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1. 发明授权

EP3044092B1 TRAILER FOR AUTONOMOUS VEHICLE 有权
公开(公告)号：EP3044092B1
公开(公告)日：2018-10-17
申请号：EP14844886.3
申请日：2014-09-11
申请人： Silicis Technologies Inc.
发明人： STIGLER, Michael J. , SETAR, Nicholas James
IPC分类号： B64F1/12
CPC分类号： 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
摘要： 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.

2. 发明授权

EP2853494B1 Power management method and system for an unmanned air vehicle 有权
公开(公告)号：EP2853494B1
公开(公告)日：2018-08-01
申请号：EP13382370.8
申请日：2013-09-26
申请人： The Boeing Company
发明人： Lemus Martin, Jose Luis , Pereira Mayán, Sergio , Ferreyra, Eduardo Gabriel
IPC分类号： B64D41/00 , H02J1/14 , H02J3/12
CPC分类号： B64C39/024 , B64C2201/06 , B64C2201/141 , B64D31/14 , B64D41/00 , B64D2041/005 , B64D2211/00 , B64D2221/00 , G05B13/0275 , G05D1/0005 , Y02T50/55 , Y02T90/36
摘要： Power management method and system for an unmanned air vehicle, wherein the unmanned air vehicle comprises a plurality of power demanding subsystems and a plurality of power sources. The invention establishes mission oriented fixed parameters. A fuzzy logic power management unit, comprised in the system, automatically calculates and assigns priorities for delivering power to the subsystems. It also automatically calculates and assigns amounts of power delivered to each subsystem and automatically decides which of the power sources to deliver power to which subsystem. The fuzzy logic power management system calculates and assigns the priorities and loads in function of a plurality of internal variables, external variables and the mission oriented fixed parameters.

3. 发明公开

EP3212502A1 MULTI-ROTOR AERIAL VEHICLE 有权
标题翻译：多旋翼空中车辆
公开(公告)号：EP3212502A1
公开(公告)日：2017-09-06
申请号：EP15854629.1
申请日：2015-10-28
申请人： ACC Innovation AB
发明人： LJUNG, Anders
IPC分类号： B64D35/04 , B64C27/08 , B64C27/12
CPC分类号： B64D35/04 , A63H27/12 , B64C39/024 , B64C2201/027 , B64C2201/04 , B64C2201/06 , B64C2201/108 , B64C2201/146 , B64C2201/148 , B64D37/00
摘要： 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.
摘要翻译：多旋翼飞行器（1,1'，1“，1”'，1“'，1”'，1“'）包括至少第一，第二和第三转子10,20,30，每个转子通过专用的第一第二和第三液压马达11,21,31，动力单元2，至少第一，第二和第三液压泵12,22,32可旋转，所述第一，第二和第三液压泵12,22,32专用于相应的第一，第二和第三液压马达11,21,31，其中每个液压泵12,22,32被布置成向每个液压马达11,21,31提供加压流体，用于给液压马达11,21,31供能并由此旋转相应的转子10,20,30，用于控制多旋翼飞行器（1,1'，1“，1”'，1“，1”''）的操作的控制单元6，其中多旋翼飞行器（1,1'，1“，1”'，1“'，1”'，1“ ）被布置成通过改变分配给每个相应液压马达11,21,31的加压流体的流动来执行，其中，向每个液压马达提供加压流体的流动液压马达11,21,31可通过至少一个控制阀13,23,33单独控制，所述至少一个控制阀13,23,33构造成控制从每个液压泵12,22,32到其专用液压马达11,21,31的加压流体的流动。

4. 发明公开

EP3044092A4 TRAILER FOR AUTONOMOUS VEHICLE 审中-公开
标题翻译： ANHÄNGERFÜR自动化FAHRZEUG
公开(公告)号：EP3044092A4
公开(公告)日：2017-08-02
申请号：EP14844886
申请日：2014-09-11
申请人： SILICIS TECH INC
发明人： STIGLER MICHAEL J , SETAR NICHOLAS JAMES
IPC分类号： B64F1/12
CPC分类号： 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
摘要： 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.
摘要翻译：所公开的实施例包括用于由命令和控制界面控制的自主车辆的拖车。拖车包括配置成将自主车辆保持在未展开配置中的拖车主体。拖车还将自主车辆锚定在展开配置中。提供系绳，其具有联接到拖车主体的第一端部和构造成联接到自主车辆的第二端部。利用绞车调节系绳的长度以使自主车辆在未展开配置和展开配置之间移动。此外，通信系统与命令和控制接口以及自主车辆通信，以控制自主车辆在未部署配置和部署配置之间的移动。

