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...
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Patent |
Sprache: | eng ; fre ; ger |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
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). |
---|