| 摘要 |
<p>An external flap vectoring mechanism on an axisymmetric gas turbine exhaust nozzle, the external flap vectoring mechanism comprising a plurality of external flaps, each such flap having first (11) and second flaps (12), the first flap pivotably connected to a sync ring (14) and the second flap pivotably connected to the aft end of the first flap thereby providing for lateral movement of the second flap relative to the first.</p> |
