CLOSURE ELEMENT WITH EXTENSIONS FOR INTERNAL PASSAGE OF COMPONENT

A closure element for an internal passage in a component, and a related method and turbine blade or nozzle are disclosed. The closure element includes a spherical body made of a first superalloy, and a plurality of extensions extending from a surface of the spherical body. The plurality of extension...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: CUI, Yan, TOLLISON, Brian Lee, ARNETT, Michael Douglas, LAYLOCK, Matthew Joseph
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:A closure element for an internal passage in a component, and a related method and turbine blade or nozzle are disclosed. The closure element includes a spherical body made of a first superalloy, and a plurality of extensions extending from a surface of the spherical body. The plurality of extensions made of the same, similar or different material other than the first superalloy. Subjecting the component to at least one thermal cycle causes a braze material to form a metallurgical bond with the spherical body, the plurality of extensions and the passage wall to seal the internal passage.