ROTATING COMPONENT BALANCE RING

A balance ring for a gas turbine engine has a ring shaped body with a first radial thickness, an anti-rotation tab extending outward from the body and at least one millable balancing feature connected to the body.

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Bibliographische Detailangaben
Hauptverfasser: HIMES, Jason D, KARNER, Peter Josef
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:A balance ring for a gas turbine engine has a ring shaped body with a first radial thickness, an anti-rotation tab extending outward from the body and at least one millable balancing feature connected to the body.