High efficiency, non-ragging, formed axial impeller
View Patent ↗An axial impeller has blades formed from sheet metal blanks that are configured from taking a desired impeller blade and mathematically “unwinding” the blade to its flat counterpart. Preferably, the impeller blade is formed from a single rolling operation. The result of a thin, elongate blade, preferably having a trailing edge that defines a helix with rearwardly skewed, forwardly raked blades, provides an efficient impeller having good anti-ragging properties.
1. A method for forming an anti-ragging impeller comprising the steps of:
providing an arcuate impeller blade blank formed of a planar sheet metal, the blank having an inside curve, an outside curve, a tip and a root;
rolling at least a portion of the blank from the root to the tip to form an impeller blade in which the inside curve forms an impeller trailing edge and the outside curve forms the impeller leading edge; and
orienting the rolled impeller blade with respect to an axis of rotation such that the trailing edge from the root to the tip approximates the properties of a helix, and the blades are capable of being assembled into an impeller.
2. The method of claim 1 wherein the rolling step is a single rolling step that produces a single rolling radius.
3. The method of claim 2 wherein the roll radius is between approximately 1.0 and 0.33 the impeller diameter.
4. The method of claim 2 wherein the roll radius is between approximately 0.9 and 0.5 the impeller diameter.
5. The method of claim 2 wherein the roll radius is between approximately 0.8 and 0.7 the impeller diameter.
6. The method of claim 2 wherein the roll radius is approximately 0.75 the impeller diameter.
7. The method of claim 2 wherein the impeller blade is concave up such that a center of the rolling radius is above the impeller blade.
8. The method of claim 2 wherein the blank is rolled about a roll axis, wherein the roll axis and the axis of rotation do not intersect.
9. The method of claim 2 wherein the rolling step comprises rolling at least a portion of the blank from tip to root.
10. The method of claim 1 wherein the rolling step is several bending steps.
11. The method of claim 1 wherein the impeller blade is elongate.
12. The method of claim 1 wherein the trailing edge approximates a helix of of a similar pitch.
13. The method of claim 1 wherein each one of the blades has a planar root portion.
14. The method of claim 13 wherein the impeller is connected to the hub by fasteners through the planar root portion of the impeller and a plate, wherein heads of the fasteners are recessed to enhance anti-ragging properties and the fasteners may engage threads tapped into the planar root portion.
15. The method of claim 1 wherein the impeller has a pitch to diameter ratio of approximately 0.2 to 5.0.
16. The method of claim 15 wherein a pitch to diameter ratio varies no more than about 20 percent from an average pitch to diameter ratio.
17. The method of claim 15 wherein a pitch to diameter ratio varies no more than about 10 percent from an average pitch to diameter ratio.
18. The method of claim 1 wherein the impeller has a pitch to diameter ratio of approximately 0.7 to 0.5.
19. The method of claim 1 wherein the impeller has a pitch to diameter ratio of approximately 0.6.
20. The method of claim 1 wherein a maximum width of the impeller blade is between 0.04 and 0.06 the impeller diameter.
21. A method for forming an anti-ragging impeller comprising the steps of:
forming an arcuate impeller blade blank out of planar sheet metal, the blank having an inside curve, an outside curve, a tip and a root;
orienting the blank with respect to a roll axis, the roll axis being above a top surface of the blank;
rolling at least a portion of the blank from the root to the tip about the roll axis to form an impeller blade in which the inside curve forms an impeller trailing edge and the outside curve forms the impeller leading edge; and
coupling the rolled impeller blade to a hub, the rolled impeller blade and the hub being configured to rotate about an axis of rotation that extends through a center of the hub, the axis of rotation and the roll axis do not intersect, the trailing edge having a blade angle at a given radial position R with respect to a horizontal plane and tangent to a cylinder whose radius is at the radial position R and whose center is coincident with the axis of rotation conforms to an angle of a pure helix of a given pitch whose center lies at the axis of rotation at the same radial position R, tangent to a similarly positioned cylinder of radius R and with respect to the horizontal plane.
22. The method of claim 21 , wherein an inner non-rolled flat portion of the blade is 39.0° with respect to the horizontal plane.