Rotating electrical machine apparatus
US-10486784-B2 · Nov 26, 2019 · US
US9951745B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9951745-B2 |
| Application number | US-201414220390-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 20, 2014 |
| Priority date | Apr 24, 2013 |
| Publication date | Apr 24, 2018 |
| Grant date | Apr 24, 2018 |
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An axial flow water turbine according to an embodiment includes a discharge ring and a runner vane. When seen in the runner meridional cross section, a straight line that passes a border between a cylindrical surface and a spherical surface of the discharge ring and that is perpendicular to a water turbine rotation axis is denoted as A. A crossing point between the straight line A and the water turbine rotation axis is denoted as B. A straight line inclined by an angle θ of 10 degrees or less is denoted as C. A cross point between the straight line C and the external peripheral end surface of the runner vane is denoted as D. In this case, the external peripheral end of the forward edge of the runner vane is located on the crossing point D.
Opening claim text (preview).
The invention claimed is: 1. An axial flow water turbine, comprising: a discharge ring in which an upstream side inner peripheral surface is formed as a cylindrical surface and a downstream side inner peripheral surface is formed as a spherical surface, and a runner vane that is provided inside of the discharge ring and that is formed such that an external peripheral end surface is formed as a spherical surface, wherein when seen in a runner meridional cross section in a design point, a first straight line that passes a border between the cylindrical surface and the spherical surface of the discharge ring and that is perpendicular to a water turbine rotation axis is denoted as A, a first crossing point between the first straight line A and the water turbine rotation axis is denoted as B, a second straight line inclined by an angle θ of more than 0 degrees and of 10 degrees or less, that is obtained by rotating the first straight line A to the upstream side about the first crossing point B, is denoted as C, a second crossing point between the second straight line C and the external peripheral end surface of the runner vane is denoted as D, and in this case, the external peripheral end of a forward edge of the runner vane is located on the second crossing point D, and an inner peripheral end of the forward edge of the runner vane is located at the upstream side with respect to the second straight line C, wherein when seen in a direction of a vane rotation axis of the runner vane, a camber line in an airfoil shape of the external peripheral end surface of the runner vane is arranged at a position deviated to a pressure surface side of the runner vane with respect to a vane rotation axis, when seen in the direction of the vane rotation axis of the runner vane, a point where a straight line extended from the vane rotation axis to the pressure surface side in a direction perpendicular to a direction of the water turbine rotation axis crosses a camber line in an airfoil shape of the external peripheral end surface of the runner vane is denoted as P, and a distance from the vane rotation axis to the point P is denoted as T, and a distance to the point P from the forward edge in the airfoil shape measured along the direction of the water turbine rotation axis is denoted as L 1 , and the runner vane is arranged to satisfy a relationship T/L 1 <1.5. 2. The axial flow water turbine according to claim 1 , wherein when seen in a runner meridional cross section, the forward edge of the runner vane is curved so as to be concave toward a downstream side. 3. The axial flow water turbine according to claim 2 , wherein when seen in the runner meridional cross section, a length of a line segment connecting an inner peripheral end of the forward edge of the runner vane and an external peripheral end is denoted as L, a maximum distance from the line segment to the forward edge of the runner vane measured in a direction perpendicular to the line segment is denoted as ΔY, and in this case, the forward edge of the runner vane is curved so as to satisfy a relationship ΔY/L <0.2.
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