Compensating for blade tip clearance deterioration in active clearance control

A method to compensate for blade tip clearance deterioration between rotating blade tips and a surrounding shroud in an aircraft gas turbine engine includes determining one or more variables based on at least one or more moving averages of one or more engine operating parameters respectively average...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MARUSCIK RONALD GEORGE, VISHNAUSKI JON MICHAEL, WISEMAN MATTHEW WILLIAM, HERRON WILLIAM LEE, KRUPP BRIAN EDWARD
Format:	Patent
Sprache:	eng
Schlagworte:	CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS
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