公开(公告)号：US08152247B2

公开(公告)日：2012-04-10

申请号：US12367933

申请日：2009-02-09

Applicant: Emmanuel Colin

Inventor： Emmanuel Colin

IPC: B60T8/78

CPC classification number: B60T8/1703 ,  B60T13/746 ,  B64C25/24 ,  F16D2121/24 ,  F16D2125/40

Abstract: A wheel brake for an aircraft, the brake comprising a support (2) that receives at least one electromechanical actuator (1) fitted with a pusher (8) facing friction elements (3) and movable under drive from an electric motor (6) to apply a braking force selectively against the friction elements. The actuator is non-reversible such that a reaction force applied on the pusher cannot cause the electric motor to turn, and the actuator is associated with elements (30, 31, 32, 33, 34) for selectively switching off an electric power supply to the electric motor, which elements allow power to be delivered to the actuator in normal circumstances, and switch off the power if (a) the measured speed of rotation (wmes) of the electric motor drops below a first predetermined threshold (S1); and (b) the commanded speed of rotation ( ω) of the electric motor drops below a second predetermined threshold (S2).

Abstract translation: 一种用于飞机的车轮制动器，所述制动器包括支撑件（2），所述支撑件（2）容纳至少一个机电致动器（1），所述机电致动器（1）装配有面向摩擦元件（3）的推动器（8）并且可在电动机（6）的驱动下移动到 选择性地对摩擦元件施加制动力。 致动器是不可逆的，使得施加在推动器上的反作用力不能导致电动机转动，并且致动器与用于选择性地关闭电力供应的元件（30,31,32,33,34）相关联， 所述电动机在正常情况下允许动力被传递到所述致动器，并且如果（a）所测量的所述电动机的转速（wmes）低于第一预定阈值（S1），则关闭所述动力。 和（b）电动机的指令旋转速度（ω）下降到第二预定阈值（S2）以下。

公开(公告)号：US20110160975A1

公开(公告)日：2011-06-30

申请号：US12977446

申请日：2010-12-23

Applicant: Stéphane MUDRY ,  Frédéric RAGOT ,  Jean-Baptiste VANEY ,  Emmanuel COLIN

Inventor： Stéphane MUDRY ,  Frédéric RAGOT ,  Jean-Baptiste VANEY ,  Emmanuel COLIN

IPC: B60T8/172

CPC classification number: B64C25/44 ,  B60T7/042 ,  B60T7/045 ,  B60T7/085 ,  B60T7/107 ,  B60T8/1703 ,  B60T13/74 ,  B60T13/741 ,  B60T2201/00 ,  F16D49/00

Abstract: The invention relates to a method of managing parking braking in a braking system for a vehicle fitted with at least one electric brake including at least one electric actuator having a pusher actuated by an electric motor for selectively applying a force against friction elements of the brake, the method comprising the steps of: establishing a series of direct adjustment tables for parking braking, corresponding to braking situations at different energy levels; when applying parking braking, selecting a direct adjustment table corresponding to a braking situation preceding the application of parking braking; and directly adjusting a parking braking force in application with the selected direct adjustment table.

Abstract translation: 本发明涉及一种在车辆制动系统中管理停车制动的方法，所述制动系统包括至少一个电动制动器，该至少一个电动制动器包括至少一个电动致动器，该电动致动器具有由电动机驱动的推动器，用于选择性地对制动器的摩擦元件施加力， 该方法包括以下步骤：对应于不同能量级别的制动情况建立一系列用于停车制动的直接调节表; 当应用停车制动时，选择与应用停车制动之前的制动情况相对应的直接调整表; 并且利用所选择的直接调整表直接调节驻车制动力。

公开(公告)号：US20110155521A1

公开(公告)日：2011-06-30

申请号：US12978159

申请日：2010-12-23

Applicant: Julien THIBAULT ,  Emmanuel COLIN

Inventor： Julien THIBAULT ,  Emmanuel COLIN

IPC: B64C25/44 ,  B64C25/42

CPC classification number: B60T8/1703 ,  B60L7/003 ,  B60T8/885 ,  B60T2270/402 ,  B60T2270/413

Abstract: The invention relates to an asymmetrical electric braking architecture for aircraft, comprising a certain number of electro-mechanical brake actuators (EBAs) for selectively applying a braking force on friction elements in order to slow down rotation of braked wheels, said architecture comprising: a brake control unit (BCU) for acting in normal mode to generate braking setpoint values in response to a braking order; electro-mechanical actuator controllers (EMACs), each including at least one inverter for supplying power to the EBAs in response to the braking setpoint values; at least one emergency brake power and control unit (EBPCU) including at least one inverter for supplying power to some of the EBAs in response to a braking order; and protection means for channeling power supplied by the EMACs or the EBPCU towards the actuators while preventing power from being diverted towards the architecture.

