Turbine housing and associated exhaust-gas turbocharger
A turbine housing of an exhaust-gas turbocharger may include at least two spiral-shaped exhaust-gas channels separated from one another via a partition. The at least two channels may be delimited radially to the outside by the turbine housing and radially to the inside by at least two spiral tongues. A first spiral tongue may be associated with one of the channels and a second spiral tongue may be associated with the other of the channels. The at least two spiral tongues may extend in opposite directions away from the partition in a direction towards the turbine housing. According to an example, the at least two spiral tongues may be configured such that, under an increasing thermomechanical loading, the first spiral tongue fails before the second spiral tongue.
1. A turbine housing of an exhaust-gas turbocharger, comprising:
at least two spiral-shaped exhaust-gas channels separated from one another via a partition, the at least two spiral-shaped exhaust-gas channels being delimited radially to the outside by an inner surface of the turbine housing and radially to the inside by at least two spiral tongues, wherein the at least two spiral tongues are respectively associated with one of the at least two spiral-shaped exhaust-gas channels and extend in opposite directions away from the partition,
wherein the at least two spiral tongues include a first spiral tongue and a second spiral tongue, wherein the first spiral tongue extends between the partition and an exhaust pipe-side region of the turbine housing, and the second spiral tongue extends between the partition and a bearing housing-side region of the turbine housing, and
wherein the at least two spiral tongues are configured such that, under an increasing thermomechanical loading, the first spiral tongue fails before the second spiral tongue;
wherein the first spiral tongue has a smaller wall thickness and a lower strength than the second spiral tongue; and
wherein one of the first and second spiral tongues include a first concave surface facing toward a respective spiral-shaped exhaust-gas channel.
2. The turbine housing according to claim 1 , wherein the first spiral tongue has a wall thickness of approximately 50% to approximately 90% of a wall thickness of the second spiral tongue, wherein the first spiral tongue has a lower strength than the second spiral tongue.
3. The turbine housing according to claim 1 , wherein at least the turbine housing and the partition are formed in one piece.
4. The turbine housing according to claim 1 , wherein the turbine housing, the partition and the at least two spiral tongues are formed in one piece, and wherein the first spiral tongue has at least one of a smaller wall thickness and a lower strength than the second spiral tongue.
5. The turbine housing according to claim 1 , wherein the turbine housing is a cast part.
6. The turbine housing according to claim 1 , wherein the at least two exhaust-gas channels are arranged axially adjacent to one another.
7. The turbine housing according to claim 1 , wherein one of the first and second spiral tongues includes the first concave surface facing toward its respective spiral-shaped exhaust-gas channel, and the other of the first and second spiral tongues includes a second concave surface facing toward its respective spiral-shaped exhaust-gas channel.
8. The turbine housing according to claim 7 , wherein one of the first and second spiral tongues includes a third concave surface opposing the first concave surface and facing away from the respective spiral-shaped exhaust-gas channel, and the other of the first and second spiral tongues includes a fourth concave surface opposing the second concave surface and facing away from the respective spiral-shaped exhaust-gas channel.
9. The turbine housing according to claim 1 , wherein the housing is a twin-scroll turbine housing.
10. An exhaust-gas turbocharger for a motor vehicle, comprising: a turbine housing, the turbine housing including:
at least two spiral-shaped exhaust-gas channels separated from one another via a partition, the at least two spiral-shaped exhaust-gas channels being delimited radially to the outside by the turbine housing and radially to the inside by at least two spiral tongues, wherein the at least two spiral tongues include a first spiral tongue associated with one of the at least two spiral-shaped exhaust-gas channels and a second spiral tongue associated with the other of the at least two spiral-shaped exhaust-gas channels, and wherein the at least two spiral tongues extend in opposite directions from the partition in a direction towards the turbine housing;
wherein the first spiral tongue extends between the partition and an exhaust pipe-side region of the turbine housing, and the second spiral tongue extends between the partition and a bearing housing-side region of the turbine housing; and
wherein the at least two spiral tongues are configured such that, under an increasing thermomechanical loading, the first spiral tongue fails before the second spiral tongue;
wherein the first spiral tongue has a smaller wall thickness and a lower strength than the second spiral tongue; and
wherein at least one of the first and second spiral tongues include a first concave surface facing toward a respective spiral-shaped exhaust-gas channel.
11. The exhaust-gas turbocharger according to claim 10 , wherein the first spiral tongue has a wall thickness of approximately 50% to approximately 90% of a wall thickness of the second spiral tongue.
12. The exhaust-gas turbocharger according to claim 11 , wherein the turbine housing, the partition and the at least two spiral tongues are configured in one piece.
13. The exhaust-gas turbocharger according to claim 10 , wherein at least the turbine housing and the partition are configured in one piece.
14. The exhaust-gas turbocharger according to claim 10 , wherein the turbine housing, the partition and the at least two spiral tongues are configured in one piece.
15. The exhaust-gas turbocharger according to claim 10 , wherein the turbine housing is a cast part.
16. The exhaust-gas turbocharger according to claim 15 , wherein the cast part is a cast steel component.
17. The exhaust-gas turbocharger according to claim 10 , wherein the at least two exhaust-gas channels are arranged axially adjacent to one another, wherein the turbine housing and the partition are configured in one piece.
18. The exhaust-gas turbocharger according to claim 10 , wherein one of the first and second spiral tongues includes the first concave surface facing toward its respective spiral-shaped exhaust-gas channel, and the other of the first and second spiral tongues includes a second concave surface facing toward its respective spiral-shaped exhaust-gas channel.
19. The exhaust-gas turbocharger according to claim 18 , wherein one of the first and second spiral tongues includes a third concave surface opposing the first concave surface and facing away from the respective spiral-shaped exhaust-gas channel, and the other of the first and second spiral tongues includes a fourth concave surface opposing the second concave surface and facing away from the respective spiral-shaped exhaust-gas channel.
20. The exhaust-gas turbocharger according to claim 10 , wherein the two spiral-shaped exhaust-gas channels are in a twin-scroll turbine arrangement.