| 摘要 |
<p>A turbine engine nozzle (120) assembly has an upstream flap (22) and a downstream flap (24) pivotally coupled thereto for relative rotation about a hinge axis (502). An actuator linkage (70) is coupled to the flaps for actuating the nozzle between a number of throat (40) area conditions. First (126) and second (124) mode struts respectively restrict rotation of the downstream flap in first and second directions.</p> |
