Finishing tool for turbomachine components

A finishing tool form assembly (58) includes a base (70) and a superabrasive (66) bonded to a surface of the base (70). The superabrasive (66) is configured to be reciprocated with the base (70) relative to a longitudinally extending recess (50) of a component (46) to finish at least one surface (54...

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Bibliographische Detailangaben
Hauptverfasser: VALENTINE, DAVID E, SCHMARTZ, JOHN M, NICOLSON, MATTHEW D
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:A finishing tool form assembly (58) includes a base (70) and a superabrasive (66) bonded to a surface of the base (70). The superabrasive (66) is configured to be reciprocated with the base (70) relative to a longitudinally extending recess (50) of a component (46) to finish at least one surface (54) of the component (46).