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公开(公告)号：US09975632B2
公开(公告)日：2018-05-22
申请号：US15095011
申请日：2016-04-08
Applicant: Drona, LLC
Inventor： Loren Alegria
CPC classification number: B64C39/022 , B64C39/024 , B64C2201/027 , B64C2201/06 , B64C2201/141 , B64D47/08 , G01C21/005 , G01C21/165 , G01S13/9303 , G01S15/02 , G01S17/933 , G01S19/13 , G05D1/0011
Abstract: A system is provided for maneuvering a payload in an air space constrained by one or more obstacles, and may include first and second aerial vehicles coupled by a tether to a ground station. Sensor systems and processors in the ground station and aerial vehicles may track obstacles and the tether's and the vehicles' positions and attitude to maneuver the payload and the tether to carry out a mission. The sensor system may include airborne cameras providing data for a scene reconstruction process and simultaneous mapping of obstacles and localization of aerial vehicles relative to the obstacles. The aerial vehicles may include a frame formed substantially of a composite material for preventing contact of the rotors with the tether segments.
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公开(公告)号：US20180086458A1
公开(公告)日：2018-03-29
申请号：US15712526
申请日：2017-09-22
Applicant: Unmanned Innovation Inc. (dba Airware)
Inventor： Thomas Skyler Sartorius , Calder Richmond Hughes , Julian Rene Alvarez , Sean David-Andrew Belardo
CPC classification number: B64C39/024 , B64C1/26 , B64C3/187 , B64C2201/021 , B64C2201/042 , B64C2201/06 , B64C2201/104 , B64C2201/146 , B64C2201/165 , B64C2211/00 , B64D9/00
Abstract: Disclosed here are unmanned aerial vehicle embodiments including some embodiments having a fuselage, tail, and wings including example embodiments with an adaptable payload section, alternatively or additionally, modular flight surfaces including tail, wings and motor, alternatively or additionally the vehicle configured for short landings with reversible thrust, alternatively or additionally, the unmanned aerial vehicle configured with direct connection to moveable flight control surfaces.
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公开(公告)号：US20180076431A1
公开(公告)日：2018-03-15
申请号：US15812836
申请日：2017-11-14
Applicant: AUTEL ROBOTICS CO., LTD
Inventor： Longxue QIU , Xingwen WU
CPC classification number: H01M2/1083 , B64C39/024 , B64C2201/042 , B64C2201/06 , H01M2220/20
Abstract: The present invention discloses an unmanned aerial vehicle and a battery thereof. The battery includes a battery body and a shell disposed on one end of the battery body. The shell has a clamp button disposed on the side opposite the unmanned aerial vehicle. One end of the clamp button is fixed on the shell and the other is used for detachably connecting with the unmanned aerial vehicle. The clamp button makes the battery detachably connect with the main body of the unmanned aerial vehicle be possible and it is very convenient for changing the battery.
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公开(公告)号：US20180069217A1
公开(公告)日：2018-03-08
申请号：US15812805
申请日：2017-11-14
Applicant: AUTEL ROBOTICS CO., LTD
Inventor： Longxue QIU , Xingwen WU
CPC classification number: H01M2/1083 , B64C39/024 , B64C2201/042 , B64C2201/06 , H01M2220/20
Abstract: The present invention discloses an unmanned aerial vehicle and a battery thereof. The battery includes a battery body and a shell disposed on one end of the battery body. The shell has a clamp button disposed on the side opposite the unmanned aerial vehicle. One end of the clamp button is fixed on the shell and the other is used for detachably connecting with the unmanned aerial vehicle. The clamp button makes the battery detachably connect with the main body of the unmanned aerial vehicle be possible and it is very convenient for changing the battery.
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公开(公告)号：US20180069216A1
公开(公告)日：2018-03-08
申请号：US15812773
申请日：2017-11-14
Applicant: AUTEL ROBOTICS CO., LTD
Inventor： Longxue QIU , Xingwen WU
CPC classification number: H01M2/1083 , B64C39/024 , B64C2201/042 , B64C2201/06 , H01M2220/20
Abstract: The present invention discloses an unmanned aerial vehicle and a battery thereof. The battery includes a battery body and a shell disposed on one end of the battery body. The shell has a clamp button disposed on the side opposite the unmanned aerial vehicle. One end of the clamp button is fixed on the shell and the other is used for detachably connecting with the unmanned aerial vehicle. The clamp button makes the battery detachably connect with the main body of the unmanned aerial vehicle be possible and it is very convenient for changing the battery.
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Patent Agency Ranking
公开(公告)号：US20170313419A1
公开(公告)日：2017-11-02
申请号：US15642069
申请日：2017-07-05
Applicant: The Boeing Company
CPC classification number: B64C39/024 , B64C2201/06 , B64C2201/141 , B64D31/14 , B64D41/00 , B64D2041/005 , B64D2211/00 , B64D2221/00 , G05B13/0275 , G05D1/0005 , Y02T50/55 , Y02T90/36
Abstract: Power management method and system for an unmanned air vehicle, wherein the unmanned air vehicle comprises a plurality of power demanding subsystems and a plurality of power sources. The invention establishes mission oriented fixed parameters. A fuzzy logic power management unit, comprised in the system, automatically calculates and assigns priorities for delivering power to the subsystems. It also automatically calculates and assigns amounts of power delivered to each subsystem and automatically decides which of the power sources to deliver power to which subsystem. The fuzzy logic power management system calculates and assigns the priorities and loads in function of a plurality of internal variables, external variables and the mission oriented fixed parameters.
