APPARATUS AND METHOD FOR NON-DESTRUCTIVE DETECTION OF FAN BLADE ELECTRICAL ISOLATION

An apparatus and method for detecting a short in a blade (70) of a gas turbine engine, the apparatus including: a first plate (92) configured to form a first capacitor (C 1 ) with the protective sheath (80) when the apparatus is located proximate to the blade (70); a second plate (94) configured to...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: DARDONA, Sameh, TOKGOZ, Cagatay
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:An apparatus and method for detecting a short in a blade (70) of a gas turbine engine, the apparatus including: a first plate (92) configured to form a first capacitor (C 1 ) with the protective sheath (80) when the apparatus is located proximate to the blade (70); a second plate (94) configured to form another capacitor (C 3 )with a portion of the airfoil (72) when the apparatus is located proximate to the blade (70); and a voltage source (96) electrically connected to the first plate (92) and the second plate (94).