External rotor aircraft motor having force isolated cantilevered rotor
US-12166399-B2 · Dec 10, 2024 · US
US10731467B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10731467-B2 |
| Application number | US-201415329959-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 30, 2014 |
| Priority date | Sep 30, 2014 |
| Publication date | Aug 4, 2020 |
| Grant date | Aug 4, 2020 |
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A turbine includes a housing including an inlet, an outlet, and a shroud section having a shroud surface extending between the inlet and the outlet; and a turbine impeller housed in the housing and including a hub and a plurality of blades disposed on an outer peripheral surface of the hub, each of the blades having a side edge extending along the shroud surface. The side edge of each of the blades has a side-edge upstream portion disposed on a side of the inlet, and a side-edge downstream portion disposed on a side of the outlet. The shroud surface has a shroud upstream portion disposed on the side of the inlet and extending along the side-edge upstream portion, and a shroud downstream portion disposed on the side of the outlet and extending along the side-edge downstream portion. The shroud upstream portion has a meridional cross-sectional shape whose inclination angle (θ 1 ) with respect to an axis (L) of the hub at the side of the inlet is smaller than in a case where the shroud upstream portion has a meridional cross-sectional shape of an arc shape and the shroud downstream portion has a meridional cross-sectional shape of a linear shape along a direction of the axis of the hub.
Opening claim text (preview).
The invention claimed is: 1. A turbine, comprising: a housing including an inlet, an outlet, and a shroud section having a shroud surface extending between the inlet and the outlet; and a turbine impeller housed in the housing and including a hub and a plurality of blades disposed on an outer peripheral surface of the hub, each of the blades having a side edge extending along the shroud surface, wherein the side edge of each of the blades has a side-edge upstream portion disposed on a side of the inlet, and a side-edge downstream portion disposed on a side of the outlet, wherein the shroud surface has a shroud upstream portion disposed on the side of the inlet and extending along the side-edge upstream portions of the blades, and a shroud downstream portion disposed on the side of the outlet and extending along the side-edge downstream portion, and wherein the shroud upstream portion has a meridional cross-sectional shape having a curvature radius R defined by following expression 1: R ≧ ( R 1 - R 2 t ) 2 + Ls 2 2 ( R 1 - R 2 t ) where R 1 is a distance in a radial direction from an axis of the hub to the inlet, R 2 t is a distance in the radial direction from the axis of the hub to the outlet, and Ls is a length of the shroud surface in a direction of the axis of the hub, and wherein the shroud downstream portion has a meridional cross-sectional of an arc shape having a curvature radius R defined by following expression 2: R = ( R 1 - R 2 t ) 2 + Ls 2 2 ( R 1 - R 2 t ) . 2. The turbine according to claim 1 , wherein a ratio Ls/D 1 of the length Ls to an inner diameter D 1 is greater than 0.16, provided that D 1 is an inner diameter of the shroud at the inlet. 3. The turbine according to claim 1 , wherein a ratio of a distance R 2 t to a distance R 1 is not more than 0.95, provided that R 1 is a distance in a radial direction from the axis of the hub to the inlet, and R 2 t is a distance in the radial direction from the axis of the hub to the outlet.
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