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公开(公告)号：US11970293B2
公开(公告)日：2024-04-30
申请号：US17705310
申请日：2022-03-26
申请人： Shaun Passley
发明人： Shaun Passley
IPC分类号： B64U20/50 , B64C3/56 , B64U40/10 , B64C39/02 , B64U30/12 , B64U30/20 , B64U70/80 , B64U101/30
CPC分类号： B64U20/50 , B64C3/56 , B64U40/10 , B64C39/024 , B64U30/12 , B64U30/20 , B64U70/80 , B64U2101/30
摘要： A drone with extendable and rotatable wings and a multiple accessory securing panel is provided. The extendable wings help increase the lift of the drone and reduce the air drag on the drone. The multiple accessory securing panel allows various tools and objects to be temporarily and selectively secured to the drone. The multiple accessories may be secured to the drone by a ground based rotating delivery unit. The drone may have a removable front nose and legs which receive power from a power unit.
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公开(公告)号：US20240025576A1
公开(公告)日：2024-01-25
申请号：US18253372
申请日：2020-12-16
申请人： AERONEXT INC.
发明人： Yoichi SUZUKI
摘要： A landing facility that enables flight vehicles to land safely even in strong winds. The landing system of the invention includes a first area for landing a flight vehicle, a windbreak part having a predetermined height and cover part at least a portion of the perimeter of the first area, and a second area located away from the windbreak part, where the flight vehicle descends to a predetermined flight altitude. The flight altitude is lower than the predetermined height of the windbreak part. The second area is an area selected from a plurality of permitted areas where vertical descent is permitted. A portion of the windbreak part comprises a net.
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公开(公告)号：US11820508B2
公开(公告)日：2023-11-21
申请号：US18058262
申请日：2022-11-22
发明人： Yu Tian
CPC分类号： B64C39/024 , B64U10/00 , B64U70/20 , B64U70/80 , B64U80/82
摘要： A combined vertical takeoff and landing UAV having a large vertical takeoff and landing UAV, a connecting device, and a small vertical takeoff and landing UAV. The connecting device having a clamping component and an adsorption component. The clamping component includes a clamping part, and a clamping groove is arranged on the clamping part. The clamping component having a snap-fitting part, and a snap-fitting groove is arranged on the snap-fitting part. The clamping groove and the snap-fitting groove are correspondingly set. A first holding space is arranged on the clamping part, and a second holding space is arranged on the snap-fitting part. The adsorption component comprises a first magnetic element located in the first holding space, and the adsorption component also comprises a second magnetic element, which is located in the second holding space.
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公开(公告)号：US11760479B2
公开(公告)日：2023-09-19
申请号：US17146944
申请日：2021-01-12
发明人： Kazuo Inoue , Kazunobu Konishi , Stephen John , Katsuhiko Asai , Shunsuke Kuhara
IPC分类号： B64C39/02 , G08G5/00 , B64U30/20 , B64U70/80 , B64U101/00
CPC分类号： B64C39/024 , G08G5/003 , B64U30/20 , B64U70/80 , B64U2101/00 , B64U2201/20
摘要： An unmanned aircraft includes: at least two generators generating forces to fly the unmanned aircraft, each including a rotor blade generating an airflow; a sensor detecting a tilt of the unmanned aircraft; and a processor controlling the generators to control flight of the unmanned aircraft. The processor: obtains an output force adjustment trigger for the generators; obtaining the trigger, causes each generator to individually operate at least until the tilt of the unmanned aircraft detected by the sensor satisfies a predetermined condition; determines a reference value related to an output force of each generator from a value related to the output force of each generator when the tilt of the unmanned aircraft satisfies the predetermined condition and a positional relationship between the generators; and controls the flight of the unmanned aircraft, using the reference values determined.
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公开(公告)号：US11745855B2
公开(公告)日：2023-09-05
申请号：US17106580
申请日：2020-11-30
申请人： Bell Textron Inc.
CPC分类号： B64C11/46 , B64C29/0025 , B64C39/024 , B64U50/13 , B64U70/80
摘要： In an embodiment, an aircraft includes an airframe and a first propulsion assembly coupled to the airframe. The first propulsion assembly includes a first rotor hub and a first plurality of rotor blades non-uniformly spaced about the first rotor hub and operable to rotate in a rotor plane with the first rotor hub. The aircraft also includes a second propulsion assembly coupled to the airframe. The second propulsion assembly includes a second rotor hub and a second plurality of rotor blades non-uniformly spaced about the second rotor hub and operable to rotate in a rotor plane with the second rotor hub.
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公开(公告)号：US12110106B2
公开(公告)日：2024-10-08
申请号：US16949414
申请日：2020-10-28
申请人： Joby Aero, Inc.
