IP Library Patent Application 13280427
Patent Application
App. No. 13/280,427

METHOD FOR CONTROLLING A FUEL INJECTOR

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Quick Facts
Patent No.
US None
App. No.
13/280,427
Abstract

A method for determining injected fuel mass delivered from an electromagnetic solenoid-activated fuel injector during a fuel injection event includes determining a sensed injection duration and a maximum injection mass flowrate during the fuel injection event, and determining the injected fuel mass for the fuel injection event based on the sensed injection duration and the maximum injection mass flowrate during the fuel injection event.

Claims (53)

1 . Method for determining injected fuel mass delivered from an electromagnetic solenoid-activated fuel injector during a fuel injection event, comprising:

determining a sensed injection duration and a maximum injection mass flowrate during the fuel injection event; and

determining the injected fuel mass for the fuel injection event based on the sensed injection duration and the maximum injection mass flowrate during the fuel injection event.

2 . The method of claim 1 , wherein determining the injected fuel mass for the fuel injection event comprises calculating the injected fuel mass in accordance with the following relationship:

M _Inj= K 2*( T _Inj* M max)

wherein

M_Inj is the injected fuel mass,

T_Inj is the sensed injection duration,

MMax is the maximum injection mass flowrate, and

K2 is a scalar term.

3 . The method of claim 2 , wherein the K2 scalar term is determined in relation to a fuel pressure.

4 . The method of claim 1 , wherein determining the sensed injection duration comprises:

determining a first time point corresponding to a discernible decrease in a fuel pressure;

determining a second time point corresponding to a discernible inflection point in an injector voltage; and

calculating the sensed injection duration as an elapsed time period between the first and second time points.

5 . The method of claim 4 , wherein said fuel pressure comprises a fuel pressure proximal to the fuel injector.

6 . The method of claim 1 , wherein determining the maximum injection mass flowrate comprises:

detecting a maximum drop in a fuel pressure during the fuel injection event; and

determining the maximum injection mass flowrate based on the maximum pressure drop in the fuel pressure during the fuel injection event.

7 . The method of claim 1 , further comprising correlating the injected fuel mass for the fuel injection event to an injector command signal for the fuel injection event.

8 . Method for operating a fuel injector, comprising:

determining a sensed injection duration for a fuel injection event comprising an elapsed time period between a discernible decrease in a fuel pressure and a discernible inflection point in an injector voltage;

determining a maximum injection mass flowrate based on a maximum pressure drop in the fuel pressure during the fuel injection event; and

determining an injected fuel mass for the fuel injection event based on the sensed injection duration and the maximum injection mass flowrate.

9 . The method of claim 8 , wherein determining the injected fuel mass for the fuel injection event comprises calculating the injected fuel mass in accordance with the following relationship:

M _Inj= K 2*( T _Inj* M max)

wherein

M_Inj is the injected fuel mass,

T_Inj is the sensed injection duration,

MMax is the maximum injection mass flowrate, and

K2 is a scalar term.

10 . The method of claim 9 , wherein the K2 scalar term is determined in relation to the fuel pressure.

11 . The method of claim 8 , wherein determining the sensed injection duration comprises:

monitoring the fuel pressure at a point proximal to the fuel injector and the injector voltage;

determining a first time point corresponding to the discernible decrease in the fuel pressure;

determining a second time point corresponding to the discernible inflection point in the injector voltage; and

calculating the sensed injection duration as an elapsed time period between the first and second time points.

12 . The method of claim 8 , wherein determining the maximum injection mass flowrate comprises:

monitoring the fuel pressure proximal to the fuel injector;

detecting the maximum drop in the fuel pressure during the fuel injection event; and

determining the maximum injection mass flowrate during the fuel injection event based on the maximum pressure drop in the fuel pressure during the fuel injection event.

13 . Method for operating an electromagnetic solenoid-activated fuel injector, comprising:

determining an elapsed time period comprising a time period between a discernible decrease in a fuel pressure proximal to the fuel injector and a discernible inflection point in an injector voltage during a fuel injection event;

determining a maximum pressure drop in the fuel pressure during the fuel injection event; and

determining an injected fuel mass based on the elapsed time period and the maximum pressure drop in the fuel pressure.

14 . The method of claim 13 , wherein determining the injected fuel mass comprises calculating the injected fuel mass in accordance with the following relationship:

M _Inj= K 2*( T _Inj* M max)

wherein

M_Inj is the injected fuel mass,

T_Inj is the elapsed time period,

MMax is a maximum injection mass flowrate corresponding to the maximum pressure drop in the fuel pressure during the fuel injection event, and

K2 is a scalar term.

15 . The method of claim 14 , wherein the K2 scalar term is determined in relation to the fuel pressure.

Assignments (3)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034186/0776 →
SECURITY AGREEMENT Recorded Jun 28, 2012
From: GM GLOBAL TECHNOLOGY OPERATIONS LLC
To: WILMINGTON TRUST COMPANY
Reel/Frame 028458/0184 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 25, 2011
From: PARRISH, SCOTT E.; ZINK, RONALD J.; NAJT, PAUL M.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 027112/0656 →