Positive locking mechanism for rotating helicopter mount
    1.
    发明授权
    Positive locking mechanism for rotating helicopter mount 有权
    旋转直升机安装的正锁定机构

    公开(公告)号:US08800421B1

    公开(公告)日:2014-08-12

    申请号:US13687469

    申请日:2012-11-28

    IPC分类号: F41A23/20 F41A23/24

    CPC分类号: F41A27/12 F41A27/00

    摘要: An apparatus for rotating and locking a first longitudinal member with respect to a second longitudinal member. One end of the first longitudinal member includes a locking mechanism having a generally arcuate outer surface with a plurality of deep and shallow notches formed therein. The notches correspond to different positions of rotation of the first and second members. One end of the second longitudinal member includes a yoke rotatably connected to the locking mechanism with a pivot pin. A locking plunger in the second longitudinal member engages the notches in the locking mechanism and is translatable between fully locked and fully unlocked positions. In the fully locked position, the first and second members are not rotatable with respect to each other.

    摘要翻译: 一种用于相对于第二纵向构件转动和锁定第一纵向构件的装置。 第一纵向构件的一端包括具有大致弓形的外表面的锁定机构,其中形成有多个深而浅的凹口。 凹口对应于第一和第二构件的不同旋转位置。 第二纵向构件的一端包括用枢轴销可转动地连接到锁定机构的磁轭。 第二纵向构件中的锁定柱塞接合锁定机构中的凹口,并且可在完全锁定和完全解锁位置之间平移。 在完全锁定位置,第一和第二构件不能相对于彼此旋转。