This invention relates to oil activated fuel injectors and, more particularly, to a system and method to control motion of an armature of the injector using closed loop operation with adaptive current or voltage wave forms.
In hydraulically actuated fuel injection systems, a control valve body is provided with a valve system having grooves or orifices which allow fluid communication between working ports, high pressure ports, and venting ports of the control valve body of the fuel injector and the inlet area. The working fluid is typically engine oil or other types of suitable hydraulic fluid which is capable of providing a pressure within the fuel injector in order to begin the process of injecting fuel into the combustion chamber.
In current configurations, a driver will deliver a current or voltage to an open side of an open coil solenoid. The magnetic force generated in the open coil solenoid will shift an armature into the open position so as to align grooves of the control valve body and the armature. The alignment of the grooves permits the working fluid to flow into an intensifier chamber from an inlet portion of the control valve body (via working ports). The high pressure working fluid then acts on an intensifier piston to compress an intensifier spring and hence compress fuel located within a high pressure plunger chamber. As the pressure in the high pressure plunger chamber increases, the fuel pressure will begin to rise above a needle check valve opening pressure. At the prescribed fuel pressure level, the needle check valve will shift against the needle spring and open the injection holes in a nozzle tip. The fuel will then be injected into the combustion chamber of the engine.
However, in such a conventional system, the armature has a tendency to bounce or repeatedly impact against the open coil during the opening stroke. During this bouncing, it is difficult to control the armature motion and hence results in the inability to efficiently control the supply of fuel to the combustion chamber of the engine. For example, in conventional systems it is not possible to quickly move the armature away from the open coil in order to minimize the bouncing effect during an injection of a pilot quantity of fuel. Accordingly, the initial quantity of fuel provided during the pre-stroke event cannot be easily controllable, resulting in a larger injection quantity of fuel than desired. This may result in a retarded start of injection, as well as the inability to control the armature and hence the injection of a small, pilot quantity of fuel. That is, during this bouncing or repeated impact, a small quantity of fuel cannot be metered accurately in order to efficiently inject this small quantity of fuel into the combustion chamber of an engine. Additionally, it is also very difficult, if not impossible, to vary the amount of fuel during this small injection.
Thus, injection shot-to-shot variations can occur on a single fuel injector.
It is also known that the bouncing phenomenon may differ from injector to injector, and over time. For example, different manufacturing tolerances may affect the bouncing phenomenon from, for example, small variations in armature diameter to different coil characteristics. Additionally, over time, in the same injector, variations may result from different operating conditions such as temperature and wear on the parts due to aging and other factors. Hence, the control of fuel quantity may vary from fuel injector to fuel injector, as well as over time with the same fuel injector. This also may lead to higher emissions and engine noise. Thus, injector shot-to-shot variations can occur on the same engine between multiple injectors.
The shot-to-shot variations mentioned above can cause idle stability issues that are detectable by the vehicle's operator and can cause decreased engine efficiency and increased emissions. Currently, manufacturing tolerances of the injector require sorting or rework to improve shot-to-shot variations.
Thus, there is a need to reduce injector shot-to-shot variations in an injection system by reducing the bounce of an armature of a control valve of the system.
An object of an embodiment is to fulfill the need referred to above. In accordance with the principles of the present invention, this objective is achieved by a method of controlling motion of an armature of a fuel injector. The armature is constructed and arranged to move between an open coil and a close coil of the injector. The method applies acceleration current of a certain polarity for a certain amount of time to the open coil with the armature disposed at the close coil. A de-latching current of a polarity opposite of that of the certain polarity is applied for a certain amount of time to the close coil to release magnetic latch on the armature thereby accelerating movement of the armature towards the open coil. A deceleration current is applied for a certain amount of time to the close coil thereby decelerating the armature prior to reaching the open coil. A latching current of the certain polarity is applied for a certain amount of time to the open coil prior to or just after impact of the armature with the open coil to magnetically latch the armature to the open coil thereby reducing bounce of the armature at impact.
In accordance with another aspect of an embodiment, a control system for controlling motion of an armature of a fuel injector includes at least one fuel injector having an armature constructed and arranged to move between an open coil and a close coil, and a controller constructed and arranged to apply 1) acceleration current of a certain polarity for a certain amount of time to the open coil with the armature disposed at the close coil, 2) de-latching current of a polarity opposite of that of the certain polarity for a certain amount of time to the close coil to release magnetic latch on the armature thereby accelerating movement of the armature towards the open coil, 3) deceleration current for a certain amount of time to the close coil thereby decelerating the armature prior to reaching the open coil; and 4) a latching current of the certain polarity for a certain amount of time to the open coil prior to or just after impact of the armature with the open coil to magnetically latch the armature to the open coil thereby reducing bounce of the armature at impact.
