公开(公告)号：US20150275992A1

公开(公告)日：2015-10-01

申请号：US14645792

申请日：2015-03-12

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Vincent GONZALES ,  Jacques BUSSIERES

IPC: F16D65/58 ,  B64C25/44 ,  F16D55/24

CPC classification number: F16D65/58 ,  B64C25/42 ,  B64C25/44 ,  F16D55/24 ,  F16D55/40 ,  F16D65/186 ,  F16D65/543 ,  F16D2121/04

Abstract: A brake actuator comprising a sleeve (1), a piston (3) sealingly slidably mounted in the sleeve to apply a braking force, the piston being provided with an internal cage (21), and a wear compensating device (10) which defines a retracted position of the piston in the sleeve by means of an axially mobile stop which is able to be moved forward by the piston during the application of a braking force and/in frictional relationship with a fixed part (12) of the wear compensating device attached to the sleeve. The mobile stop comprises a radially deformable bushing (16) which cooperates with an olive (15) which is attached to a distal end of the fixed part of the wear compensating device. The bushing comprises means for guiding its proximal end (17) against an internal face of the internal cage (21).

Abstract translation: 一种制动致动器，包括套筒（1），密封地可滑动地安装在套筒中以施加制动力的活塞（3），所述活塞设置有内部保持架（21），以及磨损补偿装置（10） 活塞在套筒中的缩回位置借助于轴向移动的止挡件，该止动件能够在施加制动力期间由活塞向前移动，并且与附接的磨损补偿装置的固定部件（12）成摩擦关系 到袖子。 移动式止动件包括可径向变形的衬套（16），该衬套与附接到磨损补偿装置的固定部分的远端的橄榄（15）配合。 衬套包括用于将其近端（17）引导到内部保持架（21）的内表面的装置。

公开(公告)号：US20150217748A1

公开(公告)日：2015-08-06

申请号：US14605488

申请日：2015-01-26

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Philippe CHICO ,  Frédéric RAGOT ,  François BONIGEN ,  Thomas LEPAGE

IPC: B60T17/22 ,  B64C25/44

CPC classification number: B60T17/221 ,  B60T8/1703 ,  B60T8/885 ,  B60T17/22 ,  B60T2270/406 ,  B64C25/44

Abstract: A method for monitoring at least two aircraft wheel electromechanical braking actuators. For each electromechanical actuator, the method includes first determining a current value representative of the power supply current of the electromechanical actuator and determining a reference current value estimated from the power supply currents of at least one other electromechanical actuator. Then, the representative current value and the reference current value are compared. Any abnormal operation of the electromechanical actuator is detected when the difference between the representative current value and the reference current value is above a predetermined threshold.

Abstract translation: 一种用于监视至少两个飞行器机电制动致动器的方法。 对于每个机电致动器，该方法包括首先确定表示机电致动器的电源电流的电流值，并确定从至少一个其它机电致动器的电源电流估计的参考电流值。 然后，比较代表电流值和参考电流值。 当代表电流值与基准电流值的差高于预定阈值时，检测出机电致动器的任何异常操作。

公开(公告)号：US09061661B2

公开(公告)日：2015-06-23

申请号：US14135924

申请日：2013-12-20

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Jean-Baptiste Vaney ,  David Frank ,  David Lemay

IPC: B60T8/00 ,  B60T8/17 ,  B60T8/26 ,  B60T7/04 ,  B60T17/22 ,  B64C25/44

CPC classification number: B60T8/1703 ,  B60T7/042 ,  B60T8/00 ,  B60T8/26 ,  B60T17/221 ,  B64C25/445

Abstract: A method of managing the braking of an aircraft, the aircraft having a plurality of wheels R1, . . . , R12, each fitted with a brake F1, . . . , F12 adapted to generate a braking force in response to brake pedals 5 being depressed. The management method comprising the steps of (1) distributing the wheels fitted with respective brakes in at least two distinct groups G1, G2, G3, G′1, G′2, G′3; (2) allocating respective braking relationships to each of the groups of wheels for determining how braking force varies as a function of the depression of the brake pedals; and (3) acting at predetermined intervals to permutate the allocation of the relationships to the groups in application of a predefined permutation relationship. The method also includes a step of modifying the permutation relationship in response to the occurrence of a predetermined event.

Abstract translation: 一种管理飞机制动的方法，该飞机具有多个轮R1。 。 。 ，R12，每个都配有制动器F1。 。 。 ，F12适于产生响应于制动踏板5被压下的制动力。 该管理方法包括以下步骤：（1）将装配有相应制动器的车轮分配在至少两个不同的组G1，G2，G3，G'1，G'2，G'3中; （2）将各个制动关系分配给每个车轮组，以确定制动力如何随制动踏板的下压而变化; 以及（3）以预定间隔起作用以将应用于预定义置换关系的关系的分配置换为组。 该方法还包括响应于预定事件的发生来修改置换关系的步骤。

公开(公告)号：US20150136899A1

公开(公告)日：2015-05-21

申请号：US14534339

申请日：2014-11-06

Applicant: Messier-Bugatti-Dowty

Inventor： Nicolas MAZARGUIL

IPC: B64C25/40

CPC classification number: B64C25/405 ,  B64C25/36 ,  Y02T50/823

Abstract: An aircraft wheel which is provided with rotational driving unit (110). The driving unit comprises a driving ring (111) which is associated with structure (112) for attaching the ring to a rim of the wheel. The attachment structure is fixed to treads (119) of the rim which further serve to retain removable brake blocks (121) with which the rim is provided.

