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公开(公告)号：US09227608B2
公开(公告)日：2016-01-05
申请号：US12539884
申请日：2009-08-12
申请人： James L. Hill , Kurt Burkhalter
发明人： James L. Hill , Kurt Burkhalter
CPC分类号： B60T8/885 , B60T8/1703 , B60T8/325 , B60T2270/402 , B60T2270/413
摘要： An electric aircraft brake control system has a plurality of wheel and brake assemblies, each having a wheel, wheel speed transducer, brake assembly and a brake actuator. Electromechanical control units are uniquely associated with and connected to certain of the wheel and brake assemblies, and each of the electromechanical control units is provided with an antiskid system as an integral portion thereof. Brake data concentrators are provided for receiving data corresponding to various aircraft operational parameters, including brake pedal position, and provide operational signals to the electromechanical control unit as a function thereof. A controller for emergency and park braking is connected to the electromechanical actuator controllers through one of the brake data concentrators to effect emergency braking action on the brake assemblies, such emergency braking action having incident antiskid control. The system allows for a redundency in brake control circuitry and operation, which increases the dispatchability of an associated aircraft by ensuring continued effective operation of the aircraft even in view of a failure of one of the redundant circuits or systems. A reduction in weight is also achieve by reducing lengthy cable runs.
摘要翻译： 电动飞机制动控制系统具有多个车轮和制动器组件，每个车轮和制动器组件具有车轮，车轮速度传感器，制动器组件和制动致动器。 机电控制单元与某些车轮和制动器组件独特地相关联并连接到其中，并且每个机电控制单元都设置有作为其整体部分的防滑系统。 提供制动数据集中器用于接收与各种飞行器操作参数对应的数据，包括制动踏板位置，并且作为其功能向机电控制单元提供操作信号。 用于紧急和停车制动的控制器通过一个制动数据集中器连接到机电致动器控制器，以对制动组件施加紧急制动作用，这种紧急制动动作具有事件防滑控制。 该系统允许在制动控制电路和操作中的冗余，其通过确保飞机的持续有效操作来增加相关飞行器的调度性，即使考虑到冗余电路或系统之一的故障。 通过减少长时间的电缆运行也可以减轻重量。
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公开(公告)号：US20110040466A1
公开(公告)日：2011-02-17
申请号：US12539884
申请日：2009-08-12
申请人： James L. Hill , Kurt Burkhalter
发明人： James L. Hill , Kurt Burkhalter
IPC分类号： G06F17/00
CPC分类号： B60T8/885 , B60T8/1703 , B60T8/325 , B60T2270/402 , B60T2270/413
摘要： An electric aircraft brake control system has a plurality of wheel and brake assemblies, each having a wheel, wheel speed transducer, brake assembly and a brake actuator. Electromechanical control units are uniquely associated with and connected to certain of the wheel and brake assemblies, and each of the electromechanical control units is provided with an antiskid system as an integral portion thereof. Brake data concentrators are provided for receiving data corresponding to various aircraft operational parameters, including brake pedal position, and provide operational signals to the electromechanical control unit as a function thereof. A controller for emergency and park braking is connected to the electromechanical actuator controllers through one of the brake data concentrators to effect emergency braking action on the brake assemblies, such emergency braking action having incident antiskid control. The system allows for a redundency in brake control circuitry and operation, which increases the dispatchability of an associated aircraft by ensuring continued effective operation of the aircraft even in view of a failure of one of the redundant circuits or systems. A reduction in weight is also achieve by reducing lengthy cable runs.
