公开(公告)号：US20180319494A1

公开(公告)日：2018-11-08

申请号：US15970621

申请日：2018-05-03

Applicant: Kamran Aflatoon

Inventor： Kamran Aflatoon

IPC: B64C39/02 ,  B64C27/08

CPC classification number: B64C39/02 ,  B60L11/1822 ,  B64C27/08 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/145 ,  B64C2201/18

Abstract: A roadside assistance system for motorists, comprising a plurality of unmanned aerial vehicles (UAVs) each having an emergency battery power supply connected to an inductive charger, an emergency detachable fuel supply, an imaging system and a visual landing software module configured to land the UAV on a predetermined target. In addition, each has an inductive charging pad electrically connected to a vehicle electrical system, the inductive charging pad bearing the predetermined to by which the UAV may deliver a charge necessary to jump a vehicle or provide an emergency recharge.

公开(公告)号：US20180308130A1

公开(公告)日：2018-10-25

申请号：US15491467

申请日：2017-04-19

Applicant: Usman Hafeez ,  David Mauer

Inventor： Usman Hafeez ,  David Mauer

IPC: G06Q30/02 ,  B64C39/02 ,  G08G5/00 ,  G09F21/10

CPC classification number: G06Q30/0265 ,  B64C39/024 ,  B64C2201/126 ,  G06Q30/0261 ,  G06Q30/0269 ,  G08G5/0069 ,  G09F21/10

Abstract: A method for executing a flight mission by one or more unmanned aerial vehicles is disclosed. The method comprises receiving, from an unmanned aerial vehicle, a data stream containing audience location information; analyzing the audience location information to determine the presence of one or more people; receiving an instruction setting a predetermined number of people; determining whether a number of people at the location is equal to or greater than the predetermined number of people; retrieving a message data file; transmitting the message data file to the unmanned aerial vehicle; and displaying, by the unmanned aerial vehicle, the message data file on a display screen integral to the first unmanned aerial vehicle. In other embodiments, individuals may present visual information to the UAV. The system then selects a response based on the visual information presented to the UAV.

公开(公告)号：US20180281939A1

公开(公告)日：2018-10-04

申请号：US15941133

申请日：2018-03-30

Applicant: The Government of the United States of America, as represented by the Secretary of the Navy

Inventor： Steven K. Tayman

IPC: B64C27/50 ,  B64C27/10 ,  B64C39/02

CPC classification number: B64C27/50 ,  B64C27/10 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/042 ,  B64C2201/08 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/18 ,  B64C2201/201

Abstract: An expendable rotary wing unmanned aircraft capable of storage in a cylindrical housing includes a longitudinally extending body having an upper end and a lower end; and a pair of counter-rotating coaxial rotors each located at respective ends of longitudinally-extending body, wherein each rotor includes two or more blades, each blade rotatably coupled to a remainder of the rotor at a hinged joint and thereby extending along a length of the body in a storage configuration and extending radially outward from the body in a flight configuration.

公开(公告)号：US20180273175A1

公开(公告)日：2018-09-27

申请号：US15914911

申请日：2018-03-07

Applicant: AIRBUS DEFENCE AND SPACE GMBH

Inventor： Marcus KLETTKE

IPC: B64C39/02 ,  G05D1/00 ,  B64D47/02 ,  G08G1/0955

CPC classification number: B64C39/024 ,  B60Q7/00 ,  B64C2201/027 ,  B64C2201/122 ,  B64C2201/126 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/208 ,  B64D47/02 ,  G05D1/0011 ,  G05D1/0094 ,  G08G1/04 ,  G08G1/0955 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0069 ,  G08G5/0078 ,  G08G5/045 ,  H04B7/18504

Abstract: An unmanned aircraft is described. The unmanned aircraft includes a signal output unit and a control unit. The control unit receives at least one signal to be output by the signal output unit. The control unit transmits at least a first signal to the signal output unit, so that the signal output unit outputs the first signal. The unmanned aircraft may be used stand-alone or autonomous as a movable signal output device, but it may also be coupled with a carrier vehicle to meet the function of a signal output device at the carrier vehicle.

