Low-restriction turbine outlet housing
View Patent ↗A low-restriction turbine outlet device ( 200 ) includes a housing ( 202 ) having an internal volume ( 208 ). The internal volume ( 208 ) includes an inlet transition portion ( 230 ) and an outlet transition portion ( 232 ). An inlet port ( 204 ) that is formed in the housing ( 202 ) is in fluid communication with an outlet port ( 206 ) that is also formed in the housing ( 202 ). A mounting flange ( 216 ) is connected to the housing ( 202 ), a first set of stiffening ribs ( 218 ) and a second set of stiffening ribs ( 220 ) each connect the mounting flange ( 216 ) to the housing ( 202 ).
1. A method of negotiating a turn in a low-flow-restriction fashion with a flow of exhaust gas that is exiting a turbine in a highly turbulent condition that has a general swirl structure, comprising the steps of:
sealably routing the flow of exhaust gas from a gas outlet of the turbine into an inlet port of a housing;
expanding and funneling the flow of exhaust gas in an inlet transition portion of an internal volume that is formed in the housing, wherein the inlet transition portion has an elliptical-conoid shape;
passing the flow of exhaust gas out of the inlet transition portion into an outlet transition portion of the internal volume, wherein the outlet transition portion has an oblate-ellipsoid shape;
exiting the flow of exhaust gas from the housing through an outlet port that fluidly communicates with the outlet transition portion, wherein the outlet port is at an angle with respect to the inlet port; and
providing a structural rigidity to the turbine with the housing when the housing is connected to the turbine and to an engine.
2. A low-restriction turbine outlet device, comprising:
a housing having an internal volume, wherein the internal volume includes an inlet transition portion and an outlet transition portion;
an inlet port formed in the housing that is in fluid communication with an outlet port formed in the housing;
a mounting flange connected to the housing;
a first set of stiffening ribs that connect the mounting flange to the housing;
a second set of stiffening ribs that connect the mounting flange to the housing; and
wherein the inlet transition portion has an elliptical-conoid shape, wherein the elliptical-conoid shape defines a vertex and a base, wherein the vertex is truncated by the inlet port, and wherein the base is oriented toward the outlet port.
3. A low-restriction turbine outlet device, comprising:
a housing having an internal volume, wherein the internal volume includes an inlet transition portion and an outlet transition portion;
an inlet port formed in the housing that is in fluid communication with an outlet port formed in the housing;
a mounting flange connected to the housing;
a first set of stiffening ribs that connect the mounting flange to the housing;
a second set of stiffening ribs that connect the mounting flange to the housing; and
wherein the outlet transition portion has an oblate-ellipsoid shape, wherein the oblate-ellipsoid shape has an equatorial radius and a polar radius, wherein the equatorial radius is greater than the polar radius.
4. The low-restriction turbine outlet device of claim 3 , wherein the equatorial radius defines a plane, and wherein the plane is substantially parallel to a perimeter of the outlet port.
5. An internal combustion engine, comprising:
an intake system that is in intermittent fluid communication with at least one combustion cylinder during operation of the engine;
an exhaust system that is in intermittent fluid communication with the combustion cylinder during operation of the engine;
a turbocharger operably connected to the engine, the turbocharger comprising
a compressor having an air inlet and an air outlet, wherein the air outlet is in fluid communication with the intake system; and
a turbine having a gas inlet and a gas outlet, wherein the gas inlet is in fluid communication with the exhaust system;
a low-restriction turbine outlet device connected to the turbine, wherein the low-restriction turbine outlet device comprises
a housing having an inlet port in fluid communication with the gas outlet of the turbine;
an outlet port in fluid communication with the inlet port via an internal volume that is formed into the housing; and
wherein the inlet transition portion has a an elliptical-conoid shape, wherein the elliptical-conoid shape defines a vertex and a base, wherein the vertex is truncated by the inlet port, and wherein the base is oriented toward the outlet port.
6. An internal combustion engine, comprising:
an intake system that is in intermittent fluid communication with at least one combustion cylinder during operation of the engine;
an exhaust system that is in intermittent fluid communication with the combustion cylinder during operation of the engine;
a turbocharger operably connected to the engine, the turbocharger comprising
a compressor having an air inlet and an air outlet, wherein the air outlet is in fluid communication with the intake system; and
a turbine having a gas inlet and a gas outlet, wherein the gas inlet is in fluid communication with the exhaust system;
a low-restriction turbine outlet device connected to the turbine, wherein the low-restriction turbine outlet device comprises
a housing having an inlet port in fluid communication with the gas outlet of the turbine;
an outlet port in fluid communication with the inlet port via an internal volume that is formed into the housing; and wherein the outlet transition portion has an oblate-ellipsoid shape, wherein the oblate-ellipsoid shape has an equatorial radius and a polar radius, wherein the equatorial radius is greater than the polar radius.
7. The internal combustion engine of claim 6 , wherein the equatorial radius defines a plane, and wherein the plane is substantially parallel to a perimeter of the outlet port.