Precise fuel flow measurement with modified fluid control valve

• US 5,895,844 A
• Filed: 05/29/1997
• Issued: 04/20/1999
• Est. Priority Date: 05/29/1997
• Status: Expired due to Fees

• Current Assignee: BRP US Incorporated (Bombardier Incorporated)
• Original Assignee: Outboard Marine Corporation (Bombardier Incorporated)
• Inventors: Krueger, William R.
• Primary Examiner(s): Dombroske, George
• Assistant Examiner(s): MCCALL, ERIC SCOTT
• Application Number:
  US08/864,505
• Time in Patent Office: 691 Days
• Field of Search: 73/118.1, 73/119 A, 73/116, 73/117.3, 123/445, 123/479
• US Class Current: 73/114.72
• CPC Class Codes: F02D 41/40 with means for controlling injection timing or duration
• CPC Class Codes: Y02T 10/40 Engine management systems

Abstract

A modified fuel injector is fitted with a position sensing device that starts sending position information to the ECU at the onset of pressurization and displacement of fuel in the injector. Thus the effective stroke of the piston in the injector valve can be made to represent the fuel that is delivered to each cylinder of an engine. A position sensor is attached to the injector valve piston assembly. By electronically measuring the amount of effective piston travel, i.e. the piston travel that commences at the onset of pressurization of the injector valve, the amount of fuel delivered to the cylinder is known.

Claims

1. A system for electronically measuring an amount of effective piston stroke travel in a fuel injector while compressing and displacing fuel in a chamber therein to determine a precise amount of fuel delivered to an engine cylinder by said piston stroke travel, the system comprising:

a first sensor means on said injector for detecting an actual amount of piston stroke travel and generating corresponding first signal;

a second sensor means on said injector for detecting both the onset and the completion of fuel compression by said piston stroke travel and generating corresponding second and third signals; and

an electronic control unit coupled to said first and second sensors and having a measuring circuit for calculating effective piston stroke travel only from the onset of said fuel compression as determined by said second signal and therefore determining a precise measurement of fuel ejected on each piston stroke.

2. The system of claim 1 wherein said second sensor means comprises:

a fuel input port associated with said fuel injector and having a fuel passageway that is coupled to said fuel injector chamber; and

an electrical switch mounted in said fuel input port, said switch being closed to generate said second signal representing the onset of fuel compression caused by said piston stroke travel when no fuel is entering said chamber and being open to generate said third signal when fuel is entering said chamber representing the completion of said fuel compression and the cessation of said piston stroke travel.

3. The system of claim 2 wherein said electrical switch mounted in said fuel input port comprises:

a ball valve in said fuel passageway;

a ball valve seat in said fuel passageway;

a resilient means for forcing said ball valve against said valve seat to normally close said fuel passageway;

said ball valve, valve seat, and said resilient means being formed of electrically conductive material with said valve seat being electrically insulated from said fuel passageway; and

electrical connection means coupled to said valve seat and said resilient means such that an electrically closed switch connection is formed to generate said second signal when said ball valve contacts said valve seat to indicate onset of fuel compression and an electrically open switch is formed when said ball valve moves away from said valve seat to generate said third signal indicating the cessation of said piston stroke travel.

4. The system of claim 3 wherein said resilient means is a spring means normally urging said ball valve to the closed position, sufficient fuel pressure causing said ball valve to overcome said spring means and move away from said valve seat to cause said third signal to be generated.

5. The system of claim 1 wherein said second sensor comprises:

a pressure sensor associated with said fuel chamber for detecting a sudden pressure change in said chamber;

an electrical switch associated with said pressure sensor for generating said second signal when said sudden pressure change occurs in said chamber.

