US5326225A
Expired / Lapsed
US
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High efficiency, low axial profile, low noise, axial flow fan
Assignee: Siemens Canada Ltd
•
Filing: 1993-07-12
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Granted: 1994-07-05
•
Expires: 2013-07-12
Abstract
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.
Inventors
- 👤 William P. Gallivan
- 👤 Haran K. Periyathamby
- 👤 Alex S. Joseph
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 20:28
CPC Classifications
F; F04; F04D; F04D29/00; F04D29/26; F04D29/32; F04D29/38; F04D29/384; F04D29/386; F04D29/08; F04D29/16; F04D29/161; F04D29/164; F04D29/325; F04D29/40; F04D29/52; F04D29/54; F04D29/541; F04D29/545; Y; Y10; Y10S; Y10S416/00; Y10S416/02
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
267 words
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 θ ε
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, θ is the camber angle of the cross section, ε 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.
Claim 2
Dependent Claim
267 words
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 θ ε
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, θ is the camber angle of the cross section, ε 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.
Claim 3
Dependent Claim
251 words
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 θ ε
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, θ is the camber of the cross section, ε 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.
Claim 4
Dependent Claim
251 words
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 θ ε
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, θ is the camber of the cross section, ε 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.
References Cited (Backward Citations)
US3842902A
Cited
US4505641A
Cited
US4406581A
Cited
US4685513A
Cited
US4566852A
Cited
US4569632A
Cited
US4548548A
Cited
US4569631A
Cited
US4684324A
Cited
US4930984A
Cited
US4900229A
Cited
US5183382A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1997-07-04 | 1998-01-03 | 1998-07-05 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2001-07-04 | 2002-01-03 | 2002-07-05 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2005-07-04 | 2006-01-03 | 2006-07-05 | $7700.00 | Window Closed / Lapsed |