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公开(公告)号：US10081432B2
公开(公告)日：2018-09-25
申请号：US14917299
申请日：2014-09-05
Applicant: UNIVERSITA DEGLI STUDI DI FIRENZE
Inventor： Guglielmo Rossi , Sandro Moretti , Nicola Casagli
CPC classification number: B64D27/26 , B64C27/08 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/123 , B64C2201/16
Abstract: A structure of drone (100) comprises a frame (110) comprising an engagement portion (110′), said engagement portion (110′) being a strip having a predetermined geometry. The structure of drone (100) also comprises a plurality of propulsion elements (120). Each propulsion element (120) is arranged, in use, to be engaged in a removable way to the engagement portion (110′) at a any point of the strip, in such a way to easily change the number and the arrangement of the propulsion elements (120) present on the engagement portion (110′).
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公开(公告)号：US20180283292A1
公开(公告)日：2018-10-04
申请号：US15953209
申请日：2018-04-13
Applicant: Airbus Defence and Space GmbH
Inventor： Juergen STEINWANDEL , Florian STAGLIANO , Jan VAN TOOR
CPC classification number: F02D29/02 , B64C39/024 , B64C2201/024 , B64C2201/042 , B64C2201/044 , B64C2201/066 , B64C2201/086 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/16 , B64D27/02 , B64D27/24 , B64D31/00 , B64D41/00 , B64D2027/026 , Y02T50/44 , Y02T50/64
Abstract: An unmanned aircraft includes a propulsion system having a diesel or kerosene internal combustion engine and a charger device for engine charging. The propulsion system can be a hybrid propulsion system or a parallel hybrid propulsion system.
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公开(公告)号：US20170025744A1
公开(公告)日：2017-01-26
申请号：US14804170
申请日：2015-07-20
Applicant: Qualcomm Incorporated
Inventor： Karoly Becze , Vincent Martin Kemler , Randy Edward Standke
CPC classification number: H01Q1/28 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/122 , B64C2201/16 , H01Q1/286 , H01Q1/46
Abstract: According to some embodiments, an unmanned vehicle includes a power supply configured to supply an electrical power signal to a motor for propelling the unmanned vehicle, a wireless communication device configured to transmit or receive a radio frequency (RF) signal, and a motor feed antenna coupled to the power supply and the wireless communication device, the motor feed antenna configured to conduct the electrical power signal from the power supply to the motor, and to transmit or receive RF signals as an antenna for the wireless communication device.
Abstract translation: 根据一些实施例，无人驾驶车辆包括被配置为向电动机提供电力信号以推进无人驾驶车辆的电源，被配置为发送或接收射频（RF）信号的无线通信设备以及电动机馈电天线 耦合到所述电源和所述无线通信设备，所述电动馈电天线被配置为将电力信号从所述电源传送到所述电动机，并且发送或接收RF信号作为所述无线通信设备的天线。
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公开(公告)号：US20150285165A1
公开(公告)日：2015-10-08
申请号：US14439502
申请日：2013-10-22
Applicant: EADS DEUTSCHLAND GMBH
Inventor： Juergen Steinwandel , Florian Stagliano , Jan Van Toor
CPC classification number: F02D29/02 , B64C39/024 , B64C2201/024 , B64C2201/042 , B64C2201/044 , B64C2201/066 , B64C2201/086 , B64C2201/088 , B64C2201/104 , B64C2201/108 , B64C2201/16 , B64D27/02 , B64D27/24 , B64D31/00 , B64D41/00 , B64D2027/026 , Y02T50/44 , Y02T50/64
Abstract: An unmanned aircraft includes a propulsion system having a diesel or kerosene internal combustion engine and a charger device for engine charging. The propulsion system can be a hybrid propulsion system or a parallel hybrid propulsion system.
Abstract translation: 无人机包括具有柴油或煤油内燃机的推进系统和用于发动机充气的充电装置。 推进系统可以是混合推进系统或并联混合推进系统。
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公开(公告)号：US20170341769A1
公开(公告)日：2017-11-30
申请号：US15606201
申请日：2017-05-26
Applicant: Neoex Systems, Inc.
Inventor： Mark Steven Haberbusch , Philip Travis Putman
CPC classification number: B64D39/06 , B64C39/024 , B64C2201/063 , B64C2201/16 , B64C2201/18 , B64D37/14 , B64D2041/005 , B64F1/28 , F17C5/007 , F17C5/02 , F17C2205/0355 , F17C2205/037 , F17C2221/012 , F17C2223/0161 , F17C2223/033 , F17C2225/0161 , F17C2225/033 , F17C2227/0107 , F17C2227/0135 , F17C2227/044 , F17C2260/032 , F17C2265/065 , F17C2270/0189
Abstract: A system and method for the transfer of cryogenic fluid fuel includes a nozzle positionable with respect to fuel tank inlet, e.g., of an unmanned aerial vehicle (UAV), a seal to seal the area where the nozzle and inlet are connected, a collapsible and expandable bellows providing an isolation volume where the fluid is transferred from the nozzle into the inlet; a vacuum is provided in the volume to avoid accumulation of fuel or other species in the volume.
