Methods and systems for adjusting a direct fuel injector

• US 10,316,786 B2
• Filed: 12/01/2014
• Issued: 06/11/2019
• Est. Priority Date: 12/01/2014
• Status: Active Grant

• Current Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Original Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Inventors: Ranga, Adithya Pravarun Re, Surnilla, Gopichandra
• Primary Examiner(s): Hamaoui, David E
• Assistant Examiner(s): Staubach, Carl C
• Application Number:
  US14/556,821
• Publication Number:
  US 20160153387A1
• Time in Patent Office: 1,653 Days
• CPC Class Codes: F02D 41/1454 the characteristics being an oxygen content or concentration or the air-fuel ratio
• CPC Class Codes: F02D 41/2467 for injectors
• CPC Class Codes: F02D 41/3094 the fuel injection being effected by at least two different injectors, e.g. one in the intake manifold and one in the cylinder

Abstract

Systems and methods for improving fuel injection of an engine that includes a cylinder receiving fuel from two different fuel injectors is disclosed. In one example, a transfer function or gain of a direct fuel injector is adjusted in response to an exhaust lambda value and a first pulse width of two pulse widths provided to an injector of a cylinder during a cylinder cycle.

Claims

1. A cylinder fueling method, comprising:

supplying a first pulse width and a second pulse width to a direct fuel injector of a first cylinder during a cycle of the first cylinder, the first pulse width operating the direct fuel injector in a non-linear operating region, the second pulse width operating the direct fuel injector in a non-ballistic operating region, and where an engine in which the direct fuel injector operates to supply fuel to the first cylinder operates with only port fuel injectors supplying fuel to the engine'"'"'s cylinders other than the first cylinder when the direct fuel injector is operating in the non-linear operating region; and

decreasing the first pulse width a plurality of times while simultaneously increasing the second pulse width the plurality of times until the first pulse width is less than a threshold pulse width.

2. The method of claim 1, where the non-linear operating region is an operating region where fuel flow through the direct fuel injector is non-linear.

3. The method of claim 1, further comprising:

adjusting a fuel injector gain or transfer function according to a lambda value resulting from the first pulse width.

4. The method of claim 1, where increasing the second pulse width includes increasing an amount of fuel injected via the second pulse width by an amount of fuel that is removed by decreasing the first pulse width during each of the plurality of times the first pulse width is decreased.

5. The method of claim 1, where the first cylinder is in the engine, and where the engine is operated at a constant speed and air mass when the direct fuel injector is operated in the non-linear operating region.

13. The method of claim 1, further comprising:

deactivating the direct fuel injector and operating the cylinder in an only port fuel injection mode when the first pulse width is less than the threshold pulse width.

14. The method of claim 13, further comprising:

supplying the first pulse width and the second pulse width to a direct fuel injector of a second cylinder after the first pulse width supplied to the direct fuel injector of the first cylinder is less than the threshold pulse width.

15. The method of claim 14, further comprising:

supplying a first fraction of fuel to the second cylinder during a cycle of the second cylinder via the direct fuel injector of the second cylinder and supplying a second fraction of fuel to the second cylinder during the cycle of the second cylinder via a port fuel injector.

16. The method of claim 15, further comprising:

operating cylinders of the engine other than the second cylinder with only port fuel injectors.

17. The method of claim 1, further comprising:

multiplying a lambda value with total number of cylinders in a bank of cylinders to determine a first value, and dividing the first value by a ratio of the first pulse width and the second pulse width to determine a fuel correction for the cylinder.

6. A method for fueling a cylinder, comprising:

operating an engine at a constant speed and air mass;

supplying a first fuel fraction to a cylinder of the engine via a first fuel injector while supplying a second fuel fraction to the cylinder via a second fuel injector; and

supplying a first pulse width and a second pulse width to the second fuel injector during a cylinder cycle in response to a request to characterize the second fuel injector;

decreasing the first pulse width a plurality of times while simultaneously increasing the second pulse width the plurality of times until the first pulse width is less than a threshold pulse width;

adjusting a control parameter of the second fuel injector in response to an exhaust lambda produced while the second fuel injector is operating in a non-linear region; and

operating the second fuel injector based on the adjusted control parameter.

7. The method of claim 6, where the first fuel injector is a port fuel injector, and where the second fuel injector is a direct fuel injector.

8. The method of claim 6, where increasing the second pulse width includes increasing an amount of fuel injected via the second pulse width by an amount of fuel that is removed by decreasing the first pulse width during each of the plurality of times the first pulse width is decreased.

9. The method of claim 8, where fuel delivered via the first pulse width and the second pulse width is based on providing a mixture in the cylinder having a lambda value of one.

10. The method of claim 6, where the control parameter is a transfer function or gain.

11. The method of claim 6, further comprising commanding the engine to operate at a constant air-fuel ratio while operating at the constant speed and air mass.

12. The method of claim 6, further comprising supplying fuel to other engine cylinders only via port fuel injectors while supplying the first pulse width and the second pulse width to the second fuel injector.