The present disclosure is directed to a control system and, more particularly, to a control system for a fuel injector.
Common rail fuel injectors provide a way to introduce fuel into the combustion chamber of an engine. Typical common rail fuel injectors include an actuating solenoid that opens a fuel injector nozzle when the solenoid is energized. Fuel is then injected into the combustion chamber as a function of the time period during which the solenoid remains energized. Accurate control of both the delivery timing and duration of fuel is important to engine performance and emissions.
To optimize engine performance and emissions, engine manufacturers may vary the times when the solenoid is energized and de-energized, as well as the magnitude of the current applied to the solenoid. One such example is described in U.S. Pat. No. 4,922,878 (the '878 patent) issued to Shinogle et al. on May 8, 1990. The '878 patent describes a solenoid control circuit that controls actuation of an injector control valve. The solenoid control circuit provides a three tier current waveform having a pull-in current level, a hold-in current level, and an intermediate current level. Energizing the solenoid at the pull-in level starts movement of the control valve and the flow of fuel to the engine. After the control valve starts to move, the current level is reduced to the intermediate level, which is less than the pull-in current level but great enough to continue movement of the control valve. The applied current is then further reduced to the hold-in level to hold the control valve at the moved position. The solenoid may then be de-energized to return the control valve to its initial position to stop the flow of fuel to the engine.
Although the solenoid control circuit of the '878 patent may sufficiently inject fuel into an engine, it may do little to minimize bouncing of the control valve and the resulting effects. In particular, due to inertia of the moving control valve and the associated fuel, upon fully opening, the control valve may tend to bounce away from an upper seat, thereby adversely affecting fuel delivery characteristics. Because the hold-in current of the '878 patent is single tiered, it may be insufficient to fully minimize control valve bouncing. Alternatively, if the hold-in current of the '878 patent is sufficient to minimize control valve bouncing, it may be inefficient for holding the control valve at the moved position after the tendency to bounce has decreased. In addition, the '878 patent does not adjust the tier levels to accommodate the effects of bouncing between closely coupled injections or dampen the closing movements of the control valve to minimize the likelihood of return bouncing.
The control system of the present disclosure solves one or more of the problems set forth above.
One aspect of the present disclosure is directed to a control system for a fuel injector. The control system includes a valve element movable between a first position and a second position, and an armature connected to the valve element. The control system includes a solenoid configured to move the armature and connected valve, and a controller in communication with the solenoid. The controller is configured to energize the solenoid at a first current level to initiate movement of the valve element from the first position toward the second position, thereby initiating an injection of fuel. The controller is also configured to energize the solenoid at a second current level less than the first current level during movement of the valve element from the first position toward the second position and to energize the solenoid at a third current level less than the second current level after the valve element has reached the second position. The controller is further configured to energize the solenoid at a fourth current level less than the third current level after the valve element has been in the second position for a predetermined period of time and to de-energize the solenoid to return the valve element to the first position, thereby stopping the injection of fuel.
Another aspect of the present disclosure is directed to a method of controlling a fuel injector having a solenoid and an armature connected to a valve element movable between a first position and a second position. The method includes energizing the solenoid at a first current level to initiate movement of the valve element from the first position toward the second position, thereby initiating an injection of fuel. The method also includes energizing the solenoid at a second current level less than the first current level during movement of the valve element from the first position toward the second position and energizing the solenoid at a third current level less than the second current level after the valve element has reached the second position. The method further includes energizing the solenoid at a fourth current level less than the third current level after the valve element has been in the second position for a predetermined period of time and de-energizing the solenoid to return the valve element to the first position, thereby stopping the injection of fuel.
Cylinder 16, piston 18, and cylinder head 20 may form a combustion chamber 22. In the illustrated embodiment, engine 10 includes six combustion chambers 22. However, it is contemplated that engine 10 may include a greater or lesser number of combustion chambers 22 and that combustion chambers 22 may be disposed in an “in-line” configuration, a “V” configuration, or any other suitable configuration.
As also shown in
Fuel system 12 may include components that cooperate to deliver injections of pressurized fuel into each combustion chamber 22. Specifically, fuel system 12 may include a tank 28 configured to hold a supply of fuel, a fuel pumping arrangement 30 configured to pressurize the fuel and direct the pressurized fuel to a plurality of fuel injectors 32 by way of a common rail 34, and a control system 35.
Fuel pumping arrangement 30 may include one or more pumping devices that function to increase the pressure of the fuel and direct one or more pressurized streams of fuel to common rail 34. In one example, fuel pumping arrangement 30 includes a low pressure source 36 and a high pressure source 38 disposed in series and fluidly connected by way of a fuel line 40. Low pressure source 36 may be a transfer pump configured to provide low pressure feed to high pressure source 38. High pressure source 38 may be configured to receive the low pressure feed and to increase the pressure of the fuel to the range of about 30–300 MPa. High pressure source 38 may be connected to common rail 34 by way of a fuel line 42. A check valve 44 may be disposed within fuel line 42 to provide for one-directional flow of fuel from fuel pumping arrangement 30 to common rail 34.
