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公开(公告)号：US20240140629A1
公开(公告)日：2024-05-02
申请号：US18278285
申请日：2022-02-23
IPC分类号： B64U70/20 , B64D1/08 , B64D1/22 , B64U10/60 , B64U30/297 , B64U80/82 , G05D1/667 , G05D1/678 , B64U101/64 , B64U101/67 , G05D105/20 , G05D109/20
CPC分类号： B64U70/20 , B64D1/08 , B64D1/22 , B64U10/60 , B64U30/297 , B64U80/82 , G05D1/667 , G05D1/678 , B64U2101/64 , B64U2101/67 , G05D2105/20 , G05D2109/20
摘要： An autonomous vehicle (AV) delivery system is configured to deliver a payload or package in a rural and/or urban environment. The AV delivery system includes a first autonomous vehicle (AV). The first AV is configured to travel between a payload receiving location and a payload drop location. The AV delivery system further includes a second autonomous vehicle (AV) coupled to the first AV. The second AV is coupled to a payload and configured to travel between the first AV and a designated drop target adjacent to a ground or receiving surface at the payload drop location.
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公开(公告)号：US20240010336A1
公开(公告)日：2024-01-11
申请号：US18039612
申请日：2021-12-01
发明人： Keenan A. Wyrobek , Brendan D. Wade , Tristan Semmelhack , Devin Williams , Gregoire Vandenbussche , Rajan Gill , Brian Boomgaard
CPC分类号： B64D1/08 , B64U10/60 , B64D1/22 , G05D1/104 , B64U2101/64
摘要： A delivery device to deliver a product from an aerial location includes a body defining a payload holding region. The delivery device may further include a coupling mechanism configured to couple the body to a primary vehicle. The delivery device may further include a control feature configured to change a flight characteristic of the body. A method for delivering a product may include positioning a first unmanned aerial vehicle within a threshold distance of a delivery location. The method may further include releasing a second unmanned vehicle from the first unmanned aerial vehicle once the first unmanned aerial vehicle is within the threshold distance. The method may further include causing the second unmanned vehicle to reach the delivery location. The method may further include activating a delivery mechanism to release the product from the second unmanned vehicle to deliver the product to the delivery location.
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公开(公告)号：US11912409B2
公开(公告)日：2024-02-27
申请号：US17234381
申请日：2021-04-19
发明人： Paul Perry , Zoltan Laszlo , Scott Parker , Nathan Goldsberry , Bryan Wade , Keenan Wyrobek , Brian Boomgaard , Zhefei Li , Sven Blaser
CPC分类号： B64C39/024 , B64C1/061 , B64C1/068 , B64D17/00 , B64D47/00 , B64U10/25 , B64U30/10 , B64U50/19
摘要： An unmanned aerial vehicle may include a fuselage and an anchor structure coupled to the fuselage and including a wing retention structure and a power module retention structure. The unmanned aerial vehicle may also include a wing releasably coupled to the wing retention structure, thereby coupling the wing to the fuselage, and a power module releasably coupled to the power module retention structure, thereby coupling the power module to the fuselage.
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公开(公告)号：US20210253244A1
公开(公告)日：2021-08-19
申请号：US17234381
申请日：2021-04-19
发明人： Paul Perry , Zoltan Laszlo , Scott Parker , Nathan Goldsberry , Bryan Wade , Keenan Wyrobek , Brian Boomgaard , Zhefei Li , Sven Blaser
摘要： An unmanned aerial vehicle may include a fuselage and an anchor structure coupled to the fuselage and including a wing retention structure and a power module retention structure. The unmanned aerial vehicle may also include a wing releasably coupled to the wing retention structure, thereby coupling the wing to the fuselage, and a power module releasably coupled to the power module retention structure, thereby coupling the power module to the fuselage.
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公开(公告)号：US10988253B2
公开(公告)日：2021-04-27
申请号：US16051240
申请日：2018-07-31
发明人： Paul Perry , Zoltan Laszlo , Scott Parker , Nathan Goldsberry , Bryan Wade , Keenan Wyrobek , Brian Boomgaard , Zhefei Li , Sven Blaser
摘要： An unmanned aerial vehicle may include a fuselage and an anchor structure coupled to the fuselage and including a wing retention structure and a power module retention structure. The unmanned aerial vehicle may also include a wing releasably coupled to the wing retention structure, thereby coupling the wing to the fuselage, and a power module releasably coupled to the power module retention structure, thereby coupling the power module to the fuselage.
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公开(公告)号：US20190135403A1
公开(公告)日：2019-05-09
申请号：US16051240
申请日：2018-07-31
发明人： Paul Perry , Zoltan Laszlo , Scott Parker , Nathan Goldsberry , Bryan Wade , Keenan Wyrobek , Brian Boomgaard , Zhefei Li , Sven Blaser
摘要： An unmanned aerial vehicle may include a fuselage and an anchor structure coupled to the fuselage and including a wing retention structure and a power module retention structure. The unmanned aerial vehicle may also include a wing releasably coupled to the wing retention structure, thereby coupling the wing to the fuselage, and a power module releasably coupled to the power module retention structure, thereby coupling the power module to the fuselage.
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公开(公告)号：USD1042225S1
公开(公告)日：2024-09-17
申请号：US29885957
申请日：2023-03-02
设计人： Gregoire Vandenbussche , Zoltan Laszlo , Eric Chrisman , Brian Boomgaard , Brendan Doyle Wade , Tristan Semmelhack , Sven Blaser , Frederik Neilsen , Keenan Wyrobek , Scott Johnston , Daniel Ingriselli , Noah Allen
摘要： FIG. 1 is a front isometric view of an aerial vehicle.
FIG. 2 is a bottom isometric view thereof.
FIG. 3 is a front elevation view thereof.
FIG. 4 is a rear elevation view thereof.
FIG. 5 is a right side elevation view thereof.
FIG. 6 is a left side elevation view thereof.
FIG. 7 is a top plan view thereof; and,
FIG. 8 is a bottom plan view thereof.
The broken lines depict portions of the aerial vehicle that form no part of the claimed design.-
公开(公告)号：US20240017860A1
公开(公告)日：2024-01-18
申请号：US18039618
申请日：2021-12-01
发明人： Keenan A. Wyrobek , Brendan D. Wade , Zoltan Laszlo , Brian Boomgaard , Joshua Liu , Gregoire Vandenbussche , Kevin Nalecz , Radhika Gurumurthy
CPC分类号： B64U80/25 , B64F1/222 , B60L53/14 , B60L2200/10
摘要： A docking system for unmanned aerial vehicles (UAVs) includes a docking housing that defines a docking compartment, and a docking assembly coupled to the docking housing and configured to suspend the UAV within the docking compartment. The docking assembly may include a guiding feature configured to receive a docking feature of the UAV and direct the UAV toward a first captured position. The docking assembly may further include an advancement assembly operatively coupled with the guiding feature and configured to move the UAV from the first captured position to a second docked position.
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