Turbine dovetail slot heat shield

Gas turbine engine turbine blade assembly includes a hollow airfoil joined to blade root, dovetail slot heat shield bonded or attached to a bottom surface of the root, and a shield outlet from heat shield open to inlet apertures extending radially through a radially inner root end of the root. Heat...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Van Derven, Christopher John, Schuppe, Christopher Thomas, Jendrix, Richard William, Stoughton, Samuel Joseph, Bibler, John David, McMillan, Charles Thomas
Format: Patent
Sprache:eng
Schlagworte:
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