2990-01-483-3818
Find complete technical information, availability, and procurement data for: 2990-01-483-3818
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A continuous combustion type engine. Consists primarily of a compressor, aircraft gas turbine engine, chamber, combustion, aircraft gas turbine engine and a turbine assembly, aircraft gas turbine engine. It may have an afterburner, turbine engine and/or 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, pneumatic power or thrust 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.
2990-01-483-3818, no name available
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