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公开(公告)号：EP3057857A1
公开(公告)日：2016-08-24
申请号：EP14854105.5
申请日：2014-10-15
Applicant: ELWHA, LLC
Inventor： HYDE, Roderick A. , WOOD, Lowell L., Jr. , DUNCAN, William David , KARE, Jordin T. , MALASKA, Stephen L. , MYHRVOLD, Nathan P. , PETROSKI, Robert C. , WEAVER, Thomas Allan
CPC classification number: B64C39/024 , B64C39/022 , B64C2201/021 , B64C2201/042 , B64C2201/046 , B64C2201/063 , B64C2201/066 , B64C2201/12 , B64C2201/127 , B64C2201/145 , B64C2201/146 , B64C2201/208 , B64F1/00 , G05D1/0094
Abstract: A motor vehicle system includes a motor vehicle including an aircraft landing portion, and an actively propelled unmanned aircraft configured to be supported on the aircraft landing portion. The vehicle and aircraft are configured such that the vehicle can provide at least one of fuel and electrical energy to the aircraft while the aircraft is supported on the aircraft landing portion.
Abstract translation: 机动车辆系统包括包括飞行器着陆部分的机动车辆和被配置为被支撑在飞行器着陆部分上的主动推进无人飞行器。 车辆和飞行器构造成使得当飞机被支撑在飞行器着陆部分上时，车辆可以向飞机提供燃料和电能中的至少一种。
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公开(公告)号：EP2686238A1
公开(公告)日：2014-01-22
申请号：EP12712014.5
申请日：2012-03-13
Applicant: Heppe, Stephen
Inventor： Heppe, Stephen
CPC classification number: B64B1/32 , B64B1/06 , B64C37/02 , B64C2201/022 , B64C2201/063
Abstract: In one example, a long endurance airship system includes a payload airship and a first logistics airship mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having design capabilities differing by at least a factor of two with regard to at least one of: power generation capability, propulsion capability, endurance capability, and lift capability, in which the first combined airship is free flying, lighter-than-air, and configured to maintain stationkeeping for greater than 30 days. Illustrative methods for long endurance airship operations are also provided.
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公开(公告)号：US10053218B2
公开(公告)日：2018-08-21
申请号：US15087015
申请日：2016-03-31
Applicant: General Electric Company
Inventor： Michael Steven Feldmann , Michael Joseph Dell'Anno , Mauricio Castillo-Effen , James Gerard Lopez , Frank Saggio, III , William J. Berendsen
CPC classification number: B64C39/024 , B64C2201/063 , B64C2201/066 , B64C2201/127 , B64C2201/141 , B64C2201/146 , F03D17/00 , G05D1/0022 , G05D1/0094 , G05D1/101 , H04B7/1851 , H04W4/025
Abstract: A system for positioning an unmanned aerial vehicle is provided including a position reference system including an electromagnetic radiation transmitter configured to modulate a transmission signal to encode location information associated with a coordinate system relative to the electromagnetic radiation transmitter. The system further includes an unmanned aerial vehicle including at least one control device configured to control a position of the unmanned aerial vehicle and an electromagnetic radiation receiver configured to receive the transmission signal. The unmanned aerial vehicle further includes a control system configured to control the at least one control device based at least in part on the location information received by the electromagnetic radiation receiver.
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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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公开(公告)号：US20170285627A1
公开(公告)日：2017-10-05
申请号：US15087015
申请日：2016-03-31
Applicant: General Electric Company
Inventor： Michael Steven Feldmann , Michael Joseph Dell'Anno , Mauricio Castillo-Effen , James Gerard Lopez , Frank Saggio, III , William J. Berendsen
CPC classification number: B64C39/024 , B64C2201/063 , B64C2201/066 , B64C2201/127 , B64C2201/141 , B64C2201/146 , F03D17/00 , G05D1/0022 , G05D1/0094 , G05D1/101 , H04B7/1851 , H04W4/025
Abstract: A system for positioning an unmanned aerial vehicle is provided including a position reference system including an electromagnetic radiation transmitter configured to modulate a transmission signal to encode location information associated with a coordinate system relative to the electromagnetic radiation transmitter. The system further includes an unmanned aerial vehicle including at least one control device configured to control a position of the unmanned aerial vehicle and an electromagnetic radiation receiver configured to receive the transmission signal. The unmanned aerial vehicle further includes a control system configured to control the at least one control device based at least in part on the location information received by the electromagnetic radiation receiver.