Abstract translation: 具有旋转驱动单元（110）的飞轮。 所述驱动单元包括驱动环（111），其与用于将所述环连接到所述车轮的轮缘的结构（112）相关联。 附接结构被固定到轮辋的胎面（119）上，其进一步用于保持提供轮辋的可移除的制动块（121）。

公开(公告)号：US20150136547A1

公开(公告)日：2015-05-21

申请号：US14541466

申请日：2014-11-14

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Pierre CHAMBARD ,  Come DORGE

IPC: F16D55/24 ,  B64C25/42 ,  B23P6/00 ,  F16D65/12

CPC classification number: F16D55/24 ,  B23P6/00 ,  B64C25/42 ,  B64C25/44 ,  F16D65/126 ,  F16D65/127 ,  F16D2069/0441 ,  F16D2200/0047 ,  Y10T29/49716

Abstract: The invention relates to a method for the reconditioning and use of brake discs of the rear stator type with studs, the method comprising the steps of using a first disc (12) during a first life, using a second disc (112) during a first life, after the first life of the first disc and the first life of the second disc, machining a friction surface on one of the discs and a rear surface on the other of the discs so that one of said surfaces comprises at least one shoulder (17) and the other of said surfaces comprises at least one notch (118), and nesting the first disc in the second disc such that the notch and the shoulder cooperate so as to centre the discs.

Abstract translation: 本发明涉及一种用于修复和使用具有螺栓的后定子类型的制动盘的方法，所述方法包括以下步骤：在第一次使用期间使用第一盘（12），在第一次使用第一盘 在第一盘的第一寿命和第二盘的第一寿命之后，在一个盘上的一个盘上和另一个盘上的后表面上加工摩擦表面，使得所述表面中的一个包括至少一个肩部（ 17），并且所述表面中的另一个包括至少一个凹口（118），并且将第一盘嵌套在第二盘中，使得凹口和肩部协作以使圆盘居中。

公开(公告)号：US20140297095A1

公开(公告)日：2014-10-02

申请号：US14224794

申请日：2014-03-25

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Jean-Baptiste VANEY

IPC: B60T17/22 ,  B64C25/42

CPC classification number: B60T17/22 ,  B60T17/221 ,  B64C25/42 ,  F16D55/36 ,  F16D66/026 ,  F16D2066/006

Abstract: A method of managing the lifetime of a stack of disks of an aircraft brake having at least one braking actuator including a pusher adapted to press selectively against the stack of disks in order to generate a braking force for an associated wheel, the method comprising the following steps, for a given flight of the aircraft: actuating the actuator to cause the pusher to come into contact with the stack of disks; deducing therefrom a stroke of the actuator, and by taking the difference with a nominal stroke stored in memory corresponding to the stack of disks when new, deducing a current level of wear (U) for the stack of disks; from the current level of wear and from the number of flights (N) flown since the new stack of disks was mounted, using an extrapolation method to estimate a potential number of flights (ΔN) before the stack of disks reaches a maximum acceptable level of wear (Umax).

Abstract translation: 一种管理飞机制动器的盘堆的寿命的方法，其具有至少一个制动致动器，所述制动致动器包括推动器，所述制动致动器适用于选择性地压靠所述盘堆，以便为相关联的车轮产生制动力，所述方法包括以下 步骤，对于飞行器的给定飞行：致动致动器以使推动器与盘堆接触; 从而推导致动器的行程，并且通过在新的时候与存储在对应于盘堆的存储器中的标称行程相差来推算出用于堆栈的当前磨损水平（U）的差异; 从目前的磨损水平以及从安装新的磁盘堆叠以来飞行的航班数（N），使用外推方法来估计磁盘堆栈达到最大可接受的潜在航班数（＆Dgr; N） 磨损水平（Umax）。

公开(公告)号：US20140180506A1

公开(公告)日：2014-06-26

申请号：US14135924

申请日：2013-12-20

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Jean-Baptiste VANEY ,  David FRANK ,  David LEMAY

IPC: B60T8/17 ,  B64C25/42 ,  B60T8/26

CPC classification number: B60T8/1703 ,  B60T7/042 ,  B60T8/00 ,  B60T8/26 ,  B60T17/221 ,  B64C25/445

Abstract: A method of managing the braking of an aircraft, the aircraft having a plurality of wheels R1, . . . , R12, each fitted with a brake F1, . . . , F12 adapted to generate a braking force in response to brake pedals 5 being depressed. The management method comprising the steps of (1) distributing the wheels fitted with respective brakes in at least two distinct groups G1, G2, G3, G′1, G′2, G′3; (2) allocating respective braking relationships to each of the groups of wheels for determining how braking force varies as a function of the depression of the brake pedals; and (3) acting at predetermined intervals to permutate the allocation of the relationships to the groups in application of a predefined permutation relationship. The method also includes a step of modifying the permutation relationship in response to the occurrence of a predetermined event.

