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.
Classification: Gas turbine engine, except aircraft nesoi, of a power not exceeding 5,000 kw
NSN 6220-01-142-3688
NSN 5998-00-070-9389
NSN 5910-01-502-9149
NSN 5910-01-085-6434
NSN 5960-01-605-9921
NSN 6320-01-567-9792
NSN 5975-01-122-5834
NSN 5905-01-569-6908
NSN 6240-01-296-6020
NSN 5910-01-118-5687
NSN 5996-01-102-1246
NSN 6110-01-545-1972