Gas or dual fuel engine

Patent metadata

Field	Value
Publication number	US-9605602-B2
Application number	US-201514641154-A
Country	US
Kind code	B2
Filing date	Mar 6, 2015
Priority date	Mar 10, 2014
Publication date	Mar 28, 2017
Grant date	Mar 28, 2017

Abstract

A method of operating a gas or dual fuel engine having a plurality of cylinders, includes monitoring a characteristic of each of the plurality of cylinders during operation of the gas or dual fuel engine. The method also includes detecting a pre-ignition condition associated with one or more cylinders of the plurality of cylinders based on the monitored characteristic. The method further includes reducing fuel supply to the one or more cylinders having the pre-ignition condition. The fuel supply to remaining cylinders of the plurality of cylinders is increased, to maintain a constant power output of the gas or dual fuel engine. The method further includes adjusting an amount of air supplied to each of the plurality of cylinders based on the increased amount of fuel supplied to the remaining cylinders, to maintain an air-to-fuel ratio within a desired range.

First claim

What is claimed is:

1. A method of operating an engine comprising a plurality of cylinders, the method comprising:
monitoring a characteristic of each of the plurality of cylinders during operation of the engine;
detecting a pre-ignition condition associated with one or more cylinders of the plurality of cylinders based on the monitored characteristic;
supplying a reduced amount of fuel to the one or more cylinders having the pre-ignition condition;
supplying an increased amount of the fuel to remaining cylinders of the plurality of cylinders, to maintain a constant power output of the engine; and
adjusting an amount of air supplied to each of the plurality of cylinders based on the increased amount of the fuel supplied to the remaining cylinders, to maintain an air-to-fuel ratio in the remaining cylinders within a predetermined range.

2. The method of claim 1 , wherein the predetermined range of air-to-fuel ratio is from 33:1 to 38:1.

3. The method of claim 1 , wherein monitoring the characteristic of each of the plurality of cylinders comprises monitoring a cylinder pressure of each of the plurality of cylinders.

4. The method of claim 1 , wherein detecting the pre-ignition condition further comprises:
determining a start of combustion in each of the plurality of cylinders based on the monitored characteristic; and
determining a time difference between the start of combustion and an ignition timing associated with each of the plurality of cylinders.

5. The method of claim 4 , wherein the engine comprises a plurality of fuel admission valves with each of the plurality of fuel admission valves being associated with each of the plurality of cylinders respectively and configured to supply the fuel to a combustion chamber of the associated cylinder, and supplying the increased amount of the fuel to the remaining cylinders of the plurality of cylinders further comprising:
increasing an opening duration of the fuel admission valves associated with the remaining cylinders when the time difference between the start of combustion and the ignition timing is less than a predetermined threshold for the one or more cylinders.

6. The method of claim 1 , wherein the engine comprises a pilot injector configured to inject a pilot fuel into a combustion chamber of each of the plurality of cylinders, the method further comprising:
determining a time difference between a start of combustion and a start of injection of pilot fuel by the pilot injector.

7. The method of claim 6 , wherein the engine comprises a plurality of fuel admission valves with each of the plurality of fuel admission valves being associated with each of the plurality of cylinders respectively and configured to supply the fuel to a combustion chamber of the associated cylinder, the method further comprising:
increasing an opening duration of the gas admission valves associated with the remaining cylinders when the time difference between the start of combustion and the start of injection of pilot fuel is less than a predetermined threshold for the one or more cylinders.

8. The method of claim 1 , wherein the engine comprises a plurality of fuel admission valves with each of the plurality of fuel admission valves being associated with each of the plurality of cylinders respectively and configured to supply the fuel to a combustion chamber of the associated cylinder, and supplying the reduced amount of the fuel to the one or more cylinders having the pre-ignition condition further comprising:
reducing an opening duration of the fuel admission valves associated with the one or more cylinders.

9. An engine comprising:
a plurality of cylinders;
a plurality of fuel admission valves, each of the plurality of fuel admission valves being associated with each of the plurality of cylinders respectively and configured to supply fuel to a combustion chamber of the associated cylinder;
a plurality of sensors, each of the plurality of sensors being associated with each of the plurality of cylinders respectively and configured to monitor a characteristic of the associated cylinder; and
a control unit operatively coupled to the plurality of sensors and the plurality of fuel admission valves, the control unit being configured to:
receive a characteristic of each of the plurality of cylinders from the plurality of sensors;
detect a pre-ignition condition associated with one or more cylinders of the plurality of cylinders based on the received characteristic;
supply a reduced amount of the fuel to the one or more cylinders having the pre-ignition condition;
supply an increased amount of the fuel to remaining cylinders of the plurality of cylinders, to maintain a constant power output of the engine; and
adjust an amount of air supplied to each of the plurality of cylinders based on the increased amount of the fuel supplied to the remaining cylinders, to maintain an air-to-fuel ratio in the remaining cylinders within a predetermined range.

10. The engine of claim 9 , wherein the control unit is configured to supply a reduced amount of the fuel to the one or more cylinders having the pre-ignition condition by reducing an opening duration of the fuel admission valves associated with the one or more cylinders.

11. The engine of claim 9 , wherein the predetermined range of air-to-fuel ratio is from 33:1 to 38:1.

12. The engine of claim 9 , wherein each of the plurality of sensors is a pressure sensor configured to detect a cylinder pressure of the associated cylinder.

13. The engine of claim 9 , wherein the control unit is configured to detect the pre-ignition condition by:
determining a start of combustion in each of the plurality of cylinders based on the received characteristic; and
determining a time difference between the start of combustion and an ignition timing associated with each of the plurality of cylinders.

14. The engine of claim 13 , wherein the control unit is configured to supply the increased amount of the fuel to the remaining cylinders by increasing an opening duration of the fuel admission valves associated with the remaining cylinders when the time difference between the start of combustion and the ignition timing is less than a predetermined threshold for the one or more cylinders.

15. The engine of claim 9 , further comprising a pilot injector configured to inject a pilot fuel into the combustion chamber of each of the plurality of cylinders.

16. The engine of claim 15 , wherein the control unit is configured to determine a time difference between a start of combustion and a start of injection of pilot fuel by the pilot injector.

17. The engine of claim 16 , wherein the control unit is further configured to increase an opening duration of the gas admission valves associated with the remaining cylinders when the time difference between the start of combustion and the start of injection of pilot fuel is less than a predetermined threshold for the one or more cylinders.

18. A control unit for controlling the operation of an engine, wherein the engine comprises a plurality of cylinders, a plurality of sensors associated with each of the cylinders and configured for determining a characteristic of each of the cylinders, and a plurality of fuel admission valves associated with each of the cylinders and configured for supplying fuel to each of the cylinders, the control unit being configured to:
receive a characteristic of each of the plurality of cylinders from the plurality of sensors;
detect a pre-ignition condition associated with one or more cylinders of the plurality of cylinders base

Assignees

• Caterpillar Motoren Gmbh & Co

Inventors

• Sixel Eike
• Stubbs Adam
• Chakrabarty Aradhita Subirkumar
• Wester Daniel
• Stazicker Rodney
• Snopko Michael Andrew
• Sivasubramanian Arvind

Classifications

• F02D41/0087

  Selective cylinder activation, i.e. partial cylinder operation (deceleration cut-off F02D41/123) · CPC title

• F02D41/0085 Primary

  Balancing of cylinder outputs, e.g. speed, torque or air-fuel ratio · CPC title

• F02D35/02

  on interior conditions · CPC title

• F02D41/401

  Controlling injection timing (F02D41/402 takes precedence) · CPC title

• F02D2200/1002

  Output torque · CPC title