Airfoil shape for a compressor

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Radial flow devices

Reexamination Certificate

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C416S243000

Reexamination Certificate

active

07540715

ABSTRACT:
An article of manufacture having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a TABLE 1. Wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape.

REFERENCES:
patent: 6832897 (2004-12-01), Urban
patent: 6910868 (2005-06-01), Hyde et al.
patent: 6994520 (2006-02-01), Humanchuk et al.
patent: 7186090 (2007-03-01), Tomberg et al.

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