Abstract translation: 本发明涉及一种用于飞行器的不对称电动制动结构，包括一定数量的机电制动致动器（EBAs），用于选择性地对摩擦元件施加制动力以减慢制动轮的旋转，所述结构包括：制动器 控制单元（BCU），用于在正常模式下作用以响应制动顺序产生制动设定值; 机电致动器控制器（EMAC），每个包括至少一个逆变器，用于响应于制动设定点值向EBAs供电; 至少一个紧急制动功率和控制单元（EBPCU），其包括至少一个用于响应于制动顺序向一些所述EBA供电的逆变器; 以及用于将由EMAC或EBPCU提供的电力引向致动器的保护装置，同时防止电力转向架构。

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：US08374764B2

公开(公告)日：2013-02-12

申请号：US12795304

申请日：2010-06-07

Applicant: Emmanuel Colin ,  Julien Thibault ,  Pierre Girod

Inventor： Emmanuel Colin ,  Julien Thibault ,  Pierre Girod

IPC: G06F19/00

CPC classification number: B60T13/741 ,  B60T8/1703

Abstract: The invention relates to a braking system architecture for an aircraft fitted with electromechanical brakes including at least one electromechanical actuator. In accordance with the invention, the architecture comprises at least one proximity unit disposed in the proximity of the brakes at the bottom of the undercarriage and including input/output means for collecting and calibrating at least signals coming from sensors associated with the brakes, and for transmitting the signals as processed in this way to control members for controlling the actuators by means of a communications bus running along the undercarriage, the proximity unit further including control means for controlling the blocking members of the actuators.

Abstract translation: 本发明涉及一种配备有包括至少一个机电致动器的机电制动器的飞行器的制动系统架构。 根据本发明，该结构包括设置在起落架底部的制动器附近的至少一个接近单元，并且包括至少用于收集和校准来自与制动器相关联的传感器的信号的输入/输出装置，并且 将以这种方式处理的信号传送到控制构件，以便通过沿着底架行进的通信总线来控制致动器，该接近单元还包括用于控制致动器的阻挡构件的控制装置。

公开(公告)号：US20090206654A1

公开(公告)日：2009-08-20

申请号：US12367933

申请日：2009-02-09

Applicant: Emmanuel Colin

Inventor： Emmanuel Colin

IPC: B60T8/17

CPC classification number: B60T8/1703 ,  B60T13/746 ,  B64C25/24 ,  F16D2121/24 ,  F16D2125/40

Abstract: The invention relates to a wheel brake for a vehicle, in particular for an aircraft, the brake comprising a support (2) that receives at least one electromechanical actuator (1) fitted with a pusher (8) facing friction elements (3) and movable under drive from an electric motor (6) to apply a braking force selectively against the friction elements. In accordance with the invention, the actuator is non-reversible such that a reaction force applied on the pusher cannot cause the electric motor to turn, and the actuator is associated with means (30, 31, 32, 33, 34) for selectively switching off an electric power supply to the electric motor, which means allow power to be delivered to the actuator in normal circumstances, and switch off said power if: the measured speed of rotation (ωmes) of the electric motor drops below a first predetermined threshold (S1); and the commanded speed of rotation ( ω) of the electric motor drops below a second predetermined threshold (S2).

Abstract translation: 本发明涉及一种用于车辆，特别是用于飞行器的车轮制动器，该制动器包括支撑件（2），所述支撑件（2）容纳至少一个机电致动器（1），所述机电致动器（1）装配有面向摩擦元件（3）的推动器（8） 在来自电动机（6）的驱动下，选择性地对摩擦元件施加制动力。 根据本发明，致动器是不可逆的，使得施加在推动器上的反作用力不能使电动机转动，并且致动器与用于选择性地切换的装置（30,31,32,33,34）相关联 断开对电动机的电力供应，这意味着在正常情况下允许动力被传递到致动器，并且如果：所测量的电动机的转速（ω）下降到第一预定阈值以下，则关闭所述功率 S1）; 并且电动马达的命令旋转速度（ omega）下降到第二预定阈值以下（S2）。

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：US07553536B1

公开(公告)日：2009-06-30

申请号：US09498363

申请日：2000-02-04

Applicant: Yves Naoumenko ,  Emmanuel Colin

Inventor： Yves Naoumenko ,  Emmanuel Colin

IPC: B32B23/02 ,  B32B5/16 ,  B32B27/32 ,  B32B27/40

CPC classification number: B32B17/10761 ,  B32B17/10018 ,  B32B17/10036 ,  B32B17/10293 ,  B32B17/10366 ,  B32B17/1077 ,  B32B27/36 ,  B32B2369/00 ,  F41H5/0407 ,  Y10T428/24777 ,  Y10T428/24802 ,  Y10T428/24876 ,  Y10T428/31565 ,  Y10T428/31736

Abstract: A laminated glazing includes at least one sheet (1) and a second sheet (2) bound to each other by an intercalated adhesive layer (3). The first sheet (1) projects beyond the second sheet (2) to form an exposed edge. The intercalated adhesive layer (3) extends over an exposed portion of the edge of the first sheet (1), and the edge of the intercalated adhesive layer (3) is at least in part covered by an intermediate element (4) suited to bond between the glazing or its constitutive elements (3) and on the body (5) through the intermediary of a cement element. This glazing has use as an automobile windshield with high crash test resistance.

