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公开(公告)号：WO2019105857A1
公开(公告)日：2019-06-06
申请号：PCT/EP2018/082351
申请日：2018-11-23
Inventor： GHOSH, Ayan
CPC classification number: B64C39/022 , B64C2201/027 , B64C2201/06 , B64C2201/122 , B64C2201/148 , H04B7/18504
Abstract: An unmanned aircraft such as a tethered drone has an electrical power connection (10) for receiving electrical power from a remote source, and a power delivery system for delivering electrical power to onboard applications equipment (14) such as radio transmitters (5, 6). To ensure that ground staff are not exposed to high levels of radiation from the transmitters, power is only delivered to the communications equipment after the aircraft has left the ground. A sensor (13) associated with the aircraft's undercarriage may be used to detect when the aircraft is airborne. The applications equipment (14) is powered from an accumulator which is only charged up from the power supply (10) after launch. In the event of a failure of the power supply (10) when airborne, the output of the accumulator is diverted to control propulsion and flight control systems (17), which are normally powered directly from the power supply (10), to allow a controlled descent, and thus shutting off the applications equipment (14) before the aircraft returns to proximity to personnel on the ground.
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公开(公告)号：WO2017117291A1
公开(公告)日：2017-07-06
申请号：PCT/US2016/069016
申请日：2016-12-28
Applicant: MOLNAR, Dezso , CANAVAN, John
Inventor： MOLNAR, Dezso , CANAVAN, John
CPC classification number: B64C39/022 , B05B17/08 , B64C39/024 , B64C2201/06 , B64C2201/128 , B64C2201/148 , B64D47/04 , B64F3/02 , B66D1/28 , B66D1/485 , B66D1/60 , F21S10/002 , G03B15/006 , G03B21/10 , G03B21/608 , G09F13/00 , G09F19/18 , G09F21/06
Abstract: A tethered unmanned aerial system (UAS) is described, wherein the flight of more UASs may be used in connection with a water and light display.
Abstract translation: 描述了系留式无人航空系统（UAS），其中更多UAS的飞行可以与水和光显示器结合使用。
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公开(公告)号：WO2017101589A1
公开(公告)日：2017-06-22
申请号：PCT/CN2016/103265
申请日：2016-10-25
Applicant: 深圳市道通智能航空技术有限公司
IPC: H01M2/10
CPC classification number: H01M2/1083 , B64C39/024 , B64C2201/042 , B64C2201/06 , H01M2220/20
Abstract: 一种无人机及其电池，其中，所述无人机电池，包括：电池本体和布置在电池本体一端的壳体，在壳体相对于无人机的一侧设置有卡扣按键，卡扣按键的一端固接在壳体上，卡扣按键的另一端用于与无人机可拆卸连接。由于在电池本体一端的壳体上设置有卡扣按键，从而能够实现无人机电池与无人机本体可拆卸连接，方便了无人机电池的更换。
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公开(公告)号：JP2017533863A
公开(公告)日：2017-11-16
申请号：JP2017543702
申请日：2015-10-28
Applicant: アーセーセー イノヴァチオン アーベー , アーセーセー イノヴァチオン アーベー
CPC classification number: B64D35/04 , A63H27/12 , B64C39/024 , B64C2201/027 , B64C2201/04 , B64C2201/06 , B64C2201/108 , B64C2201/146 , B64C2201/148 , B64D37/00
Abstract: マルチロータ航空機(1、1’、1''、1'''、1''''、1'''''、1'''''')は、少なくとも三つの油圧モータ(11、21、31)と、それぞれが前記少なくとも三つの油圧モータ(11、21、31)の一つにより回転可能な少なくとも三つのロータ(10、20、30)と、少なくとも一つのパワーユニット(2)と、それぞれが前記少なくとも三つの油圧モータ(11、21、31)の一つに加圧流体を供給して駆動することにより前記少なくとも三つのロータ(10、20、30)の一つを回転させるための少なくとも三つの第一油圧ポンプ(12、22、32)と、前記少なくとも三つの油圧モータ(11、21、31)へ分配される加圧流体の流れを変更することによって、前記マルチロータ航空機の動作制御を行なう制御ユニット(6)とを備えている。前記少なくとも三つの油圧ポンプ(12、22、32)から前記少なくとも三つの油圧モータ(11、21、31)への加圧流体の流れのそれぞれを制御する少なくとも一つの制御弁(13、23、33)によって、前記少なくとも三つの油圧モータ(11、21、31)へ分配される加圧流体の流れが個別に制御可能である。【選択図】図2
