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公开(公告)号：US07597289B2
公开(公告)日：2009-10-06
申请号：US11332835
申请日：2006-01-13
申请人： Arvin Shmilovich , Yoram Yadlin , Roger Clark , Donald Leopold
发明人： Arvin Shmilovich , Yoram Yadlin , Roger Clark , Donald Leopold
IPC分类号： B64C23/00
CPC分类号： B64C23/076 , B64C23/065 , Y02T50/164
摘要： A system and method for dissipating vortices that form at the wingtips on aircraft and from other airfoils. A jet air stream is discharged in a location at or proximate to the outer end portion of the airfoil into the vortex flow, and the jet air stream is moved cyclically back and forth. The cyclic movement can be at lower or higher frequencies to alleviate at least in part intensity of the vortex or accelerate instability of the vortex which leads to vortex dissipation.
摘要翻译： 一种用于消散在飞机和其他翼型上的翼尖处形成的涡流的系统和方法。 喷气空气流在翼型的外端部分处或附近的位置被排放到涡流中，并且喷气流被循环地前后移动。 循环运动可以在较低或更高的频率以减轻涡流的至少部分强度或加速导致涡流耗散的涡流的不稳定性。
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公开(公告)号：US20080042013A1
公开(公告)日：2008-02-21
申请号：US11747112
申请日：2007-05-10
申请人： Arvin Shmilovich , Yoram Yadlin , Roger Clark
发明人： Arvin Shmilovich , Yoram Yadlin , Roger Clark
IPC分类号： B64C23/06
CPC分类号： B64C23/076 , B64C23/065 , Y02T50/164
摘要： Active systems and methods for controlling aircraft vortices are disclosed. An apparatus in accordance with one embodiment is directed to an aircraft system that includes an airfoil having first and second oppositely facing flow surfaces and a tip. The system can further include a vortex dissipation device carried by the airfoil, with the vortex dissipation device including an orifice positioned to direct a flow of fluid outwardly from the tip, an actuator operatively coupled to the fluid flow orifice and positioned to change a manner in which flow is directed outwardly from the tip, and a controller operatively coupled to the actuator to direct the operation of the actuator. The vortex dissipation device can be activated to accelerate the rate at which vortices (e.g., wing tip vortices) dissipate after they are generated, for example, by alternately pulsing flow inwardly and outwardly through the fluid flow orifice.
摘要翻译： 公开了用于控制飞行器旋涡的主动系统和方法。 根据一个实施例的装置涉及一种飞行器系统，其包括具有第一和第二相对面向的流动表面和尖端的翼型件。 该系统还可以包括由翼型件承载的涡流耗散装置，其中涡流消散装置包括定位成将流体流从尖端向外引导的孔口，致动器可操作地联接到流体流动孔口并且定位成改变 该流动从尖端向外指向，并且控制器可操作地联接到致动器以引导致动器的操作。 涡流消散装置可以被激活以加速涡流（例如，翼尖涡流）在其产生之后消散的速率，例如通过交替地脉冲流动通过流体流动孔口向内和向外流动。
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33.发明授权公开(公告)号：US08618719B2
公开(公告)日：2013-12-31
申请号：US13536939
申请日：2012-06-28
IPC分类号： H01L41/08
摘要： A power generation device that provides power to an auxiliary system on an airborne platform, includes a piezoelectric energy harvesting device and an energy storage unit, including a battery and a power conditioner. The device extracts energy generated by turbulent airflow around the platform and stores the energy to meet future power requirements. The piezoelectric energy harvesting device is located on a portion of an inner surface of an outward shell of the platform. The stand-alone power generation device is electrically connected to the auxiliary system. The stand-alone power generation device also includes a router that connects the power generation unit to the platform electrical distribution system. Excess power generated by the device may be delivered to the platform electrical distribution system for use by other platform systems.
