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公开(公告)号：US20190118971A1
公开(公告)日：2019-04-25
申请号：US16130997
申请日：2018-09-13
申请人： AeroVironment, Inc.
CPC分类号： B64D47/08 , B64C39/024 , B64C2201/127 , B64D9/00 , B64D27/24
摘要： In one possible embodiment, a UAV payload module retraction mechanism is provided including a payload pivotally attached to a housing. A biasing member is mounted to bias the payload out of the housing and a winch is attached to the payload. An elongated flexible drawing member is coupled between the housing and the winch, the elongated drawing flexible member being capable of being drawn by the winch to retract the payload within the housing.
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公开(公告)号：US09957065B2
公开(公告)日：2018-05-01
申请号：US15156077
申请日：2016-05-16
申请人： AeroVironment, Inc.
发明人： Christopher Eugene Fisher , John Peter Zwaan , David R. Thompson , Marc L. Schmalzel , Karl R. Klingbiel , Tyson R. Jensen , Pavel Belik , Eric James Aagaard
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.
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公开(公告)号：US09950790B2
公开(公告)日：2018-04-24
申请号：US14198418
申请日：2014-03-05
申请人： AeroVironment, Inc.
发明人： Matthew Todd Keennon , Karl Robert Klingebiel , Alexander Andryukov , Bart Dean Hibbs , John Peter Zwaan
CPC分类号： B64C33/025 , B64C19/00 , B64C33/02 , B64C2201/025 , B64C2201/10 , B64C2201/146
摘要： Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.
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公开(公告)号：US20180079504A9
公开(公告)日：2018-03-22
申请号：US14198418
申请日：2014-03-05
申请人： AeroVironment, Inc.
发明人： Matthew Todd Keennon , Karl Robert Klingebiel , Alexander Andryukov , Bart Dean Hibbs , John Peter Zwaan
CPC分类号： B64C33/025 , B64C19/00 , B64C33/02 , B64C2201/025 , B64C2201/10 , B64C2201/146
摘要： Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.
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公开(公告)号：US09669947B2
公开(公告)日：2017-06-06
申请号：US14698770
申请日：2015-04-28
申请人： AeroVironment, Inc.
发明人： John Peter Zwaan , Robert James Johnston , Cris James Cornell , Philip Martin Finn , Glenn Arnold Blevins , David Wayne Ganzer
CPC分类号： B64F1/02 , B63B17/00 , B63B35/52 , B64C39/024 , B64C2201/02 , B64C2201/021 , B64C2201/104 , B64C2201/182 , B64C2201/205 , B64F1/025
摘要： Systems, devices, and methods for impacting, by a small unmanned aerial vehicle (SUAV), a net having at least three sides; and converting the kinetic energy of the SUAV into at least one of: elastic potential energy of one or more tensioned elastic cords connected to at least one corner of the net, gravitational potential energy of a frame member connected to at least one corner of the net, rotational kinetic energy of the frame member connected to at least one corner of the net, and elastic potential energy of the frame member connected to at least one corner of the net.
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公开(公告)号：US20160221676A1
公开(公告)日：2016-08-04
申请号：US14949805
申请日：2015-11-23
申请人： AeroVironment Inc.
发明人： Christopher E. Fisher , Phillip T. Tokumaru , Marc L. Schmalzel , John Peter Zwaan , Jeremy D. Tyler , Justin B. McAllister , Gabriel Torres , Pavel Belik
CPC分类号： B64C39/024 , A63H27/12 , B60K1/00 , B60K1/04 , B60K7/0007 , B60K17/356 , B60K2007/0092 , B60Y2200/52 , B63B2035/008 , B63G8/08 , B63G2008/005 , B63H21/17 , B64C27/00 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64D27/00 , B64D27/24
摘要： A quadrotor UAV including ruggedized, integral-battery, load-bearing body, two arms on the load-bearing body, each arm having two rotors, a control module mounted on the load-bearing body, a payload module mounted on the control module, and skids configured as landing gear. The two arms are replaceable with arms having wheels for ground vehicle use, with arms having floats and props for water-surface use, and with arms having pitch-controlled props for underwater use. The control module is configured to operate as an unmanned aerial vehicle, an unmanned ground vehicle, an unmanned (water) surface vehicle, and an unmanned underwater vehicle, depending on the type of arms that are attached.
摘要翻译： 一种四冲程无人机，包括加固的整体电池承载体，承载体上的两个臂，每个臂具有两个转子，安装在承重体上的控制模块，安装在控制模块上的有效载荷模块， 并配置为起落架。 两臂可以用具有地面车辆使用轮子的手臂替代，手臂具有用于水面使用的浮标和道具，并且具有用于水下使用的俯仰控制道具的武器。 控制模块被配置为根据所附接的臂的类型，作为无人驾驶飞行器，无人驾驶地面车辆，无人（水）地面车辆和无人水下航行器运行。
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公开(公告)号：US20230202678A1
公开(公告)日：2023-06-29
申请号：US18095517
申请日：2023-01-10
申请人： AeroVironment, Inc.
CPC分类号： B64D47/08 , B64C39/024 , B64D9/00 , B64D27/24 , B64U2101/30
摘要： In one possible embodiment, a UAV payload module retraction mechanism is provided including a payload pivotally attached to a housing. A biasing member is mounted to bias the payload out of the housing and a winch is attached to the payload. An elongated flexible drawing member is coupled between the housing and the winch, the elongated drawing flexible member being capable of being drawn by the winch to retract the payload within the housing.
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公开(公告)号：US11535361B2
公开(公告)日：2022-12-27
申请号：US16907480
申请日：2020-06-22
申请人： AeroVironment, Inc.
发明人： Pavel Belik , John Peter Zwaan
IPC分类号： B64C9/16 , B64F5/10 , B64C39/02 , B64C13/38 , B64C29/02 , B64D45/00 , B64C9/02 , B64C3/24 , B64C3/36 , B64F5/00
摘要： Systems, devices, and methods for an extruded wing protection and control surface comprising: a channel proximate a leading edge of the control surface, a knuckle disposed about the channel, a leading void, a trailing void, and a separator dividing the leading void and the trailing void; and a plurality of notches disposed in the extruded control surface proximate the leading edge of the control surface.
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公开(公告)号：US20210016896A1
公开(公告)日：2021-01-21
申请号：US17060071
申请日：2020-09-30
申请人： AeroVironment, Inc.
摘要： In one possible embodiment, a UAV payload module retraction mechanism is provided including a payload pivotally attached to a housing. A biasing member is mounted to bias the payload out of the housing and a winch is attached to the payload. An elongated flexible drawing member is coupled between the housing and the winch, the elongated drawing flexible member being capable of being drawn by the winch to retract the payload within the housing.
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公开(公告)号：US20200331584A1
公开(公告)日：2020-10-22
申请号：US16907480
申请日：2020-06-22
申请人： AeroVironment, Inc.
发明人： Pavel Belik , John Peter Zwaan
IPC分类号： B64C9/16 , B64F5/10 , B64C39/02 , B64C13/38 , B64C29/02 , B64D45/00 , B64C9/02 , B64C3/24 , B64C3/36 , B64F5/00
摘要： Systems, devices, and methods for an extruded wing protection and control surface comprising: a channel proximate a leading edge of the control surface, a knuckle disposed about the channel, a leading void, a trailing void, and a separator dividing the leading void and the trailing void; and a plurality of notches disposed in the extruded control surface proximate the leading edge of the control surface.
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