COMPOSITE BLADE ROOT ATTACHMENT

A preferred embodiment of the said present invention is a gas turbine engine blade root shim (40) for use between a composite blade root (18) and a wall of a slot for receiving the root in a rotor (12) of the engine. An exemplary embodiment of the shim (40) includes a longitudinally extending base (...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: THOMAS CARL MESING, JOHN ANDREW RAVENHALL
Format: Patent
Sprache:eng
Schlagworte:
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