CHEMICAL MILLING OF GAS TURBINE ENGINE BRISK

PROBLEM TO BE SOLVED: To provide a chemical milling method for changing the chord length (46) and/or the thickness (50) of at least one blade (18) in a gas turbine engine brisk (10) having a hub (14) and a plurality of metal blades (18). SOLUTION: At least one blade (18) of the brisk (10) is treated...

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Bibliographische Detailangaben
Hauptverfasser: YOUNG KURT EDWARD, GUTKNECHT JAMES EDWARD, BALLMAN STEVEN MARK, STAMM EDWARD IVAN, DAVIS BRIAN MICHAEL
Format: Patent
Sprache:eng
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