摘要翻译： 电动飞机制动控制系统具有多个车轮和制动器组件，每个车轮和制动器组件具有车轮，车轮速度传感器，制动器组件和制动致动器。 机电控制单元与某些车轮和制动器组件独特地相关联并连接到其中，并且每个机电控制单元都设置有作为其整体部分的防滑系统。 提供制动数据集中器用于接收与各种飞行器操作参数对应的数据，包括制动踏板位置，并且作为其功能向机电控制单元提供操作信号。 用于紧急和停车制动的控制器通过一个制动数据集中器连接到机电致动器控制器，以对制动组件施加紧急制动作用，这种紧急制动动作具有事件防滑控制。 该系统允许在制动控制电路和操作中的冗余，其通过确保飞机的持续有效操作来增加相关飞行器的调度性，即使考虑到冗余电路或系统之一的故障。 通过减少长时间的电缆运行也可以减轻重量。
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公开(公告)号：US20070261926A1
公开(公告)日：2007-11-15
申请号：US11433020
申请日：2006-05-11
申请人： Kevin Dalton , Kurt Burkhalter , Michael Osburn , Harold Booher
发明人： Kevin Dalton , Kurt Burkhalter , Michael Osburn , Harold Booher
IPC分类号： F16D55/08
CPC分类号： B60T13/746 , F16D2066/005 , F16D2121/24 , F16D2125/40
摘要： An electric brake actuator for the brake system of an aircraft is presented. A brake actuator includes a piston driven by a cylindrical nut and screw arrangement, driven by an appropriate motor of the actuator. Application of brake force results in a reactionary force that deflects the top cover of the actuator. The axial component of this deflection correlates directly with the brake force applied. A beam is interposed between this cover and a top cap, such that deflection of the beam correlates to applied brake face. Piezo-resistive devices are connected to the beam and, through a whetstone bridge, provide an electrical output signal correlating to applied brake force.
摘要翻译： 提出了一种用于飞机制动系统的电动制动执行器。 制动器致动器包括由由致动器的适当电动机驱动的圆柱形螺母和螺杆装置驱动的活塞。 制动力的应用产生使致动器的顶盖偏转的反作用力。 该偏转的轴向分量与施加的制动力直接相关。 在该盖和顶盖之间插入梁，使得梁的偏转与施加的制动面相关。 压电电阻器件连接到光束，并且通过砂轮桥提供与施加的制动力相关的电输出信号。
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公开(公告)号：US20090266652A1
公开(公告)日：2009-10-29
申请号：US12498577
申请日：2009-07-07
IPC分类号： F16D66/00
CPC分类号： B60T13/746 , F16D2066/005 , F16D2121/24 , F16D2125/40
摘要： An electric brake actuator and force transducer for the brake system of an aircraft is presented. A brake actuator includes a piston driven by a cylindrical nut and screw arrangement, driven by an appropriate motor of the actuator. Application of brake force results in a reactionary force that deflects the top cover of the actuator. The axial component of this deflection correlates directly with the brake force applied. A beam is interposed between this cover and a top cap, such that deflection of the beam correlates to applied brake face. Piezo-resistive devices are connected to the beam and, through a whetstone bridge, provide an electrical output signal correlating to applied brake force.
摘要翻译： 提出了用于飞机制动系统的电动制动器致动器和力传感器。 制动器致动器包括由由致动器的适当电动机驱动的圆柱形螺母和螺杆装置驱动的活塞。 制动力的应用产生使致动器的顶盖偏转的反作用力。 该偏转的轴向分量与施加的制动力直接相关。 在该盖和顶盖之间插入梁，使得梁的偏转与施加的制动面相关。 压电电阻器件连接到光束，并且通过砂轮桥提供与施加的制动力相关的电输出信号。
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公开(公告)号：US07565953B2
公开(公告)日：2009-07-28
申请号：US11433020
申请日：2006-05-11
CPC分类号： B60T13/746 , F16D2066/005 , F16D2121/24 , F16D2125/40
摘要： An electric brake actuator for the brake system of an aircraft is presented. A brake actuator includes a piston driven by a cylindrical nut and screw arrangement, driven by an appropriate motor of the actuator. Application of brake force results in a reactionary force that deflects the top cover of the actuator. The axial component of this deflection correlates directly with the brake force applied. A beam is interposed between this cover and a top cap, such that deflection of the beam correlates to applied brake face. Piezo-resistive devices are connected to the beam and, through a whetstone bridge, provide an electrical output signal correlating to applied brake force.
