Turbine de-swirl elements
View Patent ↗A turbocharger including a turbocharger housing, a rotor and a heat shroud. The turbocharger housing includes a turbine housing affixed to a bearing housing. The rotor includes an axial turbine wheel with a hub, and a shaft extending through the bearing housing. The hub defines a back-disk surface that faces the bearing housing, and the bearing-housing defines an outer surface facing the turbine hub. The turbine housing forms a radial scroll, and the heat shroud forms a curved portion turning that radial scroll direction to an axial direction. The heat shroud establishes a back-disk cavity between a bearing-housing turbine-end-wall outer surface, the turbine-wheel back-disk surface, the curved portion of the heat shroud, and a cylindrical outer surface of a turbine-end portion of the shaft. The heat shroud includes flat ribs within the back-disk cavity to impede the circumferential flow of exhaust gas within the back-disk cavity.
1. A turbocharger configured to receive an exhaust gas stream from an engine, and to compress input air into a pressurized air stream, comprising:
a turbocharger housing including a turbine housing affixed to a bearing housing, wherein the turbine housing forms a scroll directing the exhaust gas stream inward toward an axis of rotor rotation;
a rotor rotatably mounted within the turbocharger housing to rotate around the axis of rotor rotation, the rotor including an axial turbine wheel, a compressor wheel, and a shaft extending along the axis of rotor rotation and connecting the turbine wheel to the compressor wheel through the bearing housing, wherein the turbine wheel is configured with a hub and a plurality of axial turbine blades, the hub defining a turbine-wheel back-disk surface facing the bearing housing, and wherein the bearing-housing defines a turbine-end-wall outer surface facing the turbine hub; and
a heat shroud forming a curved portion that turns the scroll direction of the exhaust gas stream to an axial direction toward the plurality of axial turbine blades, the heat shroud establishing a turbine-wheel back-disk cavity between a bearing-housing turbine-end-wall outer surface, the turbine-wheel back-disk surface, the curved portion of the heat shroud, and a cylindrical outer surface of a turbine-end portion of the shaft; and
one or more de-swirl elements extending through the turbine-wheel back-disk cavity, the de-swirl elements being sized, shaped and located within the turbine-wheel back-disk cavity to impede the circumferential flow of exhaust gas within the turbine-wheel back-disk cavity.
2. The turbocharger of claim 1 , wherein the de-swirl elements are structurally supported by the heat shroud.
3. The turbocharger of claim 2 , wherein the de-swirl elements are integral with the heat shroud.
4. The turbocharger of claim 1 , wherein the de-swirl elements are structurally supported by a bearing-housing turbine-end wall.
5. The turbocharger of claim 4 , wherein the de-swirl elements are integral with the bearing-housing turbine-end wall.
6. The turbocharger of claim 1 , wherein the de-swirl elements are a plurality of flat ribs that extend radially and axially across the turbine-wheel back-disk cavity.
7. The turbocharger of claim 6 , wherein the ribs extend, within a safe operating margin, to the turbine-wheel back-disk and the cylindrical outer surface of the turbine-end portion of the shaft.
8. The turbocharger of claim 1 , wherein the scroll is a radial flow scroll.