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公开(公告)号:US11868143B2
公开(公告)日:2024-01-09
申请号:US17605899
申请日:2020-04-23
申请人: AEROVIRONMENT, INC.
发明人: Derek Lisoski , Bart Dean Hibbs
IPC分类号: G05D1/04 , B64C39/02 , G05D1/00 , B64U101/00
CPC分类号: G05D1/042 , B64C39/024 , G05D1/0005 , B64U2101/00
摘要: Systems, devices, and methods including: at least one unmanned aerial vehicle (UAV); at least one battery pack comprising at least one battery; and at least one motor of the at least one UAV, where the at least one battery is configured to transfer energy to the at least one motor; where power from the at least one motor is configured to ascend the at least one UAV to a second altitude when the at least one battery is at or near capacity, and where the second altitude is higher than the first altitude; and where power from the at least one motor is configured to descend the at least one UAV to the first altitude after the Sun has set to conserve energy stored in the at least one battery.
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公开(公告)号:US20220212789A1
公开(公告)日:2022-07-07
申请号:US17605910
申请日:2020-04-23
申请人: AEROVIRONMENT, INC.
发明人: Derek Lisoski , Bart Dean Hibbs
摘要: Systems, devices, and methods including: at least one unmanned aerial vehicle (UAV); at least one flight control computer (FCC) associated with each UAV, where the FCC controls movement of each UAV; at least one computing device associated with a ground control station; where the at least one FCC maintains a first flight pattern of a respective UAV of the at least one UAV above the ground control station; where the at least one computing device is configured to transmit a transition signal to the at least one FCC to transition the respective UAV of the at least one UAV from the first flight pattern to a second flight pattern in response to a wind speed exceeding a set threshold relative to a flight speed of the respective UAV of the at least one UAV.
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公开(公告)号:US20200023960A1
公开(公告)日:2020-01-23
申请号:US16285958
申请日:2019-02-26
申请人: AEROVIRONMENT, INC.
发明人: Dana J. Taylor , Phillip T. Tokumaru , Bart Dean Hibbs , William Martin Parks , David Wayne Ganzer , Joseph Frederick King
IPC分类号: B64C29/00 , B64C39/02 , G05D1/08 , B64C11/32 , B64C27/605 , B64C29/02 , B64C27/26 , B64C27/54 , B64D27/24
摘要: A flight control apparatus for fixed-wing aircraft includes a first port wing and first starboard wing, a first port swash plate coupled between a first port rotor and first port electric motor, the first port electric motor coupled to the first port wing, and a first starboard swash plate coupled between a first starboard rotor and first starboard electric motor, the first starboard electric motor coupled to the first starboard wing.
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公开(公告)号:US10266258B2
公开(公告)日:2019-04-23
申请号:US15923878
申请日:2018-03-16
申请人: AeroVironment, Inc.
发明人: Matthew Todd Keennon , Karl Robert Klingebiel , Alexander Andryukov , Bart Dean Hibbs , John Peter Zwaan
摘要: Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.
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公开(公告)号:US10103592B2
公开(公告)日:2018-10-16
申请号:US15668577
申请日:2017-08-03
申请人: AeroVironment, Inc.
IPC分类号: H02K9/00 , H02K3/14 , H02K3/30 , H02K3/32 , H02K3/47 , H02K16/02 , H02K7/14 , H02K9/06 , H02K9/14 , H02K9/22 , H02K21/12
摘要: In one possible implementation, a motor is provided including a rotor and a stator. Front cooling fins are thermally coupled to a front of the stator, and rear cooling fins are thermally coupled to a rear portion of the stator. The winding is between the front and rear cooling fins.
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公开(公告)号:US09957044B2
公开(公告)日:2018-05-01
申请号:US14247062
申请日:2014-04-07
申请人: AeroVironment, Inc.
发明人: Matthew Todd Keennon , Karl Robert Klingebiel , Alexander Andryukov , Bart Dean Hibbs , John Peter Zwaan
CPC分类号: B64C33/025 , B64C19/00 , B64C33/02 , B64C2201/025 , B64C2201/10 , B64C2201/146
摘要: Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.
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公开(公告)号:US09750161B2
公开(公告)日:2017-08-29
申请号:US14630819
申请日:2015-02-25
申请人: AeroVironment Inc.
IPC分类号: H05K7/20 , H01L23/36 , H01L23/373 , B64D13/06
CPC分类号: H05K7/20509 , B64D2013/0614 , H01L23/36 , H01L23/373 , H01L2924/0002 , H05K7/20545 , Y10T428/233 , Y10T428/24322 , Y10T428/24661 , Y10T428/24694 , H01L2924/00
摘要: A heat transfer system for use within an avionics bay of an aircraft is provided by the present disclosure that includes, in one form, an aircraft panel comprising an upper skin, a lower skin, and a foam core disposed between the upper skin and the lower skin. At least one heat conducting array extends through the foam core and between the upper skin and the lower skin, the heat conducting array defining at least one upper cap, at least one lower cap, and a wall portion extending between the upper cap and the lower cap, the upper cap being disposed proximate avionics within the avionics bay. A heat conducting spreader is disposed between the lower cap of the heat conducting array and the lower skin of the aircraft panel.
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公开(公告)号:US11581769B2
公开(公告)日:2023-02-14
申请号:US16132420
申请日:2018-09-16
申请人: AeroVironment, Inc.
IPC分类号: H02K3/14 , H02K7/14 , H02K16/02 , H02K9/22 , H02K3/47 , H02K9/14 , H02K9/06 , H02K9/02 , H02K3/30 , H02K3/32 , H02K21/12
摘要: In one possible implementation, a motor is provided including a rotor and a stator. Front cooling fins are thermally coupled to a front of the stator, and rear cooling fins are thermally coupled to a rear portion of the stator. The winding is between the front and rear cooling fins.
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公开(公告)号:US20230017339A1
公开(公告)日:2023-01-19
申请号:US17783486
申请日:2020-12-07
申请人: AEROVIRONMENT, INC.
发明人: Bart Dean Hibbs
摘要: Systems, devices, and methods for: an unmanned aerial vehicle (UAV); at least one sensorless motor of the UAV, the at least one sensorless motor comprising a set of windings and a rotor; at least one propeller connected to the at least one sensorless motor; a microcontroller in communication with the at least one sensorless motor, wherein the microcontroller is configured to: determine a rotation rate of the at least one propeller; determine a rotation direction of the at least one propeller; provide an output to stop the at least one propeller if at least one of: the determined rotation rate is not a desired rotation rate and the determined rotation direction is not a desired rotation direction; and provide an output to start the at least one propeller if the at least one propeller is stopped at the desired rotation rate and the desired rotation direction.
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公开(公告)号:US20220177113A1
公开(公告)日:2022-06-09
申请号:US17684019
申请日:2022-03-01
申请人: AEROVIRONMENT, INC.
发明人: Bart Dean Hibbs
摘要: Systems, devices, and methods including an unmanned aerial vehicle (UAV); one or more inner wing panels of the UAV; one or more outer wing panels of the UAV; at least one inboard propeller attached to at least one engine disposed on the one or more inner wing panels; at least one tip propeller attached to at least one engine disposed on the one or more outer wing panels; at least one microcontroller configured to: determine an angular position of the at least one inboard propeller; and send a signal to halt rotation of the at least one inboard propeller such that the at least one inboard propeller is held in an attitude that provides for clearance of the propeller blade to the ground upon landing.
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