B60T8/00 ,  B60T8/1703 ,  B60T8/321 ,  B60T13/741 ,  B60T17/221 ,  B60T2270/402

Abstract: The invention relates to an aircraft braking circuit having brakes with electromechanical actuators for braking wheels located at the bottom end of at least one undercarriage. In accordance with the invention, a remote unit is located at the bottom of the undercarriage close to the actuators and connected to a certain number of said actuators, the remote unit receiving a power supply via a power supply cable going down along the undercarriage, and having as many controlled switches as connected actuators for selectively powering blocking members fitted to the connected actuators, the switches being controlled independently of one another by software parking orders generated by a control unit and passing via a single communications bus going down along the undercarriage to the remote unit.

Abstract translation: 本发明涉及一种具有制动器的制动器，其具有用于位于至少一个起落架底端的制动轮的机电致动器。 根据本发明，远程单元位于起落架底部靠近致动器并连接到一定数量的所述致动器，远程单元经由沿起落架向下运动的电源电缆接收电源，以及 具有与连接的致动器一样多的受控开关作为连接的致动器，用于选择性地为安装到所连接的致动器的阻挡构件提供动力，所述开关由控制单元产生的软件停车指令彼此独立地控制，并且经由沿着起落架向下运行的单个通信总线通过 远程单元。