Other objects, features and characteristics of the present invention, as well as the methods of operation and the functions of the related elements of the structure, the combination of parts and economics of manufacture will become more apparent upon consideration of the following detailed description and appended claims with reference to the accompanying drawings, all of which form a part of this specification.
The invention will be better understood from the following detailed description of the preferred embodiments thereof, taken in conjunction with the accompanying drawings, wherein like reference numerals refer to like parts, in which:
With reference to
The fuel injector, generally indicated at 100, can be of the type disclose din U.S. Pat. No. 7,216,630 B2, the content of which is hereby incorporated by reference into this specification. The fuel injector 100 includes a control valve body 102 as well as an intensifier body 120 and a nozzle 140. The control valve body 102 includes an inlet area 104 which is in fluid communication with working ports 106. At least one groove or orifice (hereinafter referred to as grooves) 108 is positioned between and in fluid communication with the inlet area 104 and the working ports 106. At least one of vent hole 110 (and preferably two ore more) is located in the control body 102 which is in fluid communication with the working ports 106.
An armature 112, in the form of a spool, having at least one groove or orifice (hereinafter referred to as grooves) 114 is slidably mounted within the control valve body 102. An open coil 118 and a closed coil 116 are positioned on opposing sides of the armature 112 and are energized via a driver (not shown) to drive the armature 112 between a closed position and an open position. In the open position, the grooves 114 of the armature 112 are aligned with the grooves 108 of the valve control body 102 thus allowing the working fluid to flow between the inlet area 104 and the working ports 106 of the valve control body 102.
The intensifier body 120 is mounted to the valve control body 102 via any conventional mounting mechanism. A seal 122 (e.g., o-ring) may be positioned between the mounting surfaces of the intensifier body 120 and the valve control body 102. A piston 124 is slidably positioned within the intensifier body 120 and is in contact with an upper end of a plunger 126. An intensifier spring 128 surrounds a portion (e.g., shaft) of the plunger 126 and is further positioned between the piston 124 and a flange or shoulder 129 formed on an interior portion of the intensifier body 120. The intensifier spring 128 urges the piston 122 and the plunger 126 towards a first position proximate to the valve control body 102. A pressure release hole 130 is formed in the body of the intensifier body 120. The pressure release hole 130 may be further positioned adjacent the plunger 126.
As shown in
With reference to
Returning to
With reference to
As used herein, the “negative current” is a de-latching current of a polarity opposite of that of the acceleration current to release the armature 112 from the close coil 116, allowing an earlier motion and increase acceleration of the armature 112 toward the open coil 118. More particularly, on simple coil pole piece and armature, when the coil is energized, the coil pulls the armature to the coil. When electrical power is removed, the armature continues to be latched to the pole piece as the stored magnet field holds the parts. By applying an opposite polarity current (the negative current), the stored magnetic field is removed. The application of this negative current allows the opposite coil and pole piece assembly to pull armature with less magnetic resistance from unpowered coil resulting in faster acceleration and improved stability of motion.
The acceleration current D to open coil 118 can be stepped down to 20 amps at T2. Also at T2, a second application of negative current N2 (or deceleration current) is applied on the close coil 116 to decelerate the armature 112 by applying electromagnetic force on the close coil 116 when the armature is moving in the opposite direction toward the open coil 118. The polarity of the N2 is shown to be opposite that of the acceleration current D, but the polarity of N2 is immaterial once the magnetic field is drained from the close coil 116. The acceleration current D to open coil 118 can be stepped down to 12 amps at T3. Stepping-down of the current D helps control bounce of the armature 112. At T4, a peak pulse of 25 amps as a latching current is applied to the open coil 118 prior to or just after impact of the armature 112 with the open coil 118 to magnetically latch the armature 112 to the open coil 118 thereby eliminating or at least reducing the bounce of the armature 112 at impact.
As should be known to those of skill in the art, inductance is a property associated with the wire wound about the open coil or the closed coil. The origin of inductance is that the current flowing through the wire builds up a magnetic field around the wire. Energy is stored in this field and when the current changes in the coil, some energy must be transferred to or from the field which occurs by the field causing a voltage drop across the conductor while the current is changing. The voltage drop (back EMF) will be proportional to the derivative of the current change over time, and the sign of the voltage will be such as to try to resist the change in current. By monitoring this back EMF, an indication of the armature 112 travel and impact can be obtained (by knowing the current provided to the open coil and the distance the armature must travel to the open coil).
With reference to
Advantages of the embodiment include:
The foregoing preferred embodiments have been shown and described for the purposes of illustrating the structural and functional principles of the present invention, as well as illustrating the methods of employing the preferred embodiments and are subject to change without departing from such principles. Therefore, this invention includes all modifications encompassed within the scope of the following claims.
This application claims the benefit of the earlier filing date of U.S. Provisional Application No. 61/005,150, filed on Dec. 3, 2007, which is incorporated by reference herein in its entirety.
Number | Date | Country | |
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61005150 | Dec 2007 | US |