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 5905-00-615-8396
NSN 6685-01-512-8831
NSN 5920-01-556-0912
NSN 6685-00-770-2052
NSN 6110-01-396-6087
NSN 5935-00-907-2391
NSN 5835-01-398-3859
NSN 6145-00-498-2738
NSN 5935-00-127-2482
NSN 5996-01-516-7144
NSN 5999-01-079-9649
NSN 5945-01-540-0909