Engine having a turbocharger coupler
View Patent ↗A turbo assembly may include a coupling member, a heat shield, and a turbo mechanism. The coupling member may include first and second ends and an annular body extending between the first and second ends. The first end may fix the coupling member to an exhaust manifold of an engine and the annular body may define an exhaust gas channel that receives exhaust gas from the exhaust manifold. The annular body may include a coolant passage that receives a coolant fluid. The heat shield may extend axially within the exhaust gas channel and radially between the annular body and an exhaust gas flow within the exhaust gas channel to limit an amount of heat transferred from the exhaust gas to the annular body. The turbo mechanism may include a housing fixed to the second end of the coupling member and in communication with the exhaust gas channel to receive the exhaust gas therefrom.
1. A turbo assembly comprising:
a coupling member including first and second ends and a first annular body extending between the first and second ends, the first end being adapted to fix the coupling member to an exhaust manifold of an engine and the first annular body defining an exhaust gas channel that receives exhaust gas from the exhaust manifold, the first annular body including a coolant passage therein that receives a coolant fluid;
a heat shield extending axially within the exhaust gas channel to limit an amount of heat transferred from the exhaust gas to the first annular body; and
a turbo mechanism including a housing fixed to a second end of the coupling member and in communication with the exhaust gas channel to receive the exhaust gas therefrom.
2. The turbo assembly of claim 1 , wherein the coolant passage in the first annular body is an annular coolant passage forming a loop in the first annular body.
3. The turbo assembly of claim 1 , wherein the first end of the coupling member includes a first flange that is adapted to fix the coupling member to the exhaust manifold, the heat shield including a first end disposed axially outwardly from the first flange and overlying the first flange to form a gasket between the coupling member and the exhaust manifold.
4. The turbo assembly of claim 3 , wherein a second end of the heat shield is free from axial restraint to allow for thermal expansion of the heat shield.
5. The turbo assembly of claim 3 , wherein a second end of the heat shield includes a radially outwardly extending portion that radially secures the heat shield within the exhaust gas channel.
6. The turbo assembly of claim 1 , wherein the heat shield includes an axially extending second annular body, a portion of the second annular body being radially offset from a radially inner surface of the first annular body.
7. The turbo assembly of claim 6 , wherein the radial offset forms an air gap radially between the heat shield and the coupling member.
8. The turbo assembly of claim 7 , wherein the air gap is axially aligned with the coolant passage.
9. The turbo assembly of claim 1 , wherein the coupling member is integrally formed with the housing of the turbo mechanism.
10. An engine assembly comprising:
an exhaust manifold including an outlet;
a coupling member including first and second ends and a first annular body extending between the first and second ends, the first end fixing the coupling member to the outlet of the exhaust manifold, the first annular body defining an exhaust gas channel that receives exhaust gas from the exhaust manifold, a coolant passage being defined within the first annular body that receives a coolant fluid;
a heat shield extending axially within the exhaust gas channel to limit an amount of heat transferred from the exhaust gas to the first annular body; and
a turbo mechanism including a housing fixed to a second end of the coupling member and in communication with the exhaust gas channel to receive the exhaust gas therefrom.
11. The engine assembly of claim 10 , wherein the coolant passage in the first annular body is an annular coolant passage that forms a loop in the first annular body.
12. The engine assembly of claim 10 , wherein the first end of the coupling member includes a first flange that fixes the coupling member to the exhaust manifold and the heat shield includes a first end disposed axially outwardly from the first flange and overlying the first flange to form a gasket between the coupling member and the exhaust manifold.
13. The engine assembly of claim 12 , wherein a second end of the heat shield is free from axial restraint to allow for thermal expansion of the heat shield.
14. The engine assembly of claim 12 , wherein a second end of the heat shield includes a radially outwardly extending portion that radially secures the heat shield within the exhaust gas channel.
15. The engine assembly of claim 10 , wherein the heat shield includes an axially extending second annular body, a portion of the second annular body being radially offset from a radially inner surface of the first annular body.
16. The engine assembly of claim 15 , wherein the radial offset forms an air gap radially between the heat shield and the coupling member.
17. The engine assembly of claim 16 , wherein the air gap is axially aligned with the coolant passage.
18. The engine assembly of claim 10 , wherein the exhaust manifold is integrally formed with a cylinder head of the engine assembly.
19. The engine assembly of claim 18 , wherein the exhaust manifold and the cylinder head are formed from a single casting.
20. The engine assembly of claim 10 , wherein the coupling member is integrally formed with the housing of the turbo mechanism.