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Patent Agency Ranking
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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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：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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