Airfoil with supplemental cooling channel adjacent leading edge

An airfoil, and in a disclosed embodiment a rotor blade, has film cooling holes formed at a leading edge. A supplemental film cooling channel is positioned near the leading edge, but spaced toward the trailing edge from the leading edge. The supplemental film cooling channel directs film cooling air...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Cunha, Frank J, Pietraszkiewicz, Edward F, Kontrovitz, David M, Levine, Jeffrey R, Chon, Young, Mongillo, Dominic, Teller, Bret
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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