Turbocharger compressor anti-surge engine control strategy and method

Patent metadata

Field	Value
Publication number	US-9683498-B2
Application number	US-201514716603-A
Country	US
Kind code	B2
Filing date	May 19, 2015
Priority date	May 19, 2015
Publication date	Jun 20, 2017
Grant date	Jun 20, 2017

Abstract

A method for operating an internal combustion engine includes monitoring engine parameters using an electronic controller, determining a surge speed limit for the engine based on a compressor map, determining an offset engine speed based on a margin between the surge speed limit and an engine speed, determining a minimum engine speed based on the margin, applying the offset engine speed to an engine speed signal to provide an adjusted engine speed, and applying the adjusted engine speed to a desired engine speed when a speed of the engine approaches the surge speed limit.

First claim

We claim:

1. A method for operating an engine, comprising:
monitoring engine parameters using an electronic controller;
determining a surge speed limit for the engine based on a compressor map, the surge speed limit for the engine representing an engine speed below which operating conditions of a compressor of the engine will cause the compressor to surge;
determining an offset engine speed based on a margin between the surge speed limit and the engine speed;
determining a minimum engine speed based on the margin;
applying the offset engine speed to an engine speed signal to provide an adjusted engine speed; and
applying the adjusted engine speed to a desired engine speed when a speed of the engine approaches the surge speed limit.

2. The method of claim 1 , further comprising delimiting the adjusted engine speed between a maximum threshold engine speed and the minimum engine speed.

3. The method of claim 1 , wherein determining the surge speed limit includes interrogating the compressor map to determine a surge mass airflow for the compressor, the surge mass airflow representing an airflow through the compressor at an engine operating pressure ratio across the compressor that will cause the compressor to operate in a surge condition.

4. The method of claim 3 , further comprising calculating a ratio between an engine mass airflow (MAF) and the surge mass airflow to determine a MAF surge ratio.

5. The method of claim 4 , wherein the MAF surge ratio is a non-dimensional parameter that is less than one when the engine is operating at an engine MAF that is more than the surge mass airflow.

6. The method of claim 4 , wherein determining the surge speed limit further includes multiplying the engine speed with the MAF surge ratio to yield the surge speed limit.

7. The method of claim 1 , further comprising applying the adjusted engine speed to the desired engine speed commanded by an operator using the adjusted engine speed.

8. An internal combustion engine, comprising:
a turbocharger having a turbine connected to an exhaust system of the internal combustion engine and a compressor connected to an intake system of the internal combustion engine;
a mass airflow (MAF) sensor disposed to provide a MAF signal that is indicative of an engine MAF entering the compressor;
at least one pressure sensor disposed to provide a pressure signal that is indicative of a pressure ratio across the compressor;
an engine speed sensor disposed to provide an engine speed signal that is indicative of an engine speed of the internal combustion engine;
an electronic controller associated with the internal combustion engine and arranged to receive and monitor the MAF signal, the pressure signal and the engine speed signal, the electronic controller operating to provide a desired engine speed signal to the internal combustion engine;
wherein the electronic controller is programmed to:
store in non-volatile memory a compressor map onto which an operating point of the compressor can be determined based on the MAF signal and the pressure signal, the compressor map further including a surge line at which the compressor will operate in a surge condition;
determine, based on the compressor map, a surge speed limit for the engine speed, the surge speed limit representing the engine speed below which the compressor will surge;
determine an offset engine speed based on a margin between the surge speed limit and the speed of the internal combustion engine;
determine a minimum desired engine speed based on the margin;
apply the offset engine speed to the engine speed signal to provide an adjusted engine speed; and

apply the adjusted engine speed to the desired engine speed signal.

9. The internal combustion engine of claim 8 , wherein the electronic controller is further programmed to delimit the adjusted engine speed between a maximum threshold engine speed and the minimum desired engine speed.

10. The internal combustion engine of claim 8 , wherein the electronic controller is further programmed to interrogate the compressor map to determine a surge MAF for the compressor, the surge MAF representing an airflow through the compressor at an engine operating pressure ratio across the compressor that will cause the compressor to operate in a surge condition.

11. The internal combustion engine of claim 10 , wherein the electronic controller is further programmed to calculate a ratio between the engine MAF and the surge MAF to determine a MAF surge ratio.

12. The internal combustion engine of claim 11 , wherein the MAF surge ratio is a non-dimensional parameter that is less than one when the internal combustion engine is operating at an engine MAF that is more than the surge MAF.

13. The internal combustion engine of claim 11 , wherein the electronic controller is further programmed to multiply the speed of the internal combustion engine with the MAF surge ratio to yield the surge speed limit.

14. The internal combustion engine of claim 8 , wherein the electronic controller is further programmed to adjust the speed of the internal combustion engine to a desired engine speed commanded by an operator using the adjusted engine speed.

15. A method for operating an engine having a turbine connected to an exhaust system of the engine and a compressor connected to an intake system of the engine, the method comprising:
receiving in a controller a MAF signal that is indicative of an engine MAF entering the compressor;
receiving in the controller a pressure signal that is indicative of a pressure ratio across the compressor;
receiving in the controller an engine speed signal that is indicative of an engine speed; and
using the controller to control a speed of the engine;
wherein the controller is programmed to:
store in non-volatile memory a compressor map onto which an operating point of the compressor can be determined based on the MAF signal and the pressure signal, the compressor map further including a surge line at which the compressor will operate in a surge condition;
determine, based on the compressor map, a surge speed limit for the engine speed, the surge speed limit representing the engine speed below which the compressor will surge;
determine an offset engine speed based on a margin between the surge speed limit and the speed of the engine;
determine a minimum desired engine speed based on the margin;
apply the offset engine speed to the engine speed signal to provide an adjusted engine speed; and

apply the adjusted engine speed to a desired engine speed signal.

16. The method of claim 15 , wherein the controller is further programmed to delimit the adjusted engine speed between a maximum threshold engine speed and the minimum desired engine speed.

17. The method of claim 15 , wherein the controller is further programmed to interrogate the compressor map to determine a surge MAF for the compressor, the surge MAF representing an airflow through the compressor at an engine operating pressure ratio across the compressor that will cause the compressor to operate in a surge condition.

18. The method of claim 17 , wherein the controller is further programmed to calculate a ratio between the engine MAF and the surge MAF to determine a MAF surge ratio.

19. The method of claim 18 , wherein the MAF surge ratio is a non-dimensional parameter that is less than one when the engine is operating at an engine MAF that is more than the surge MAF.

20. The method of claim 18 , wherein the controller is further programmed to multiply the speed of t

Assignees

• Caterpillar Inc

Inventors

• Joshi Urvish
• Barnes Travis
• Cler Eric W
• Krishnamurthygopalan Anand
• Hutchison Eric A
• Tamhane Kirti
• Schifferer Andrew N
• Bowman Tyler
• Sergott Kevin
• Mowers Matthew
• Puckett Daniel R

Classifications

• F02D41/0225

  in relation with the gear ratio or shift lever position · CPC title

• F02D41/18

  by measuring intake air flow · CPC title

• F02D41/0007 Primary

  for control of turbo-charged or super-charged engines (control of the pumps per se F02B37/12) · CPC title

• F02D31/001

  Electric control of rotation speed · CPC title

• F02B2037/125

  Control for avoiding pump stall or surge · CPC title