METHOD OF GREASING AND COOLING FRONT SUPPORT OF THE ROTOR OF THE GAS TURBINE ENGINE Russian patent published in 2017 - IPC F02C7/06 

FIELD: engines and pumps.

SUBSTANCE: invention relates to a method for lubricating aviation gas turbine engines (GTE) and can be used in engines where the drive of oil units is carried out directly from the GTE rotor, and oil units and oil system communications are installed inside the GTE. Method of lubrication and cooling the front of the rotor of the gas turbine engine support provided with a circulation lubrication system, wherein air entering the engine cools the oil tank and the oil is taken further to the supports, with cooling of the oil tank body, combined with a heat exchanger and disposed inside the motor between the cook and the front support a rotor carried by air entering through the open air towards the oncoming flow channels in the spinner, while in the next stage of movement air proceeds into the rotor front support housing for its further cooling.

EFFECT: invention allows to increase the efficiency of oil cooling in the oil tank, the cooling efficiency of the front support of the GTE rotor, with the reduction of the mass and dimensions of the engine.

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