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公开(公告)号：US20110171065A1
公开(公告)日：2011-07-14
申请号：US12685355
申请日：2010-01-11
CPC分类号： A61L2/22 , A61L2202/15 , A61L2202/16 , A61L2202/25 , B05B5/03 , B05B5/1608
摘要： An electrostatic spraying system for decontamination of a vehicle is described. The system includes a wheeled platform sized to fit inside the vehicle, at least one tank operable to contain one or more decontaminant agents, the tanks supported by said wheeled platform, a plurality of nozzles affixed to the wheeled platform, wherein each nozzle is positioned for distribution of the decontaminant agents in at least one pre-determined direction, an electrostatic charging system connected to each of the nozzles for applying an electrostatic charge to the decontaminant agents as the agents are dispersed, and at least one compressor in communication with the tanks for pressurizing the decontaminant agents. The one or more compressors are capable of providing a pressure sufficient to provide a constant distribution of the decontaminant agents through the electrostatic nozzles.
摘要翻译： 描述了用于车辆去污的静电喷涂系统。 该系统包括尺寸适于装配在车辆内的轮式平台，至少一个罐，可操作以容纳一种或多种去污剂，由所述轮式平台支撑的罐，固定到轮式平台的多个喷嘴，其中每个喷嘴定位成 在至少一个预定方向上分配净化剂;静电充电系统，连接到每个喷嘴，用于当试剂分散时向静电荷施加静电荷;以及至少一个压缩机，其与罐相连通 对净化剂加压。 一个或多个压缩机能够提供足以提供去污剂通过静电喷嘴的恒定分布的压力。
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2.发明申请FLIGHT CONTROL USING MULTIPLE ACTUATORS ON PRIMARY CONTROL SURFACES WITH TABS 有权使用多个执行器在主控制表面与飞行员的飞行控制公开(公告)号：US20090146003A1
公开(公告)日：2009-06-11
申请号：US11953567
申请日：2007-12-10
IPC分类号： B64C9/10
CPC分类号： B64C9/10
摘要： A flight control system for an aircraft directs a primary surface that is pivotable with respect to the aircraft with a moveable tab located at the end of the primary surface. A primary surface actuator maintains a position of the primary surface. A tab actuator moves the tab with respect to the primary flight control surface. A controller configured to coordinate the movement of the primary flight control surface with the movement of the tab by deflecting the tab with respect to the primary flight control surface, thereby allowing aerodynamic forces acting upon the deflected tab to position the primary flight control surface at a desired position. The primary flight control surface can then be maintained at the desired position by the primary surface actuator.
摘要翻译： 用于飞行器的飞行控制系统引导主表面，该主表面可相对于飞行器枢转，具有位于主表面的端部的可移动的突片。 主表面致动器保持主表面的位置。 翼片致动器相对于主飞行控制表面移动翼片。 控制器，被配置为通过相对于主飞行控制表面偏转翼片来协调主飞行控制表面与翼片的移动的移动，从而允许作用在偏转翼片上的空气动力力将主飞行控制表面定位在 所期望的职位。 然后，主飞行控制表面可以由主表面致动器保持在期望的位置。
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3.发明申请公开(公告)号：US20110080123A1
公开(公告)日：2011-04-07
申请号：US12968751
申请日：2010-12-15
CPC分类号： H02K41/031 , H02K3/47 , H02K16/00 , H02K21/14 , H02K2201/18
摘要： In an embodiment, an actuator includes a plurality of stator windings adapted to produce a first stator magnetic field that translates along a stator axis, and to produce a second stator magnetic field that rotates around the stator axis. In addition, the actuator includes a rotor, coupled to a shaft, and positioned within a central stator channel. The rotor is adapted to produce a first rotor magnetic field that translates along a shaft axis and to produce a second rotor magnetic field that rotates around the shaft axis. An actuator system includes an actuator and an actuator controller unit, which is adapted to produce actuator inputs. An embodiment of a method for controlling the actuator includes providing actuator inputs to produce a translating magnetic field in the stator, a translating magnetic field in the rotor, a rotating magnetic field in the stator, and a rotating magnetic field in the rotor.
摘要翻译： 在一个实施例中，致动器包括适于产生沿着定子轴线平移的第一定子磁场并且产生围绕定子轴线旋转的第二定子磁场的多个定子绕组。 此外，致动器包括联接到轴并且定位在中心定子通道内的转子。 转子适于产生沿轴线平移的第一转子磁场并产生围绕轴线旋转的第二转子磁场。 致动器系统包括致动器和致动器控制器单元，其适于产生致动器输入。 用于控制致动器的方法的实施例包括提供致动器输入以在定子中产生平移磁场，转子中的平移磁场，定子中的旋转磁场和转子中的旋转磁场。
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公开(公告)号：US20090146013A1
公开(公告)日：2009-06-11
申请号：US11952317
申请日：2007-12-07
IPC分类号： B64C9/00
摘要： Systems and techniques are described for actuating a control surface about a pivot point using variable moments. A bracket having a moment arm is coupled to the pivot point such that the bracket is rotatable about the pivot point to actuate the surface. A power actuator has a shaft coupled to the bracket at a coupling point on the moment arm such that actuation force applied to the shaft results in a moment produced about the pivot point. A linear actuator is configured to adjust the location of the coupling point with respect to the pivot point to thereby changing the moment arm and the moment produced about the pivot point as the bracket rotates. By adjusting the distance between the pivot point and the coupling point, the moments produced about the pivot point can be increased while conserving actuator power.
