公开(公告)号：US20180093768A1

公开(公告)日：2018-04-05

申请号：US15394473

申请日：2016-12-29

Applicant: SONY INTERACTIVE ENTERTAINMENT INC.

Inventor： Dennis Castleman ,  Ruxin Chen ,  Frank Zhao ,  Glenn Black

IPC: B64C39/02 ,  B64D47/08

CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/06 ,  B64C2201/108 ,  B64C2201/18

Abstract: The present disclosure is related to unmanned aerial vehicles or drones that have a capability of quickly swapping batteries. This may be accomplished even as the drone continues to fly. A drone consistent with the present disclosure may drop one battery and pickup another using an attachment mechanism. Attachment mechanisms of the present disclosure may include electro-magnets, mechanical actuators, pins, or hooks. Systems consistent with the present disclosure may also include locations where replacement batteries may be provided to aircraft via actuation devices coupled to a physical location.

公开(公告)号：US09896196B1

公开(公告)日：2018-02-20

申请号：US15600296

申请日：2017-05-19

Applicant: Kaiser Enterprises, LLC

Inventor： James Kaiser

IPC: B64C27/20 ,  B64D27/04 ,  B64D35/06 ,  B64C27/50 ,  B64D27/24

CPC classification number: B64C27/10 ,  B64C25/06 ,  B64C27/14 ,  B64C27/20 ,  B64C27/50 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/06 ,  B64D17/80 ,  B64D27/24 ,  B64D35/06 ,  B64D2211/00

Abstract: A manned or unmanned aircraft has a main body with a circular shape and a circular outer periphery. One or more rotor blades extend substantially horizontally outward from the main body at or about the circular outer periphery. In addition, one or more counter-rotation blades extend substantially horizontally outward from said main body at or about the circular outer periphery, but vertically offset from the main rotor blades. The rotor blades and counter-rotation blades can be folded upward into a storage position. In addition, the unmanned aircraft can have solar panels positioned about the top housing and fuselage of the aircraft.

公开(公告)号：US20170313272A1

公开(公告)日：2017-11-02

申请号：US15653009

申请日：2017-07-18

Applicant: INTERNATIONAL BUSINESS MACHINES CORPORATION

Inventor： Guillaume Hoareau ,  Johannes J. Liebenberg ,  John G. Musial ,  Todd R. Whitman

IPC: B60R16/04 ,  B60L11/00 ,  B60R16/033

CPC classification number: B60R16/04 ,  B60L11/00 ,  B60R16/033 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/06 ,  B64C2201/066 ,  B64C2201/108 ,  B64C2201/128

Abstract: An apparatus and method for replacing a power source element is provided. The apparatus includes a multiple compartment housing attached to a vehicle, power source elements, a controller, and a communications interface. The power source elements are placed within receptacles of the multiple compartment housing. Each power source element is electrically connected to an input power coupler for electrical connection to the vehicle such that each power source element is configured to supply power to the vehicle independently without requiring power supplied by any other power source element. The controller is configured to monitor a power level of each power source element and generate an associated power level reading. The communication interface is configured to retrieve each associated power level reading from the controller and to an external system.

公开(公告)号：US09771163B2

公开(公告)日：2017-09-26

申请号：US14231003

申请日：2014-03-31

Applicant: The Boeing Company

Inventor： Rich P. Ouellette

IPC: B64D41/00 ,  B64F1/04 ,  B64F3/02 ,  B64D27/24 ,  B64D27/02

CPC classification number: B64D41/00 ,  B64C2201/06 ,  B64C2201/08 ,  B64D27/24 ,  B64D2027/026 ,  B64F1/04 ,  B64F3/02 ,  Y10S903/902

Abstract: Short takeoff and landing aircraft are disclosed. An example fixed wing aircraft includes a primary power source to provide power to a propulsion unit, a secondary power source to provide power to the propulsion unit, and a detachable power coupling to transfer power to the secondary power source from a source external to the fixed wing aircraft during takeoff.

