公开(公告)号：WO2014025444A3

公开(公告)日：2015-06-25

申请号：PCT/US2013042026

申请日：2013-05-21

Applicant: ARLTON PAUL E ,  ARLTON DAVID J

Inventor： ARLTON PAUL E ,  ARLTON DAVID J

IPC: B64C27/00

CPC classification number: B64C27/10 ,  B64C27/24 ,  B64C27/26 ,  B64C27/605 ,  B64C29/02 ,  B64C39/024 ,  B64C2027/8236 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/205 ,  B64C2201/206

Abstract: A rotary wing vehicle includes a body structure having an elongated tubular backbone or core, and a counter-rotating coaxial rotor system having rotors with each rotor having a separate motor to drive the rotors about a common rotor axis of rotation. The rotor system is used to move the rotary wing vehicle in directional flight.

Abstract translation: 旋转翼车辆包括具有细长管状骨架或芯体的主体结构，以及具有转子的反向旋转同轴转子系统，每个转子具有单独的电动机，以围绕公共转子旋转轴线驱动转子。 转子系统用于在定向飞行中移动旋翼机。

公开(公告)号：WO2009048666A2

公开(公告)日：2009-04-16

申请号：PCT/US2008/070598

申请日：2008-07-21

Applicant: KEAVENEY, Kevin

Inventor： KEAVENEY, Kevin

IPC: B64C39/00

CPC classification number: B64C39/024 ,  B64C2201/102 ,  B64C2201/203 ,  B64C2201/206

Abstract: The invention is a method for launching and recovering a child aircraft, manned or unmanned, as well as providing a method for continuous flight to and from a parent aircraft, manned or unmanned, from a pylon that is mounted externally or internally on the parent aircraft. The pylon mechanics are contained within the pylon, and controlled from the parent aircraft, through hard wiring or electronic signals via a data link, facilitated by antennas on both the parent aircraft and the pylon.

Abstract translation: 本发明是一种用于发射和恢复载人或无人驾驶的儿童飞机的方法，以及提供一种方法，用于连续飞行从载客人员或无人驾驶的母机飞行员从外部或内部安装在母飞机上的塔架 。 塔架机械装置包含在塔架内，并由母机通过硬接线或电子信号通过数据链路进行控制，由母机和塔架上的天线辅助。

公开(公告)号：US20180257780A1

公开(公告)日：2018-09-13

申请号：US15454359

申请日：2017-03-09

Applicant: Jeffrey Sassinsky

Inventor： Jeffrey Sassinsky

IPC: B64D5/00 ,  B64C39/02 ,  G08G5/00 ,  B64D47/08 ,  B64D7/00 ,  F41H13/00 ,  F41B13/10 ,  F41H9/00 ,  F41H11/02

CPC classification number: F41H11/02 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/12 ,  B64C2201/182 ,  B64C2201/206 ,  B64D7/00 ,  B64D47/08 ,  B64F1/02 ,  F41B13/10 ,  F41H9/00 ,  F41H9/04 ,  F41H11/04 ,  F41H13/00 ,  F41H13/0012 ,  F41H13/0062

Abstract: The present invention is a device, system(s) and/or method(s) for disrupting, capturing, and/or disabling and unmanned aerial vehicle(s) in flight, on the ground, or preparing for flight that may or may not be under the control of the invention operator. In certain embodiments, the invention is supported and carried by an unmanned aerial vehicle that is controlled by a ground operator, a computer process and associate hardware, or any combination thereof. In other embodiments, the invention contains physical destruction devices such as projectiles, explosives, spikes, electric shock generators, etc. The invention is manipulated to track, intercept, capture, disrupt, disable and/or move a target unmanned aerial vehicle. In certain embodiments, the invention includes materials able to contain, at least in part, hazardous materials and/or conditions caused by the target unmanned aerial vehicle. In certain embodiments, the invention interfaces with external unmanned aerial vehicle detection/tracking systems. A unique design element in certain embodiments is the ability to limit the potential of the captured aerial vehicle escaping the device and/or falling to the ground. Another unique design element in certain embodiments is the ability of the invention to limit collateral damage caused by the captured unmanned aerial vehicle or apparatuses contained thereon. Another unique design element is the ability of the invention to interface with external unmanned aerial vehicle detection/tracking systems.