摘要翻译： 描述了使用可变力矩来驱动关于枢转点的控制表面的系统和技术。 具有力臂的支架联接到枢转点，使得支架能够围绕枢转点旋转以致动表面。 动力致动器具有在力臂上的联接点处联接到支架的轴，使得施加到轴的致动力导致围绕枢转点产生的力矩。 线性致动器构造成调节联接点相对于枢转点的位置，从而改变力矩臂和当支架旋转时围绕枢转点产生的力矩。 通过调节枢转点和联接点之间的距离，可以增加围绕枢轴点产生的力矩，同时节省致动器功率。
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公开(公告)号：US20120181856A1
公开(公告)日：2012-07-19
申请号：US13428768
申请日：2012-03-23
IPC分类号： B60L1/00
CPC分类号： B60L7/14 , H02J7/1438 , H02J7/34
摘要： An actuator control system includes a controller and a buck-boost circuit. The controller is configured to direct power from a power source to an actuator. The actuator is coupled to a control device to apply a force related to operation of a vehicle. The buck-boost circuit is configured to direct excess power generated by the actuator to an energy storage device when an actuator power level satisfies an anticipated power level.
摘要翻译： 致动器控制系统包括控制器和降压 - 升压电路。 控制器被配置为将电力从电源引导到致动器。 致动器联接到控制装置以施加与车辆的操作相关的力。 降压 - 升压电路被配置为当致动器功率电平满足预期功率电平时，将由致动器产生的过剩功率引导到能量存储装置。
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公开(公告)号：US20100084509A1
公开(公告)日：2010-04-08
申请号：US12245916
申请日：2008-10-06
IPC分类号： B64C25/16
CPC分类号： B64C25/16 , B64C2025/003
摘要： Apparatus and methods provide for the use of a lift-producing body with a landing gear assembly in order to provide a lifting force during landing gear operations that reduces the load on the landing gear actuator. According to embodiments, the lift-producing body may be configured for attachment to the landing gear assembly. The lift-producing body may be reconfigured while the landing gear assembly is being retracted or deployed in order to maximize the aerodynamic lift created by the lift-producing body or to minimize the drag induced by the lift-producing body.
摘要翻译： 装置和方法提供了使用具有起落架组件的升降机主体，以便在起落架操作期间提供提升力，从而减小起落架致动器的负载。 根据实施例，提升产生主体可被构造成附接到起落架组件。 升降机产生主体可以在起落架组件被缩回或展开的同时重新配置，以便最大限度地提高由提升产生机构产生的空气动力升力，或者最小化由提升产生机构引起的阻力。
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公开(公告)号：US20120043924A1
公开(公告)日：2012-02-23
申请号：US12861010
申请日：2010-08-23
CPC分类号： H01M2/1077 , H01M2/12 , H01M10/425 , H01M10/441 , H01M10/46 , H01M10/482 , H02J7/0031
摘要： A battery system including a housing that defines an internal volume and a venting system that fluidly couples the internal volume with an atmosphere surrounding the housing and a support structure within the internal volume, the support structure being configured to support a number of battery cell modules in the internal volume.
摘要翻译： 一种电池系统，包括限定内部容积的壳体和将内部容积与围绕壳体的气氛以及内部容积内的支撑结构流体耦合的排气系统，所述支撑结构被配置为支撑多个电池单元模块 内部音量。
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公开(公告)号：US20100109581A1
公开(公告)日：2010-05-06
申请号：US12264488
申请日：2008-11-04
CPC分类号： B60L7/14 , H02J7/1438 , H02J7/34
摘要： Systems and methods are provided for capturing and using power generated by the application of an external force or by an inertial force on a vehicle control device that back-drive or forward-drive an actuator coupled to the control device. An actuator is coupled to a control device configured to apply a force related to operation of a vehicle. A bus is configured to conduct power to the actuator. An actuator control system is configured to receive power from a power source via an electrical bus and direct the power to the actuator. The actuator control system is also configured to monitor an actuator power level to determine when the actuator power level does not meet an anticipated power level. When the actuator power level exceeds the anticipated power level, the excess power generated is directed to an energy storage device. When the actuator power level is less than the anticipated power level, supplemental power is distributed from the energy storage device to the bus.
摘要翻译： 提供了系统和方法，用于捕获和使用通过施加外力或通过惯性力而产生的电力，该车辆控制装置用于后驱动或前向驱动耦合到控制装置的致动器。 致动器联接到被配置为施加与车辆的操作相关的力的控制装置。 总线被配置为向致动器供电。 致动器控制系统被配置为经由电总线从电源接收电力并将电力引导到致动器。 致动器控制系统还被配置为监视致动器功率水平以确定致动器功率水平何时不满足预期的功率水平。 当致动器功率级别超过预期功率水平时，产生的多余功率被引导到储能装置。 当执行器功率水平低于预期功率水平时，补充功率从能量存储装置分配到总线。
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