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公开(公告)号：USD1069646S1
公开(公告)日：2025-04-08
申请号：US29885958
申请日：2023-03-02
Applicant: Zipline International Inc.
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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
Applicant: ZIPLINE INTERNATIONAL INC.
Inventor： Paul Perry , Zoltan Laszlo , Scott Parker , Nathan Goldsberry , Bryan Wade , Keenan Wyrobek , Brian Boomgaard , Zhefei Li , Sven Blaser
CPC classification number: B64C39/024 , B64C1/061 , B64C1/068 , B64D17/00 , B64D47/00 , B64U10/25 , B64U30/10 , B64U50/19
Abstract: 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
Applicant: ZIPLINE INTERNATIONAL INC.
Inventor： Paul Perry , Zoltan Laszlo , Scott Parker , Nathan Goldsberry , Bryan Wade , Keenan Wyrobek , Brian Boomgaard , Zhefei Li , Sven Blaser
Abstract: 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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Patent Agency Ranking
公开(公告)号：US10988253B2
公开(公告)日：2021-04-27
申请号：US16051240
申请日：2018-07-31
Applicant: Zipline International Inc.
Inventor： Paul Perry , Zoltan Laszlo , Scott Parker , Nathan Goldsberry , Bryan Wade , Keenan Wyrobek , Brian Boomgaard , Zhefei Li , Sven Blaser
Abstract: 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
Applicant: Zipline International Inc.
Inventor： Paul Perry , Zoltan Laszlo , Scott Parker , Nathan Goldsberry , Bryan Wade , Keenan Wyrobek , Brian Boomgaard , Zhefei Li , Sven Blaser
Abstract: 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：US20240140629A1
公开(公告)日：2024-05-02
申请号：US18278285
申请日：2022-02-23
Applicant: ZIPLINE INTERNATIONAL INC.
Inventor： Brian Boomgaard , Zoltan Laszlo , Keenan A. Wyrobek
IPC: 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 classification number: B64U70/20 , B64D1/08 , B64D1/22 , B64U10/60 , B64U30/297 , B64U80/82 , G05D1/667 , G05D1/678 , B64U2101/64 , B64U2101/67 , G05D2105/20 , G05D2109/20
Abstract: 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：USD1042225S1
公开(公告)日：2024-09-17
申请号：US29885957
申请日：2023-03-02
Applicant: Zipline International Inc.
Designer： 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
Abstract: 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
Applicant: ZIPLINE INTERNATIONAL INC.
Inventor： Keenan A. Wyrobek , Brendan D. Wade , Zoltan Laszlo , Brian Boomgaard , Joshua Liu , Gregoire Vandenbussche , Kevin Nalecz , Radhika Gurumurthy
CPC classification number: B64U80/25 , B64F1/222 , B60L53/14 , B60L2200/10
Abstract: 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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