Transition duct aft end frame cooling and related method

A transition duct for a gas turbine includes a tubular body having a forward end and an aft end, the aft end surrounded by a frame component; an interior closure band within the aft end, covering interior top, bottom and side wall surfaces of the frame; and a plurality of cooling channels between th...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Davis, Jr, Lewis B, Chila, Ronald J, McMahan, Kevin W
Format: Patent
Sprache:eng
Online-Zugang:Volltext bestellen
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