METHOD FOR EXTRACTING ROTOR DYNAMIC ORBIT FROM BLADE TIP CLEARANCE AND TIME OF ARRIVAL MEASUREMENTS

A system for determining rotor-dynamic orbit information including an engine case supporting at least one engine stage, each at least one engine stage including a rotor having blades; at least one blade tip sensor operatively coupled to the engine case and in operative communication with the blades;...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Varney, Philip Andrew, Lomenzo, Richard A, Koetsch, Christopher T
Format: Patent
Sprache:eng ; fre ; ger
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