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81. 发明申请

US20160031335A1 PORTABLE CHARGING CABLE WITH IN-LINE CONTROLLER 有权
公开(公告)号：US20160031335A1
公开(公告)日：2016-02-04
申请号：US14875909
申请日：2015-10-06
申请人： AEROVIRONMENT, INC.
发明人： David Paul Soden , Albert Joseph Flack , Herman Joseph Steinbuchel, IV , Larry Hayashigawa , Brendan Francis O'Donnell , Francis Patrick Wong , Robert Barrosa
IPC分类号： B60L11/18 , H02J7/00
CPC分类号： B60L11/1816 , B60L3/04 , B60L11/1818 , B60L11/1838 , B60L11/1872 , B60L2230/12 , B60L2230/16 , B60L2240/36 , B60L2250/10 , H02J7/0021 , H02J7/0026 , H02J7/0042 , H02J7/0045 , H02J7/0047 , H02J7/007 , H05K7/00 , Y02T10/7005 , Y02T10/7088 , Y02T90/121 , Y02T90/128 , Y02T90/14 , Y02T90/16 , Y02T90/163
摘要： A portable electric vehicle support equipment (EVSE) unit is formed as a cord of plural insulated conductors and a flexible outer sheath enclosing said plural insulated conductors. The cord includes an EVSE docking connector on a docking end of the cord and a utility plug on a utility end of the cord, said cord being divided into a docking section terminated at said docking connector and a utility section terminated at said utility connector. The cord further includes an in-line EVSE controller and a housing enclosing said controller, said housing sealed with said flexible outer sheath and disposed at an intermediate section of said cord between said docking and utility sections.

82. 发明申请

US20160025457A1 MULTIMODE UNMANNED AERIAL VEHICLE 审中-公开
标题翻译：多模式无人驾驶航空器
公开(公告)号：US20160025457A1
公开(公告)日：2016-01-28
申请号：US14832688
申请日：2015-08-21
申请人： AeroVironment, Inc.
发明人： Carlos Thomas Miralles
IPC分类号： F41G7/22 , G05D1/12 , G05D1/00 , B64C39/02
CPC分类号： F41G7/2246 , B64C39/024 , B64C2201/121 , B64C2201/141 , F41G7/008 , F41G7/2206 , F41G7/2253 , F41G7/2293 , F41G9/002 , G05D1/0094 , G05D1/12 , G08G5/0069
摘要： A system comprising an unmanned aerial vehicle (UAV) configured to transition from a terminal homing mode to a target search mode, responsive to an uplink signal and/or an autonomous determination of scene change.
摘要翻译：一种系统，其包括被配置为响应于上行链路信号和/或场景变化的自主确定而从终端归属模式转换到目标搜索模式的无人机（UAV）。

83. 发明申请

US20150367742A1 EVSE KIT INCLUDING A PORTABLE CHARGING CABLE, AN IN-LINE EVSE CONTROLLER AND AN INTERFACE TOOL 有权
标题翻译： EVSE套件，包括便携式充电电缆，一个在线EVSE控制器和一个接口工具
公开(公告)号：US20150367742A1
公开(公告)日：2015-12-24
申请号：US14841995
申请日：2015-09-01
申请人： AEROVIRONMENT, INC.
发明人： David Paul Soden , Albert Joseph Flack , Herman Joseph Steinbuchel, IV , Larry Hayashigawa , Brendan Francis O'Donnell , Francis Patrick Wong , Robert Barrosa
IPC分类号： B60L11/18
CPC分类号： B60L11/1816 , B60L3/04 , B60L11/1818 , B60L11/1838 , B60L11/1872 , B60L2230/12 , B60L2230/16 , B60L2240/36 , B60L2250/10 , H02J7/0021 , H02J7/0026 , H02J7/0042 , H02J7/0045 , H02J7/0047 , H02J7/007 , H05K7/00 , Y02T10/7005 , Y02T10/7088 , Y02T90/121 , Y02T90/128 , Y02T90/14 , Y02T90/16 , Y02T90/163
摘要： A portable electric vehicle support equipment (EVSE) kit is provided consisting of an EVSE cord and an interface tool providing external access to a serial port through the control pilot conductor.
摘要翻译：提供了一种便携式电动车辆支持设备（EVSE）套件，由EVSE线和接口工具组成，通过控制导频导体提供对串行端口的外部访问。