摘要： An aerial vehicle may have a fuselage, a first wing member, and a second wing member. The fuselage may have a nose end and a tail end. The first wing member may extend from the fuselage and comprise a first drive motor coupled to the first rotor. The second wing member may also extend from the fuselage substantially opposite the first wing member and may comprise a second drive motor coupled to a second rotor. A first motor may be coupled to rotate the first wing member and the first rotor about a first axis substantially perpendicular to a fuselage axis extending from the nose end to the tail end. A second motor may be coupled to rotate the second wing member and the second rotor about a second axis substantially perpendicular to the fuselage axis. A controller circuit may be configured to differentially actuate the first motor and the second motor.
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公开(公告)号：US20240239525A1
公开(公告)日：2024-07-18
申请号：US18622562
申请日：2024-03-29
申请人： Shaun Passley
发明人： Shaun Passley
IPC分类号： B64U20/50 , B64C3/56 , B64C39/02 , B64U30/12 , B64U30/20 , B64U40/10 , B64U70/80 , B64U101/30
CPC分类号： B64U20/50 , B64C3/56 , B64U40/10 , B64C39/024 , B64U30/12 , B64U30/20 , B64U70/80 , B64U2101/30
摘要： A drone with extendable and rotatable wings and a multiple accessory securing panel is provided. The extendable wings help increase the lift of the drone and reduce the air drag on the drone. The multiple accessory securing panel allows various tools and objects to be temporarily and selectively secured to the drone. The multiple accessories may be secured to the drone by a ground based rotating delivery unit. The drone may have a removable front nose and legs which receive power from a power unit.
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公开(公告)号：US11721008B2
公开(公告)日：2023-08-08
申请号：US17490393
申请日：2021-09-30
申请人： AeroVironment, Inc.
发明人： Phillip T Tokumaru
IPC分类号： G06T7/00 , G06T7/90 , G06T3/40 , B64C39/02 , G06V20/10 , G06V10/143 , G06V20/17 , B64U70/80 , B64U101/30
CPC分类号： G06T7/00 , B64C39/024 , G06T3/4015 , G06T7/90 , G06V10/143 , G06V20/17 , G06V20/188 , B64U70/80 , B64U2101/30 , G06T2207/10024 , G06T2207/10036 , G06T2207/30188
摘要： A method and system including: an aerial vehicle including: a first camera comprising a first sensor having at least red, green, and blue color channels, where the blue color channel is sensitive to near-infrared (NIR) wavelengths; a first optical filter disposed in front of the first sensor, wherein the first optical filter is configured to block wavelengths below green, between red and NIR, and longer wavelength NIR; a processor having addressable memory in communication with the first camera, where the processor is configured to: capture at least one image of vegetation from the first camera; provide red, green, and NIR color channels from the captured image from the first camera; and determine at least one vegetative index based on the provided red, green, and NIR color channels.
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公开(公告)号：US11697498B2
公开(公告)日：2023-07-11
申请号：US17176301
申请日：2021-02-16
申请人： SONY CORPORATION , SONY EUROPE B.V.
发明人： Anders Isberg , Pär Spjuth , Hannes Bergkvist , Peter Exner , Shaun Lee
IPC分类号： B64C39/02 , B64F1/36 , B64F1/10 , G06Q50/28 , G06Q10/0631 , B64U70/80 , B64U101/30 , B64U101/60
CPC分类号： B64C39/024 , B64F1/10 , B64F1/364 , G06Q10/06315 , G06Q50/28 , B64U70/80 , B64U2101/30 , B64U2101/60 , B64U2201/10
摘要： A system performs a control method to launch an unmanned aerial vehicle, UAV. The control method includes calculating a selected altitude, relative to a reference level, for launching the UAV, operating a lifting arrangement to vertically elevate the UAV to the selected altitude, and causing the UAV to be launched from the selected altitude. Elevating the UAV may improve the performance of the UAV in terms of range, power consumption, ability to carry payload, transit time to destination, etc. The selected altitude may be calculated as a function of parameter data representing any of the UAV, the lifting arrangement, or surrounding conditions. An apparatus is further provided to determine an optimal location of the system in relation to a plurality of destinations of UAVs to be elevated by the system.
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公开(公告)号：US20230142923A1
公开(公告)日：2023-05-11
申请号：US17918234
申请日：2021-04-12
发明人： Haroon B. Oqab , George B. Dietrich , Joon Chung , Mohsen Rostami
CPC分类号： G05D1/0038 , G05D1/0044 , G09B9/301 , B64U70/40 , B64U70/80 , G05D1/0027 , B25J9/1612 , G05D1/005 , B64U2201/10
摘要： A system and method for remote control of a mobile device is provided herein. The system includes a primary receiver for providing primary command and control of the mobile device; a secondary receiver for providing secondary command and control of the mobile device; the mobile device configured to respond to command and control signals sent by any of the primary receiver and the secondary receiver; and a relay platform for relaying the command and control signals throughout the system. The primary receiver may include an extended reality component.
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