Turbine wheel, a turbine and use thereof
A turbine wheel for low-pressure ratio applications is disclosed. The ratio of the outlet area of the wheel (A 2 ) to the inlet area of the wheel (A 1 ) is less than approximately 0.4. In an embodiment, the wheel is a radial or mixed-flow wheel.
1. An exhaust system for a vehicle comprising:
a turbocharger; and
a turbocompound unit comprising a turbine downstream of the turbocharger, wherein the turbine is configured to operate with an inlet to outlet pressure ratio between 1.02 and 1.2 and comprises:
a turbine wheel for low pressure ratio applications, wherein the ratio of the outlet area of the wheel (A 2 ), the outlet area defined as the area described by rotating a first edge of a blade of the turbine wheel about the axis, the first edge being an edge arranged to be adjacent an outlet, to the inlet area of the wheel (A 1 ), the inlet area defined as the area described by rotating a second edge of the blade of the turbine wheel about the axis, the second edge being an edge arranged to be adjacent an inlet, is between 0.3 and 0.4, wherein the ratio of the radius of the root of the blades adjacent the outlet to the radius of the tip of the blades adjacent the outlet is between 0.2 and 0.7.
2. The exhaust system according to claim 1 , wherein a ratio of the radius of the tip of the blades adjacent the outlet to the radius of the tip of the blades adjacent the inlet is less than 1.0.
3. The exhaust system according to claim 1 , wherein a ratio of the radius of the tip of the blades adjacent the outlet to the radius of the tip of the blades adjacent the inlet is between 0.6 and 0.9.
4. The exhaust system according to claim 1 , wherein the exit relative flow angle is less than −55 degrees.
5. The exhaust system according to claim 1 , wherein the exit relative flow angle is between −41 degrees and −55 degrees.
6. The exhaust system according to claim 1 and further being a radial-flow turbine wheel.
7. The exhaust system according to claim 1 and further being a mixed-flow turbine wheel.
8. The exhaust system according to claim 1 and further comprising a shroud at least partly covering the turbine wheel to define an inlet and an outlet of the turbine.
9. The exhaust system according to claim 1 , wherein a ratio of a radius (R 3 ) of a hub of the turbine wheel adjacent the outlet to a radius (R 4 ) of the outlet defined by the shroud is less than 0.7.
10. The exhaust system according to claim 1 , wherein a ratio of a radius (R 4 ) of the outlet defined by the shroud to a radius (R 1 ) of the inlet defined by the shroud is less than 1.0.
11. A turbine according to claim 8 , wherein a ratio of a radius (R 3 ) of a hub of the turbine wheel adjacent the outlet to a radius (R 4 ) of the outlet defined by the shroud is between 0.2 and 0.7.
12. A turbine according to claim 8 wherein a ratio of a radius (R 4 ) of the outlet defined by the shroud to a radius (R 1 ) of the inlet defined by the shroud is between 0.6 and 0.9.