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    • 4. 发明授权
    • Aircraft electrical connector with differential engagement and operational retention forces
    • 具有差异接合和操作保持力的飞机电气连接器
    • US07980875B2
    • 2011-07-19
    • US12645451
    • 2009-12-22
    • Anatoly GosisScott Takayuki KoizumiFolkert Fred KochWolfgang OttChristopher A. Tacklind
    • Anatoly GosisScott Takayuki KoizumiFolkert Fred KochWolfgang OttChristopher A. Tacklind
    • H01R13/15
    • H01R13/639H01R4/48H01R4/489H01R13/18H01R13/193H01R13/62933H01R2201/26
    • An aircraft electrical connector is provided with features to allow facile engagement with an aircraft and strong retention forces. The aircraft electrical system may include the aircraft electrical connector having a unique biasing mechanism and modular construction, wherein the biasing mechanism is configured to place differential forces onto mating electrical connectors from an aircraft. The biasing mechanism may be operatively coupled to a handle or trigger, which may be easily engageable by an operator. In one embodiment, an electrical connector may include a cam plate disposed between electrical connectors. The cam plate is configured to place differential forces on mating connectors inserted into the electrical connectors. In another embodiment, an electrical connector includes a moveable shaft that is disposed between electrical connectors. The shaft is configured to bias the position of the electrical connectors to place differential engagement and retention forces on mating connectors inserted into the electrical connectors.
    • 飞机电连接器具有允许与飞行器轻松接合和强大的保持力的特征。 飞行器电气系统可以包括具有独特的偏置机构和模块化结构的飞行器电连接器,其中偏置机构被配置为将差分力放置在与飞机相配的电连接器上。 偏置机构可以可操作地联接到手柄或触发器,其可以容易地由操作者接合。 在一个实施例中,电连接器可以包括设置在电连接器之间的凸轮板。 凸轮板被配置为将差分力放置在插入到电连接器中的配合连接器上。 在另一个实施例中,电连接器包括设置在电连接器之间的可移动轴。 轴构造成偏置电连接器的位置,以将差动接合和保持力插入插入到电连接器中的配合连接器上。