SEALS FOR ROTARY DEVICES AND METHODS OF PRODUCING THE SAME

In one aspect, a seal for a turbine engine includes a seal body disposed at a base of a turbine engine blade and a wing portion extending axially from said seal body. The wing portion has a first portion substantially parallel with a centerline of the engine and an angled upturn portion. The first p...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: KAREFF SPENCER AARON, PIERSALL MATTHEW ROBERT
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:In one aspect, a seal for a turbine engine includes a seal body disposed at a base of a turbine engine blade and a wing portion extending axially from said seal body. The wing portion has a first portion substantially parallel with a centerline of the engine and an angled upturn portion. The first portion extends between the seal body and the angled upturn portion. An angle between the engine centerline and the angled upturn portion is between about 0 degrees and about 90 degrees.