Method for regulating a boost pressure of an engine

Patent metadata

Field	Value
Publication number	US-9470141-B2
Application number	US-201314133231-A
Country	US
Kind code	B2
Filing date	Dec 18, 2013
Priority date	Dec 20, 2012
Publication date	Oct 18, 2016
Grant date	Oct 18, 2016

Abstract

In a method for regulating a boost pressure of an engine which has a compressor, an actual boost pressure and a setpoint boost pressure are used as input parameters. The setpoint boost pressure is regulated in such a way that a pressure ratio in the compressor does not exceed a limit pressure ratio. A reference boost pressure is ascertained based on a speed of the engine and a load of the engine. A flow and/or a pressure of air supplied to the engine is/are detected and an associated flow signal and/or pressure signal is generated. The smaller of the reference boost pressure and a limit boost pressure is used as a setpoint boost pressure. The limit boost pressure is ascertained based on a limit boost pressure ratio and a speed of the compressor.

First claim

What is claimed is:

1. A method for regulating a boost pressure of an engine which has a compressor, the method comprising:
ascertaining a reference boost pressure based on a speed of the engine and a load of the engine;
detecting at least one of a flow and a pressure of air supplied to the engine, and generating at least one of an associated flow signal and a pressure signal;
using a smaller of the reference boost pressure and a limit boost pressure as a setpoint boost pressure; and
regulating the setpoint boost pressure in such a way that a pressure ratio in the compressor does not exceed a limit boost pressure ratio;
wherein the limit boost pressure ratio is ascertained based on a magnitude of a change over time of the at least one of the flow signal and the pressure signal, and
wherein the limit boost pressure is ascertained based on the limit boost pressure ratio and a speed of the compressor.

2. The system as recited in claim 1 , wherein the limit boost pressure ratio is ascertained based on the magnitude of the change over time of the flow signal.

3. The system as recited in claim 1 , wherein the limit boost pressure ratio is ascertained based on the magnitude of the change over time of the pressure signal.

4. The method as recited in claim 1 , wherein the limit boost pressure ratio is ascertained as exceeding a magnitude of the change over time of the at least one of the flow signal and the pressure signal.

5. The method as recited in claim 4 , wherein the change over time of the flow signal is ascertained as a change of the flow signal per unit of time.

6. The method as recited in claim 4 , wherein the pressure of the air supplied to the engine is detected at least one of upstream and downstream from the compressor.

7. The method as recited in claim 4 , wherein the flow signal is corrected with respect to a reference pressure and a reference temperature.

8. The method as recited in claim 4 , wherein the limit boost pressure ratio is additionally ascertained from a zero crossing of the flow signal.

9. The method as recited in claim 4 , wherein the limit boost pressure is ascertained in such a way that the speed of the compressor is reduced corresponding to the change over time of the at least one of the flow signal and the pressure signal.

10. The method as recited in claim 9 , wherein the speed of the compressor is reduced by opening a bypass valve of the compressor.

11. A pressure boost system for an engine, comprising:
a compressor; and
a regulation device for regulating a boost pressure of the engine, the regulation device including:
an ascertaining arrangement configured to ascertain a reference boost pressure based on a speed of the engine and a load of the engine;
a detecting arrangement configured to detect at least one of a flow and a pressure of air supplied to the engine, and generating at least one of an associated flow signal and a pressure signal;
a selecting arrangement configured to select a smaller of the reference boost pressure and a limit boost pressure as a setpoint boost pressure; and
a regulating arrangement configured to regulate the setpoint boost pressure in such a way that a pressure ratio in the compressor does not exceed a limit boost pressure ratio;
wherein the limit boost pressure ratio is ascertained based on a magnitude of a change over time of the at least one of the flow signal and the pressure signal, and
wherein the limit boost pressure is ascertained based on the limit boost pressure ratio and a speed of the compressor.

12. The system as recited in claim 11 , wherein the engine includes at least one fuel cell.

Assignees

• Bosch Gmbh Robert

Inventors

• Kemmer Helerson
• Steidten Thomas
• Intorp Jens
• Zirkel Daniel

Classifications

• Y02T10/12

  Improving ICE efficiencies · CPC title

• H01M8/04111

  using a compressor turbine assembly · CPC title

• F02B37/12 Primary

  Control of the pumps · CPC title

• H01M2250/20

  Fuel cells in motive systems, e.g. vehicle, ship, plane · CPC title

• F02D41/18

  by measuring intake air flow · CPC title