# US 7,461,508 B2 · Method and device for regulating the charge pressure of an internal combustion engine

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- Number: US 7,461,508 B2
- Document ID: US7461508B2
- Status: Granted
- Kind: B2
- Application number: 11/281,690
- Filed: 2005-11-16
- Published: 2006-06-15
- Granted: 2008-12-09
- Earliest claimed: 2004-11-25
- Assignees: Robert Bosch GmbH
- Inventors: Ulrich Rosin; Thomas Bleile; Michael Scheidt
- Web page: https://patentgrep.com/patent/US7461508B2

## CPC

- F02D 41/0007: {for control of turbo-charged or super-charged engines (control of the pumps per se F02B37/12)}
- F02D 41/1448: {the characteristics being an exhaust gas pressure}
- F02B 37/004: {with exhaust drives arranged in series}
- F02B 37/013: with exhaust-driven pumps arranged in series
- F02B 37/16: by bypassing charging air
- F02B 37/18: by bypassing exhaust {from the inlet to the outlet of turbine or to the atmosphere}
- F02D 2041/1419: {the control loops being cascaded, i.e. being placed in series or nested}
- F02D 2200/0406: Intake manifold pressure
- Y02T 10/12: Improving ICE efficiencies
- F02D: CONTROLLING COMBUSTION ENGINES (vehicle fittings, acting on a single sub-unit only, for automatically controlling vehicle speed B60K31/00; conjoint control of vehicle sub-units of different type or different function, road vehicle drive control systems for purposes other than the control of a single sub-unit B60W)
- F02B: INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL (gas-turbine plants F02C; hot-gas or combustion-product positive-displacement engine plants F02G)
- Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION

## Abstract

A method and a device are provided for regulating the charge pressure of an internal combustion engine having at least two exhaust gas turbochargers that set a target charge pressure rapidly and without overshooting. A first actuating element is provided with which the charge pressure of a first exhaust gas turbocharger is set, and a second actuating element is provided with which the charge pressure of a second exhaust gas turbocharger is set. Dependent on the exhaust gas back pressure prevailing in the exhaust gas channel at the output of the internal combustion engine, a first controlled variable is determined for the first actuating element, and a second controlled variable is determined for the second actuating element.

## Claims

### Claim 1

A method for regulating a charge pressure of an internal combustion engine having at least two exhaust-gas turbochargers, comprising:
providing a first actuating element for setting a charge pressure of a first exhaust-gas turbocharger;
providing a second actuating element for setting a charge pressure of a second exhaust gas turbocharger; and
determining, dependent on an exhaust-gas back pressure prevailing in an exhaust-gas channel at an output of the internal combustion engine, a first controlled variable for the first actuating element and a second controlled variable for the second actuating element, wherein the first controlled variable and the second controlled variable are determined as a function of one and the same exhaust-gas back pressure prevailing in the exhaust-gas channel at the output of the internal combustion engine.

### Claim 2 (depends on 1)

The method as recited in claim 1, further comprising:
determining by a first regulator a target exhaust-gas back pressure from a deviation between a target charge pressure and an actual charge pressure; and
deriving by a second regulator the first and second controlled variables for the first and second actuating elements, based on a deviation between the target exhaust-gas back pressure and one of a measured and estimated actual exhaust-gas back pressure.

### Claim 3 (depends on 2)

The method as recited in claim 2, wherein the target exhaust-gas back pressure is limited to a predetermined range.

### Claim 4 (depends on 2)

The method as recited in claim 2, wherein the first controlled variable influences one of: a) a variable geometry of a turbine of the first exhaust-gas turbocharger; b) an opening cross-section of a first bypass around the turbine of the first exhaust-gas turbocharger; and c) an opening cross-section of a second bypass around a compressor of the first exhaust-gas turbocharger.

