Compressor impeller thickness profile with localized thick spot

Fluid reaction surfaces (i.e. – impellers) – Rotor having flow confining or deflecting web – shroud or... – Radially extending web or end plate

Reexamination Certificate

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C416S235000, C416S23600R

Reexamination Certificate

active

07112043

ABSTRACT:
An air foil includes a leading edge, a trailing edge, a hub contour, and a tip contour, whereby the hub contour and tip contour extend between the leading and trailing edges to define a blade surface therebetween. A localized thick spot is disposed between the leading edge and the trailing edge and extends from a first point on the hub contour to a second point on the tip contour. The localized thick spot includes a generally sheared profile and is operable to provide the air foil with a desired strength while concurrently providing desired aerodynamic properties.

REFERENCES:
patent: 4865520 (1989-09-01), Hetzel et al.
patent: 6905309 (2005-06-01), Nussbaum et al.
patent: WO 8000468 (1980-03-01), None
Dresser-Rand; Isopac Compressor Impeller Upgrade; “Driving down operating costs by increasing compressor efficiency” (2000-2003); pp. 1-2.
Clean Dry Air, Inc.; Centrifugal Air Compressor Surge; “What word strikes fear in the heart of centrifugal compressor operators? SURGE!” (Aug. 2000); pp. 1-4.
Compressor Surge; “Dissection of Surge in a High Speed Centrifugal Compressor Using Digital PIV”; Mark P. Wernet and Michelle Bright; (Jan. 1999); pp. 1-2.

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