公开(公告)号：US20170256763A1

公开(公告)日：2017-09-07

申请号：US15598914

申请日：2017-05-18

Applicant: AUTEL ROBOTICS CO., LTD.

Inventor： Longxue QIU ,  Xingwen WU

IPC: H01M2/10 ,  B64C39/02

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.

公开(公告)号：US09704292B2

公开(公告)日：2017-07-11

申请号：US15168503

申请日：2016-05-31

Applicant: Lee Priest ,  Charlie Terry ,  Joshua Godwin

Inventor： Lee Priest ,  Charlie Terry ,  Joshua Godwin

IPC: G06T17/05 ,  H04W16/22 ,  G05D1/10 ,  G06T7/00 ,  B64C39/02 ,  B64D47/08 ,  H04W16/20 ,  H04L12/24 ,  G06T7/73 ,  G05D1/00 ,  H04L12/26

CPC classification number: G06T17/05 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/06 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/141 ,  B64D47/08 ,  G05D1/0094 ,  G06T7/337 ,  G06T7/55 ,  G06T7/75 ,  G06T7/97 ,  G06T2200/08 ,  G06T2207/10028 ,  G06T2207/10032 ,  G06T2207/30184 ,  H04L41/145 ,  H04L41/22 ,  H04L43/0811 ,  H04W16/20 ,  H04W16/225

Abstract: A virtual site survey method at a cell site utilizing three-dimensional (3D) models for remote performance includes obtaining a plurality of photographs of a cell site comprising one or more of a cell tower and one or more buildings and interiors thereof; subsequent to the obtaining, processing the plurality of photographs to define a three dimensional (3D) model of the cell site based on one or more objects of interest in the plurality of photographs; and remotely performing a site survey of the cell site utilizing a Graphical User Interface (GUI) of the 3D model to collect and obtain information about the cell site, the cell tower, the one or more buildings, and the interiors thereof.

公开(公告)号：US09623949B2

公开(公告)日：2017-04-18

申请号：US13048625

申请日：2011-03-15

Applicant: Stephen Heppe

Inventor： Stephen Heppe

IPC: B64B1/00 ,  B64C37/02

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.

公开(公告)号：US20170021943A1

公开(公告)日：2017-01-26

申请号：US15291870

申请日：2016-10-12

Applicant: Aurora Flight Sciences Corporation

Inventor： James Peverill ,  Adam Woodworth ,  Benjamin Freudberg ,  Dan Cottrell

IPC: B64F1/02 ,  B60L11/18 ,  B64C39/02

CPC classification number: B64F1/02 ,  B60L11/1816 ,  B60L11/1838 ,  B60L2200/10 ,  B64C25/68 ,  B64C39/024 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/06 ,  B64C2201/066 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/182 ,  B64D47/04 ,  B64D47/08 ,  B64F1/362 ,  G05D1/101 ,  G06K9/0063 ,  Y02T10/7005 ,  Y02T10/7072 ,  Y02T90/121 ,  Y02T90/128 ,  Y02T90/14 ,  Y02T90/16 ,  Y02T90/163

Abstract: A capturing hook for engaging a cable during capture and release of an aerial vehicle may comprise a first and second gate pivotally supported at their first ends by a base portion and each being movable between a closed position and an open position, but spring-biased to the closed position. The capturing hook may further include a latch device comprising a movable locking part biased by a return spring to a locked position to lock the second gate in the closed position.

Abstract translation: 用于在捕捉和释放空中飞行器期间接合电缆的捕获钩可以包括第一和第二门，其第一和第二门在其第一端处由基部枢转地支撑，并且每个可在关闭位置和打开位置之间移动，但是弹簧偏置到 关闭位置。 捕获钩还可以包括闩锁装置，其包括由复位弹簧偏压到锁定位置的可移动锁定部件，以将第二闸门锁定在关闭位置。

公开(公告)号：US20160368590A1

公开(公告)日：2016-12-22

申请号：US15052699

申请日：2016-02-24

Applicant: Karem Aircraft, Inc.

