FIELD: engines and pumps.
SUBSTANCE: gas turbine engine comprises inlet device, compressor, combustion chamber, turbine and nozzle. Gas turbine engine comprises also disks of compressor and engine running independently in opposite directions and furnished inner-gearing gear rims fitted on their hubs, and parallel shafts with gear wheels arranged between compressor and turbine.
EFFECT: high specific performances of engine, low specific weight.
3 dwg
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