FIELD: gas turbine engine engineering. SUBSTANCE: conical journal 2 of ceramic turbine 1 is arranged in the space defined by bore of sleeve 5 of metal shaft 4 of compressor 5. The sleeve and journal are interconnected with bayonet joint formed by projections and hollows. Metal stop ring 10 having radial recesses 14 on face 13 is secured inside the sleeve by pins 11. The overrunning thrust clutch is formed by race 16 with rolling bodies and recess 14 on pin 2 and disk 10. The centering conjugated surfaces 19,20 of journal 2 and sleeve 5 can be spherical. The torque is transmitted from turbine 1 to compressor 3 through rolling bodies 15 and pins 11. EFFECT: enhanced reliability. 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF ASSEMBLING METAL-CERAMIC ROTOR OF TURBINE AND METAL-CERAMIC ROTOR OF TURBINE | 0 |
|
SU1816869A1 |
| ASSEMBLY PROCESS FOR METAL-CERAMIC ROTOR | 0 |
|
SU1815335A1 |
| TWO-STROKE AXIAL DIESEL ENGINE | 1997 |
|
RU2128774C1 |
| TURBOCOMPRESSOR WITH INTERNAL COMBUSTION ENGINE SUPERCHARGING CONTROL SYSTEM AT OVERHANGING POSITION OF WHEELS | 1991 |
|
RU2053412C1 |
| GAS TURBINE ENGINE | 2013 |
|
RU2539403C1 |
| GAS TURBINE TURBO COMPRESSOR ROTOR | 2011 |
|
RU2487274C1 |
| INTERNAL COMBUSTION ENGINE | 1997 |
|
RU2146010C1 |
| TURBO-ELECTRO-GENERATOR | 2009 |
|
RU2427714C1 |
| CERMENT ROTOR FOR TURBINE | 0 |
|
SU1663201A1 |
| SUPPORT OF SHAFT ROTOR OF LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE (VERSIONS), BODY OF SHAFT SUPPORT AND BODY OF BALL-BEARING ROTOR SHAFT SUPPORT | 2016 |
|
RU2614020C1 |
