METHOD OF TESTING THE GAS-TURBINE ENGINE BLADES AND DEVICE FOR ITS REALIZATION Russian patent published in 1994 - IPC

Abstract RU 2024837 C1

FIELD: aircraft construction. SUBSTANCE: blades are fixed on the test stand rim and are rotated with the constant speed 15-20 turn-overs/min. In so doing the abrasive particles (20-50 microns) are mixed in the gas flow removed out of the engine combustion chamber when the temperature is changed from 650 till 850 C. Then the abrasion of the tested workpiece surface is evaluated by each temperature change and by the particle size. EFFECT: enhanced accuracy of measurements. 2 cl, 1 dwg

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RU 2 024 837 C1

Authors

Shkrabak V.S.

Mukhametzhanov K.S.

Rybnikov A.I.

Selivanova M.A.

Dates

1994-12-15Published

1991-09-06Filed