METHOD OF TREATMENT OF GAS-TURBINE ENGINES BLADES Russian patent published in 2010 - IPC B24B19/14 

Abstract RU 2379170 C1

FIELD: machine building.

SUBSTANCE: instrument is actuated into rotation at a rate directly proportional to value of fillet radiuses of treated edge of point of blade and actuated into contact to edge. It is implemented oscillation of blade relative to longitudinal axis, passing through centers of fillet radiuses of edge of point, with frequency, which is changed directly proportional to fillet radiuses values of edge of point. Instrument is displaced lengthwise edge of point at a rate inversely proportional of values of its fillet radiuses.

EFFECT: there is increased shaping accuracy of variable-profile of fillet of edge of point of blade and provided minimal removing of material at treatment, providing to round an edge by radius 0,04 mm.

2 cl, 2 dwg

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RU 2 379 170 C1

Authors

Gurfinskij Leonid Il'Ich

Pupovskij Anatolij Filimonovich

Roman'Ko Nikolaj Grigor'Evich

Seregin Jurij Nikolaevich

Krajnikov Aleksandr Vjacheslavovich

Pajkin Aleksandr Grigor'Evich

Dates

2010-01-20Published

2008-04-30Filed