Two-stage turbocharger system with integrated exhaust manifold and bypass assembly
View Patent ↗A two-stage turbocharger system includes an exhaust manifold formed separately from the high-pressure and low-pressure turbine housings. The exhaust manifold defines a bypass passage, and a bypass valve is disposed in the bypass passage for opening and closing the passage. The exhaust manifold also defines an inter-turbine passage. The turbine housings of the high-pressure and low-pressure turbochargers are releasably connected to the exhaust manifold such that exhaust gas received into the exhaust manifold bypasses the high-pressure turbine and flows through the bypass passage to the low-pressure turbine when the bypass valve is in the open position, and the exhaust gas flows through the high-pressure turbine and then through the inter-turbine passage to the low-pressure turbine when the bypass valve is in the closed position.
1. A two-stage turbocharger system for an internal combustion engine, comprising:
a high-pressure turbocharger comprising a high-pressure turbine housing defining an exhaust gas inlet and an exhaust gas outlet commonly located at one end of the high-pressure turbine housing;
a low-pressure turbocharger comprising a low-pressure turbine housing defining an exhaust gas inlet at one end of the low-pressure turbine housing;
an exhaust manifold formed separately from the high-pressure and low-pressure turbine housings and structured and arranged to be coupled to an engine to receive exhaust gas from the engine, the exhaust manifold having a first end and an opposite second end, and defining an inter-turbine passage having an inlet and an outlet and further defining a bypass passage having a first end and an opposite second end, and a bypass valve mounted in the exhaust manifold, the bypass valve being movable between a closed position closing the bypass passage and an open position opening the bypass passage, the inlet of the inter-turbine passage and the first end of the bypass passage being commonly located at the first end of the exhaust manifold, the outlet of the inter-turbine passage and the second end of the bypass passage being commonly located at the second end of the exhaust manifold;
the one end of the high-pressure turbine housing being releasably connected by a single joint to the first end of the exhaust manifold such that the exhaust gas outlet of the high-pressure turbine housing is connected to the inlet of the inter-turbine passage and the exhaust gas inlet of the high-pressure turbine housing is connected to the first end of the bypass passage; and
the one end of the low-pressure turbine housing being releasably connected by a single joint to the second end of the exhaust manifold such that the exhaust gas inlet of the low-pressure turbine housing is connected to the outlet of the inter-turbine passage and to the second end of the bypass passage.
2. The two-stage turbocharger system of claim 1 , wherein the first end of the exhaust manifold defines a first flange and the second end of the exhaust manifold defines a second flange, and each of the high- and low-pressure turbine housings defines a flange at the one end thereof, and wherein a first flange joint is formed between the flange of the high-pressure turbine housing and the first flange of the exhaust manifold, and a second flange joint is formed between the flange of the low-pressure turbine housing and the second flange of the exhaust manifold.
3. The two-stage turbocharger system of claim 1 , wherein the bypass valve comprises a swing valve comprising a valve member held by a swing arm that pivots about an axis fixed in the exhaust manifold, and a valve seat disposed in the exhaust manifold for engagement by the valve member when the bypass valve is in the closed position.
4. The two-stage turbocharger of claim 3 , wherein the valve seat comprises an insert formed separately from the exhaust manifold and mounted in the exhaust manifold.
5. The two-stage turbocharger of claim 4 , wherein the valve seat comprises a ring having a cylindrical portion and a flange joined to one end of the cylindrical portion and extending radially outwardly from said one end, the exhaust manifold comprising a wall surrounding the bypass passage, the wall defining an annular recess in which the cylindrical portion of the valve seat is received, the wall further defining a groove surrounding the recess, a resiliently compressible sealing ring being disposed in the groove and engaging the flange of the valve seat, the flange compressing the sealing ring to form a sealed connection between the valve seat and the exhaust manifold.
6. An exhaust manifold for releasably coupling with high-pressure and low-pressure turbine housings of a two-stage turbocharger system, the exhaust manifold comprising:
a manifold member structured and arranged to be coupled to an engine to receive exhaust gas from the engine, the manifold member having a first end and an opposite second end, and defining an inter-turbine passage having an inlet and an outlet and further defining a bypass passage having a first end and an opposite second end, and a bypass valve mounted in the manifold member, the bypass valve being movable between a closed position closing the bypass passage and an open position opening the bypass passage, the inlet of the inter-turbine passage and the first end of the bypass passage being commonly located at the first end of the manifold member, the outlet of the inter-turbine passage and the second end of the bypass passage being commonly located at the second end of the manifold member.
7. The exhaust manifold of claim 6 , further comprising a first flange located at the first end of the manifold member proximate the inlet of the inter-turbine passage and the first end of the bypass passage, and a second flange located at the second end of the manifold member proximate the outlet of the inter-turbine passage and the second end of the bypass passage.
8. The exhaust manifold of claim 6 , wherein the bypass valve comprises a swing valve comprising a valve member held by a swing arm that pivots about an axis fixed in the exhaust manifold, and a valve seat disposed in the manifold member for engagement by the valve member when the bypass valve is in the closed position.
9. The exhaust manifold of claim 8 , wherein the valve seat comprises an insert formed separately from the manifold member and mounted in the manifold member.
10. The exhaust manifold of claim 9 , wherein the valve seat comprises a ring having a cylindrical portion and a flange joined to one end of the cylindrical portion and extending radially outwardly from said one end, the manifold member comprising a wall surrounding the bypass passage, the wall defining an annular recess in which the cylindrical portion of the valve seat is received, the wall further defining a groove surrounding the recess, a resiliently compressible sealing ring being disposed in the groove and engaging the flange of the valve seat, the flange compressing the sealing ring to form a sealed connection between the valve seat and the manifold member.
11. A two-stage turbocharger system for an internal combustion engine, comprising:
a high-pressure turbocharger comprising a high-pressure turbine housing defining an exhaust gas inlet and an exhaust gas outlet;
a low-pressure turbocharger comprising a low-pressure turbine housing defining an exhaust gas inlet;
an exhaust manifold formed separately from the high-pressure and low-pressure turbine housings and structured and arranged to be coupled to an engine to receive exhaust gas from the engine, the exhaust manifold having a first end and an opposite second end, the exhaust manifold defining an inter-turbine passage having an inlet and an outlet and further defining a bypass passage having a first end and an opposite second end, and a bypass valve mounted in the exhaust manifold, the bypass valve being movable between a closed position closing the bypass passage and an open position opening the bypass passage, the inlet of the inter-turbine passage and the first end of the bypass passage being commonly located at the first end of the exhaust manifold, the outlet of the inter-turbine passage and the second end of the bypass passage being commonly located at the second end of the exhaust manifold; and
the exhaust gas inlet of the high-pressure turbine housing being connected to the first end of the bypass passage, the exhaust gas outlet of the high-pressure turbine being connected to the inlet of the inter-turbine passage, and the exhaust gas inlet of the low-pressure turbine housing being connected to the outlet of the inter-turbine passage and to the second end of the bypass passage.