电池连接器
By introducing a flexible element design into the battery connector, the problems of connector wear and weight in the prior art are solved, enabling a lightweight and convenient battery replacement process, and ensuring the reliability and high current transmission of the connector.
CN115606045BActive Publication Date: 2026-07-17GRIFF AVIATION AS
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- GRIFF AVIATION AS
- Filing Date
- 2021-05-26
- Publication Date
- 2026-07-17
AI Technical Summary
Technical Problem
Existing battery connectors are prone to wear and breakage due to stress during replacement, and their complex and bulky design makes it difficult to achieve lightweight and convenient operation.
Method used
The design incorporates housing and connector elements, utilizing flexible elements to support the space between the connector elements and the housing in both horizontal and vertical directions, providing a flexible connection and reducing the risk of wear and breakage.
Benefits of technology
A lightweight battery connector structure has been achieved, ensuring convenience and reliability during battery replacement, reducing connector failures, and enabling the transmission of high current.
✦ Generated by Eureka AI based on patent content.
Smart Images
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Abstract
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。
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