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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
发明人： Tyler P. McNish , Stefan C. Aprodu , Keenan A. Wyrobek , William Hetzler , Bijal Mehta , Ryan Alam
IPC分类号： 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分类号： 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
摘要： 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
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：US11765494B2
公开(公告)日：2023-09-19
申请号：US17138526
申请日：2020-12-30
发明人： Keenan A. Wyrobek , Gavin K. Ananda Krishnan , Brendan J. D. Wade , Philip M. Green , Thomas O. Teisberg , Rohit H. Sant
CPC分类号： H04R1/086 , H04R1/026 , H04R1/028 , H04R2410/07 , H04R2499/13
摘要： 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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公开(公告)号：US20220011786A1
公开(公告)日：2022-01-13
申请号：US17138285
申请日：2020-12-30
发明人： 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
摘要： 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
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：US10029788B2
公开(公告)日：2018-07-24
申请号：US15229099
申请日：2016-08-04
发明人： Peter Abeles , Keenan Wyrobek
摘要： 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：US20240336360A1
公开(公告)日：2024-10-10
申请号：US18628323
申请日：2024-04-05
IPC分类号： B64D1/12
CPC分类号： B64D1/12
摘要： Containers and parachutes for payloads to be delivered via an aerial delivery system are disclosed. In one example, a system for aerial delivery of a payload includes a parachute having a canopy, a plurality of legs extending from the canopy, one or more attachment features arranged on an end of the legs. The system also includes a payload container with a plurality of anchors and where the plurality of anchors are integral with the payload container and receive the one or more attachment features.
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公开(公告)号：US12024283B2
公开(公告)日：2024-07-02
申请号：US17113324
申请日：2020-12-07
发明人： Ethan C. Anderson
CPC分类号： B64C39/024 , H05K9/0007 , H05K9/0015 , H05K9/0037
摘要： A circuit board assembly for association with an aircraft includes a circuit board and an electromagnetic interference component connected to the circuit board. The circuit board assembly may further include an enclosure having an electromagnetic signal permissive layer and an electromagnetic signal blocking layer. The electromagnetic signal permissive layer may include a housing that define a volume. The housing may enclose the electromagnetic interference component on the circuit board. The electromagnetic signal blocking layer defines a conductive barrier about the electromagnetic interference component.
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公开(公告)号：US20230396909A1
公开(公告)日：2023-12-07
申请号：US18233952
申请日：2023-08-15
发明人： Keenan A. Wyrobek , Gavin K. Ananda Krishnan , Brendan J.D. Wade , Philip M. Green , Thomas O. Teisberg , Rohit H. Sant
CPC分类号： H04R1/086 , H04R1/026 , H04R1/028 , H04R2410/07 , H04R2499/13
摘要： 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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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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