High structural efficiency blades and devices using same

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Laminated – embedded member or encased material

Reexamination Certificate

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Details

C416S232000, C416S24100B, C416S21000A

Reexamination Certificate

active

07322798

ABSTRACT:
A blade for a rotor has integral stiffeners with at least one of unidirectional caps configured to carry blade bending loads in axial tension or webs to carry transverse shear resulting from blade bending.

REFERENCES:
patent: 2637405 (1953-05-01), Stanley
patent: 2961053 (1960-11-01), Prewitt et al.
patent: 4339230 (1982-07-01), Hill
patent: 5547629 (1996-08-01), Diesen et al.
patent: 6942461 (2005-09-01), Wobben

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