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    • 7. 发明申请
    • LOCKING MECHANISMS FOR RAM AIR TURBINES
    • 用于RAM空气涡轮机的锁定机构
    • US20160312865A1
    • 2016-10-27
    • US14692800
    • 2015-04-22
    • HAMILTON SUNDSTRAND CORPORATION
    • Christopher S. ProkupDavid G. BannonMark A. OsbornGregory J. BradleyWilliam E. Seidel
    • F16H21/06
    • F16H21/06B64D41/007F16H21/44
    • A locking mechanism for a ram air turbine (RAT) includes a base clevis configured to mount to a housing and to have a base link clevis connector portion defining a plurality of base link clevis connector arms and a base link clevis having a base connector portion defining base connector arms that are configure to movably connect to the base link clevis connector arm. The locking mechanism also includes a pin operatively connecting the base connector portion to the base link clevis connector portion in a rotatable relationship and a spring positioned around the pin, wherein a first spring end abuts the base clevis and a second spring end abuts the base link clevis to bias the base link clevis to an unlocked position. A sleeve is positioned between the spring and the pin to maintain a wind diameter of the spring.
    • 用于冲压式空气涡轮机(RAT)的锁定机构包括:底座,其构造成安装到壳体,并具有限定多个基座连接钩连接器臂的基座连接件连接器部分和具有限定 基座连接器臂被配置为可移动地连接到基座连杆U形夹连接器臂。 锁定机构还包括可操作地将基座连接器部分以可旋转关系连接到基座连接器连接器部分的销和围绕销钉定位的弹簧,其中第一弹簧端邻接底座,并且第二弹簧端邻接基座连杆 U形夹将底座连接器U形夹偏压到未锁定位置。 套筒位于弹簧和销之间,以保持弹簧的风直径。