公开(公告)号：US10035597B2

公开(公告)日：2018-07-31

申请号：US15238200

申请日：2016-08-16

Applicant: Douglas Desrochers ,  David Desrochers

Inventor： Douglas Desrochers ,  David Desrochers

IPC: B64C25/00 ,  B64D1/08 ,  B64C39/02 ,  B64D17/80 ,  B64C1/30

CPC classification number: B64D1/08 ,  B64C1/30 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/082 ,  B64C2201/108 ,  B64C2201/12 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/206 ,  B64D1/10 ,  B64D1/12 ,  B64D17/38 ,  B64D17/80

Abstract: An unmanned aerial system (UAS) including a sonotube deployable multicopter (SDM) having a plurality of rotors for propulsion, a plurality of extension arms, and a central pivot device. Each extension arm supports at least one of the plurality of rotors. The central pivot device supports the plurality of extension arms radially extending from the central pivot device. Pivotal movement of a first arm-support structure of the central pivot device relative to a second arm-support structure of the central pivot device rotates a first pair of the plurality of extension arms in unison relative to a second pair of the plurality of extension arms. The pivotal movement is biased to rotate the plurality of extension arms from a compact configuration to an expanded configuration while the UAS is airborne. The SDM configured to be held inside a sonoshell in the compact configuration.

公开(公告)号：US20170369169A1

公开(公告)日：2017-12-28

申请号：US15375590

申请日：2016-12-12

Applicant: KOREA INSTITUTE OF SCIENCE AND TECHNOLOGY

Inventor： Taikjin LEE ,  Suk Woo NAM ,  Chang Won YOON ,  Hyun Seo PARK ,  Young Min JHON ,  Seok LEE ,  Min-Jun CHOI

IPC: B64D5/00 ,  B64C39/02

CPC classification number: B64D5/00 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/082 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/206

Abstract: The present invention relates to an unmanned aerial vehicle system having a multi-rotor type rotary wing. The unmanned aerial vehicle system having a multi-rotor type rotary wing includes a first unmanned aerial vehicle, at least one second unmanned aerial vehicle, and a bridge that connects the first unmanned aerial vehicle and the at least one second unmanned aerial vehicle to be separable from each other, wherein the at least one second unmanned aerial vehicle is moveable by the first unmanned aerial vehicle in a state where the at least one second unmanned aerial vehicle is coupled to the first unmanned aerial vehicle by the bridge without being driven, and the at least one second unmanned aerial vehicle is separable from the first unmanned aerial vehicle which is in flight.

公开(公告)号：US09849983B2

公开(公告)日：2017-12-26

申请号：US15535431

申请日：2015-12-04

Applicant: ALFRED-WEGENER-INSTITUT

Inventor： Andreas Herber ,  Dirk Kalmbach ,  Ruediger Gerdes ,  Hans-Joerg Bayer

IPC: B64D3/02 ,  B64C39/02 ,  B64C3/16 ,  F41J9/10 ,  B64C1/00

CPC classification number: B64D3/02 ,  B64C3/16 ,  B64C39/022 ,  B64C2001/0045 ,  B64C2201/104 ,  B64C2201/12 ,  B64C2201/141 ,  B64C2201/206 ,  F41J9/10

Abstract: An aerodynamically shaped, active towed body includes a fuselage curved along its vertical and horizontal longitudinal plane. The fuselage has a unit chamber and a load chamber. A transverse plane of the fuselage is triangular, two upper corners being located on an upper face of the fuselage and a lower corner being located on a lower face of the fuselage. Each of two wings is subdivided into a small and a large segment. The small segment points downwards and is attached to the fuselage in a region of the lower corner and the large segment points upwards and is attached to the small segment. Each of the small segments comprise an additional load chamber. The towed body further includes a tail fin, rudders that are each adjustable by the control device and a coupling for the towing cable.

公开(公告)号：US20170297445A1

公开(公告)日：2017-10-19

申请号：US15132255

申请日：2016-04-19

Applicant: SHENZHEN FLYEAH INTELLIGENT TECHNOLOGY CO., LTD.

Inventor： Junxiong ZHENG ,  Daniel Yin LIU ,  Hongyu RAN

IPC: B60L11/18 ,  B64F1/36 ,  B64C39/02 ,  B64D5/00

CPC classification number: B64D5/00 ,  B60L53/14 ,  B60L53/37 ,  B64C37/02 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/066 ,  B64C2201/082 ,  B64C2201/108 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/182 ,  B64C2201/206 ,  B64D2203/00

Abstract: A cone shaped docking and releasing mechanism provides rigid connection between a parent UAV and a sub UAV to form a spliced double unmanned aerial vehicle system with improved cruising duration ability by providing sub UAV battery with charging function. It comprises a parent UAV, a sub UAV and a docking mechanism with charging ports. The parent UAV and the sub UAV are connected with each other through the docking mechanism to form a double UAV system, the docking mechanism is a cone structure and comprises a charging output component connected with the parent UAV internal control system, a charging circuit connected with a sub UAV control system and a charging input component connected with the charging circuit.

