Centrifugal pump
US-2018135641-A1 · May 17, 2018 · US
US10458423B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10458423-B2 |
| Application number | US-201715613330-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 5, 2017 |
| Priority date | Jun 6, 2016 |
| Publication date | Oct 29, 2019 |
| Grant date | Oct 29, 2019 |
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An impeller of this disclosure includes a hub having a ring shape; and a plurality of blades that are provided on an outer periphery of the hub, wherein the blade has a trailing edge formed such that an inner side of a radial width of the blade is curved in a direction opposite to a rotation direction, in a plan view as viewed in a direction of a rotation axis.
Opening claim text (preview).
What is claimed is: 1. An impeller comprising: a hub having a ring shape; and a plurality of blades that are provided on an outer periphery of the hub, wherein a blade of the plurality of blades has a trailing edge formed such that an inner side of a radial width of the blade is curved in a direction opposite to a rotation direction, in a plan view as viewed in a direction of a rotation axis, wherein in the plan view as viewed in the direction of the rotation axis, the blade has a leading edge that is curved in the rotation direction, and wherein in the plan view as viewed in the direction of the rotation axis, the leading edge is formed such that an outer end of the leading edge is located closer to a side in the rotation direction than a straight line connecting the rotation center and a hub-side end of the leading edge. 2. The impeller according to claim 1 , wherein the blade has a shape such that a side close to the trailing edge swells toward a suction side. 3. The impeller according to claim 1 , wherein the blade is formed such that a chord length at an outermost side in a radial direction is longer that a chord length at a side closest to a rotation center. 4. The impeller according to claim 1 , wherein in a view as viewed in a direction perpendicular to the rotation axis, the leading edge is formed such that the outer end of the leading edge comes outward out of an end, which is the outer peripheral surface of the hub, on the leading edge. 5. The impeller according to claim 1 , wherein the blade is formed such that the outer end of the leading edge is curved toward the pressure side. 6. The impeller according to claim 1 , wherein in the plan view as viewed in the direction of the rotation axis, two blades adjacent to each other are formed such that a part of the leading edge of one blade overlaps with a part of the trailing edge of the other blade. 7. The impeller according to any one of claims 1 , wherein the trailing edge is located on a plane substantially flush with the end of the hub on the trailing edge. 8. A fan comprising: the impeller according to claim 1 ; and a motor configured to rotate the impeller. 9. The fan according to claim 8 , further comprising: a casing, wherein the casing includes: a base portion on which the motor is disposed; a sidewall portion that is provided along the outer periphery of the blade and covers the outer periphery of the leading edge of the blade; and a connection portion that connects the sidewall portion and the base portion. 10. An impeller comprising: a hub having a ring shape; and a plurality of blades that are provided on an outer periphery of the hub, wherein a blade of the plurality of blades has a trailing edge formed such that an inner side of a radial width of the blade is curved in a direction opposite to a rotation direction, in a plan view as viewed in a direction of a rotation axis, wherein the blade is formed such that a maximum camber at the outermost side in the radial direction of the blade and a maximum camber at a side closest to the rotation center are larger than a maximum camber at an approximate center of the radial width. 11. The impeller according to claim 10 , wherein the maximum camber at the outermost side in the radial direction and the maximum camber at the side closest to the rotation center are larger than 0.2% of a chord length, and the maximum camber at the approximate center of the radial width is less than 0.2% of the chord length.
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