### Claim 5 (depends on 4)

The method as recited in claim 4, wherein the second controlled variable influences one of: a) a variable geometry of a turbine of the second exhaust-gas turbocharger; b) an opening cross-section of a third bypass around the turbine of the second exhaust-gas turbocharger; and c) an opening cross-section of a fourth bypass around a compressor of the second exhaust-gas turbocharger.

### Claim 6 (depends on 2)

The method as recited in claim 2, wherein the second controlled variable influences one of: a) a variable geometry of a turbine of the second exhaust-gas turbocharger; b) an opening cross-section of a third bypass around the turbine of the second exhaust-gas turbocharger; and c) an opening cross-section of a fourth bypass around a compressor of the second exhaust-gas turbocharger.

### Claim 7 (depends on 1)

The method as recited in claim 1, wherein the target exhaust-gas back pressure is limited to a predetermined range.

### Claim 8 (depends on 7)

The method as recited in claim 7, wherein the first controlled variable influences one of: a) a variable geometry of a turbine of the first exhaust-gas turbocharger; b) an opening cross-section of a first bypass around the turbine of the first exhaust-gas turbocharger; and c) an opening cross-section of a second bypass around a compressor of the first exhaust-gas turbocharger.

### Claim 9 (depends on 8)

The method as recited in claim 8, wherein the second controlled variable influences one of: a) a variable geometry of a turbine of the second exhaust-gas turbocharger; b) an opening cross-section of a third bypass around the turbine of the second exhaust-gas turbocharger; and c) an opening cross-section of a fourth bypass around a compressor of the second exhaust-gas turbocharger.

### Claim 10 (depends on 7)

The method as recited in claim 7, wherein the second controlled variable influences one of: a) a variable geometry of a turbine of the second exhaust-gas turbocharger; b) an opening cross-section of a third bypass around the turbine of the second exhaust-gas turbocharger; and c) an opening cross-section of a fourth bypass around a compressor of the second exhaust-gas turbocharger.

### Claim 11 (depends on 1)

The method as recited in claim 1, wherein the first controlled variable influences one of: a) a variable geometry of a turbine of the first exhaust-gas turbocharger; b) an opening cross-section of a first bypass around the turbine of the first exhaust-gas turbocharger; and c) an opening cross-section of a second bypass around a compressor of the first exhaust-gas turbocharger.

### Claim 12 (depends on 11)

The method as recited in claim 11, wherein the second controlled variable influences one of: a) a variable geometry of a turbine of the second exhaust-gas turbocharger; b) an opening cross-section of a third bypass around the turbine of the second exhaust-gas turbocharger; and c) an opening cross-section of a fourth bypass around a compressor of the second exhaust-gas turbocharger.

### Claim 13 (depends on 1)

The method as recited in claim 1, wherein the second controlled variable influences one of: a) a variable geometry of a turbine of the second exhaust-gas turbocharger; b) an opening cross-section of a third bypass around the turbine of the second exhaust-gas turbocharger; and c) an opening cross-section of a fourth bypass around a compressor of the second exhaust-gas turbocharger.

### Claim 14

A device for regulating a charge pressure of an internal combustion engine having at least two exhaust-gas turbochargers, comprising:
a first actuating element for setting a charge pressure of a first exhaust-gas turbocharger;
a second actuating element for setting a charge pressure of a second exhaust gas turbocharger; and
a control arrangement for determining, dependent on an exhaust-gas back pressure prevailing in an exhaust-gas channel at an output of the internal combustion engine, a first controlled variable for the first actuating element and a second controlled variable for the second actuating element, wherein the first controlled variable and the second controlled variable are determined as a function of one and the same exhaust-gas back pressure prevailing in the exhaust-gas channel at the output of the internal combustion engine.

### Claim 15 (depends on 14)

The device as recited in claim 14, wherein the control arrangement includes:
a first regulator for determining a target exhaust-gas back pressure from a deviation between a target charge pressure and an actual charge pressure; and
a second regulator for deriving the first and second controlled variables for the first and second actuating elements, based on a deviation between the target exhaust-gas back pressure and one of a measured and estimated actual exhaust-gas back pressure.
