METHOD OF DIAGNOSTICS OF GAS-TURBINE ENGINE COMPRESSOR Russian patent published in 1998 - IPC

Abstract RU 2118807 C1

FIELD: checking of mechanical condition of gas-turbine engines. SUBSTANCE: air temperature is additionally measured upstream and upstream and downstream of compressor in check mode of gas turbine engine operation nпк.red = const. Method includes determination of value of compressor air heating reduced to standard atmospheric conditions, as well as reduced value of relative variation of compressor air heating in process of operation. This value is used to find critical (as to gas-dynamic stability) value of degree of wear of compressor flow-through part elements. Reserve of stability of gas-turbine engine compressor is judged by relation of wear degrees. EFFECT: enhanced checking. 2 dwg

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RU 2 118 807 C1

Authors

Cherenkov S.V.

Sushentsov V.M.

Vlasov K.V.

Berezin G.V.

Khalutin A.V.

Barmin O.V.

Dates

1998-09-10Published

1995-02-24Filed