84. 发明申请

US20150319769A1 DYNAMIC TRANSMISSION CONTROL FOR A WIRELESS NETWORK 审中-公开
标题翻译：无线网络的动态传输控制
公开(公告)号：US20150319769A1
公开(公告)日：2015-11-05
申请号：US14702445
申请日：2015-05-01
申请人： AeroVironment, Inc.
发明人： John F. GRABOWSKY , Phillip T. TOKUMARU , Robert J. KNISKERN , Nicholas S. CURRENS , Allan L. LEVINE
IPC分类号： H04W72/08 , H04W72/04 , H04W72/12
摘要： In one possible embodiment, a wireless network with dynamic transmission control is provided that includes a multiple of nodes. The nodes include an arbiter and multiple client nodes. The arbiter is configured to control an operation of the client nodes by defining communications operation cycles and allocating a bandwidth to each of the client nodes on a cycle by cycle basis in response to requests for bandwidth from the client nodes.
摘要翻译：在一个可能的实施例中，提供了包括多个节点的具有动态传输控制的无线网络。节点包括仲裁器和多个客户端节点。仲裁器被配置为通过定义通信操作周期并响应于来自客户端节点的带宽请求逐周期地为每个客户端节点分配带宽来控制客户端节点的操作。

85. 发明申请

US20150267996A1 Launch Tube Restraint System For Unmanned Aerial Vehicle (UAV) 有权
标题翻译：无人机（UAV）发射管约束系统
公开(公告)号：US20150267996A1
公开(公告)日：2015-09-24
申请号：US14281680
申请日：2014-05-19
申请人： AeroVironment, Inc.
发明人： Guan H. Su , Marcos Henry Rodriguez
IPC分类号： F41F3/00 , B64C39/02
CPC分类号： B64F1/04 , B64C39/024 , B64C2201/08 , B64C2201/084 , B64C2201/088 , B64C2201/201 , B64F1/06 , F41B11/80 , F41F3/00 , F41F3/042 , F41F3/052 , F41F3/073
摘要： An unmanned aerial launch vehicle (UAV) launch apparatus is disclosed that includes a UAV (400) having an exterior surface, an aerial vehicle (AV) tab (510) extending from the exterior surface, a tube (440) containing the UAV (400), the tube (440) including a tab stop (515) configured to controllably hinder travel of the AV tab (510) past the tab stop (515), and a pair of opposing tab guides (700, 705) configured to position the AV tab (510) for travel over the tab stop (515).
摘要翻译：公开了一种无人驾驶飞行器（UAV）发射装置，其包括具有外表面的UAV（400），从外表面延伸的飞行器（AV）突片（510），包含无人机（400）的管（440）），所述管（440）包括构造成可控制地阻碍所述AV突片（510）经过所述突片止动件（515）的移动的突片止动件（515），以及一对相对的突片引导件（700,705），其被配置为 AV选项卡（510），用于在制表位（515）上移动。

