Internal combustion engine system for exhaust gas recovery

Patent metadata

Field	Value
Publication number	US-11022055-B2
Application number	US-201615738640-A
Country	US
Kind code	B2
Filing date	Jun 20, 2016
Priority date	Jun 23, 2015
Publication date	Jun 1, 2021
Grant date	Jun 1, 2021

Abstract

An internal combustion engine system includes an internal combustion engine, a first turbine unit receiving exhaust gases from the internal combustion engine, the turbine unit having a compressor for compressing intake air and feeding the intake air by an air intake line to the internal combustion engine, and an exhaust gas recirculation line connecting the air intake line with an exhaust as line of the internal combustion engine at a position upstream the first turbine unit. A bypass line connects the exhaust gas recirculation line to the exhaust gas line at a position downstream of the turbine unit, the bypass line having an arrangement for controlling the exhaust gas flow from the exhaust gas recirculation line to the exhaust gas line.

First claim

The invention claimed is:

1. An internal combustion engine system,
comprising: an internal combustion engine,
a first turbine unit receiving exhaust gases from the internal combustion engine, the turbine unit having a compressor for compressing intake air and feeding the intake air by means of an air intake line to the internal combustion engine,
an exhaust gas recirculation line connecting the air intake line with an exhaust gas line of the internal combustion engine at a position upstream the first turbine unit, the exhaust gas line having at least one branch, and
a bypass line connecting the exhaust gas recirculation line to the exhaust gas line at a position downstream of the turbine unit,
at least one valve is provided in the exhaust gas recirculation line for each branch of the exhaust gas line for controlling the amount of recirculated exhaust gas, wherein the bypass line is connected to the exhaust gas recirculation line at a position located downstream the at least one valve between the at least one valve and a position where the exhaust gas recirculation line connects to the air intake line,
wherein the bypass line comprises means configured to control the exhaust gas flow from the exhaust gas recirculation line to the exhaust gas line in order to increase temperature of the exhaust gas downstream of the turbine unit and upstream of an aftertreatment system of the engine, the aftertreatment system including a diesel particle filter and a selective catalytic reduction system,
wherein the bypass line is connected to the exhaust gas line at a position located upstream of both of the diesel particle filter and the selective catalytic reduction system of the aftertreatment system.

2. The internal combustion engine system according to claim 1 , wherein the means configured to control the exhaust gas flow from the exhaust gas recirculation line to the exhaust gas line is a bypass valve.

3. The internal combustion engine system according to claim 2 , further comprising a controller configured to control the operation of the bypass valve depending on the internal combustion engine load, internal combustion engine speed, turbine speed, and/or the lambda value of the internal combustion engine.

4. The internal combustion engine system according to claim 1 , wherein the exhaust gas line comprises a first branch allowing exhaust gas to flow from a first set of cylinders to the first turbine unit, and a second branch allowing exhaust gas to flow from a second set of cylinders to the first turbine unit, and wherein each one of the branches is in communication with the at least one valve provided in the exhaust gas recirculation line.

5. The internal combustion engine system according to claim 1 , wherein the first turbine unit is a turbocharger unit.

6. The internal combustion engine system according to claim 1 , further comprising a second turbine unit arranged downstream of the first turbine unit such that the second turbine unit receives exhaust gas flowing out from the first turbine unit, wherein the bypass line is connecting the exhaust gas recirculation line to the exhaust gas line at a position downstream of the second turbine unit.

7. The internal combustion engine system according to claim 6 , wherein the second turbine unit is a turbocharger unit.

8. The internal combustion engine system according to claim 6 , wherein the second turbine unit is a turbocompound unit.

9. The internal combustion engine system according to claim 8 , wherein the bypass line is connecting the exhaust gas recirculation line to an exhaust gas collector of the turbocompound unit.

10. The internal combustion engine system according to claim 9 , wherein the exhaust gas collector is in fluid communication with a buffer gas duct which leads into the exhaust gas collector, whereby the buffer gas duct is arranged to supply exhaust gas from an exhaust collector seal positioned in the vicinity of a turbine wheel of the turbocompound unit for preventing oil from escaping from an associated bearing housing to a diffuser duct of the turbocompound unit.

11. The internal combustion engine system according to claim 9 , wherein the exhaust gas collector forms an annular flow path for the exhaust gases.

12. The internal combustion engine system according to claim 11 , wherein a buffer gas duct extends from a buffer gas inlet arranged at the outer periphery of the exhaust collector.

13. The internal combustion engine system according to claim 12 , wherein the buffer gas inlet is arranged at a circumferential position of 170°-190° measured from the circumferential position of a center of an exhaust outlet of the exhaust gas collector.

14. A vehicle comprising an internal combustion engine system according to claim 1 .

15. A method for an internal combustion engine system, the system comprising an internal combustion engine, and a first turbine unit receiving exhaust gases from the internal combustion engine, the turbine unit having a compressor for compressing intake air and feeding the intake air by means of an air intake line to the internal combustion engine, comprising: providing an exhaust gas recirculation line connecting the an intake line with an exhaust gas line of the internal combustion engine at a position, upstream the first turbine unit, the exhaust gas line having at least one branch, providing: a bypass line connecting the exhaust gas recirculation line to the exhaust gas line at a position downstream of the turbine unit and at a position upstream of both of a diesel particle filter and a selective catalytic reduction system of an aftertreatment system, a bypass valve controlling the exhaust gas flow from the exhaust gas recirculation line to the exhaust gas line in order to increase temperature of the exhaust gas downstream of the turbine unit and upstream of the aftertreatment system of the engine, and providing at least one valve in the exhaust gas recirculation for each branch of the exhaust gas line for controlling the amount of recirculated exhaust gas, wherein the bypass line is connected to the exhaust as recirculation line at a position located downstream the at least one valve between the at least one valve and a position where the exhaust gas recirculation line connects to the air intake line.

Assignees

• Volvo Truck Corp

Inventors

• Aronsson Ulf
• Bauer Martin
• Adlouni Mohammed

Classifications

• F02M26/38

  with two or more EGR valves disposed in parallel · CPC title

• F02M26/08

  for engines having two or more intake charge compressors or exhaust gas turbines, e.g. a turbocharger combined with an additional compressor · CPC title

• F02B37/025

  Multiple scrolls or multiple gas passages guiding the gas to the pump drive · CPC title

• F02M26/42

  having two or more EGR passages; EGR systems specially adapted for engines having two or more cylinders · CPC title

• F02B37/18

  by bypassing exhaust {from the inlet to the outlet of turbine or to the atmosphere} · CPC title