公开(公告)号：US20170225802A1

公开(公告)日：2017-08-10

申请号：US15518966

申请日：2015-10-13

Applicant: Systems Engineering Associates Corporation

Inventor： David A. Lussier ,  Andrew Delisle ,  Brian Charpentier

IPC: B64F1/22 ,  B60L11/18 ,  E04H12/18 ,  B63B35/50 ,  G01S19/03 ,  E04H12/00 ,  B64C39/02 ,  B64D47/08

CPC classification number: B64F1/222 ,  B60L53/36 ,  B63B35/50 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/08 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/201 ,  B64C2201/206 ,  B64C2201/208 ,  B64D47/08 ,  B64F1/00 ,  B64F1/007 ,  B64F1/22 ,  E04H12/003 ,  E04H12/18 ,  G01S19/03 ,  H02J7/355 ,  Y02E10/766

Abstract: An unmanned aerial vehicle (UAV) system provides for UAV deployment and remote, unattended operation with reduced logistics requirements. The system includes a launcher that can include one or more containers, or hangars, configured to house vertical take-off and landing (VTOL) UAVs. The system can further include a VTOL UAV orientation and charging module configured to mechanically position a UAV within a container and facilitate electrical mating and charging of a battery in the UAV. These operations, and others, can be performed by remote command that can initiate a series of pre-programmed steps. The UAV system can further include a power generation and storage subsystem, a security subsystem, a command and control subsystem and a communications subsystem. Command, control and communications can be provided between a remote station and the UAV.

公开(公告)号：US20170166308A1

公开(公告)日：2017-06-15

申请号：US15238200

申请日：2016-08-16

Applicant: Douglas Desrochers ,  David Desrochers

Inventor： Douglas Desrochers ,  David Desrochers

IPC: B64D1/08 ,  B64D17/80 ,  B64C1/30 ,  B64C39/02

CPC classification number: B64D1/08 ,  B64C1/30 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/082 ,  B64C2201/108 ,  B64C2201/12 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/206 ,  B64D17/80

Abstract: An unmanned aerial system (UAS) including a sonotube deployable multicopter (SDM) having a plurality of rotors for propulsion, a plurality of extension arms, and a central pivot device. Each extension arm supports at least one of the plurality of rotors. The central pivot device supports the plurality of extension arms radially extending from the central pivot device. Pivotal movement of a first arm-support structure of the central pivot device relative to a second arm-support structure of the central pivot device rotates a first pair of the plurality of extension arms in unison relative to a second pair of the plurality of extension arms. The pivotal movement is biased to rotate the plurality of extension arms from a compact configuration to an expanded configuration while the UAS is airborne. The SDM configured to be held inside a sonoshell in the compact configuration.

公开(公告)号：US20170158326A1

公开(公告)日：2017-06-08

申请号：US15230439

申请日：2016-08-07

Applicant: Korea Aerospace Research Institute

Inventor： Sang Cherl LEE ,  Sun Hee WOO ,  Sang Il AHN ,  Eun Kyou KIM ,  Young Min CHO ,  Dae Hwan HYUN ,  Jin Ho LEE ,  Hae Jin CHOI

IPC: B64C39/02 ,  B64D17/00 ,  B64F1/00

CPC classification number: B64C39/024 ,  B60L53/30 ,  B60L53/51 ,  B60L2200/10 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/082 ,  B64C2201/122 ,  B64C2201/141 ,  B64C2201/18 ,  B64C2201/201 ,  B64C2201/206 ,  B64D1/08 ,  B64D17/00 ,  H04B7/18504 ,  Y02T10/7005 ,  Y02T10/7088 ,  Y02T50/55 ,  Y02T90/12 ,  Y02T90/121 ,  Y02T90/14 ,  Y02T90/16

Abstract: Disclosed herein is an apparatus for remote sensing using a drone. An apparatus for remote sensing using a drone includes: a drone station which communicates with a server through a satellite and includes a containment portion at an upper portion and a post portion at a lower portion; and a drone which is contained in a containment portion of the drone station and communicates with the drone station, and further includes: a solar panel which is installed at the drone station and converts solar energy into electric energy; an capacitor which is installed at the drone station and stores electric energy generated by the solar panel; and a charging container access deck which is installed at the containment portion and charges the drone.