Turbine compressor wheel with axially extended blades
A compressor wheel for a turbocharger has an improved geometry that provides improved performance as compared with a comparably sized conventional compressor wheel by having the radially inward portion of the primary blades sweep upwardly into the upper region of the hub portion. The through bore and integral nut of conventional compressor wheels is eliminated and replaced with a blade extension that has an angled upper edge which extends downwardly and radially outwardly from the hub portion, effectively increasing the size of the blade, the amount of air movement and the amount of power generated, without increasing the overall cost, size or mass of the compressor wheel.
1. A compressor wheel for a turbocharger, comprising:
a metal body having a generally circular shaped base portion, a hub portion extending perpendicularly from the base portion, and a plurality of primary blades, each of the plurality of primary blades extending upwardly from the base portion and radially outwardly from the hub portion, and each of the plurality of primary blades having an inducer portion that has an upper edge which includes a first section that extends downwardly and radially outwardly at an angle from the hub portion to define a triangular shaped portion of the blade, a substantially horizontal section that extends radially outwardly from the first section to a radially distal end of the upper edge, and a convex edge that extends downwardly from the radially distal end of the upper edge to an exducer portion of the primary blade, the exducer portion of the primary blade having an upper concave edge that extends radially outwardly and downwardly from the inducer portion and a radially distal vertical edge that extends downwardly from the upper edge of the exducer portion to the base portion.
2. The compressor wheel of claim 1 , in which the angle between an axial direction of the hub portion and the angled section of the upper edge of the inducer portion of each of the plurality of primary blades is from 10 to 40 degrees.
3. The compressor wheel of claim 1 , in which the angle between an axial direction of the hub portion and the angled upper edge of the exducer portion of each of the plurality of primary blades is from 45 to 75 degrees.
4. The compressor wheel of claim 1 , further comprising a plurality of secondary blades, each secondary blade being disposed between radially adjacent primary blades, and each secondary blade having a height and surface area that is less than the height and surface area of a primary blade.
5. The compressor wheel of claim 1 , in which the compressor wheel has a height measured from a bottom of the base portion to a top of the hub portion and a diameter measured across the width of the base portion and includes an internally threaded bore extending axially along and terminating within the hub portion such that the internally threaded bore does not extend through a top of the hub portion.
6. A turbocharger system for a vehicle, comprising:
a turbine including a turbine wheel configured to be driven by exhaust gases from an internal combustion engine;
a shaft axially coupled at a first end to the turbine wheel;
a compressor including a compressor wheel axially coupled at a second end of the shaft, the compressor wheel including a metal body having a generally circular shaped base portion, a hub portion extending perpendicularly from the base portion, and a plurality of primary blades, each of the plurality of primary blades extending upwardly from the base portion and radially outwardly from the hub portion, and each of the plurality of primary blades having an inducer portion that has an upper edge which includes a first section that extends downwardly and radially outwardly at an angle from the hub portion to define a triangular shaped portion of the blade, and a substantially horizontal section that extends radially outwardly from the first section to a radially distal end of the upper edge, and a convex edge that extends downwardly from the radially distal end of the upper edge to an exducer portion of the primary blade, the exducer portion of the primary blade having an upper concave edge that extends radially outwardly and downwardly at an angle from the inducer portion and a radially distal vertical edge that extends downwardly from the upper edge of the exducer portion to the base portion.
7. The turbocharger system of claim 6 , in which the angle between an axial direction of the hub portion and the angled section of the upper edge of the inducer portion of each of the plurality of primary blades is from 10 to 40 degrees.
8. The turbocharger system of claim 6 , in which the angle between an axial direction of the hub portion and the angled section of the upper edge of the exducer portion of each of the plurality of primary blades is from 45 to 75 degrees.
9. The turbocharger system of claim 6 , further comprising a plurality of secondary blades, each secondary blade being disposed between radially adjacent primary blades, and each secondary blade having a height and surface area that is less than the height and surface area of a primary blade.
10. The turbocharger system of claim 6 , in which the compressor wheel has a height measured from a bottom of the base portion to a top of the hub portion and a diameter measured across the width of the base portion and includes an internally threaded bore extending axially along and terminating within the hub portion such that the internally threaded bore does not extend through a top of the hub portion.
11. A motor vehicle comprising:
a vehicle frame;
an internal combustion engine supported on the vehicle frame;
a turbine wheel configured to be driven by exhaust gases from the internal combustion engine;
a shaft axially coupled at a first end to the turbine wheel; and
a compressor including a compressor wheel axially coupled at a second end of the shaft, the compressor wheel including a metal body having a generally circular shaped base portion, a hub portion extending perpendicularly from the base portion, and a plurality of primary blades, each of the plurality of primary blades extending upwardly from the base portion and radially outwardly from the hub portion, and each of the plurality of primary blades having an inducer portion that has an upper edge which includes a first section that extends downwardly and radially outwardly at an angle from the hub portion to define a triangular shaped portion of the blade, a substantially horizontal section that extends radially outwardly from the first section to a radially distal end of the upper edge, and a convex edge that extends downwardly from the radially distal end of the upper edge to an exducer portion of the primary blade, the exducer portion of the primary blade having an upper concave edge that extends radially outwardly and downwardly from the inducer portion and a radially distal vertical edge that extends downwardly from the upper edge of the exducer portion to the base portion.
12. The motor vehicle of claim 11 , in which the angle between an axial direction of the hub portion and the angled section of the upper edge of the inducer portion of each of the plurality of primary blades is from 10 to 40 degrees.
13. The motor vehicle of claim 11 , in which the angle between an axial direction of the hub portion and the angled section of the upper edge of the exducer portion of each of the plurality of primary blades is from 45 to 75 degrees.
14. The motor vehicle of claim 11 , further comprising a plurality of secondary blades, each secondary blade being disposed between radially adjacent primary blades, and each secondary blade having a height and surface area that is less than the height and surface area of a primary blade.
15. The motor vehicle of claim 11 , in which the compressor wheel has a height measured from a bottom of the base portion to a top of the hub portion and a diameter measured across the width of the base portion and includes an internally threaded bore extending axially along and terminating within the hub portion such that the internally threaded bore does not extend through a top of the hub portion.