Blade
The invention relates to a blade for a fan impeller. In particular, the invention relates to the geometric configuration of the blade in its end area facing a hub. Furthermore, the invention relates to a fan impeller. A blade according to the invention for a fan impeller has an end area facing a hub, whereby the blade has at least one rib in the end area facing the hub, whereby the rib has an outer contour that simulates a flow profile.
1. A blade for a fan impeller with an end area facing a hub, characterized in that the blade has at least one rib in the end area facing the hub, wherein the at least one rib has a starting point (P 1 ) at a shoulder of the blade leading to the hub and extends away from the hub to an end point (P 2 ), the at least one rib having an outer contour (A) that extends from the starting point (P 1 ) to the end point (P 2 ), wherein the outer contour (A) simulates a flow profile and forms an angle ( 3 ) between −45° and +45° with respect to a radial direction of the shoulder, wherein the ratio of the maximum wall thickness (tw) of the blade to the maximum profile thickness (tmax) of the blade is in the range from 0.1 to 0.9, wherein the at least one rib has an end geometry in an area of the outer contour (A), wherein the end geometry creates a saw-tooth profile, and wherein the end geometry of the at least one rib forms an angle (a) in the range from −1° to +45° or from 10 to 450 relative to the outer contour (A).
2. The blade according to claim 1 , characterized in that the ratio of the maximum wall thickness (t_w) of the blade to the maximum profile thickness (t_max) of the blade is in the range from 0.2 to 0.6.
3. The blade according to claim 1 , characterized in that the ratio of the thickness (b) of the at least one rib to the wall thickness (t_w) of the blade is in the range 0.1 to 2.
4. The blade according to claim 3 , characterized in that the ratio of the thickness (b) of the at least one rib to the wall thickness (t_w) of the blade is in the range from 0.5 to 1.5.
5. The blade according to claim 1 , characterized in that a further course of the at least one rib from the end area facing the hub is configured to be rectilinear.
6. The blade according to claim 1 , characterized in that a further course of the at least one rib from the end area facing the hub is configured to be curved counterclockwise to the left of the radial direction (r).
7. The blade according to claim 1 , characterized in that a further course of the at least one rib from the end area facing the hub is configured to be curved clockwise to the right of the radial direction (r).
8. The blade according to claim 1 , characterized in that the end geometry of the at least one rib forms the angle (α) in the range from −1° to −30° or from 1° to +30° relative to the outer contour (A).
9. The blade according to claim 1 , characterized in that the at least one rib includes a plurality of ribs, wherein between any two of the plurality of ribs, there is a gap and whereby the ratio of the width (s) of the gap to the thickness (b) of the at least one rib is in the range from 0.2 to 5.
10. The blade according to claim 9 , characterized in that between any two of the plurality of ribs, there is a gap and whereby the ratio of the width(s) of the gap to the thickness (b) of one of the any two of the plurality of ribs is in the range from 0.5 to 1.5.
11. The blade according to claim 1 , characterized in that the starting point (P 1 ) of the at least one rib in the end area facing the hub where the blade is connected to the hub is situated closer to the hub on the blade higher in the axial direction than the end point (P 2 ) of the at least one rib.
12. A fan impeller with a hub, characterized in that the fan impeller has at least one blade according to claim 1 .
13. A fan impeller according to claim 12 , characterized in that the fan impeller is an axial fan impeller.
14. A fan impeller according to claim 12 , characterized in that the fan impeller is a radial fan impeller.