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Patent Agency Ranking
公开(公告)号：US20160214728A1
公开(公告)日：2016-07-28
申请号：US14917299
申请日：2014-09-05
Applicant: UNIVERSITA DEGLI STUDI DI FIRENZE
Inventor： Guglielmo ROSSI , Sandro MORETTI , Nicola CASAGLI
CPC classification number: B64D27/26 , B64C27/08 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/123 , B64C2201/16
Abstract: A structure of drone (100) comprises a frame (110) comprising an engagement portion (110′), said engagement portion (110′) being a strip having a predetermined geometry. The structure of drone (100) also comprises a plurality of propulsion elements (120). Each propulsion element (120) is arranged, in use, to be engaged in a removable way to the engagement portion (110′) at a any point of the strip, in such a way to easily change the number and the arrangement of the propulsion elements (120) present on the engagement portion (110′).
Abstract translation: 无人机（100）的结构包括具有接合部分（110'）的框架（110），所述接合部分（110'）是具有预定几何形状的条带。 无人机（100）的结构还包括多个推进元件（120）。 每个推进元件（120）在使用中被布置成以可移除的方式接合到条带的任何点处的接合部分（110'），以便容易地改变推进器的数量和布置 存在于接合部分（110'）上的元件（120）。
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公开(公告)号：US20160096613A1
公开(公告)日：2016-04-07
申请号：US14849814
申请日：2015-09-10
Applicant: Jonathon Thomas Johnson , Elizabeth V.M. Johnson
Inventor： Jonathon Thomas Johnson , Elizabeth V.M. Johnson
CPC classification number: B64C39/024 , B64C25/32 , B64C29/04 , B64C2025/325 , B64C2201/021 , B64C2201/048 , B64C2201/088 , B64C2201/104 , B64C2201/16 , B64C2201/18
Abstract: Current aircraft technology comprises of fixed wing, multi rotor and vectored engine design. The synthesis of fixed wing technology and vectoring engine technology has been implemented but limited to traditional fixed wing design aircraft. The aircraft presented has been designed with an innovation in airframe expectation, improved vectoring engine design system, and landing gear system.
Abstract translation: 目前的飞机技术包括固定翼，多转子和矢量引擎设计。 固定翼技术和矢量引擎技术的综合已经实施，但仅限于传统的固定翼设计飞机。 所提出的飞机设计具有机身预期的创新，改进的矢量引擎设计系统和起落架系统。
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公开(公告)号：US20230259145A1
公开(公告)日：2023-08-17
申请号：US17747142
申请日：2022-05-18
Applicant: Skydio, Inc.
CPC classification number: G05D1/0646 , G05D1/106 , H04W4/021 , B64C39/024 , B64C2201/146 , B64C2201/16
Abstract: An unmanned aerial vehicle (UAV) comprises a flight control system and an electromechanical system directed by the flight control system. The flight control system is configured to track a position of a beacon that is in motion and monitor a difference between an actual position of the unmanned aerial vehicle and a desired position of the unmanned aerial vehicle relative to the position of the beacon. The flight control system configures one or more flight objectives based on one or more factors comprising whether the difference between the actual position and the desired position exceeds a threshold, wherein the flight objectives comprise a velocity objective and a position objective. The flight control system also commands the electromechanical system based at least on the one or more flight objectives.
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公开(公告)号：US09735465B2
公开(公告)日：2017-08-15
申请号：US14804170
申请日：2015-07-20
Applicant: Qualcomm Incorporated
Inventor： Karoly Becze , Vincent Martin Kemler , Randy Edward Standke
CPC classification number: H01Q1/28 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/122 , B64C2201/16 , H01Q1/286 , H01Q1/46
Abstract: According to some embodiments, an unmanned vehicle includes a power supply configured to supply an electrical power signal to a motor for propelling the unmanned vehicle, a wireless communication device configured to transmit or receive a radio frequency (RF) signal, and a motor feed antenna coupled to the power supply and the wireless communication device, the motor feed antenna configured to conduct the electrical power signal from the power supply to the motor, and to transmit or receive RF signals as an antenna for the wireless communication device.
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公开(公告)号：US09567079B2
公开(公告)日：2017-02-14
申请号：US14849814
申请日：2015-09-10
Applicant: Jonathon Thomas Johnson , Elizabeth V. M. Johnson
Inventor： Jonathon Thomas Johnson , Elizabeth V. M. Johnson
CPC classification number: B64C39/024 , B64C25/32 , B64C29/04 , B64C2025/325 , B64C2201/021 , B64C2201/048 , B64C2201/088 , B64C2201/104 , B64C2201/16 , B64C2201/18
Abstract: Current aircraft technology comprises of fixed wing, multi rotor and vectored engine design. The synthesis of fixed wing technology and vectoring engine technology has been implemented but limited to traditional fixed wing design aircraft. The aircraft presented has been designed with an innovation in airframe expectation, improved vectoring engine design system, and landing gear system.
Abstract translation: 目前的飞机技术包括固定翼，多转子和矢量引擎设计。 固定翼技术和矢量引擎技术的综合已经实施，但仅限于传统的固定翼设计飞机。 所提出的飞机设计具有机身预期的创新，改进的矢量引擎设计系统和起落架系统。
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