WO2020094042A1 - 接触线、接触网、无人机和充电杆 - Google Patents
接触线、接触网、无人机和充电杆 Download PDFInfo
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/37—Charging when not in flight
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- H—ELECTRICITY
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- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/0042—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/02—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from ac mains by converters
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- B—PERFORMING OPERATIONS; TRANSPORTING
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Abstract
Description
Claims (18)
- 一种接触线,其特征在于,主要由表面绞合层和由所述表面绞合层包裹的芯体组成;所述表面绞合层主要由多根金属单线和多根绝缘间隔线绞合而成,至少存在两根不相邻的金属单线,在间隔它们的两翼绞合线中各设置有至少一根绝缘间隔线,所述绝缘间隔线由绝缘材料制成、或内含导体外面包覆绝缘材料;所述芯体的表层为绝缘材料;由此表面绞合层具有至少两个表面导体,相互间绝缘,呈螺旋状围绕所述芯体分布。
- 根据权利要求1所述的接触线,其特征在于,还包括表面绝缘层,包覆所述表面绞合层。
- 根据权利要求1或2所述的接触线,其特征在于,所述表面绞合层的金属单线和绝缘间隔线的分布为周期分布,每个周期为连续出现n根金属单线,然后再连续出现m根绝缘间隔线,周期的数量为2、3、4或6,n和m大于零,n和m可以相等,也可以不相等。
- 根据权利要求1或2所述的接触线,其特征在于,所述芯体具有内部导体,被绝缘材料包围。
- 根据权利要求1或2所述的接触线,其特征在于,还包括光纤,设置在表面绞合层的绞合线或芯体内。
- 根据权利要求1或2所述的接触线,其特征在于,所述芯体为抗拉部件或包括抗拉部件。
- 一种接触网,包括充电线路电源、电杆和至少一根如权利要求1所述的接触线,所述接触线由所述电杆架空安装,所述接触线的表面导体被全部或部分地分配为充电线路,所述充电线路电源的输出端接入所述充电线路。
- 根据权利要求7所述的接触网,其特征在于,所述充电线路电源是一组沿线分布的降压装置,还包括馈电线路电源,所述接触线的芯体内还具有被绝缘材料包围的内部导体;所述接触线的内部导体被全部或部分地分配为馈电线路,所述馈电线路电源的输出端和所述降压装置的高压输入端并联接入所述馈电线路;所述降压装置的低压输出端并联接入所述充电线路。
- 根据权利要求7或8所述的接触网,其特征在于,还包括控制装置,所述控制装置包括计算机控制模块、开关部件、通信模块;所述计算机控制模块分别连接所述开关部件和通信模块;所述开关部件设置在所述充电线路电源至充电线路的连接线中;所述通信模块至少包括WIFI模块、无人机无线电模块、电力线载波模块、移动电话网络模块中的一种。
- 根据权利要求9所述的接触网,其特征在于,所述接触线还包括设置在表面绞合层的绞合线或芯体内的光纤,所述控制装置还包括光纤通信模块,与所述光纤和所述计算机控制模块连接。
- 根据权利要求7或8所述的接触网,其特征在于,所述接触线还包括设置在表面绞合层的绞合线或芯体内的光纤,还包括光纤通信模块、控制装置和本地通信模块;所述控制装置包括计算机控制模块、开关部件,所述计算机控制模块连接所述开关部件,所述开关部件设置在所述充电线路电源至充电线路的连接线中;所述光纤通信模块,与所述光纤、所述计算机控制模块和所述本地通信模块连接;所述本地通信模块至少包括WIFI模块、无人机无线电模块、电力线载波模块中的一种。
- 一种无人机,包括机体、电池充电电路,其特征在于,还包括位于机体上部的挂钩,和连接所述挂钩和所述机体的立臂,所述挂钩内侧上部设置有金属触头,通过引线与充电电路连接,挂钩的形式包括以下两种情况中的至少一种:A,一个挂钩具有至少两个金属触头,沿挂钩上部内边分开布置;B,至少具有两个挂钩,它们的开口方向在它们中心连线的同一侧。
- 根据权利要求12所述的无人机,其特征在于,具有两个开口方向相同并与它们中心连线垂直的挂钩,每个挂钩具有两个金属触头,沿挂钩上部内边分开布置。
- 根据权利要求12所述的无人机,其特征在于,还包括位于挂钩下侧的夹握器和电机;所述电机固定在所述立臂上部,其转轴联接所述夹握器,驱动所述夹握器在放下和夹握两个角度位置间运动;所述夹握器内侧设置有金属触头,通过引线和所述电池充电电路连接。
- 根据权利要求12所述的无人机,其特征在于,所述挂钩通过一个转轴和所述立臂连接,还包括位于挂钩下侧的夹握器,所述夹握器通过另一个转轴和所述立臂连接,还包括一个转角放大传动机构,连接所述挂钩和夹握器;所述夹握器内侧设置有金属触头,通过引线和所述电池充电电路连接;所述转角放大传动机构为连杆链接的双杠杆、长孔-销链接的双杠杆、齿轮传动、内齿皮带传动中的一种。
- 根据权利要求12、13、14或15所述的无人机,其特征在于,所述金属触头的工作面上具有锋利的突起。
- 一种充电杆,包括充电线路电源、立柱,其特征在于,还包括接触臂,一端固定在所述立柱的上部,所述接触臂包括至少两个表面导体和一个表面绝缘的芯体,所述表面导体,按固定节距,呈螺旋状围绕所述芯体分布,被全部或部分地分配为充电线路,所述充电线路电源的输出端接入所述充电线路。
- 根据权利要求17所述的充电杆,其特征在于,还包括控制装置,所述控制装置包括计算机控制模块、开关部件、通信模块;所述计算机控制模块分别连接所述开关部件和通信模块;所述开关部件设置在所述充电线路电源至充电线路的连接线中;所述通信模块至少包括WIFI模块、无人机无线电模块、电力线载波模块、移动电话网络模块中的一种。
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CN201811312194.3A CN111161916A (zh) | 2018-11-07 | 2018-11-07 | 接触线、接触网、无人机和充电杆 |
CN201811312194.3 | 2018-11-07 |
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DE102022116329A1 (de) | 2022-06-30 | 2024-01-04 | Bayerische Motoren Werke Aktiengesellschaft | Flugdrohne, Flugdrohnensicherheitssystem und Verfahren zum Betreiben einer Flugdrohne |
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2018
- 2018-11-07 CN CN201811312194.3A patent/CN111161916A/zh active Pending
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US7398946B1 (en) * | 2004-10-04 | 2008-07-15 | United States Of America As Represented By The Secretary Of The Air Force | Power line sentry charging |
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DE102022116329A1 (de) | 2022-06-30 | 2024-01-04 | Bayerische Motoren Werke Aktiengesellschaft | Flugdrohne, Flugdrohnensicherheitssystem und Verfahren zum Betreiben einer Flugdrohne |
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