(1)Centrifugal + 2 stage axial/ with stationary inlet guide vanes fore of 1st stage axial stator..
Torque distribution (internal): direct-drive, triple stage dampers (hydrualic type, uses engine oil which is compressed)
Oil system:Gerotor pumped, zero-loss, closed loop, 2 filter, intake cooler(check it out!), 4 chip detectors throughout.
Fuel management:cooled, zero loss, fadec controlled simple hydromechanical unit, failsafe simple design.
Variable ~455 up to ~2550 output SHP @ max power 28, 475~ turbine - tip rpm.
any transport aircraft, simply attach a prop
just about any rotorcraft big and small
possibly for use with a ground generator
ground power unit
Alternator(12-24-36-48 kvh 400 hertz, 200-1000 watts derp)
Four accessory drives, 2 fore, 2 aft.
2 Primary output driveshafts 1 fore, 1 aft
Quad rotor ceramic, slotted %10 tungsten alloy, electricaly actuated variable rotor /gearbox/compressor braking - may also be FADEC adjustable/init as well.
Starter is electric, 12-24-48 volts, 3 phase, 30 amps, 17,349 rpm (rpm @ starter shaft)
30 seconds on 5 minutes off (X2), lastly after 2 attempts than 30 minutes off, exceed? than inspect/serv/replace starter motor and gearbox.