Inventor： Abe Karem ,  Benjamin Tigner

IPC: B64C3/42 ,  B64C39/02 ,  B64D27/24 ,  B64F5/00 ,  G05D1/00

CPC classification number: B64C3/42 ,  B64C3/16 ,  B64C11/28 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/06 ,  B64C2201/104 ,  B64C2201/122 ,  B64C2201/165 ,  B64D27/24 ,  B64D2211/00 ,  B64F5/10 ,  G05D1/0011 ,  G05D1/0088 ,  H02S10/40 ,  H02S20/30 ,  H02S40/38 ,  Y02T50/12 ,  Y02T50/44 ,  Y02T50/62

Abstract: Methods of manufacturing and operating a solar powered aircraft having segmented wings that can be reconfigured during flight to optimize collection of solar energy are described. The aircraft have rigid construction that is resistant to inclement weather and is configured to rely on free flight control at high altitude and under conventional conditions, thereby providing flight duration in excess of 2 months. The aircraft is particularly suitable for use as part of a telecommunications network.

Abstract translation: 描述了制造和操作具有分段翼的太阳能飞行器的方法，其可在飞行期间重新配置以优化太阳能收集。 飞机具有刚性结构，耐恶劣天气，并配置为依靠高空和常规条件下的自由飞行控制，从而提供超过2个月的飞行时间。 该飞机特别适合用作电信网络的一部分。

公开(公告)号：US20160313744A1

公开(公告)日：2016-10-27

申请号：US14693600

申请日：2015-04-22

Applicant: Paul Amelio ,  David Katz ,  Alfonso Amelio

Inventor： Paul Amelio ,  David Katz ,  Alfonso Amelio

IPC: G05D1/10 ,  B64C27/08 ,  B64D47/08 ,  B64C39/02

CPC classification number: G05D1/101 ,  B64C27/08 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/06 ,  B64D47/08 ,  G01R15/142 ,  G01R19/2513 ,  G01R22/063 ,  H04Q9/00 ,  H04Q2209/40 ,  H04Q2209/43

Abstract: A system and method for providing power to and monitoring the energy usage includes at least one electrical control unit having an unmanned vehicle, at least one electrical control unit, a sensor enabled to monitor a given condition; a power source; a processor configured to be in communication with the at least one sensor and said power source, said processor further configured to manage communications with said management system; an unmanned vehicle releasibly coupled to said electrical control unit, said processor being adapted to release said unmanned vehicle to enable the unmanned vehicle to separate from said electrical control unit, wherein said sensor is enabled to monitor at least one of the following: voltage, current, real power, apparent power, reactive power, frequency, total harmonic distortion, arc fault, plug loads, power factor, GFI, AFI, light, temperature, humidity, methane, carbon monoxide, motion, thermal, occupancy, radio frequency, audio, video, infrared, and combinations thereof and wherein said unmanned vehicle can travel to various locations.

Abstract translation: 用于向能量使用提供电力并监测能量使用的系统和方法包括至少一个具有无人驾驶车辆的电气控制单元，至少一个电气控制单元，能够监测给定条件的传感器; 电源; 处理器，被配置为与所述至少一个传感器和所述电源通信，所述处理器还被配置为管理与所述管理系统的通信; 可释放地联接到所述电气控制单元的无人驾驶车辆，所述处理器适于释放所述无人驾驶车辆，以使所述无人驾驶车辆能够与所述电气控制单元分离，其中所述传感器能够监视以下至少一个：电压，电流 ，实际功率，视在功率，无功功率，频率，总谐波失真，电弧故障，插头负载，功率因数，GFI，AFI，光，温度，湿度，甲烷，一氧化碳，运动，热，占用，射频，音频 ，视频，红外及其组合，并且其中所述无人驾驶车辆可以行驶到各个位置。