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公开(公告)号：US10395543B2
公开(公告)日：2019-08-27
申请号：US15659735
申请日：2017-07-26
Applicant: Zipline International Inc.
Inventor： Andrew Chambers , Bryan Wade , Catalin Drula , David Halley , Igor Napolskikh , Keenan Wyrobek , Keller Rinaudo , Nicholas Brake , Ryan Oksenhorn , Ryan Patterson , William Hetzler
Abstract: An Unmanned Aerial System configured to receive a request from a user and fulfill that request using an Unmanned Aerial Vehicle. The Unmanned Aerial System selects a distribution center that is within range of the user, and deploys a suitable Unmanned Aerial Vehicle to fulfill the request from that distribution center. The Unmanned Aerial System is configured to provide real-time information about the flight route to the Unmanned Aerial Vehicle during its flight, and the Unmanned Aerial Vehicle is configured to dynamically update its mission based on information received from the Unmanned Aerial System.
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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：US11958629B2
公开(公告)日：2024-04-16
申请号：US17388963
申请日：2021-07-29
Applicant: ZIPLINE INTERNATIONAL INC.
Inventor： Tyler P. McNish , Stefan C. Aprodu , Keenan A. Wyrobek , William Hetzler , Bijal Mehta , Ryan Alam
IPC: B64F1/222 , B64C39/02 , B64F1/02 , B64F1/04 , B64F1/06 , B64F1/32 , B64U10/25 , B64U30/10 , B64U50/19 , B64U70/00 , B64U70/30 , B64U80/00 , B64U101/60
CPC classification number: B64F1/222 , B64C39/024 , B64F1/029 , B64F1/04 , B64F1/06 , B64F1/32 , B64U10/25 , B64U30/10 , B64U50/19 , B64U70/00 , B64U70/30 , B64U80/00 , B64U2101/60
Abstract: Described herein is an elevated unmanned aerial vehicle (UAV) station. The elevated UAV station includes an elevated platform and a conveyance device configured to raise a payload to the elevated platform. The elevated unmanned UAV station may further include a launch device configured to cause a takeoff of a UAV from the elevated platform. The elevated UAV station may further include a recovery device configured to cause a controlled landing of the UAV at the elevated platform. The elevated UAV station may be associated with a payload housing structure to establish a system for payload storage and launch.
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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：US11765494B2
公开(公告)日：2023-09-19
申请号：US17138526
申请日：2020-12-30
Applicant: ZIPLINE INTERNATIONAL INC.
Inventor： Keenan A. Wyrobek , Gavin K. Ananda Krishnan , Brendan J. D. Wade , Philip M. Green , Thomas O. Teisberg , Rohit H. Sant
CPC classification number: H04R1/086 , H04R1/026 , H04R1/028 , H04R2410/07 , H04R2499/13
Abstract: Described herein is a sensor probe for association with a portion of an aircraft. The sensor probe includes a microphone assembly having a portion configured to receive audio signals. The sensor probe further includes a nosecone associated with the microphone assembly. The nosecone assembly is configured to shield the portion of the microphone assembly from noise generated by direct impact of an airflow for a plurality of local flow angles.
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Patent Agency Ranking
公开(公告)号：US20220011786A1
公开(公告)日：2022-01-13
申请号：US17138285
申请日：2020-12-30
Applicant: ZIPLINE INTERNATIONAL INC.
Inventor： Thomas O. Teisberg , Rohit H. Sant , Matthew O. Derry , Michael J. Demertzi , Gavin K. Ananda Krishnan , Keenan A. Wyrobek , Vasumathi Raman , Brendan J.D. Wade , Blair R. Hagen , Randall R. Patterson , Philip M. Green
Abstract: An acoustic detection system of an aircraft receives a first signal, where the first signal is a multichannel audio signal. The multichannel audio signal is determined to be associated with at least one intruding aircraft based on the multichannel audio signal. An avoidance maneuver is commanded for the aircraft based on a track of the intruding aircraft generated based on the multichannel audio signal and a second signal providing additional information about the intruding aircraft.
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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：US10328805B1
公开(公告)日：2019-06-25
申请号：US14872974
申请日：2015-10-01
Applicant: Romotive, Inc.
Inventor： Keenan Wyrobek , James Laird Martz, III , Keller Rinaudo
Abstract: An electric vehicle system includes a battery management system that optimizes the performance and useful life of vehicle batteries by selecting the optimal batteries in an inventory for each electric vehicle mission based on the mission energy requirements, the energy storage capacities of batteries, and the predicted performance degradation of batteries.
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公开(公告)号：US10029788B2
公开(公告)日：2018-07-24
申请号：US15229099
申请日：2016-08-04
Applicant: Zipline International Inc.
Inventor： Peter Abeles , Keenan Wyrobek
Abstract: An unmanned aircraft system includes a testing and calibration system that enables automated testing of movable parts of an unmanned aircraft. The testing and calibration system uses a camera-based technique to determine the position and angle of movable parts, in order to establish whether or not those parts are moving in a manner consistent with correct function.
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公开(公告)号：US12155982B2
公开(公告)日：2024-11-26
申请号：US18233952
申请日：2023-08-15
Applicant: ZIPLINE INTERNATIONAL INC.
Inventor： Keenan A. Wyrobek , Gavin K. Ananda Krishnan , Brendan J. D. Wade , Philip M. Green , Thomas O. Teisberg , Rohit H. Sant
Abstract: Described herein is a sensor probe for association with a portion of an aircraft. The sensor probe includes a microphone assembly having a portion configured to receive audio signals. The sensor probe further includes a nosecone associated with the microphone assembly. The nosecone assembly is configured to shield the portion of the microphone assembly from noise generated by direct impact of an airflow for a plurality of local flow angles. In some examples, the nosecone includes a tip and a body portion, wherein a diameter of the body portion of the nosecone is smaller than a length of the nosecone and the nosecone is configured to mitigate drag of the sensor probe in an airflow. In some examples, the nosecone further includes a mount assembly downstream of the nosecone and positioned rearward of the tip and including a mount aperture in fluid communication within an external environment of the sensor probe and configured to direct airflow from the external environment rearward, the microphone positioned downstream of the mount assembly and secured in a perpendicular orientation relative to a direction of airflow exiting the mount aperture, and an acoustic corridor to transmit the audio signal extending from an opening at an external environment of the sensor probe to the microphone via the mount aperture, wherein the opening is defined by a side of the nosecone.
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