TURBO-COMPRESSOR OF GAS-TURBINE ENGINE Russian patent published in 2011 - IPC F04D29/32 

Abstract RU 2414628 C1

FIELD: engines and pumps.

SUBSTANCE: engine rotor has discs with hubs having splines taken out from under the bed on external elements; at that, hubs are located relative to the disc bed axis so that the ratio of surface areas is F1/F2=1.0…1.9, where: F1 - section area of front part of the hub in location place of external element with splines, and F2 - section area of rear part of the hub.

EFFECT: increasing service life and operability of the engine by providing alignment and elimination of rotor vibrations owing to re-distribution of thicknesses as to width of disc hubs.

3 dwg

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RU 2 414 628 C1

Authors

Tunkin Anatolij Ivanovich

Dates

2011-03-20Published

2009-08-31Filed