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Patent Agency Ranking
公开(公告)号：US09764837B2
公开(公告)日：2017-09-19
申请号：US14942600
申请日：2015-11-16
Applicant: TOP FLIGHT TECHNOLOGIES, INC.
Inventor： Long N. Phan , Sanjay Emani Sarma , Cody Miles Wojcik , Eli M. Davis , Benjamin Arthur Sena , Julian Lemus
IPC: B64C27/08 , B64C39/02 , B64D27/02 , B64C27/00 , B64D33/08 , B64D27/24 , B64D1/08 , B64D1/22 , B64F3/02 , G05D1/10
CPC classification number: B64C39/024 , B64C27/001 , B64C27/08 , B64C2201/027 , B64C2201/042 , B64C2201/044 , B64C2201/063 , B64C2201/066 , B64C2201/108 , B64D1/08 , B64D1/22 , B64D27/02 , B64D27/24 , B64D33/08 , B64D2027/026 , B64D2221/00 , B64F3/02 , G05D1/101 , Y02T50/44 , Y02T50/64
Abstract: An unmanned aerial vehicle comprising at least one rotor motor. The rotor motor is powered by a micro hybrid generation system. The micro hybrid generator system comprises a rechargeable battery configured to provide power to the at least one rotor motor, a small engine configured to generate mechanical power, a generator motor coupled to the small engine and configured to generate AC power using the mechanical power generated by the small engine, a bridge rectifier configured to convert the AC power generated by the generator motor to DC power and provide the DC power to either or both the rechargeable battery and the at least one rotor motor, and an electronic control unit configured to control a throttle of the small engine based, at least in part, on a power demand of at least one load, the at least one load including the at least one rotor motor.
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公开(公告)号：US09751626B2
公开(公告)日：2017-09-05
申请号：US15262177
申请日：2016-09-12
Applicant: Top Flight Technologies, Inc.
Inventor： Long N. Phan , Sanjay Emani Sarma , Cody Miles Wojcik , Eli M. Davis , Benjamin Arthur Sena , Julian Lemus
IPC: B64C27/08 , B64C39/02 , B64D27/02 , B64C27/00 , B64D33/08 , B64D27/24 , B64D1/08 , B64D1/22 , B64F3/02 , G05D1/10
CPC classification number: B64C39/024 , B64C27/001 , B64C27/08 , B64C2201/027 , B64C2201/042 , B64C2201/044 , B64C2201/063 , B64C2201/066 , B64C2201/108 , B64D1/08 , B64D1/22 , B64D27/02 , B64D27/24 , B64D33/08 , B64D2027/026 , B64D2221/00 , B64F3/02 , G05D1/101 , Y02T50/44 , Y02T50/64
Abstract: An unmanned aerial vehicle comprising at least one rotor motor. The rotor motor is powered by a micro hybrid generation system. The micro hybrid generator system comprises a rechargeable battery configured to provide power to the at least one rotor motor, a small engine configured to generate mechanical power, a generator motor coupled to the small engine and configured to generate AC power using the mechanical power generated by the small engine, a bridge rectifier configured to convert the AC power generated by the generator motor to DC power and provide the DC power to either or both the rechargeable battery and the at least one rotor motor, and an electronic control unit configured to control a throttle of the small engine based, at least in part, on a power demand of at least one load, the at least one load including the at least one rotor motor.
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公开(公告)号：US20170197725A1
公开(公告)日：2017-07-13
申请号：US15400796
申请日：2017-01-06
Applicant: Singapore Technologies Aerospace Ltd
Inventor： Chi Hui Frederic FOO , Han Lin HSI
CPC classification number: B64C39/024 , B64C2039/105 , B64C2201/063 , B64C2201/082 , B64C2201/104 , B64C2201/121 , B64C2201/141 , B64C2201/182 , B64C2201/185 , Y02T50/12
Abstract: An apparatus and method for aerial recovery of an unmanned aerial vehicle (UAV) are provided. The apparatus includes a rigid base having a first section and a second section, wherein the first section is securely mounted to a floor of an aircraft. The apparatus further includes a servicing platform moveably mounted to the base and configured to move along a direction parallel to a longitudinal axis of the aircraft such that in an extended position, the servicing platform at least partially protrudes from a rear cargo door of the aircraft, wherein the servicing platform comprises a capturing mechanism configured to capture the UAV in the extended position.
