FIELD: machine building.
SUBSTANCE: turbojet consists of three combustion chambers with the gas-air circuits connected to the nozzles, turbine and compressors. One combustion chamber is located between the compressor and the turbine, and the other two - behind it, one around the other. The air flows into the internal combustion chamber through the turbine windows from the joined centrifugal compressor, which takes it out of the internal cavity, and washes the first chamber.
EFFECT: invention is directed to expand the range of work of the turbojet engine and to cool its parts.
1 dwg
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RU2764941C1 |
