Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Having wear liner – sheathing or insert
Patent
1998-08-17
1999-12-21
Look, Edward K.
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Having wear liner, sheathing or insert
416219R, 416229A, 416248, 416220R, 416239, B63H 126
Patent
active
060041013
ABSTRACT:
A gas turbine engine fan blade includes an airfoil and dovetail having an integral aluminum core and a fatigue resistant reinforcing sheath.
Busbey Bruce C.
Jackson Joseph J.
Schilling Jan C.
General Electric Company
Herkamp Nathan D.
Hess Andrew C.
Look Edward K.
Nguyen Ninh
LandOfFree
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