2840-12-379-2598

Aircraft Gas Turbine Engine

2840123792598 123792598

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. View more Aircraft Gas Turbine Engine

2840-12-379-2598 ENGINE,GAS TURBINE,AIRCRAFT 2840123792598 123792598

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Data Last Changed
January 2024
NATO Update Count
1
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NSN 2840-12-379-2598 (Generic Image) 1/1

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2840-12-095-1442 Machine Screw 2840-12-095-0214 Power T Worm Sleeve 2840-12-350-8512 Heatshield 2840-12-379-2598

2840-12-379-2598 Demil Restrictions 2840-12-379-2598

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2840-12-379-2598 is a Aircraft Gas Turbine Engine

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