The present invention relates to a fuel injector system, and more particularly to a method of determining the end of motion of a fuel injector spool control valve.
Fuel injectors typically use a high pressure fluid acting on a relatively large area intensifier piston to compress fuel under a smaller area plunger. When fuel pressure is raised above a valve opening pressure, a needle check valve lifts to open the nozzle outlet, and fuel sprays into the combustion space within an engine.
To accurately control the timing of each injection event, the fuel injectors commonly include a solenoid actuated spool valve that opens and closes the fuel injector to the high pressure actuation fluid. The spool valve is essentially an armature movable relative to a solenoid coil located at each axial end of the spool valve.
Each injection event is initiated by energizing one coil to move the control valve to an open position, and each injection event is ended by actuating a second solenoid coil opposite the first coil to move the spool valve back to its closed position. The fluid-actuated fuel injector de-couples the injection quantity and timing from the operation of the engine to provide flexibility of main pilot fuel quantity, timing, and duration.
As the spool valve moves toward the actuated coil, the magnetic field within the unpowered coil varies, thereby producing an opposing voltage or back emf voltage signal in the unpowered coil. Typically, the back emf voltage signal is examined to determine when the spool has reached its full open or closed position. Control of the injection event through actuation of the coils is thereby effected through a feedback control loop.
Although effective, distinguishing when the spool valve has reached the end of travel through examination of the back emf may be difficult and relatively imprecise due to the extremely small timing envelope of an injection event. Moreover, end of travel determinations is further complicated due to dragging of the spool valve, otherwise known as “stiction” which may alter the back emf signal.
Accordingly, it is desirable to provide a method of reliably determining when a fuel injector spool control valve reaches the end of motion.
The fuel injector system according to the present invention measures a back emf signal from an unpowered spool valve coil. A first derivative filtered signal and a second derivative filtered signal are then calculated from the measured signal. When the spool valve reaches the end of travel, either open or closed position, a flat slope is generated on the falling edge of the measured signal. However, determining exactly when this steep slope occurs is rather difficult when so examining the back emf signal directly considering the extremely small timing envelope of an injection event window and the constant slope change of the signal. By calculating the second derivative, however, the steep slope is readily apparent when the second derivative crosses zero. A comparator thereby need only determine when the second derivative is zero to identify that the spool valve has reached the end of travel.
The present invention therefore provides a method of reliably determining when a fuel injector spool control valve reaches the end of motion.
The various features and advantages of this invention will become apparent to those skilled in the art from the following detailed description of the currently preferred embodiment. The drawings that accompany the detailed description can be briefly described as follows:
A first and second opposed electric coil 38, 40 are mounted at each end of the electrically controlled spool valve 16. Each coil 38, 40 is connected to a power source (illustrated schematically at 42) and a controller (illustrated schematically at 44). The electrically controlled spool valve 16 is attracted to the coil 38, 40 which is selectively energized by the power source 42. Concurrently, the controller 44 measures a signal (
As generally known, when a coil 38, 40 is energized, the spool valve 16 begins moving toward the energized coil 38, 40. A stop 41 or the like is preferably located at each end of the spool valve 16. To initiate an injection, the spool valve 18 is moved to a first position in which the fluid supply passage 24 is opened and high pressure actuation fluid acts upon an intensifier piston (illustrated schematically at 46), and begins moving it toward a fuel pressurization chamber (illustrated schematically at 48). Fuel pressurization chamber 48 receives fuel from the fuel source 32 through fuel supply passage 34. Piston 46 increases pressure within the fuel pressurization chamber 48 until the pressure rises to a level which opens a needle valve member (illustrated schematically at 50) and fuel is sprayed thorough the nozzle outlet 36.
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Furthermore, it still is worth stating that the present invention is not limited to a microprocessor based control system. The system may be implemented in a non-microprocessor based electronic system (either digital or analog).
The foregoing description is exemplary rather than defined by the limitations within. Many modifications and variations of the present invention are possible in light of the above teachings. The preferred embodiments of this invention have been disclosed, however, one of ordinary skill in the art would recognize that certain modifications would come within the scope of this invention. It is, therefore, to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described. For that reason the following claims should be studied to determine the true scope and content of this invention.
The present application claims priority to U.S. Provisional Patent Application Ser. No. 60/276,220, filed Mar. 15, 2001 and U.S. Provisional Patent Application Ser. No. 60/278,223, filed Mar. 23, 2001.
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Number | Date | Country |
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WO 9413991 | Jun 1994 | WO |
Number | Date | Country | |
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20020130192 A1 | Sep 2002 | US |
Number | Date | Country | |
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60278223 | Mar 2001 | US | |
60276220 | Mar 2001 | US |