Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Radial flow devices
Reexamination Certificate
2006-10-25
2009-06-02
Nguyen, Ninh H (Department: 3745)
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Radial flow devices
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.
DeIvenois Paul
Latimer Jeremy
Cusick Ernest G.
General Electric Company
Landgraff Frank A.
Nguyen Ninh H
LandOfFree
Airfoil shape for a compressor does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Airfoil shape for a compressor, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Airfoil shape for a compressor will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-4143989