86. 发明申请

US20150115966A1 EVSE WELDED CONTACTOR DETECTOR 审中-公开
标题翻译： EVSE焊接接触器检测器
公开(公告)号：US20150115966A1
公开(公告)日：2015-04-30
申请号：US14403570
申请日：2013-05-24
申请人： AeroVironment, Inc.
发明人： Scott Garret Berman , Albert Flack , Keith Kolb , Ming Bai
IPC分类号： G01R31/02 , B60L11/18 , G01R31/00
摘要： In at least one embodiment, provided is an electric vehicle supply equipment having a line power contactor including a first line power input and a second line power input and a first line power output and a second line power output. It further has a welded contactor detector with a contactor sense circuit, the sense circuit having a first line shunt resistor network connected from the first line power contactor output to ground and a second line shunt resistor network connected from the first line power contactor output to ground. In another embodiment provided is an EVSE including a welded contactor detector with a contactor sense circuit having a bias resistor connected between the hot line relay input and the neutral line relay output.
摘要翻译：在至少一个实施例中，提供了具有线路功率接触器的电动车辆供应设备，其包括第一线路功率输入和第二线路功率输入以及第一线路功率输出和第二线路功率输出。它还具有具有接触器感测电路的焊接接触器检测器，感测电路具有从第一线路功率接触器输出连接到地的第一线路分流电阻网络和从第一线路功率接触器输出连接到地的第二线路分流电阻器网络。在另一实施例中，提供了一种EVSE，其包括具有接触器感测电路的焊接式接触器检测器，该接触器检测电路具有连接在热线路继电器输入端和中性线路继电器输出端之间的偏置

87. 发明申请

US20150115890A1 INTEGRATED BATTERY UNIT WITH COOLING AND PROTECTION EXPEDIENTS FOR ELECTRIC VEHICLES 有权
标题翻译：集成电池单元，用于电动车辆的冷却和保护性能
公开(公告)号：US20150115890A1
公开(公告)日：2015-04-30
申请号：US14468279
申请日：2014-08-25
申请人： AEROVIRONMENT, INC.
发明人： Blake E. Dickinson , Larry Hayashigawa
IPC分类号： B60L11/18 , H01M10/625 , H01M10/613 , H01M10/63
CPC分类号： B66F9/07595 , B60L3/0069 , B60L11/1816 , B60L11/185 , B60L11/1874 , H01M2/1077 , H01M10/46 , H01M10/613 , H01M10/625 , H01M10/63 , H01M10/6557 , H01M10/6563 , H01M2220/20 , Y02E60/12
摘要： Methods of and apparatus for removing heat generated by cells of a battery pack. The methods and apparatus may employ one or more fan modules disposed between or next to cells of the battery pack, or one or more fans directly mounted to the battery pack or battery pack case housing the cells. Further, a motor controller isolation system operates to electrically isolate the motor controller of the electric vehicle when the battery pack is being charged. The motor controller isolation system may be integrated with the integrated battery pack and thermal and ventilation system. The integrated system, or “integrated battery unit (IBU),” is preferably manufactured in a manner that requires no, modifications to the electric vehicle in which the IBU is installed.
摘要翻译：用于去除电池组的电池产生的热量的方法和装置。方法和装置可以采用一个或多个风扇模块，该风扇模块设置在电池组单体之间或旁边，或者一个或多个直接安装在容纳电池的电池组或电池组壳体上的风扇。此外，电动机控制器隔离系统操作以在电池组被充电时电隔离电动车辆的电动机控制器。电机控制器隔离系统可与集成电池组和热通风系统集成。集成系统或“集成电池单元（IBU）”优选以不需要修改安装IBU的电动车辆的方式制造。

