Gas turbine engine nozzle actuation system
    1.
    发明授权
    Gas turbine engine nozzle actuation system 失效
    气体涡轮发动机喷嘴启动系统

    公开(公告)号:US3630633A

    公开(公告)日:1971-12-28

    申请号:US3630633D

    申请日:1970-05-07

    申请人: FORD MOTOR CO

    发明人: STOCKTON THOMAS R

    IPC分类号: F01D17/16 F04D27/00 F04D27/02

    CPC分类号: F01D17/162

    摘要: An actuation system includes crank arms connected to the nozzle blades for pivoting them, the crank arms being movable in an arcuate path by pure tangential forces applied by the combined axial and rotary movement of an internally mounted shaft that is moved by a pair of fluid-interconnected servos.