摘要翻译： 提出了一种用于飞机制动系统的电动制动执行器。 制动器致动器包括由由致动器的适当电动机驱动的圆柱形螺母和螺杆装置驱动的活塞。 制动力的应用产生使致动器的顶盖偏转的反作用力。 该偏转的轴向分量与施加的制动力直接相关。 在该盖和顶盖之间插入梁，使得梁的偏转与施加的制动面相关。 压电电阻器件连接到光束，并且通过砂轮桥提供与施加的制动力相关的电输出信号。
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公开(公告)号：US06003954A
公开(公告)日：1999-12-21
申请号：US917252
申请日：1997-08-25
CPC分类号： F16D55/36 , F16D2065/1368 , F16D2065/1392
摘要： A beam key and wheel assembly for aircraft brakes is presented. A beam key is pinned at one end to the aircraft wheel and is engaged proximate an opposite end to a pad on an outrigger flange of the wheel. The pad has a milled arcuate surface which is congruent with and nestingly receives a similar arcuate surface of a foot member. The foot has a channel formed therein on a side opposite the arcuate surface, the channel matingly receiving a base on a bottom surface of the beam key. A bolt passes through the beam key, foot, and pad on the outrigger flange to secure the elements together.
摘要翻译： 提出了用于飞机制动器的梁键和轮组件。 梁键在一端被固定在飞行器轮上，并且接近靠近轮的外伸支架法兰上的垫的相对端。 该垫具有与铣削的弓形表面，该表面与脚件的类似弧形表面一致并且嵌套。 脚在与弓形表面相对的一侧上形成有通道，该通道配合地接收在梁键的底表面上的基部。 螺栓穿过外伸支架法兰上的梁键，脚和垫，将元件固定在一起。
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公开(公告)号：US08668276B2
公开(公告)日：2014-03-11
申请号：US13182889
申请日：2011-07-14
申请人： John M. Hall , William J. Burley , Mark P. Dyko , Kurt Burkhalter
发明人： John M. Hall , William J. Burley , Mark P. Dyko , Kurt Burkhalter
IPC分类号： B64C25/36
CPC分类号： B64C25/36 , F16D2065/1368 , F16D2065/1372 , F16D2065/138 , F16D2065/785
摘要： A heat shield segment includes at least one tab extending from an outboard end, the tab adapted to secure the heat shield segment against radial and axial movement. The at least one tab is received over a retaining ring positioned within a tube well of a wheel. The retaining ring is received in recesses formed in the inner surface of drive keys spaced around the interior of the tube well. The heat shield segment is secured at the inboard end by a fastener, and is spaced from the tube well by a spacer positioned between the heat shield segment and the tube well. The at least one tab of the heat shield segment allows for easy assembly and maintenance of the heat shield assembly formed by a plurality of the heat shield segments.
摘要翻译： 隔热片段包括从外侧端部延伸的至少一个翼片，所述翼片适于固定所述隔热片段以抵抗径向和轴向运动。 该至少一个突片被容纳在位于轮的管井内的保持环上。 保持环被容纳在形成在围绕管井内部的驱动键的内表面中的凹部中。 隔热板段通过紧固件在内侧固定，并且通过位于隔热板段和管井之间的间隔件与管井隔开。 隔热片段的至少一个翼片允许容易地组装和维护由多个隔热板段形成的隔热罩组件。
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公开(公告)号：US20130015697A1
公开(公告)日：2013-01-17
申请号：US13182889
申请日：2011-07-14
申请人： John M. Hall , William J. Burley , Mark P. Dyko , Kurt Burkhalter
发明人： John M. Hall , William J. Burley , Mark P. Dyko , Kurt Burkhalter
CPC分类号： B64C25/36 , F16D2065/1368 , F16D2065/1372 , F16D2065/138 , F16D2065/785
摘要： A heat shield segment includes at least one tab extending from an outboard end, the tab adapted to secure the heat shield segment against radial and axial movement. The at least one tab is received over a retaining ring positioned within a tube well of a wheel. The retaining ring is received in recesses formed in the inner surface of drive keys spaced around the interior of the tube well. The heat shield segment is secured at the inboard end by a fastener, and is spaced from the tube well by a spacer positioned between the heat shield segment and the tube well. The at least one tab of the heat shield segment allows for easy assembly and maintenance of the heat shield assembly formed by a plurality of the heat shield segments.
摘要翻译： 隔热片段包括从外侧端部延伸的至少一个翼片，所述翼片适于固定所述隔热片段以抵抗径向和轴向运动。 该至少一个突片被容纳在位于轮的管井内的保持环上。 保持环被容纳在形成在围绕管井内部的驱动键的内表面中的凹部中。 隔热板段通过紧固件在内侧固定，并且通过位于隔热板段和管井之间的间隔件与管井隔开。 隔热片段的至少一个翼片允许容易地组装和维护由多个隔热板段形成的隔热罩组件。
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