METHOD AND SYSTEM FOR TURBOJET CONTROL Russian patent published in 2014 - IPC F01D21/00 

Abstract RU 2507403 C2

FIELD: engines and pumps.

SUBSTANCE: signal E10 typical of rotor vibration level in turbojet operation is received to define rotor rotation mode E20 during operation. Signal amplitude E40 is compared with at least one predetermined vibration threshold depending upon rotor rotation mode. In case amplitude peak exceeds said threshold signal E50 in strobe pulse formed around amplitude peak to define (E60) is phenomenon caused said amplitude peak is either a mechanical impact at turbojet rotor or a signal electronic disturbance.

EFFECT: reliable detection of faults.

10 cl, 8 dwg

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RU 2 507 403 C2

Authors

Zhere Valerio

Griffaton Zhjul'En

Gijeman Gregori

Dates

2014-02-20Published

2009-10-09Filed