Abstract translation: 一种管理飞机制动的方法，该飞机具有多个轮R1。 。 。 ，R12，每个都配有制动器F1。 。 。 ，F12适于产生响应于制动踏板5被压下的制动力。 该管理方法包括以下步骤：（1）将装配有相应制动器的车轮分配在至少两个不同的组G1，G2，G3，G'1，G'2，G'3中; （2）将各个制动关系分配给每个车轮组，以确定制动力如何随制动踏板的下压而变化; 以及（3）以预定间隔起作用以将应用于预定义置换关系的关系的分配置换为组。 该方法还包括响应于预定事件的发生来修改置换关系的步骤。

公开(公告)号：US20140175860A1

公开(公告)日：2014-06-26

申请号：US14132630

申请日：2013-12-18

Applicant: Messier-Bugatti-Dowty

Inventor： Marie-Laure De CRESCENZO ,  Christophe VERDURMEN ,  Jacques BUSSIERE

IPC: B64C25/36

CPC classification number: B64C25/36 ,  B60B25/00 ,  B64C25/44 ,  F16D55/24 ,  F16D2065/1392

Abstract: An aircraft wheel comprising two half-wheels (1, 2) assembled together by means of bolt fasteners (10; 110) clamping together disks of the half-wheels, each bolt fastener comprising a bolt (11; 111) with an end forming a screw head (12; 112) and a threaded end (13; 113) for receiving a nut (14; 114), the wheel also being fitted with drive keys (20; 120) that are fitted to one of the half-wheels for driving brake disks in rotation, the wheel being characterized in that each drive key has a first end (23; 123) that is shaped to co-operate with the screw head of one of the bolts so that said first end is held and prevented from moving when the key is in place on the wheel.

Abstract translation: 一种飞轮，其包括通过将半轮的盘夹在一起的螺栓紧固件（10; 110）组装在一起的两个半轮（1,2），每个螺栓紧固件包括螺栓（11; 111），端部形成 螺钉头（12; 112）和用于接收螺母（14; 114）的螺纹端（13; 113），所述轮还装配有驱动键（20; 120），所述驱动键安装到所述半轮之一， 所述车轮的特征在于，每个驱动钥匙具有第一端（23; 123），所述第一端被成形为与所述螺栓之一的螺钉头配合，使得所述第一端被保持和防止 当钥匙在车轮上就位时移动。

公开(公告)号：US20140137680A1

公开(公告)日：2014-05-22

申请号：US14075642

申请日：2013-11-08

Applicant: Messier-Bugatti-Dowty

Inventor： Ludovic LEGLIZE

IPC: B60G15/12 ,  F16H25/20

CPC classification number: B60G15/12 ,  B64C25/18 ,  B64C25/22 ,  F16H25/20 ,  F16H25/2021 ,  Y10T74/18648

Abstract: The invention relates to an actuator comprising a cylinder (1) in which a rod (2) is mounted to slide, the actuator having a screw (8) extending inside the rod to co-operate with a nut (7) secured to the rod, the screw being driven in rotation by a motor (10), the actuator being characterized in that a hydraulic chamber (CH) filled with hydraulic fluid is arranged inside the actuator by means of a floating piston (20) sliding in sealed manner against the rod inside of the actuator, the hydraulic chamber being in fluid flow communication with an accumulator (21) via a solenoid valve (22) that is controllable between a closed state in which the chamber is isolated from the accumulator, and a fluid-passing state in which the hydraulic chamber and the accumulator are in communication, calibrated resistance being exerted against the passage of fluid from the chamber towards the accumulator.

Abstract translation: 本发明涉及一种致动器，包括一个气缸（1），其中安装有杆（2）以滑动，致动器具有在杆内延伸的螺钉（8），以与固定在杆上的螺母（7）配合 所述螺杆由马达（10）旋转驱动，所述致动器的特征在于，通过浮动活塞（20）将致动器内的充满液压流体的液压室（CH）布置在所述致动器内，所述浮动活塞（20）以密封方式滑动 所述液压室经由电磁阀（22）与蓄能器（21）流体连通，所述电磁阀（22）可在所述室与所述蓄能器隔离的关闭状态和流体通过状态 其中液压室和蓄能器连通，校准的阻力被施加抵抗流体从腔室朝向蓄能器的通道。

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。