Abstract translation: 层压玻璃包括至少一个片（1）和通过插层的粘合剂层（3）彼此结合的第二片（2）。 第一片（1）突出超过第二片（2）以形成暴露的边缘。 插入的粘合剂层（3）在第一片材（1）的边缘的暴露部分上延伸，并且插入的粘合剂层（3）的边缘至少部分地被适合于键合的中间元件（4）覆盖 在玻璃窗或其构成元件（3）之间和通过水泥元件的中间在主体（5）之间。 这种玻璃用作具有高抗碰撞试验阻力的汽车挡风玻璃。

公开(公告)号：US08733847B2

公开(公告)日：2014-05-27

申请号：US12978159

申请日：2010-12-23

Applicant: Julien Thibault ,  Emmanuel Colin

Inventor： Julien Thibault ,  Emmanuel Colin

IPC: B60T13/00 ,  B60T8/88

CPC classification number: B60T8/1703 ,  B60L7/003 ,  B60T8/885 ,  B60T2270/402 ,  B60T2270/413

Abstract: An asymmetrical electric braking architecture for aircraft, having plural electro-mechanical brake actuators (EBAs) for selectively applying a braking force on friction elements of braked wheels. The architecture comprises (1) a brake control unit (BCU) for acting in normal mode to generate braking setpoint values in response to a braking order, (2) electro-mechanical actuator controllers (EMACs), each including at least one inverter for supplying power to the EBAs in response to the braking setpoint values, (3) at least one emergency brake power and control unit (EBPCU) including at least one inverter for supplying power to some of the EBAs in response to a braking order; and (4) protection means for channeling power supplied by the EMACs or the EBPCU towards the actuators while preventing power from being diverted towards the architecture.

Abstract translation: 一种用于飞行器的不对称电动制动结构，具有用于选择性地对制动轮的摩擦元件施加制动力的多个机电制动致动器（EBAs）。 该架构包括（1）用于在正常模式下作用以响应于制动顺序产生制动设定值的制动控制单元（BCU），（2）机电致动器控制器（EMAC），每个包括至少一个用于供应的逆变器 （3）至少一个紧急制动功率和控制单元（EBPCU），其包括至少一个逆变器，用于响应于制动顺序向一些EBA供电; 和（4）用于将由EMAC或EBPCU提供的电力引向致动器的保护装置，同时防止电力转向架构。

公开(公告)号：US09169006B2

公开(公告)日：2015-10-27

申请号：US12977446

申请日：2010-12-23

Applicant: Stéphane Mudry ,  Frédéric Ragot ,  Jean-Baptiste Vaney ,  Emmanuel Colin

Inventor： Stéphane Mudry ,  Frédéric Ragot ,  Jean-Baptiste Vaney ,  Emmanuel Colin

IPC: B60T8/172 ,  B64C25/44 ,  B60T7/04 ,  B60T7/08 ,  B60T7/10 ,  B60T8/17 ,  B60T13/74

CPC classification number: B64C25/44 ,  B60T7/042 ,  B60T7/045 ,  B60T7/085 ,  B60T7/107 ,  B60T8/1703 ,  B60T13/74 ,  B60T13/741 ,  B60T2201/00 ,  F16D49/00

Abstract: The invention relates to a method of managing parking braking in a braking system for a vehicle fitted with at least one electric brake including at least one electric actuator having a pusher actuated by an electric motor for selectively applying a force against friction elements of the brake, the method comprising the steps of: establishing a series of direct adjustment tables for parking braking, corresponding to braking situations at different energy levels; when applying parking braking, selecting a direct adjustment table corresponding to a braking situation preceding the application of parking braking; and directly adjusting a parking braking force in application with the selected direct adjustment table.

Abstract translation: 本发明涉及一种在车辆制动系统中管理停车制动的方法，所述制动系统包括至少一个电动制动器，该至少一个电动制动器包括至少一个电动致动器，该电动致动器具有由电动机驱动的推动器，用于选择性地对制动器摩擦元件施加力， 该方法包括以下步骤：对应于不同能量级别的制动情况建立一系列用于停车制动的直接调节表; 当应用停车制动时，选择与应用停车制动之前的制动情况相对应的直接调整表; 并且利用所选择的直接调整表直接调节驻车制动力。