FRONT SUPPORT OF LP TURBINE ROTOR OF TWO-SHAFT GAS TURBINE ENGINE Russian patent published in 2013 - IPC F02C7/06 

Abstract RU 2482303 C1

FIELD: engines and pumps.

SUBSTANCE: bearing is designed radial-thrust, splines and mating splines of one of splined joints are designed screw-type in the shape of multi-start thread, which threads are directed to the opposite side from direction of HP rotor rotation with possibility of axial displacement of a spring to create axial force on outer ring of the bearing during engine operation after the mode of its start. Also there is a fixing device restricting axial displacement of the spring in direction from the bearing.

EFFECT: eliminating defect of slipping motion during engine operation.

2 cl, 3 dwg

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RU 2 482 303 C1

Authors

Erichev Dmitrij Jur'Evich

Kikot' Nikolaj Vladimirovich

Rajkov Jurij Vasil'Evich

Fomina Ol'Ga Nikolaevna

Dates

2013-05-20Published

2011-12-22Filed