A battery connector (7) for connecting a replaceable battery (6) to an aircraft (1), the battery connector comprising: a housing (10) configured to be secured to one of the replaceable battery (6) and the aircraft (1); and a connector element (14) comprising a first connection portion (15) configured to be releasably connected to an external connection element (4) of the other of the replaceable battery (6) and the aircraft (1). The connector element (14) further comprises a second connection portion (18) configured to be fixedly connected with the replaceable battery (6) or the aircraft (1) to which the housing (10) is configured to be fixed. The connector element (14) is supported in the housing (10) by at least one flexible element (19) in the horizontal direction (XY), said at least one flexible element (19) being positioned at least partially between the connector element (14) and the housing (10) such that there is a space between the connector element (14) and the housing (10) in the horizontal direction (XY). The connector element (14) is supported in the housing (10) in the vertical direction (Z) by an upper flexible element (21) positioned between an upper portion (23) of the connector element (14) and the housing (10) and a lower flexible element (22) positioned between a lower portion (24) of the connector element (14) and the housing (10) such that there is a space between the connector element (14) and the housing (10) in the vertical direction (Z).
一种用于将可更换电池(6)连接至飞行器(1)的电池连接器(7),该电池连接器包括:壳体(10),该壳体构造成固定至可更换电池(6)和飞行器(1)中的一者;和连接器元件(14),该连接器元件包括第一连接部分(15),该第一连接部分构造成以可释放的方式连接至可更换电池(6)和飞行器(1)中的另一者的外部连接元件(4)。连接器元件(14)还包括第二连接部分(18),该第二连接部分构造成与壳体(10)构造成所固定至的可更换电池(6)或飞行器(1)固定地连接。连接器元件(14)由至少一个挠性元件(19)沿水平方向(XY)支承在壳体(10)中,所述至少一个挠性元件(19)至少部分地定位在连接器元件(14)与壳体(10)之间,使得连接器元件(14)与壳体(10)之间在水平方向(XY)上存在空间。连接器元件(14)由上挠性元件(21)和下挠性元件(22)沿竖向方向(Z)支承在壳体(10)中,上挠性元件(21)定位于连接器元件(14)的上部部分(23)与壳体(10)之间,下挠性元件(22)定位于连接器元件(14)的下部部分(24)与壳体(10)之间,使得连接器元件(14)与壳体(10)之间在竖向方向(Z)上存在空间。
Battery connector
电池连接器
2023-01-13
Patent
Electronic Resource
Chinese
IPC: | H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |