US4610601A
Expired / Lapsed
US
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Method of making axial fan impeller
Assignee: Individual
•
Filing: 1984-07-02
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Granted: 1986-09-09
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Expires: 2004-07-02
Abstract
Abstract The axial fan produced by the novel method may have a cylindrical shroud, an impeller mounted coaxially within the shroud, and a bell-shaped deflector extending across the exhaust to redirect the airflow toward radially outward directions. A malleable blank may be cut and shaped to form the impeller having at least three blades, the peripheries of which define a cylinder coaxial with the shroud. The impeller should have a depth-to-radius ratio exceeding 0.5.
Inventors
- 👤 Sten R. Gerfast
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 19:46
CPC Classifications
F; F03; F03D; F03D1/00; F03D1/04; Y; Y02; Y02E; Y02E10/00; Y02E10/70; Y02E10/72; Y02P; Y02P70/00; Y02P70/50; Y10; Y10S; Y10S416/00; Y10S416/03; Y10T; Y10T29/00; Y10T29/49; Y10T29/49316; Y10T29/49327
Claims Analysis
Total Claims: 15
Claim 1
Independent Claim
183 words
A method of making an axial fan impeller comprising the steps of (a) forming in a flat malleable blank n generally radial cuts extending from first points equally spaced along a central circle, n being an integer of at least 3, n symmetrical first spiral cuts, each extending outwardly from a second point on said circle between adjacent first points to a third point on an adjacent generally radial cut, and n symmetrical second spiral cuts extending from fourth points at the outward extremities of the generally radial cuts, each second spiral cut extending generally parallel to the radially adjacent first spiral cut, an extension of each second spiral cut terminating at the next second spiral cut, (b) shaping each portion of the blank between radially adjacent first and second spiral cuts to provide n air-driving blades, the peripheries of which along the n second spiral cuts together generally define a cylinder coaxial with said central circle, and (c) forming each portion of the blank between said central circle and one of said first spiral cuts not to extend radially beyond the circle.
Claim 2
Independent Claim
183 words
A method of making an axial fan impeller comprising the steps of (a) forming in a flat malleable blank n generally radial cuts extending from first points equally spaced along a central circle, n being an integer of at least 3, n symmetrical first spiral cuts, each extending outwardly from a second point on said circle between adjacent first points to a third point on an adjacent generally radial cut, and n symmetrical second spiral cuts extending from fourth points at the outward extremities of the generally radial cuts, each second spiral cut extending generally parallel to the radially adjacent first spiral cut, an extension of each second spiral cut terminating at the next second spiral cut, (b) shaping each portion of the blank between radially adjacent first and second spiral cuts to provide n air-driving blades, the peripheries of which along the n second spiral cuts together generally define a cylinder coaxial with said central circle, and (c) forming each portion of the blank between said central circle and one of said first spiral cuts not to extend radially beyond the circle.
Claim 3
Dependent Claim
26 words
A method of forming an impeller as defined in claim 1 wherein in step (b) the blades are shaped to have a depth-to-radius ratio exceeding 0.5.
Claim 4
Dependent Claim
56 words
A method of forming an impeller as defined in claim 2 wherein in step (a) the blank is so formed that each of said second points is further from the first point of the generally radial cut to which its first spiral cut extends than it is to the first point of another generally radial cut.
Claim 5
Dependent Claim
46 words
A method of forming an impeller as defined in claim 2 wherein in step (c) portions of the blank between said central circle and a first spiral cut are folded to define together approximately a cylinder having a radius substantially equal to that of the circle.
Claim 6
Dependent Claim
55 words
A method of forming an impeller as defined in claim 2 wherein each of the second spiral cuts formed in step (a) extends beyond the generally radial cut toward which it is directed so that a small portion of each blade extends radially beyond an adjacent blade before the blank is formed into an impeller.
Claim 7
Dependent Claim
30 words
A method of forming an impeller as defined in claim 2 including the added step of fitting a thin reinforcing ring around the n air-driving blades near their trailing edges.
Claim 8
Dependent Claim
18 words
A method of forming an impeller as defined in claim 6 wherein said reinforcing ring is a wire.
Claim 9
Dependent Claim
67 words
A method of forming an impeller as defined in claim 7, in step (a) of which notches are formed at the peripheries of the blades shaped in step (b), and in said step (b) the blades to be shaped so that the cylinder generally defined by their peripheries is slightly less than the diameter of the wire ring and the wire ring flexes the blades slightly inwardly.
Claim 10
Independent Claim
182 words
A method of making an axial fan comprising the steps of (a) forming in a flat malleable blank n generally radial cuts extending from first points equally spaced along a central circle, n being an integer of at least 3, n symmetrical first spiral cuts, each extending outwardly from a second point on said circle between adjacent first points to a third point on an adjacent generally radial cut, and n symmetrical second spiral cuts extending from fourth points at the outward extremities of the generally radial cuts, each second spiral cut extending generally parallel to the radially adjacent first spiral cut, an extension of each second spiral cut terminating at the next second spiral cut, (b) shaping each portion of the blank between radially adjacent first and second spiral cuts to provide n air-driving blades, the peripheries of which along the n second spiral cuts together generally define a cylinder coaxial with said central circle, (c) forming each portion of the blank between said central circle and one of said first spiral cuts not to extend radially beyond the circle, and
Claim 11
Independent Claim
182 words
A method of making an axial fan comprising the steps of (a) forming in a flat malleable blank n generally radial cuts extending from first points equally spaced along a central circle, n being an integer of at least 3, n symmetrical first spiral cuts, each extending outwardly from a second point on said circle between adjacent first points to a third point on an adjacent generally radial cut, and n symmetrical second spiral cuts extending from fourth points at the outward extremities of the generally radial cuts, each second spiral cut extending generally parallel to the radially adjacent first spiral cut, an extension of each second spiral cut terminating at the next second spiral cut, (b) shaping each portion of the blank between radially adjacent first and second spiral cuts to provide n air-driving blades, the peripheries of which along the n second spiral cuts together generally define a cylinder coaxial with said central circle, (c) forming each portion of the blank between said central circle and one of said first spiral cuts not to extend radially beyond the circle, and
Claim 12
Dependent Claim
14 words
(d) rotatably mounting the impeller produced by steps (a-c) coaxially within a cylindrical shroud.
Claim 13
Dependent Claim
14 words
(d) rotatably mounting the impeller produced by steps (a-c) coaxially within a cylindrical shroud.
Claim 14
Dependent Claim
46 words
A method of making an axial fan as defined in claim 9, in step (b) of which the blades are shaped so that the diameter of the cylinder approximately defined by the peripheries of the blades is slightly smaller than the inside diameter of the shroud.
Claim 15
Dependent Claim
44 words
A method of making an axial fan as defined in claim 10, in step (b) of which the blades are shaped so that the periphery of each blade in the vicinity of its trailing edge tapers inwardly from said cylinder toward that trailing edge.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1989-09-08 | 1990-03-10 | 1990-09-09 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-09-08 | 1994-03-10 | 1994-09-09 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-09-08 | 1998-03-10 | 1998-09-09 | $7700.00 | Window Closed / Lapsed |