Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Cantilever blade
Reexamination Certificate
2005-05-31
2005-05-31
Look, Edward K. (Department: 3745)
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Cantilever blade
C416S22300B, C416SDIG002, C416S242000, C416S243000
Reexamination Certificate
active
06899526
ABSTRACT:
A compressor airfoil includes opposite pressure and suction sides joined together at leading and trailing edges and extending in span between a root and tip. The airfoil includes stagger increasing above the root and decreasing above a midspan pitch section thereof.
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Smith et al, “Sweep and Dihedral Effects in Axial-Flow Turbomachinery, ” ASME 62-WA-102, 1962, pp: 1-14.
Doloresco Bryan Keith
Wood Peter John
Andes William S.
Conte Francis L.
Edgar Richard A
General Electric Company
Look Edward K.
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