Method and systems for reducing heat loss to a turbocharger during cold engine starting

Patent metadata

Field	Value
Publication number	US-11499471-B2
Application number	US-202117156886-A
Country	US
Kind code	B2
Filing date	Jan 25, 2021
Priority date	Jan 25, 2021
Publication date	Nov 15, 2022
Grant date	Nov 15, 2022

Abstract

Systems and methods for reducing heat loss to a turbocharger during cold engine starting are described. In one example, a turbocharger bypass pipe and a turbocharger turbine pipe are oriented at forty five degrees relative to a longitudinal axis of a catalyst so that a turbocharger turbine may be completely bypassed, thereby increasing the amount of energy that may be transferred to the catalyst.

First claim

The invention claimed is:

1. An engine system, comprising:
a catalyst including a plurality of flow chambers;
a turbine pipe outlet arranged at about 45 degrees relative to a centerline of the catalyst;
a turbine bypass passage pipe outlet arranged at about 45 degrees relative to the centerline of the catalyst;
a three-way valve configured to distribute exhaust gas to the turbine bypass passage pipe outlet and the turbine pipe outlet; and
an actuator to adjust a position of the three-way valve.

2. The engine system of claim 1 , further comprising a controller including executable instructions stored in non-transitory memory that cause the controller to substantially fully close an inlet to a turbine pipe via the actuator during an engine cold start.

3. The engine system of claim 1 , where the turbine pipe outlet and the turbine bypass passage pipe outlet are coupled to a housing for the catalyst.

4. The engine system of claim 1 , where the three-way valve is positioned at an inlet of a turbine pipe and at an inlet of a turbine bypass passage pipe.

5. The engine system of claim 4 , where the three-way valve is positioned between the inlet of the turbine pipe and the inlet of the turbine bypass passage pipe.

6. The engine system of claim 1 , where the three-way valve is positioned at the turbine bypass passage pipe outlet and at the turbine pipe outlet.

7. The engine system of claim 6 , where the three-way valve is positioned between the turbine pipe outlet and the turbine bypass passage pipe outlet.

8. A method for operating a turbocharger three-way valve, comprising:
adjusting a position of the turbocharger three-way valve to prevent exhaust gas flow through a turbine during an engine cold start;
flowing exhaust gases to a catalyst via a turbine bypass passage pipe that is arranged at about 45 degrees relative to a centerline of the catalyst during the engine cold start;
adjusting the position of the turbocharger three-way valve to allow exhaust gas flow through the turbine after the engine cold start and to prevent exhaust gas flow through the turbine bypass passage pipe after the engine cold start, wherein the exhaust gases flow from the turbine through a turbine pipe that is arranged about 45 degrees relative to a centerline of the catalyst.

9. The method of claim 8 , where the turbocharger three-way valve is positioned at an outlet of the turbine bypass passage pipe and at an outlet of a turbine pipe.

10. The method of claim 8 , where the position of the turbocharger three-way valve is adjusted via an actuator and a controller.

11. The method of claim 8 , further comprising adjusting the position of the turbocharger three-way valve to permit exhaust gas flow through the turbine and the turbine bypass passage pipe.

12. The method of claim 11 , where the turbocharger three-way valve is positioned at an inlet of the turbine bypass passage pipe and at an inlet of a turbine pipe.

13. The method of claim 11 , where the centerline of the catalyst runs parallel with a longitudinal axis of cells included in the catalyst.

Assignees

• Ford Global Tech Llc

Inventors

• Zhang Xiaogang
• Moilanen Peter
• Host Ray
• Wooldridge Steven
• Ruona William Charles
• Yi Jianwen

Classifications

• F02B37/02 Primary

  Gas passages between engine outlet and pump drive, e.g. reservoirs · CPC title

• F01N2240/36

  an exhaust flap · CPC title

• F02B37/183 Primary

  Arrangements of bypass valves or actuators therefor · CPC title

• F01N2340/06

  Arrangement of the exhaust apparatus relative to the turbine of a turbocharger · CPC title

• F02B37/186 Primary

  Arrangements of actuators or linkage for bypass valves · CPC title