TURBOJET ENGINE Russian patent published in 1997 - IPC

Abstract RU 2096643 C1

FIELD: aeronautical engineering; surface and water transport. SUBSTANCE: turbojet engine includes case 1 made in form of semi-closed spindle-shaped chamber, axial shaft 2 mounted inside case in supports 3, compressor with blades mounted at inlet hole, combustion chamber 5, turbine with blades having inner side 7 and outer side 8 formed by spirals shaped grooves 9 in tail section of case; depth of these grooves increases smoothly in direction of outlet nozzle. Case is mounted for axial rotation in bearings 10. Engine is also provided with injectors 11, jet nozzle 12 and cooling blades 13. EFFECT: enhanced reliability. 3 cl, 6 dwg

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RU 2 096 643 C1

Authors

Dedenev Sergej Nikolaevich

Dates

1997-11-20Published

1995-02-28Filed