Turbine e exhaust nozzle control (NSN 2995-01-433-6462)
Special Features
Soriginal item name -- convergent exhaust nozzle control, this redesigned nozzle control incorporates enhanced temperature capability to withstand higher-than-expected-operating temperatures that will extend its functional life
End Application
F100-pw-129 aircraft engine
Criticality Code Justification
Agav
General Description
Controls/positions the exhaust nozzle in order to vary engine thrust and fan stall margin; translates signalsreceived from deec into mechanical output by incorporating electro/hydraulicservovalve and resolver, converting bleed air pressure to rotational torque through airmotor
