-
公开(公告)号：US20170228692A1
公开(公告)日：2017-08-10
申请号：US15018696
申请日：2016-02-08
Applicant: Brandon Thomas Pargoe
Inventor： Brandon Thomas Pargoe
IPC: G06Q10/08 , G07C9/00 , H04W4/02 , A61J1/00 , G05B11/01 , B65D43/16 , B65D43/26 , B65D81/38 , B64C39/02 , H04W4/00
CPC classification number: G06Q10/0836 , A47G29/141 , A47G2029/147 , B64C39/024 , B64C2201/042 , B64C2201/128 , B64C2201/201 , B65D43/16 , B65D43/26 , B65D81/3813 , G06Q10/0832 , G07C9/00563 , G07C9/00896 , G07C2009/0092 , H04W4/021 , H04W4/80
Abstract: Certain exemplary embodiments can provide an AirBox constructed to receive deliveries from a drone. The AirBox can comprise an automatically openable lid; and a wireless receiver that is constructed to receive data concerning a delivery from the drone. The automatically openable lid can open to receive the delivery from the drone.
-
302.发明申请公开(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
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：US20170197765A1
公开(公告)日：2017-07-13
申请号：US15468461
申请日：2017-03-24
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor： Dengfeng HU , Aiqing LIU
CPC classification number: B65D45/18 , B25H3/02 , B64C39/024 , B64C2201/042 , B64C2201/066 , B64C2201/201 , B65D25/2852 , B65D43/163 , B65D45/20 , B65D85/68 , B65D2255/00 , B65D2585/687 , H02J7/0044 , H02J7/0045 , H02J7/0068
Abstract: A case comprises a case body, a case cover, and a snap-fitting assembly comprising a snap-fitting member and a connecting member for fastening the case cover and the case body. The connecting member comprises a first end and a second end opposite to each other. The first end of the connecting member is rotatably connected to one of the case body and the case cover. The other one of the case body and the case cover is provided with a snapping block. The second end of the connecting member is rotatably connected to the snap-fitting member. The snap-fitting member comprises a snapping part configured to be snapped with the snapping block.
-
公开(公告)号：US20170166305A1
公开(公告)日：2017-06-15
申请号：US15175161
申请日：2016-06-07
Applicant: Paul E. Arlton , David J. Arlton
Inventor： Paul E. Arlton , David J. Arlton
IPC: B64C27/605 , B64C39/02 , B64C27/14 , B64C27/10
CPC classification number: B64C27/605 , B64C7/00 , B64C27/10 , B64C27/14 , B64C39/024 , B64C2027/8236 , B64C2027/8281 , B64C2201/027 , B64C2201/042 , B64C2201/082 , B64C2201/102 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/201 , B64C2201/203 , B64C2201/205
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.
-
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
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.
-
Patent Agency Ranking
306.发明申请公开(公告)号：US20170158319A1
公开(公告)日：2017-06-08
申请号：US15434735
申请日：2017-02-16
Applicant: Hood Technology Corporation
CPC classification number: B64C27/32 , B64C1/30 , B64C11/48 , B64C25/10 , B64C27/26 , B64C39/024 , B64C2201/021 , B64C2201/027 , B64C2201/082 , B64C2201/108 , B64C2201/12 , B64C2201/182 , B64C2201/201 , B64C2201/206 , B64D3/00 , B64D5/00 , B64D2221/00 , B64F1/02 , B64F1/04
Abstract: The present disclosure provides various embodiments of a multicopter-assisted launch and retrieval system generally including: (1) a multi-rotor modular multicopter attachable to (and detachable from) a fixed-wing aircraft to facilitate launch of the fixed-wing aircraft into wing-borne flight; (2) a storage and launch system usable to store the modular multicopter and to facilitate launch of the fixed-wing aircraft into wing-borne flight; and (3) an anchor system usable (along with the multicopter and a flexible capture member) to retrieve the fixed-wing aircraft from wing-borne flight.
-
307.发明申请公开(公告)号：US20170144776A1
公开(公告)日：2017-05-25
申请号：US15042053
申请日：2016-02-11
Applicant: AeroVironment, Inc.
CPC classification number: B64F1/222 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/088 , B64C2201/182 , B64C2201/201 , B64F1/005 , B64F1/02 , B64F1/04 , B64F1/24
Abstract: An unmanned aerial vehicle (UAV) storage and launch system, including: a UAV pod having an interior; and a telescoping UAV landing surface disposed in the interior of the UAV pod; where the telescoping UAV landing surface may translate up toward a top opening of the UAV pod, translate down into an interior of the UAV pod, or rotate relative to the UAV pod.
-
308.发明授权公开(公告)号：US09650133B2
公开(公告)日：2017-05-16
申请号：US15042090
申请日：2016-02-11
Applicant: AeroVironment, Inc.
CPC classification number: B64F1/005 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/066 , B64C2201/088 , B64C2201/104 , B64C2201/12 , B64C2201/141 , B64C2201/165 , B64C2201/18 , B64C2201/201 , B64F1/12
Abstract: A vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV) system including: a rearward facing tang extending from a rear fuselage portion of a VTOL UAV; one or more metallic contacts disposed on an exterior surface of the tang; a UAV pod including a landing surface; and an opening disposed in the landing surface to receive the tang.
-
公开(公告)号：US20170113815A1
公开(公告)日：2017-04-27
申请号：US15331464
申请日：2016-10-21
Applicant: Todd A. James , Michael W. Westerfield , Bryan C. James
Inventor： Todd A. James , Michael W. Westerfield , Bryan C. James
CPC classification number: B64F1/222 , B64C39/024 , B64C2201/042 , B64C2201/201 , B64F1/12 , B64F1/362 , H01R27/02 , H01R31/06 , H01R33/00
Abstract: Exemplary drone operations support base embodiments disclosed herein may be used to shelter, repower and/or service drones associated therewith. A drone operations support base may include an enclosure with an entryway that permits drone ingress and egress with respect to the enclosure. Drone launching/landing, drone storage and drone power source repowering areas may be associated with a given drone base. A transfer device may be provided to move drones between the various drone base areas. The transfer device may also be adapted to transfer drone power sources between the drone repowering area and drones located elsewhere within the drone base for repowering of the power sources and of the drones.
-
公开(公告)号：US20170043870A1
公开(公告)日：2017-02-16
申请号：US15336584
申请日：2016-10-27
Applicant: SZ DJI TECHNOLOGY Co., LTD.
Inventor： Xumin Wu , Xiaolong Wu , Sungki Lee , Jiyuan Ao , Zhuang Feng
CPC classification number: B64C39/024 , B64C1/30 , B64C27/08 , B64C27/12 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/12 , B64C2201/201 , B64D47/08
Abstract: Systems and methods are provided for transformation of a UAV from an extended state to a compacted state. The UAV can be transported in the compacted state. The UAV can comprise one or more segmented arms that can be folded to reduce the volume of the UAV. The segmented arms can be sealed to prevent ambient air, dirt, and or water vapor from entering the segmented arm. The UAV can comprise a cooling and air filtering system on-board the UAV.
Abstract translation: 提供了将UAV从扩展状态转换为压缩状态的系统和方法。 无人机可以在压实状态下运输。 UAV可以包括一个或多个分段的臂，其可被折叠以减小无人机的体积。 分段臂可以被密封以防止环境空气，污垢和/或水蒸气进入分段臂。 无人机可以包括无人机上的冷却和空气过滤系统。
-
-
-
-
-
-
-
-
-
Search Results
551
records
(took 0.046 seconds)
