Repairing method for a turbine nozzle segment

A method for repairing a turbine nozzle segment (10) having at least one vane (34) disposed between outer and inner bands (14,16) includes separating the inner band (16) from the nozzle segment (10), and joining the inner band (16) to a newly manufactured replacement casting (30) having an outer ban...

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Bibliographische Detailangaben
Hauptverfasser: CALDWELL, JAMES MICHAEL, LIELAND, KENNETH MORAND, NICHOLS, GLENN HERBERT, CADDELL, JAMES WALTER JR
Format: Patent
Sprache:eng ; fre ; ger
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