US2024287999A1PendingUtilityA1
Impeller blade with uneven spacing
Est. expiryFeb 23, 2043(~16.5 yrs left)· nominal 20-yr term from priority
F04D 29/666F04D 29/30F04D 29/281F04D 17/06A46B 2200/104A46B 15/0051A45D 20/50F04D 29/328
43
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Claims
Abstract
An impeller assembly configured to produce low noise is provided. In one embodiment, an impeller assembly is provided having a hollow cylindrical hub body with a sleeve extending therethrough. The sleeve is configured to receive a driveshaft of a motor to couple the impeller assembly to the motor. The impeller assembly includes a plurality of impeller blades extending radially outward therefrom. Each blade of the plurality of impeller blades is unevenly distributed around a circumference of the hub body.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . An impeller assembly, comprising:
a generally cylindrical hollow hub body; a sleeve extending through the hub body, the sleeve includes a central bore therethrough configured to receive a driveshaft for coupling the impeller assembly to a motor; a plurality of vanes extending between the sleeve and the hub body; and a plurality of impeller blades extending radially outward from the hub body and being unevenly distributed around a circumference of the hub body.
2 . The impeller assembly of claim 1 wherein each impeller blade of the plurality of impeller blades is angled relative to a longitudinal axis of the hub body.
3 . The impeller assembly of claim 1 wherein the plurality of impeller blades comprises an odd number of impeller blades.
4 . The impeller assembly of claim 1 wherein each blade of the plurality of impeller blades includes an outer rim having a first vertex and a second vertex, and wherein a first distance between the first vertex of each impeller blade and a corresponding first vertex of a consecutive impeller blade in the clockwise direction differs from a second distance between the first vertex of each impeller blade and a corresponding first vertex of a consecutive impeller blade in the counterclockwise direction.
5 . The impeller assembly of claim 1 wherein a center of mass of the impeller assembly is positioned along a longitudinal axis of the hub body.
6 . The impeller assembly of claim 1 , wherein rotation of the hub body is configured to cause the plurality of impeller blades to create a pressure wave, and wherein at least two of plurality of impeller blades create pressure waves at different frequencies.
7 . The impeller assembly of claim 1 , further comprising a cylindrical covering disposed around the plurality of impeller blades.
8 . The impeller assembly of claim 7 , wherein the cylindrical covering includes a plurality of diffusing apertures.
9 . An impeller assembly comprising:
a hub body including an inner surface and an outer surface, wherein the inner surface comprises a recess; a sleeve extending through a center of the hub body, wherein the sleeve is configured to receive a driveshaft to physically couple the impeller assembly to a motor; a plurality of vanes extending from the sleeve to the inner surface; and a plurality of impeller blades extending radially outward from the outer surface and spaced around a circumference of the outer surface, wherein each blade of the plurality of impeller blades includes an outer edge having a first vertex and a second vertex, and wherein a first distance between the first vertex of each blade and a corresponding first vertex of an immediately adjacent blade in the clockwise direction differs from a second distance between the first vertex of each blade and a corresponding first vertex of an immediately adjacent blade in the counterclockwise direction.
10 . The impeller assembly of claim 9 , wherein each of the plurality of impeller blades is angled related to a longitudinal axis of the sleeve.
11 . The impeller assembly of claim 9 , wherein a center of mass of the impeller assembly is positioned along a longitudinal axis of the hub body.
12 . The impeller assembly of claim 9 , wherein rotation of the hub body is configured to cause the plurality of impeller blades to create a pressure wave, and wherein at least two of plurality of impeller blades have pressure waves that differ from one.
13 . The impeller assembly of claim 9 , wherein rotation of the hub body is configured to cause the plurality of impeller blades to produce a blade passage frequency with a magnitude in the sound pressure level range of 55 to 65 dB(A) when measured at 1 meter away from the plurality of impeller blades.
14 . The impeller assembly of claim 9 , wherein the plurality of impeller blades comprises an uneven number of impeller blades.
15 . The impeller assembly of claim 9 , further comprising a cylindrical covering disposed around the plurality of impeller blades.
16 . The impeller assembly of claim 15 , wherein the cylindrical covering includes a plurality of diffusing apertures.
17 . The impeller assembly of claim 9 , wherein each of the plurality of vanes is spaced equidistant from each other around the sleeve.Join the waitlist — get patent alerts
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