FIELD: engines and pumps.
SUBSTANCE: nuclear gas turbine engine incorporates the first and second loops, compressor fitted on outer shaft at least one turbine wheel air intake, jet nozzle and nuclear reactor with heat carrier circulation lines. Aforesaid engine incorporates also Striling engine arranged behind turbine, blower and combustion chamber. Said Stirling engine is linked to inner shaft and communicates via heat carrier circulation lines with nuclear reactor. Blower is fitted on inner shaft, while combustion chamber is arranged between compressor and turbine.
EFFECT: higher efficiency and reliability.
6 cl, 6 dwg
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| COMBINED NUCLEAR BOOST AIRCRAFT ENGINE | 2008 |
|
RU2391525C1 |
