Turbocharger with a radial-axial turbine wheel
A turbocharger has a shaft with a rotational axis, a radial/axial turbine wheel which is arranged in a turbine housing and which is connected to the shaft in a non-rotatable manner, and a bearing housing which adjoins the turbine housing and which contains a lateral wall facing the turbine housing. A sub-region of the lateral wall of the bearing housing forms a sub-region of the rear wall of the turbine housing. The sub-region of the bearing housing has two sub-sections, one of which runs diagonally to the rotational axis in an inflow direction of an exhaust gas flow conducted into the turbine housing and the second of which runs in a radial direction relative to the rotational axis of the shaft and parallel to the rear wall of the turbine wheel. The two sub-sections are connected to each other via an exhaust gas flow separation edge of the bearing housing.
1. An exhaust-gas turbocharger, comprising:
a shaft having an axis of rotation;
a turbine housing;
a radial-axial turbine wheel disposed in said turbine housing and connected rotationally conjointly to said shaft, said radial-axial turbine wheel having a rear wall; and
a bearing housing adjacent said turbine housing and having a side wall facing toward said turbine housing,
said side wall of said bearing housing having a first sub-portion, a second sub-portion, and a flank;
said first sub-portion running obliquely with respect to the axis of rotation of said shaft, said first sub-portion for guiding exhaust gasses toward said radial-axial turbine wheel;
said second sub-portion running in a radial direction with respect to the axis of rotation of said shaft and parallel to said rear wall of said radial-axial turbine wheel;
said first and second sub-portions being connected to one another via an exhaust-gas flow separation edge of said bearing housing;
said exhaust-gas flow separation edge including a corner connected to said second sub-portion via said flank, said corner having a corner angle enclosed by said first sub-portion and said flank; and
said flank extending away from said first sub-portion in a direction towards said shaft;
wherein a curved transition region is formed between said second sub-portion and said flank; and
wherein said rear wall of said turbine wheel has, in an upper end region thereof, a corner formed at a first spacing distance from said corner of said exhaust-gas flow separation edge in a radially inward direction.
2. The exhaust-gas turbocharger according to claim 1 , wherein said first sub-portion ends at said corner.
3. The exhaust-gas turbocharger according to claim 2 , wherein said first sub-portion is rectilinear in section.
4. The exhaust-gas turbocharger according to claim 2 , wherein said first sub-portion is curved in section.
5. The exhaust-gas turbocharger according to claim 1 , wherein a top side of said turbine wheel has a second spacing to said corner of said exhaust-gas flow separation edge inwardly in an inflow direction of the exhaust-gas flow.
6. The exhaust-gas turbocharger according to claim 5 , wherein said flank runs parallel to the top side of said turbine wheel.
7. The exhaust-gas turbocharger according to claim 5 , wherein a ratio of said second spacing to a diameter of said rear wall of said turbine wheel lies in the range between 0.005 and 0.025.
8. The exhaust-gas turbocharger according to claim 1 , wherein said rear wall of said turbine wheel is disposed at a third spacing distance from said second sub-portion.
9. The exhaust-gas turbocharger according to claim 8 , wherein a ratio of said third spacing to a diameter of said rear wall of said turbine wheel lies in a range between 0.005 and 0.025.
10. The exhaust-gas turbocharger according to claim 1 , wherein said bearing housing has a water core adjacent said exhaust-gas flow separation edge.
11. The exhaust-gas turbocharger according to claim 1 , wherein said side wall of said bearing housing which faces toward said turbine housing carries a protective layer in a region of said first sub-portion, of said second sub-portion and of said flank.
12. The exhaust-gas turbocharger according to claim 11 , wherein said protective layer is composed of a material that is resistant to elevated temperatures, to oxidation and to corrosion.