Repair of nickel-based alloy turbine disk

A method of adding material to a nickel-based superalloy component, such as a gas turbine rotor disk, without damaging the underlying material and without creating an unacceptable level of cracking. The method is advantageously applied in the repair of Alloy 706 turbine rotors having experienced ope...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Segletes, David Scott, Seth, Brij B, Kottilingam, Srikanth C, Ditzel, Peter Jon
Format: Patent
Sprache:eng
Online-Zugang:Volltext bestellen
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