Description:

C/o: blade nozzle 24, ring-inner 2, ring-outer 2, segment 2, segment 2, spacer-in 2, spacer-out 2, instruction turbine 1; .

Special Features:

C/o: blade nozzle 24, ring-inner 2, ring-outer 2, segment 2, segment 2, spacer-in 2, spacer-out 2, instruction turbine 1;

Properties:

A single stationary item designed for the purpose of directing air at the proper angle and velocity to a rotor, turbine, nonaircraft gas turbine engine. it has provisions for attaching to a case (3), turbine, nonaircraft gas turbine engine. it may have an inner support shroud.