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49.发明申请公开(公告)号：US20150123462A1
公开(公告)日：2015-05-07
申请号：US13998443
申请日：2013-11-01
Applicant: Brian Kamradt
Inventor： Brian Kamradt
CPC classification number: B67D7/845 , B64C39/024 , B64C2201/024 , B64C2201/063 , B64C2201/128 , B64C2201/141 , B64C2201/182 , B67D7/02 , B67D7/0401 , B67D7/78 , B67D2210/00089
Abstract: An unmanned self-sustained fuel dispensing station for fuels of all sorts (gasoline, pesticides, water, fertilizers etc.) a tank, docking, and coupling system for unmanned aerial vehicles (UAV) of the vertical takeoff types. The station can be independent of public power and communication utilities and can operate by remote control without an on-site attendant. The preferred system has a central command center with a control computer in communication with a station control computer located at one or more satellite stations through a communications link. The station control computer can be controlled remotely by the command center. The station control computer programming has control over the activities of the station through an electrical generation subsystem with a solar array, battery bank, battery charger and standby generator; a fuel dispensing subsystem; a security subsystem with video cameras; a communications link and a status sensor subsystem.
Abstract translation: 用于各种类型燃料（汽油，农药，水，肥料等）的无人自助燃料分配站，用于垂直起飞类型的无人机（UAV）的坦克，对接和联接系统。 该站可以独立于公共电力和通信设施，并且可以在没有现场话务员的情况下通过遥控器操作。 优选的系统具有中央指挥中心，控制计算机通过通信链路与位于一个或多个卫星站的台站控制计算机进行通信。 站控制电脑可以由指挥中心远程控制。 台站控制计算机编程通过具有太阳能阵列，电池组，电池充电器和备用发电机的发电子系统控制电站的活动; 燃料分配子系统; 带摄像机的安全子系统; 通信链路和状态传感器子系统。
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公开(公告)号：US20130255986A1
公开(公告)日：2013-10-03
申请号：US13848753
申请日：2013-03-22
Applicant: ICON POLYMER GROUP LIMITED
Inventor： Timothy Denzil Price , Calvin Tan
IPC: F16L11/22
CPC classification number: F16L11/22 , B60L3/0046 , B60L3/0069 , B60L3/04 , B60L53/16 , B60L53/18 , B60L2200/10 , B60L2240/36 , B60L2240/662 , B64C39/024 , B64C2201/063 , B64C2201/066 , B64D39/00 , B64D39/06 , F16L11/127 , H01R12/77 , H01R13/005 , H01R13/6683 , H01R2201/26 , Y02T10/7005 , Y02T10/7088 , Y02T10/7291 , Y02T90/121 , Y02T90/14 , Y02T90/16
Abstract: A hose is disclosed for conveying fluids. The hose has a wall defining a fluid carrying tube and a power and/or data transmission cable is integrated into said wall. Also disclosed is a user definable module that is removably attachable to the distal end of a fluid conveying hose. The hose being releasably connectable to a fluid receiving entity to provide fluid to said entity. The fluid conveying hose has a wall defining a fluid carrying tube and a power and/or data transmission cable integrated into that wall. The user definable module is connectable to the cable and has components to measure at least one measurable parameter at the end of the hose and/or provide electrical connection between the cable and said fluid receiving entity for the transmission of data and/or power along the hose via said user definable interface. Also disclosed is a method of configuring a hose for fluid transfer. The method includes the step of selecting a user definable module and attaching the selected module to a distal end of the hose prior to connecting said hose to a fluid receiving entity.
Abstract translation: 公开了用于输送流体的软管。 软管具有限定流体输送管的壁，并且将功率和/或数据传输电缆集成到所述壁中。 还公开了可拆卸地附接到流体输送软管的远端的用户可定义的模块。 软管可释放地连接到流体接收实体以向所述实体提供流体。 流体输送软管具有限定流体输送管和集成到该壁中的电力和/或数据传输电缆的壁。 用户可定义的模块可连接到电缆，并且具有测量软管端部的至少一个可测量参数的组件和/或在电缆和所述流体接收实体之间提供电连接，用于沿着所述电缆传输数据和/或电力 软管通过用户可定义的界面。 还公开了一种配置用于流体转移的软管的方法。 该方法包括在将所述软管连接到流体接收实体之前，选择用户可定义模块并将所选模块附接到软管的远端的步骤。
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