TURBOJET ENGINE Russian patent published in 1997 - IPC

Abstract RU 2096642 C1

FIELD: aeronautical engineering; surface and water transport. SUBSTANCE: turbojet engine includes case 1 provided with inlet hole 2 and outlet hole 3 and mounted in bearings 4 for axial rotation. Bearings are mounted in supports-step beatings 5. Compressor 6 provided with blades 7 is rigidly secured inside case 1 at inlet hole 2 by means of rim 8. Compressor blades 7 form axial hole 9 where injector 10 is mounted. Turbine 11 provided with blades 12 is rigidly secured at outlet hole 3 by means of rim 13. Turbine blades 12 form outlet nozzle 14 of engine. EFFECT: enhanced efficiency. 3 dwg

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RU 2 096 642 C1

Authors

Dedenev Sergej Nikolaevich

Dates

1997-11-20—Published

1995-01-31—Filed