Asymmetric split-inlet turbine housing
View Patent ↗A turbine housing for a turbocharger for use in a reciprocating internal combustion engine includes a housing having a housing axis and configured to house a rotatable shaft having a turbine wheel disposed thereon. The housing includes a volute having a volute chamber disposed around the housing axis for receiving the turbine wheel. The volute has a first volute inlet providing a first flow path in fluid communication with the volute chamber and second volute inlet providing a second flow path in fluid communication with the volute chamber. The first volute inlet is circumferentially spaced about the housing axis from the second volute inlet by a phase angle α. The first volute inlet is also radially spaced about the housing axis from the second volute inlet, and may also be axially spaced from the second volute inlet along the housing axis.
1. A turbine housing for a rotatable turbine wheel of a turbocharger, comprising:
a housing having a housing axis and configured to house a rotatable shaft having a turbine wheel disposed thereon;
a volute having a volute chamber disposed around the housing axis for receiving the turbine wheel;
a first volute inlet providing a first flow path and fluid communication with the volute chamber; and
a second volute inlet providing a second flow path and fluid communication with the volute chamber, the first volute inlet circumferentially spaced about the housing axis from the second volute inlet.
2. The turbine housing of claim 1 , wherein the first volute inlet is axially spaced along the housing axis from the second volute inlet.
3. The turbine housing of claim 1 , wherein the circumferential spacing comprises a phase angle a of about 40° to 110°.
4. The turbine housing of claim 1 , wherein the housing comprises a single volute having a single volute passage that curves inwardly toward and is in fluid communication with the turbine volute chamber, the single volute passage comprising the first flow path and second flow path.
5. The turbine housing of claim 1 , wherein the housing comprises a first volute and a second volute having a shared volute passage that curves inwardly toward and is in fluid communication with the turbine volute chamber, the volute passage comprising the first flow path associated with the first volute and the second flow path associated with the second volute.
6. The turbine housing of claim 1 , wherein the housing comprises a first volute having a first volute passage that curves inwardly toward and is in fluid communication with the turbine volute chamber, the first volute passage comprising the first flow path, and a second volute having a second volute passage that curves inwardly toward and is in fluid communication with a turbine volute chamber, the second volute passage comprising the second flow path.
7. The turbine housing of claim 6 , wherein the first volute passage and second volute passage are separated by a septum extending therebetween.
8. The turbine housing of claim 6 , wherein the first volute passage has a first cross-sectional area and the second volute passage has a second cross-sectional area, and wherein each of the first cross-sectional area and second cross-sectional area each generally decrease in a direction from the first volute inlet and the second volute inlet, respectively toward the turbine volute chamber.
9. A turbocharger, comprising:
a turbocharger housing;
a shaft that is rotatably disposed within the turbocharger housing, the shaft having a first end and a second end;
a compressor disposed on the first end of the shaft; and
a turbine wheel disposed on the second end of the shaft, the turbocharger housing comprising a volute having a volute chamber disposed around a longitudinal axis of the shaft and the turbine wheel, the volute having a first volute inlet providing a first flow path and fluid communication with the volute chamber and a second volute inlet providing a second flow path and fluid communication with the volute chamber, the first volute inlet circumferentially spaced about the axis of the shaft from the second volute inlet.
10. An engine assembly, comprising:
an engine comprising a first cylinder bank having a first cylinder head and a second cylinder bank having a second cylinder head, the first cylinder bank and the second cylinder bank having an opposed or V-type configuration about a common crank shaft, the first cylinder head having a first inboard exhaust outlet and the second cylinder head having a second inboard exhaust outlet; and
a turbocharger assembly in fluid communication with the first and second cylinder heads, the turbocharger assembly having a turbine housing, comprising:
a housing having a housing axis and configured to house a rotatable shaft having a turbine wheel disposed therein;
a volute having a volute chamber disposed around the housing axis for receiving the turbine wheel;
a first volute inlet providing a first flow path and fluid communication with the volute chamber; and
a second volute inlet providing a second flow path and fluid communication with the volute chamber, the first volute inlet circumferentially spaced about the housing axis from the second volute inlet, the first volute inlet fluidly coupled to the first exhaust outlet and the second volute inlet fluidly coupled to the second exhaust outlet.
11. The engine assembly of claim 10 , wherein the housing comprises a single volute having a single volute passage that curves inwardly toward and is in fluid communication with the turbine volute chamber, the single volute passage comprising the first flow path and second flow path.
12. The engine assembly of claim 10 , wherein housing comprises a first volute and a second volute having a shared volute passage that curves inwardly toward and is in fluid communication with the turbine volute chamber, the volute passage comprising the first flow path associated with the first volute and the second flow path associated with the second volute.
13. The engine assembly of claim 10 , wherein the housing comprises a first volute having a first volute passage that curves inwardly toward and is in fluid communication with the turbine volute chamber, the first volute passage comprising the first flow path, and a second volute having a second volute passage that curves inwardly toward and is in fluid communication with a turbine volute chamber, the second volute passage comprising the second flow path.
14. The engine assembly of claim 10 , wherein the phase angle αis about 40° to 110°.
15. The engine assembly of claim 10 , wherein the first cylinder head and the second cylinder head are interchangeable.
16. The engine assembly of claim 10 , wherein the turbocharger assembly is located between the first cylinder head and the second cylinder head.
17. The engine assembly of claim 16 , wherein the housing comprises a first exhaust conduit that is fluidly coupled to the first exhaust outlet and in fluid communication with the first volute inlet, and a second exhaust conduit that is fluidly coupled to the second exhaust outlet and in fluid communication with the second volute inlet.
18. The engine assembly of claim 17 , wherein the first exhaust conduit has a first flexible section and the second exhaust conduit has a second flexible section.
19. The engine assembly of claim 10 , wherein the first exhaust outlet and the second exhaust outlet are axially offset with respect to one another.
20. The engine assembly of claim 10 , wherein the first cylinder head includes a first integrally formed internal exhaust manifold in fluid communication with the first exhaust outlet and the second cylinder head includes a second integrally formed internal exhaust manifold in fluid communication with the second exhaust outlet.