5. 发明公开

EP2889221A1 Short takeoff and landing aircraft 有权
标题翻译：起飞和着陆时间短的飞机
公开(公告)号：EP2889221A1
公开(公告)日：2015-07-01
申请号：EP14187036.0
申请日：2014-09-30
申请人： The Boeing Company
发明人： Ouellette, Rich P.
IPC分类号： B64F1/04 , B64F3/02
CPC分类号： B64D41/00 , B64C2201/06 , B64C2201/08 , B64D27/24 , B64D2027/026 , B64F1/04 , B64F3/02 , Y10S903/902
摘要： A short takeoff and landing fixed wing aircraft (200) includes a primary powertrain (302) to provide power to a propulsion unit (208), a secondary powertrain (304) to provide power to the propulsion unit (208), and a detachable power coupling to transfer power to the secondary powertrain (304) from a source external to the fixed wing aircraft during takeoff.
摘要翻译：短距起飞和降落固定翼飞机（200）包括向推进单元（208）提供动力的主动力系（302），向推进单元（208）提供动力的次动力系（304），以及可拆卸动力耦合以在起飞期间将动力从固定翼飞机外部的源传递到次动力传动系（304）。

6. 发明授权

EP2664539B1 A method of and apparatus for extending the operation of an unmanned aerial vehicle 有权
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
申请人： The Boeing Company
发明人： Scarlatti, David , Campillo Esteban, David , Casado Magana, Enrique Juan
IPC分类号： B60L11/18 , G05D1/00 , B64C39/02
CPC分类号： G05D1/00 , B60L11/1822 , B60L2200/10 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/06 , Y02T10/7005 , Y02T10/7072 , Y02T90/124 , Y02T90/14
摘要： 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.

7. 发明公开

EP3212502A4 MULTI-ROTOR AERIAL VEHICLE 有权
公开(公告)号：EP3212502A4
公开(公告)日：2018-04-04
申请号：EP15854629
申请日：2015-10-28
申请人： ACC INNOVATION AB
发明人： LJUNG ANDERS
IPC分类号： B64D35/04 , A63H27/00 , B64C27/08 , B64C27/12 , B64C39/02 , B64D37/00
CPC分类号： B64D35/04 , A63H27/12 , B64C39/024 , B64C2201/027 , B64C2201/04 , B64C2201/06 , B64C2201/108 , B64C2201/146 , B64C2201/148 , B64D37/00
摘要： 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.

8. 发明公开

EP3244468A1 UNMANNED AERIAL VEHICLE BATTERY AND UNMANNED AERIAL VEHICLE 有权
标题翻译：无人机空中车辆电池和无人机空中车辆
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
申请人： Autel Robotics Co., Ltd.
发明人： QIU, Longxue , WU, Xingwen
IPC分类号： H01M2/10
CPC分类号： H01M2/1083 , B64C39/024 , B64C2201/042 , B64C2201/06 , H01M2220/20
摘要： 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.
摘要翻译：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。

9. 发明公开

EP3044092A2 TRAILER FOR AUTONOMOUS VEHICLE 审中-公开
标题翻译：拖车自主车
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
申请人： Silicis Technologies Inc.
发明人： STIGLER, Michael J. , SETAR, Nicholas James
IPC分类号： B64F1/12
CPC分类号： 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
摘要： 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.

10. 发明公开

EP2664539A1 A method of and apparatus for extending the operation of an unmanned aerial vehicle 有权
标题翻译：为延伸的无人驾驶飞行器的操作的方法和装置
公开(公告)号：EP2664539A1
公开(公告)日：2013-11-20
申请号：EP12382181.1
申请日：2012-05-17
申请人： The Boeing Company
发明人： Scarlatti, David , Campillo Esteban, David , Casado Magana, Enrique Juan
IPC分类号： B64C39/02
CPC分类号： G05D1/00 , B60L11/1822 , B60L2200/10 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/06 , Y02T10/7005 , Y02T10/7072 , Y02T90/124 , Y02T90/14
摘要： 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.
摘要翻译：扩展操作无人驾驶飞行器（UAV）的（100）的方法，是游离缺失盘。该方法包括以下步骤：（a）检测到那样船上的UAV耗尽低于阈值水平的能量存储装置（110）; （B）操作所述UAV，以便在基站（200）降落; 和（c）至少发起基站的手术引起更换机构（220），其以从UAV除去上板的能量存储装置的UAV，并用另一种能量存储设备（120）来代替此。因此，其他步骤游离缺失盘。另外，UAV（100），一个基站（200）和布置成执行所述方法的步骤的指令和控制装置（400）是圆盘游离缺失。

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