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公开(公告)号：JP2014500827A
公开(公告)日：2014-01-16
申请号：JP2013543164
申请日：2011-09-23
Applicant: ザ・ボーイング・カンパニーThe Boeing Company
Inventor： ブライアン ジェー． ティロットソン， , タマイラ イー． ロス， , ジョン エル． ヴィアン，
CPC classification number: G05D1/101 , B64C2201/027 , B64C2201/042 , B64C2201/06 , B64C2201/145 , B64C2201/146
Abstract: 無人ビークルが提供される。 無人ビークルは、無人ビークルを、ビーム源から放出されるエネルギービームに対して誘導するように構成されたナビゲーションシステムと、エネルギーをビームから受け取るように構成された電力受給器と、受け取ったエネルギーを貯蔵して無人ビークルに選択的に給電するために利用するように構成されたエネルギー貯蔵システムとを含む。
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Patent Agency Ranking
公开(公告)号：KR1020170101200A
公开(公告)日：2017-09-05
申请号：KR1020177014767
申请日：2015-10-28
Applicant: 에이씨씨 이노베이션 에이비
Inventor： 엘정,앤더스
CPC classification number: B64D35/04 , A63H27/12 , B64C39/024 , B64C2201/027 , B64C2201/04 , B64C2201/06 , B64C2201/108 , B64C2201/146 , B64C2201/148 , B64D37/00
Abstract: 멀티로터항공기(1, 1', 1", 1"', 1"", 1""', 1""")로서, 각각이전용제1, 제2, 및제3 유압모터(11, 21, 31)에의해회전가능한적어도제1, 제2, 및제3 로터(10, 20, 30), 동력유닛(2), 상기각각의제1, 제2, 및제3 유압모터(11, 21, 31)에전용되는적어도제1, 제2, 및제3 유압펌프(12, 22, 32), 여기서, 상기각 유압펌프(12, 22, 32)는유압모터(11, 21, 31)에동력을공급하여각각의로터(10, 20, 30)를회전시키는각각의유압모터(11, 21, 31)에가압유체를제공하도록배치됨, 상기멀티로터항공기(1, 1', 1", 1"',1"",1""',1""")의작동을제어하기위한제어유닛(6)을포함하고, 상기멀티로터항공기(1, 1', 1", 1"', 1"", 1""', 1""")의제어는각각의유압모터(11, 21, 31)에분배된가압유체의흐름을변경함으로써수행되도록배치되고, 상기각각의유압모터(11, 21, 31)에제공된가압유체의흐름은각각의유압펌프(12, 22, 32)로부터전용유압모터(11, 21, 31)로의가압유체의흐름을제어하도록구성된적어도하나의제어밸브(13, 23, 33)에의해각각제어가능하다.
Abstract translation: 作为多旋翼飞行器1,1'，1“，1”'，1“”，1“的第二和第三液压马达11,21和31， 第二和第三转子（10,20,30），动力单元（2）以及第一，第二和第三液压马达（11,21,31） 其中至少第一，第二和第三液压泵12,22和32分别专用于向液压马达11,21和31供电， 1“，1”，1“，1”，1“，2'，1” “1" ” '1" “” 多转子飞行器（1，1，和用于控制的动作的控制单元6）'，1”，1" ”，1 “”，1“ 一个“”，1“”“）控制各个液压马达（11，21，31）加压的改变流体的流动被布置成由进行，每个所述液压马达（11，21，31分区）的 所提供的加压流体的流动从每个液压泵12,22传递， （13,23,33），其被配置为分别控制加压流体到加压流体源（11,21,31）的流动。
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公开(公告)号：EP2664539B1
公开(公告)日：2018-07-18
申请号：EP12382181.1
申请日：2012-05-17
Applicant: The Boeing Company
CPC classification number: G05D1/00 , B60L11/1822 , B60L2200/10 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/06 , Y02T10/7005 , Y02T10/7072 , Y02T90/124 , Y02T90/14
Abstract: A method of extending the operation of an unmanned aerial vehicle (UAV) (100) is disclosed. The method comprises the following steps: (a) detecting that an energy storage device (110) on board the UAV is depleted below a threshold level; (b) operating the UAV so as to land at a base station (200); and (c) at least initiating operation of the base station to cause a replacement mechanism (220) thereof to remove the energy storage device on board the UAV from the UAV and to replace this with another energy storage device (120). Other steps are also disclosed. In addition, a UAV (100), a base-station (200) and a command-and-control device (400) arranged to carry out steps of the method are disclosed.