摘要翻译： 向空中平台上的辅助系统提供电力的发电装置包括压电能量收集装置和包括电池和功率调节器的能量存储单元。 该设备提取由平台周围的湍流气流产生的能量，并存储能量以满足未来的功率要求。 压电能量收集装置位于平台的外壳的内表面的一部分上。 独立发电装置电连接到辅助系统。 独立发电装置还包括将发电单元连接到平台配电系统的路由器。 由设备产生的过多功率可以被传送到平台配电系统以供其他平台系统使用。
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34.发明申请AUTONOMOUS POWER GENERATION UNIT FOR AUXILIARY SYSTEM ON AN AIRBORNE PLATFORM 有权用于AIRBORNE平台辅助系统的自动发电机组公开(公告)号：US20100176692A1
公开(公告)日：2010-07-15
申请号：US12351538
申请日：2009-01-09
IPC分类号： H02N2/18
摘要： A stand-alone power generation device that provides power to an auxiliary system on an airborne platform, includes a piezoelectric energy harvesting device and an energy storage unit, including a battery and a power conditioner. The device extracts energy generated by turbulent airflow around the platform and stores the energy to meet future power requirements. The piezoelectric energy harvesting device is located on a portion of an inner surface of an outward shell of the platform. The stand-alone power generation device is electrically connected to the auxiliary system. The stand-alone power generation device also includes a router that connects the power generation unit to the platform electrical distribution system. Excess power generated by the device may be delivered to the platform electrical distribution system for use by other platform systems.
摘要翻译： 向空中平台上的辅助系统提供电力的独立发电装置包括压电能量收集装置和包括电池和功率调节器的能量存储单元。 该设备提取由平台周围的湍流气流产生的能量，并存储能量以满足未来的功率要求。 压电能量收集装置位于平台的外壳的内表面的一部分上。 独立发电装置电连接到辅助系统。 独立发电装置还包括将发电单元连接到平台配电系统的路由器。 由设备产生的过多功率可以被传送到平台配电系统以供其他平台系统使用。
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35.发明授权公开(公告)号：US08232706B2
公开(公告)日：2012-07-31
申请号：US12351538
申请日：2009-01-09
IPC分类号： H01L41/08
摘要： A stand-alone power generation device that provides power to an auxiliary system on an airborne platform, includes a piezoelectric energy harvesting device and an energy storage unit, including a battery and a power conditioner. The device extracts energy generated by turbulent airflow around the platform and stores the energy to meet future power requirements. The piezoelectric energy harvesting device is located on a portion of an inner surface of an outward shell of the platform. The stand-alone power generation device is electrically connected to the auxiliary system. The stand-alone power generation device also includes a router that connects the power generation unit to the platform electrical distribution system. Excess power generated by the device may be delivered to the platform electrical distribution system for use by other platform systems.
摘要翻译： 向空中平台上的辅助系统提供电力的独立发电装置包括压电能量收集装置和包括电池和功率调节器的能量存储单元。 该设备提取由平台周围的湍流气流产生的能量，并存储能量以满足未来的功率要求。 压电能量收集装置位于平台的外壳的内表面的一部分上。 独立发电装置电连接到辅助系统。 独立发电装置还包括将发电单元连接到平台配电系统的路由器。 由设备产生的过多功率可以被传送到平台配电系统以供其他平台系统使用。
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公开(公告)号：US20140119878A1
公开(公告)日：2014-05-01
申请号：US13662466
申请日：2012-10-27
CPC分类号： B64C21/04 , B64C2230/04 , Y02T50/166 , Y10T29/4932
摘要： A system and methods for a self-rotating fluidic traverse actuator are presented. A turbine rotates in response to a fluid flow, and an outer cylinder with a longitudinal slot that ejects the fluid flow. An inner cylinder rotates inside the outer cylinder in response to a rotation of the turbine and at least one helical slot of the inner cylinder ejects the fluid flow into the longitudinal slot.
摘要翻译： 提出了一种自旋流体横动执行器的系统和方法。 涡轮机响应于流体流动而旋转，并且具有喷射流体流动的具有纵向狭槽的外筒。 内圆柱体响应于涡轮机的旋转而在外筒内旋转，并且内圆柱体的至少一个螺旋槽将流体流喷射到纵向槽中。
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37.发明授权公开(公告)号：US08632031B2
公开(公告)日：2014-01-21
申请号：US13178556
申请日：2011-07-08
IPC分类号： B64C23/00
CPC分类号： B64C21/04 , B64C9/38 , B64C21/08 , B64C23/06 , B64C2230/04 , B64C2230/06 , Y02T50/162
摘要： Systems and methods for reducing the trailing vortices and lowering the noise produced by the side edges of aircraft flight control surfaces, tips of wings and winglets, and tips of rotor blades. A noise-reducing, wake-alleviating device is disclosed which incorporates an actuator and one or more air-ejecting slot-shaped openings coupled to that actuator and located on the upper and/or lower surfaces and/or the side edges of an aircraft flight control surface or the tip of a wing, winglet or blade. The actuation mechanism produces sets of small and fast-moving air jets that traverse the openings in the general streamwise direction. The actuation destabilizes the flap vortex structure, resulting in reduced intensity of trailing vortices and lower airplane noise.
