High efficiency, low axial profile, low noise, axial flow fan
AssigneeSiemens Automotive Corporation
InventorsWilliam P. Gallivan, Haran K. Periyathamby, Alex S. Joseph
Life of this patent
Estimating the term…
Abstract
The fan blades have a particular geometry that combines high efficiency, low axial profile, and low noise in an axial flow fan. The fan also comprises a circular outer band that coacts with a surrounding shroud structure to form a labyrinth air seal. The shroud structure comprises two parts that cooperatively define a radially inwardly open groove within which a flange of the fan band is received to form the labyrinth seal.
Claims2
A one-piece high efficiency, low axial profile, low noise, axial flow fan comprising a hub that is rotatable about an axis, a plurality of skewed, airfoil-shaped fan blades distributed circumferentially around said hub and extending both radially and axially away from said hub, each blade having a root joining with said hub, a circular band that is concentric with and spaced radially outwardly from said hub, each blade having a crest joining with said band, and wherein the axially rearward face of said hub, the axially rearward edge of said band and the tails of said blades occupy a common plane that is perpendicular to said axis, and in which each of said blades is constructed substantially in accordance with parameters defined as
- ______________________________________ R C .theta. .epsilon. Y OFFSET SKEW (p.u.) (p.u.) (deg.) (deg) (mm) (adjusted) ______________________________________ 0.43 0.87 42 71.7 0 0.0 0.50 0.80 27 75.6 0 2.5 0.57 0.67 19 75.9 0 3.7 0.64 0.54 18 75.8 0 2.4 0.72 0.47 17 74.9 0 0.9 0.79 0.40 17 73.1 0 -1.2 0.86 0.34 17 72.3 0 -4.4 0.93 0.29 17 72.3 0 -8.0 1.00 0.23 20 72.8 0 -15.4 ______________________________________
- wherein R(p.u.) is radial distance from axis as a function of the fan's radius, C(p.u.) is chord length of the blade's airfoil-shaped cross section at the corresponding radial distance as a fraction of the cross section's radial distance, .theta. is the camber angle of the cross section, .epsilon. is the stagger angle of the cross section, and Y-OFFSET is measured between the trailing edge of the cross section and the back of the hub.
A one-piece high efficiency, low axial profile, low noise, axial flow fan comprising a hub that is rotatable about an axis, a plurality of skewed, airfoil-shaped fan blades distributed circumferentially around said hub and extending both radially and axially away from said hub, each blade having a root joining with said hub, a circular band that is concentric with and spaced radially outwardly from said hub, each blade having a crest joining with said band, and wherein the axially rearward face of said hub, the axially rearward edge of said band and the tails of said blades occupy a common plane that is perpendicular to said axis, and in which each of said blades is constructed substantially in accordance with parameters defined as
- ______________________________________ R C .theta. .epsilon. Y OFFSET SKEW (p.u.) (p.u.) (deg.) (deg) (mm) (adjusted) ______________________________________ 72.5 63 42 71.7 0 -4.3 84.5 68 27 75.6 0 -1.8 96.5 65 19 75.9 0 -0.6 108.5 59 18 75.8 0 -1.9 120.5 57 17 74.9 0 -3.4 132.5 53 17 73.1 0 -5.5 144.5 49 17 72.3 0 -8.7 156.5 46 17 72.3 0 -12.3 168.5 39 20 72.8 0 -19.7 ______________________________________
- wherein R(p.u.) is radial distance from axis, C(p.u.) is chord length of the blade's airfoil-shaped cross section at the corresponding radial distance, .theta. is the camber of the cross section, .epsilon. is the stagger angle of the cross section, and the Y-OFFSET is measured between the trailing edge of the cross section and the back of the hub.
Dependencies are inferred from the claim text.