公开(公告)号：US20180268719A1

公开(公告)日：2018-09-20

申请号：US15542631

申请日：2015-11-03

Applicant: GUANGZHOU XAIRCRAFT TECHNOLOGY CO., LTD.

Inventor： WULIE GUAN ,  JIAXIANG CHEN ,  YAOLIN HUANG

IPC: G08G5/00 ,  G05D1/10 ,  B64C39/02 ,  G07C5/00

CPC classification number: G08G5/0034 ,  B64C39/024 ,  B64C2201/126 ,  B64C2201/14 ,  G05D1/00 ,  G05D1/101 ,  G07C5/008 ,  G08G5/0013 ,  G08G5/0069

Abstract: The present disclosure relates to a scheduling method and system for an unmanned aerial vehicle, an unmanned aerial vehicle, and a server for scheduling an unmanned aerial vehicle. The method comprises the following steps: obtaining identity feature data of an unmanned aerial vehicle, and sending the identity feature data to a server; receiving a task instruction sent by the server and matching the identity feature data, wherein the task instruction is generated by the server according to a preset task datasheet; performing a corresponding task according to the task instruction. The above scheduling method and system for the unmanned aerial vehicle, the unmanned aerial vehicle, the server for scheduling the unmanned aerial vehicle can achieve large-scale dispatching of unmanned aerial vehicles and facilitate the use of the unmanned aerial vehicle for people.

公开(公告)号：US10019000B2

公开(公告)日：2018-07-10

申请号：US13551287

申请日：2012-07-17

Applicant: Royce A. Levien ,  Richard T. Lord ,  Robert W. Lord ,  Mark A. Malamud ,  John D. Rinaldo, Jr. ,  Lowell L. Wood, Jr.

Inventor： Royce A. Levien ,  Richard T. Lord ,  Robert W. Lord ,  Mark A. Malamud ,  John D. Rinaldo, Jr. ,  Lowell L. Wood, Jr.

IPC: B64C19/00 ,  B64C39/02 ,  G06Q10/02 ,  G07B15/02 ,  G05D1/00 ,  G06F7/76 ,  A61M5/20 ,  G06Q10/08 ,  G06F19/00

CPC classification number: G05D1/00 ,  A61M5/20 ,  B64C39/024 ,  B64C2201/00 ,  B64C2201/12 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/141 ,  G06F7/76 ,  G06F19/3456 ,  G06Q10/08 ,  G16H20/10 ,  G16H40/67

Abstract: Structures and protocols are presented for configuring an unmanned aerial device to perform a task, alone or in combination with other entities, or for using data resulting from such a configuration or performance.

公开(公告)号：US10005556B2

公开(公告)日：2018-06-26

申请号：US15332170

申请日：2016-10-24

Applicant: Mohammad Rastgaar Aagaah ,  Evandro M. Ficanha ,  Nina Mahmoudian

Inventor： Mohammad Rastgaar Aagaah ,  Evandro M. Ficanha ,  Nina Mahmoudian

IPC: B64C39/02 ,  B64D3/00 ,  G05D1/00 ,  F41B11/80 ,  F41H11/02 ,  F41H13/00

CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/12 ,  B64C2201/121 ,  B64C2201/126 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/182 ,  B64D3/00 ,  F41B11/80 ,  F41H11/02 ,  F41H13/0006 ,  G05D1/0094

Abstract: A drone includes a plurality of rotors disposed at and around a base and operable to fly and steer the drone. At least one net launcher is disposed at the base and is operable to launch a net toward a target object. A control is responsive to a signal indicative of a detected target object, and the control, responsive to such a signal, is operable to aim the net launcher toward the target object and to launch the net toward the target object.