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公开(公告)号：EP3212502A4
公开(公告)日：2018-04-04
申请号：EP15854629
申请日：2015-10-28
Applicant: ACC INNOVATION AB
Inventor： LJUNG ANDERS
CPC classification number: B64D35/04 , A63H27/12 , B64C39/024 , B64C2201/027 , B64C2201/04 , B64C2201/06 , B64C2201/108 , B64C2201/146 , B64C2201/148 , B64D37/00
Abstract: Multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″) comprising, at least a first, second and third rotor 10, 20, 30, each rotatable by a dedicated first second and third hydraulic motor 11, 21, 31, a power unit 2, at least a first, second and third hydraulic pump 12, 22, 32 dedicated to the respective first, second and third hydraulic motor 11, 21, 31, wherein each hydraulic pump 12, 22, 32 is arranged to provide pressurized fluid to each hydraulic motor 11, 21, 31 for powering the hydraulic motor 11, 21, 31 and thereby rotating the respective rotor 10, 20, 30, a control unit 6 for controlling the operation of the multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″), wherein the control of the multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″) is arranged to be performed by altering the flow of pressurized fluid distributed to each respective hydraulic motor 11, 21, 31, wherein, wherein the flow of pressurized fluid provided to each hydraulic motor 11, 21, 31 is individually controllable by means of at least one control valve 13, 23, 33 configured to control the flow of pressurized fluid from each hydraulic pump 12, 22, 32 to its dedicated hydraulic motor 11, 21, 31.
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公开(公告)号：EP3244468A1
公开(公告)日：2017-11-15
申请号：EP16863190.1
申请日：2016-10-25
Applicant: Autel Robotics Co., Ltd.
Inventor： QIU, Longxue , WU, Xingwen
IPC: H01M2/10
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.
Abstract translation: 本发明公开了一种无人机及其电池。 电池包括电池主体和设置在电池主体的一端上的外壳。 壳体在无人驾驶飞行器的对面设置有夹紧按钮。 夹紧按钮的一端固定在壳体上，另一端用于与无人驾驶飞行器可拆卸地连接。 夹式按钮使得电池可拆卸地与无人机的主体连接在一起，并且更换电池非常方便。
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公开(公告)号：EP3044092A2
公开(公告)日：2016-07-20
申请号：EP14844886.3
申请日：2014-09-11
Applicant: Silicis Technologies Inc.
Inventor： STIGLER, Michael J. , SETAR, Nicholas James
IPC: B64F1/12
CPC classification number: B60P3/11 , B60P7/06 , B60P7/0876 , B64B1/10 , B64B1/50 , B64B1/58 , B64B1/66 , B64C39/022 , B64C39/024 , B64C2201/022 , B64C2201/06 , B64C2201/101 , B64C2201/12 , B64C2201/121 , B64C2201/125 , B64C2201/127 , B64C2201/148 , B64C2201/208 , B64F1/14 , B64F3/02 , G08C17/02
Abstract: The disclosed embodiments include a trailer for an autonomous vehicle controlled by a command and control interface. The trailer includes a trailer body configured to retain the autonomous vehicle in an undeployed configuration. The trailer also anchors the autonomous vehicle in a deployed configuration. A tether is provided having a first end coupled to the trailer body and a second end that is configured to couple to the autonomous vehicle. A winch is utilized to adjust a length of the tether to move the autonomous vehicle between the undeployed configuration and deployed configuration. Further, a communication system communicates with the command and control interface and the autonomous vehicle to control movement of the autonomous vehicle between the undeployed configuration and deployed configuration.
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