摘要翻译： 用于减少尾部涡流并降低由飞行器飞行控制表面的侧缘，翼和小翼的尖端以及转子叶片的尖端产生的噪声的系统和方法。 公开了一种降噪的尾流缓冲装置，其包括致动器和联接到该致动器并且位于飞行器飞行器的上和/或下表面和/或侧边缘上的一个或多个空气喷射槽形开口 控制面或翼，小翼或叶片的尖端。 致动机构产生一组在一般流向方向上穿过开口的小而快速移动的空气射流。 该致动使翼片涡旋结构变得不稳定，导致后退涡流的强度降低，飞机噪音降低。
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38.发明申请AUTONOMOUS POWER GENERATION UNIT FOR AUXILIARY SYSTEM ON AN AIRBORNE PLATFORM 有权用于AIRBORNE平台辅助系统的自动发电机组公开(公告)号：US20120299446A1
公开(公告)日：2012-11-29
申请号：US13536939
申请日：2012-06-28
IPC分类号： H02N2/18
摘要： A power generation device that provides power to an auxiliary system on an airborne platform, includes a piezoelectric energy harvesting device and an energy storage unit, including a battery and a power conditioner. The device extracts energy generated by turbulent airflow around the platform and stores the energy to meet future power requirements. The piezoelectric energy harvesting device is located on a portion of an inner surface of an outward shell of the platform. The stand-alone power generation device is electrically connected to the auxiliary system. The stand-alone power generation device also includes a router that connects the power generation unit to the platform electrical distribution system. Excess power generated by the device may be delivered to the platform electrical distribution system for use by other platform systems.
摘要翻译： 向空中平台上的辅助系统提供电力的发电装置包括压电能量收集装置和包括电池和功率调节器的能量存储单元。 该设备提取由平台周围的湍流气流产生的能量，并存储能量以满足未来的功率要求。 压电能量收集装置位于平台的外壳的内表面的一部分上。 独立发电装置电连接到辅助系统。 独立发电装置还包括将发电单元连接到平台配电系统的路由器。 由设备产生的过多功率可以被传送到平台配电系统以供其他平台系统使用。
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39.发明申请公开(公告)号：US20120256049A1
公开(公告)日：2012-10-11
申请号：US13178556
申请日：2011-07-08
IPC分类号： B64C21/04
CPC分类号： B64C21/04 , B64C9/38 , B64C21/08 , B64C23/06 , B64C2230/04 , B64C2230/06 , Y02T50/162
摘要： Systems and methods for reducing the trailing vortices and lowering the noise produced by the side edges of aircraft flight control surfaces, tips of wings and winglets, and tips of rotor blades. A noise-reducing, wake-alleviating device is disclosed which incorporates an actuator and one or more air-ejecting slot-shaped openings coupled to that actuator and located on the upper and/or lower surfaces and/or the side edges of an aircraft flight control surface or the tip of a wing, winglet or blade. The actuation mechanism produces sets of small and fast-moving air jets that traverse the openings in the general streamwise direction. The actuation destabilizes the flap vortex structure, resulting in reduced intensity of trailing vortices and lower airplane noise.
摘要翻译： 用于减少尾部涡流并降低由飞行器飞行控制表面的侧缘，翼和小翼的尖端以及转子叶片的尖端产生的噪声的系统和方法。 公开了一种降噪的尾流缓冲装置，其包括致动器和联接到该致动器并且位于飞行器飞行器的上和/或下表面和/或侧边缘上的一个或多个空气喷射槽形开口 控制面或翼，小翼或叶片的尖端。 致动机构产生一组在一般流向方向上穿过开口的小而快速移动的空气射流。 该致动使翼片涡旋结构变得不稳定，导致后退涡流的强度降低，飞机噪音降低。
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