公开(公告)号：US20180175495A1

公开(公告)日：2018-06-21

申请号：US15382644

申请日：2016-12-17

Applicant: ANDREW BENNETT ,  Krzysztof Orzel

Inventor： ANDREW BENNETT ,  Krzysztof Orzel

IPC: H01Q1/42 ,  H01Q3/34 ,  H01Q1/00 ,  G01S7/00

CPC classification number: H01Q1/42 ,  B64C1/36 ,  B64C39/024 ,  B64C2201/126 ,  B64C2201/146 ,  B64D47/08 ,  B64F1/362 ,  G01S7/003 ,  G01S13/426 ,  G01S13/66 ,  G01S13/726 ,  G01S13/86 ,  G01S13/87 ,  G01S13/878 ,  G01S13/88 ,  G01S2013/0245 ,  G01S2013/0254 ,  G05D1/0011 ,  H01Q1/005 ,  H01Q1/28 ,  H01Q1/3233 ,  H01Q1/34 ,  H01Q3/34 ,  H01Q21/22

Abstract: A radar enclosure that includes two side wall components, a top aerodynamically streamlined shape component, the two side wall components extending from the base surface to the a top aerodynamically streamlined shape component forming an enclosure cavity, and an antenna supporting component disposed in the enclosure cavity and configured to support a phased array antenna, the phased array antenna being disposed at an angle with respect to a normal to the base surface is disclosed. The networking of the radar with such enclosures increases the radar coverage by adding to the possible collection of locations and thus potentially increasing the data to be analyzed—ultimately increasing the accuracy of the readings.

公开(公告)号：US09922282B2

公开(公告)日：2018-03-20

申请号：US15195735

申请日：2016-06-28

Applicant: LIMITLESS COMPUTING, INC.

Inventor： Errin T. Weller ,  Jeffrey B. Franklin

IPC: G05D1/02 ,  G06K19/07 ,  B64C39/02 ,  B64D47/08 ,  G05D1/00 ,  B64D45/00 ,  G08G5/00 ,  B64F5/10 ,  B64F5/60 ,  G06F3/00 ,  G06F11/00 ,  G06Q10/00 ,  G06Q50/30

CPC classification number: G06K19/0723 ,  B64C39/024 ,  B64C2201/125 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/146 ,  B64D45/00 ,  B64D47/08 ,  B64F5/10 ,  B64F5/60 ,  G06F3/00 ,  G06F3/0482 ,  G06F11/00 ,  G06Q10/00 ,  G06Q50/30 ,  G08G5/0013 ,  G08G5/0026 ,  G08G5/0069

Abstract: Methods and systems for an Automated Readiness Evaluation System (ARES), which is adapted for use with unmanned aircraft systems (UAS). The ARES (and UAS with such an ARES) is configured for a particular task or application selected by the user based upon their level of specific knowledge. The system may include: hardware components with communication protocols; a task, module data, and skill level repository; a user device; and an optional base system. Methods are provided for configuration, calibration, error checking, and operation of a UAS whereby the ARES serves as a mission planner by calculating the mission parameters for a user-selected task to minimize mission failure by determining the variables for task completion.

公开(公告)号：US20180043984A1

公开(公告)日：2018-02-15

申请号：US15233927

申请日：2016-08-10

Applicant: Bell Helicopter Textron Inc.

Inventor： Daniel Bryan Robertson ,  Kirk Landon Groninga ,  Frank Bradley Stamps

IPC: B64C3/10 ,  B64C9/00 ,  B64C39/02

CPC classification number: B64C3/10 ,  B64C9/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/108 ,  B64C2201/126

Abstract: An inflight connection system for aircraft having at least one wing with a wingtip includes, for each aircraft, a primary connector selectively extendable from the wingtip, an alignment connector selectively extendable from the wingtip and a male and female connector assembly disposed proximate the wingtip. The primary connectors extend a greater distance from the wingtips than the alignment connectors such that the primary connectors form a first connection between the aircraft when the aircraft are flying in a connection pattern. Thereafter, retraction of the primary connectors reduces wingtip separation of the aircraft such that the alignment connectors form a second connection between the aircraft establishing coarse alignment therebetween. Thereafter, retraction of the primary and alignment connectors further reduces wingtip separation of the aircraft such that the male and female connector assemblies form a third connection between the aircraft establishing fine alignment therebetween.