FIELD: engines and pumps.
SUBSTANCE: invention relates to gas turbines, namely, to turbo-machine high rpm loaded rotors. The gas turbine engine disk-to-shaft joint incorporates the disk external member fitted on the shaft shank splines. The turbine disk external member is furnished with axial diametrically opposite slots with their cross-section sizes exceeding those of lengthwise cross-section of the nut locking axially the turbine disk by 0.1 to 1.0 mm.
EFFECT: higher reliability of turbine operation.
2 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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| TURBOJET ENGINE TURBINE | 2013 |
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RU2534678C1 |