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公开(公告)号：US20170297672A1
公开(公告)日：2017-10-19
申请号：US15297051
申请日：2016-10-18
Applicant: STRATOSPHERIC AIRSHIPS, LLC
Inventor： Stephen B. Heppe
CPC classification number: B64B1/00 , B64C37/02 , B64C2201/022 , B64C2201/06
Abstract: In one example, a long endurance airship system includes a first combined airship with a payload airship and a first logistics airship. The first combined airship is configured for stationkeeping at a predetermined station during meteorological conditions with wind speeds below a predetermined threshold. The airship system also includes a second combined airship which is a reconfiguration of the first combined airship and includes the payload airship and a second logistics airship. The second combined airship is configured for stationkeeping at the predetermined station in all meteorological conditions, including meteorological conditions with wind speeds above the predetermined threshold.
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公开(公告)号：US09688415B2
公开(公告)日：2017-06-27
申请号：US14963716
申请日：2015-12-09
Applicant: AAI Corporation
Inventor： Brandon R. Hall
CPC classification number: B64D37/04 , B64C39/024 , B64C2201/021 , B64C2201/06 , B64D37/06 , B64D37/16
Abstract: An aircraft hybrid fuel system includes a main tank and a set of flexible bladders, the main tank and the set of flexible bladders defining a fuel containment space. The system further includes a set of pathways coupling the set of flexible bladders to the main tank. The set of pathways is constructed and arranged to vent gas out of the set of flexible bladders into the main tank while fuel from a fuel source is provided into the fuel containment space defined by the main tank and the set of flexible bladders. Along these lines, each flexible bladder can be provisioned with a fuel port to provide fuel, and a separate vent port to vent gas to the main tank.
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公开(公告)号：US09646205B2
公开(公告)日：2017-05-09
申请号：US14830987
申请日：2015-08-20
Applicant: HCL Technologies Ltd.
Inventor： Siva Sakthivel Sadasivam , Murali Krishnaan G , Vishal Chaudhary
CPC classification number: G06K9/00536 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/06 , B64C2201/066 , B64C2201/123 , B64C2201/126 , B64C2201/141 , B64C2201/146 , B64C2201/148 , G06K9/627 , G06K2209/19
Abstract: Disclosed is a system and method for facilitating testing of a plurality of devices using a drone. At first, a locating module locates position of the drone relative to the plurality of devices. Further, a receiving module receives an image, of a device of the plurality of devices, from image capturing unit of the drone. Then, a comparing module compares the image with a reference image corresponding to the device. Based on the comparison, a determining module determines an action to be performed for testing the device. Further, a facilitating module facilitates the testing by enabling a snout associated with the drone to perform the action on the device.
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60.发明申请公开(公告)号：US20160046387A1
公开(公告)日：2016-02-18
申请号：US14462152
申请日：2014-08-18
Applicant: Sunlight Photonics Inc.
Inventor： SERGEY V. FROLOV , MICHAEL CYRUS , ALLAN J. BRUCE , JOHN PETER MOUSSOURIS
IPC: B64D47/00 , B64D35/02 , B64C19/00 , B64D31/00 , H04B7/185 , B64B1/00 , G08G5/00 , G05D1/10 , G08G5/04 , B64D33/00 , B64C39/02
CPC classification number: B64D47/00 , B64B1/00 , B64C19/00 , B64C39/02 , B64C2201/022 , B64C2201/042 , B64C2201/06 , B64C2201/122 , B64C2201/143 , B64D31/00 , B64D33/00 , B64D35/02 , G05D1/104 , G08G5/0069 , H04B7/18508
Abstract: Embodiments of methods and apparatus for providing distributed airborne wireless communications are provided herein. In some embodiments, a communication fleet includes: an airborne communication payload subdivided into multiple payload sections; and a plurality of airborne platforms each including a payload section, wherein each airborne platform comprises an airframe, a propulsion system, a power system, and flight control electronics, wherein the propulsion system is configured to provide propulsion power and thrust to maintain level flight, ascend, descend and maneuver the airborne platform, wherein the power system provides electrical power to the propulsion system, the flight control electronics, and the payload section, and wherein the flight control electronics provide capability to control a position, speed, and flight pattern of the airborne platform.
Abstract translation: 本文提供了用于提供分布式机载无线通信的方法和装置的实施例。 在一些实施例中，通信车队包括：被分为多个有效载荷部分的机载通信有效载荷; 以及多个机载平台，每个机载平台各自包括有效载荷部分，其中每个机载平台包括机体，推进系统，电力系统和飞行控制电子设备，其中所述推进系统被配置为提供推进力和推力以维持水平飞行， 上升，下降和操纵机载平台，其中电力系统向推进系统，飞行控制电子装置和有效载荷部分提供电力，并且其中飞行控制电子装置提供控制位置，速度和飞行模式的能力 机载平台。
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