6. A system of claim 1 wherein said second sensor means comprises:

an injector fuel output port having a fuel passageway coupled to said fuel injector chamber;

a needle valve in said fuel injector port biased in a normally closed position;

an electrical switch associated with said needle valve for generating said second signal indicating respectively when said needle valve is opened, thus representing the onset of fuel compression and corresponding fuel flow from said injector during the time said needle valve is opened and generating said third signal when said needle valve is closed; and

an electronic control unit coupled to said electrical switch to determine precise measurement of fuel ejected on each piston stroke.

7. The system of claim 6 wherein said electrical switch comprises:

an electrically conductive ring associated with said fuel injector needle valve; and

an electrically conductive ring seat on and electrically insulated from a body portion of said fuel injector for breaking electrical contact with said electrically conductive ring only when said needle valve is open and for making electrical contact when said needle valve is closed to generate said second and third signals thus providing an indication of the onset and completion of fuel compression to thereby provide a precise indication of fuel flow from said injector.

8. The system of claim 7 further comprising spring means normally urging said needle valve to said closed position such that sufficient fuel pressure in said chamber caused by said moving piston causes said onset of fuel compression and overcomes said spring means to open said needle valve and generate said second signal.

9. The system of claim 1 wherein said first sensor means comprises:

a light source and a light receiver mounted in spaced relationship on said fuel injector; and

a light interrupting means attached to said piston and interposed between said spaced light source and said light receiver for generating said first signal representing actual travel of said piston.

10. The system of claim 9 wherein said light interrupting means comprises a series of comb-like teeth that produces light pulses representing distance traveled by said piston.

11. The system of claim 9 wherein said light source and said light receiver are fiber-optic cables that carry light to and from said light interrupting means.

12. The system of claim 10 wherein said light interrupting means comprises a sloping surface on said piston that allows more light to be passed to said receiver as a function of distance traveled by said piston.

13. The system of claim 1 wherein said first sensor means comprises an inductive pickup associated with said piston for generating said first signal by producing a varying inductance representing actual piston movement.

14. The system of claim 13 wherein said inductive pickup comprises:

a metal core associated with and moving with said piston; and

a coil of electrically conductive wire on said fuel injector and wound around said core such that movement of said core within said coil produces said variable inductance.

15. The system of claim 1 wherein said first sensor comprises a variable capacitor associated with said piston such that movement of said piston causes a change in said capacitance to generate said first signal.

16. The system of claim 15 wherein said variable capacitor comprises:

a first plate fixedly attached to said fuel injector; and

a second plate adjacent said first plate to form said capacitor, said second plate being associated with said piston such that piston movement changes the adjacent position of said second plate with respect to said first plate to change the capacitance and generate said first signal that represents actual movement of said piston.

17. The system of claim 1 further comprising:

a needle valve in said fuel injector movable between a closed and an open position;

bias means associated with said needle valve to bias said needle valve in the normally closed position;

a special calibration signal transmitted to said fuel injector by said electronic control unit to move said piston to generate sufficient pressure to cause said second sensor to generate said second signal but not sufficient to open said needle valve; and

said first signal generated by said first sensor as said piston moves being coupled to said electronic control unit for calculating leakage rate of fuel around said piston, said leakage rate being utilized by said electronic control unit as a correction factor when calculating fuel delivery during normal operations of said fuel injector.

18. The system of claim 1 further comprising:

a signal multiplexer having an input coupled to said electronic control unit and having a plurality of outputs;

a fuel injector coupled to each multiplexer output; and

a timing device coupled to said electronic control unit for causing the measurement of fuel delivered by each fuel injector on cyclically timed basis such that only one measuring circuit in said electronic control unit can be used sequentially with each fuel injector to measure fuel delivered thereby.

19. The system of claim 1 further including:

an air flow sensor for generating a signal representing air being used by said engine, said air flow sensor signal being coupled to said electronic control unit;

force generating means associated with said piston and being coupled to said electronic control unit for receiving current therefrom to cause said piston to move; and

said electronic control unit calculating the actual engine fuel/air ratio and providing said current to said force generating means to vary the fuel being injected to achieve a desired engine fuel/air ratio.