88. 发明申请

US20150014475A1 Vertical Takeoff and Landing (VTOL) Air Vehicle 审中-公开
标题翻译：垂直起飞和着陆（VTOL）空中飞行器
公开(公告)号：US20150014475A1
公开(公告)日：2015-01-15
申请号：US14270320
申请日：2014-05-05
申请人： AEROVIRONMENT, INC.
发明人： Dana J. Taylor , Phillip T. Tokumaro , Bart Dean Hibbs , William Martin Parks , David Wayne Ganzer , Christopher Eugene Fisher , Jason Sidharthadev Mukherjee , Joseph Frederick King
IPC分类号： B64C27/26 , B64C9/00 , B64C29/00 , B64C27/54 , B64C39/02 , G05D1/08 , B64C5/02 , B64C25/00
CPC分类号： B64C29/0025 , B64C11/32 , B64C27/26 , B64C27/54 , B64C27/605 , B64C29/00 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/165 , B64D27/24 , G05D1/0858
摘要： A flight control apparatus for fixed-wing aircraft includes a first port wing and first starboard wing, a first port swash plate coupled between a first port rotor and first port electric motor, the first port electric motor coupled to the first port wing, and a first starboard swash plate coupled between a first starboard rotor and first starboard electric motor, the first starboard electric motor coupled to the first starboard wing.
摘要翻译：用于固定翼飞行器的飞行控制装置包括第一端口翼和第一右舷翼，第一端口旋转斜盘联接在第一端口转子和第一端口电动机之间，第一端口电动机连接到第一端口翼，第一右舷斜盘联接在第一右舷转子和第一右舷电动机之间，第一右舷电动机联接到第一右舷翼。

89. 发明申请

US20140312745A1 Electric Motor 审中-公开
标题翻译：电动马达
公开(公告)号：US20140312745A1
公开(公告)日：2014-10-23
申请号：US14179428
申请日：2014-02-12
申请人： AeroVironment, Inc.
发明人： William Nicoloff , QinZhong Yu
IPC分类号： H02K1/17 , H02K7/14
CPC分类号： H02K1/17 , H02K7/14 , H02K29/03 , H02K2213/03
摘要： An asymmetric brushless direct current (DC) motor having a stator having a plurality of magnets and a rotor having a plurality of armatures where the vector sum of magnetic forces between each armature and each respective magnet is zero at every angular rotation position of the rotor with respect to the stator in the motor's non-energized state.
摘要翻译：一种具有多个磁体的定子的非对称无刷直流（DC）电动机和具有多个电枢的转子，其中每个电枢和每个相应磁体之间的磁力的矢量和为零，转子的每个角度旋转位置为零，相对于电机处于非通电状态的定子。

90. 发明申请

US20140291443A1 Aircraft Grounding System 有权
标题翻译：飞机接地系统
公开(公告)号：US20140291443A1
公开(公告)日：2014-10-02
申请号：US14149730
申请日：2014-01-07
申请人： AeroVironment, Inc.
发明人： Christopher E. Fisher , John Peter Zwaan , David R. Thompson , Marc L. Schmalzel , Karl R. Klingbiel , Tyson R. Jensen , Pavel Belik , Eric James Aagaard
IPC分类号： B64F1/12
CPC分类号： B64F1/12 , B05B1/02 , B29C65/48 , B29L2031/3076 , B64C39/024 , B64F1/16 , Y10T156/10 , Y10T156/1788
摘要： Liquid dispensing assemblies including adhesive anchoring assemblies configured to adhere to a support surface external to a device such as a vehicle. An air vehicle includes (a) a fluid adhesive container assembly detachably attached to the air vehicle, wherein the fluid adhesive container assembly comprises: (i) an adhesive container comprising fluid adhesive; and (ii) one or more fibers, wherein the one or more fibers are configured, or a brush of fibers, or a fabric of fibers, is configured to conduct the fluid adhesive and to structurally support an adhesive bond between the one or more fibers and a surface; and (b) means for dispensing the fluid adhesive from the fluid adhesive container, to the one or more fibers.
摘要翻译：液体分配组件包括被配置为粘附到诸如车辆的装置外部的支撑表面的粘合剂锚固组件。一种空中交通工具包括（a）可拆卸地附接到空中交通工具的流体粘合剂容器组件，其中流体粘合剂容器组件包括：（i）包含流体粘合剂的粘合剂容器; 和（ii）一种或多种纤维，其中所述一种或多种纤维构成，或纤维刷或纤维织物构造成导电流体粘合剂，并且在结构上支撑所述一种或多种纤维之间的粘合剂结合和表面; 和（b）用于将流体粘合剂从流体粘合剂容器分配到一个或多个纤维的装置。

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