Model: 380278-1 AND 1300-1048-8

Special Features:

Pneumatic shaft power output, 190.0 shaft horsepower rating, 6000.0 rpm shaft horsepower speed rating, 40700.0 air horsepower rating, 460.0 lb per minute air flow, 80.0 psi discharge pressure, 0.0 altitute at which horsepower is rated, 130.0 degrees fahrenheit horsepower rated, 7500 hr of operation between overhauls, jet fuel, ac, 120.0/208.0 v, centrifugal switch, dual pad drive, fuel control, igniter, oil cooler, oil pump, starter, load control valve, inclosure, base frame mounting, steel container accommodates engine, 42.630 in. Max o/a lg, 27.810 in. Nom o/a height, 29.460 in. Nom o/a width

Properties:

A continuous combustion type engine. consists primarily of a compressor, nonaircraft gas turbine engine; chamber, combustion, nonaircraft gas turbine engine and a turbine assembly, nonaircraft gas turbine engine. it may have a fan section. air is compressed and heated by a combustible fuel and expanded through the turbine. it is designed to furnish a source of rotary shaft and/or pneumatic power. the pneumatic power is obtained by a bleedoff of the engine compressor. for a complete operating power unit, mounted on a base, see power unit, gas turbine engine.