One or both of low pressure and high pressure sources 36, 38 may be operably connected to engine 10 and driven by crankshaft 24. Low and/or high pressure sources 36, 38 may be connected with crankshaft 24 in any manner readily apparent to one skilled in the art where a rotation of crankshaft 24 will result in a corresponding rotation of a pump drive shaft. For example, a pump driveshaft 46 of high pressure source 38 is shown in
Fuel injectors 32 may be disposed within cylinder heads 20 and connected to common rail 34 by way of a plurality of fuel lines 50. Each fuel injector 32 may be operable to inject an amount of pressurized fuel into an associated combustion chamber 22 at predetermined timings, fuel pressures, and fuel flow rates. The timing of fuel injection into combustion chamber 22 may be synchronized with the motion of piston 18. For example, fuel may be injected as piston 18 nears a top-dead-center position in a compression stroke to allow for compression-ignited-combustion of the injected fuel. Alternatively, fuel may be injected as piston 18 begins the compression stroke heading towards a top-dead-center position for homogenous charge compression ignition operation. Fuel may also be injected as piston 18 is moving from a top-dead-center position towards a bottom-dead-center position during an expansion stroke for a late post injection to create a reducing atmosphere for aftertreatment regeneration.
Control system 35 may control operation of each fuel injector 32. In particular, control system 35 may include a controller 53 that communicates with fuel injectors 32 by way of a plurality of communication lines 51. Controller 53 may be configured to control a fuel injection timing, amount, and duration by applying a predetermined current waveform or sequence of current waveforms to each fuel injector 32.
Controller 53 may embody in a single microprocessor or multiple microprocessors that include a means for controlling an operation of fuel injector 32. Numerous commercially available microprocessors can be configured to perform the functions of controller 53. It should be appreciated that controller 53 could readily embody a general work machine or engine microprocessor capable of controlling numerous work machine or engine functions. Controller 53 may include all the components required to run an application such as, for example, a memory, a secondary storage device, and a processor, such as a central processing unit or any other means known in the art for controlling fuel injectors 32. Various other known circuits may be associated with controller 53, including power supply circuitry, signal-conditioning circuitry, solenoid driver circuitry, communication circuitry, and other appropriate circuitry.
As illustrated in
Injector body 52 may embody a cylindrical member configured for assembly within cylinder head 20 and having one or more passageways. Specifically, injector body 52 may include a central bore 100 configured to receive solenoid actuator 59, a fuel inlet 102 and fuel outlet 104 in communication with central bore 100, and a control chamber 106. Control chamber 106 may be in communication with central bore 100 via a control passageway 108 and in direct communication with needle valve element 58. Control chamber 106 may be selectively drained of or supplied with pressurized fuel to affect motion of needle valve element 58. Injector body 52 may also include a supply passageway 110 that fluidly communicates central bore 100 with nozzle member 56.
Housing 54 may embody a cylindrical member having a central bore 60 for receiving guide 55 and nozzle member 56, and an opening 62 through which a tip end 64 of nozzle member 56 protrudes. A sealing member such as, for example, an o-ring (not shown) may be disposed between guide 55 and nozzle member 56 to restrict fuel leakage from fuel injector 32.
Guide 55 may also embody a cylindrical member having a central bore 68 configured to receive needle valve element 58 and a return spring 90. Return spring 90 may be disposed between a stop 92 and a seating surface 94 to axially bias needle valve element 58 toward tip end 64. A spacer 96 may be disposed between return spring 90 and seating surface 94 to reduce wear of the components within fuel injector 32. It is contemplated that an additional spacer (not shown) may be disposed between return spring 90 and stop 92 to further reduce component wear.
Nozzle member 56 may likewise embody a cylindrical member having a central bore 72 and a pressure chamber 71. Central bore 72 may be configured to receive needle valve element 58. Pressure chamber 71 may hold pressurized fuel supplied from supply passageway 110 in anticipation of an injection event. Nozzle member 56 may also include one or more orifices 80 to allow the pressurized fuel to flow from pressure chamber 71 through central bore 72 into combustion chambers 22 of engine 10, as needle valve element 58 is moved away from orifices 80.
Needle valve element 58 may be an elongated cylindrical member that is slidingly disposed within guide 55 and nozzle member 56. Needle valve element 58 may be axially movable between a first position at which a tip end of needle valve element 58 blocks a flow of fuel through orifices 80, and a second position at which orifices 80 are open to allow a flow of fuel into combustion chamber 22. It is contemplated that needle valve member 58 may be a multi-member element having a needle member and a piston member or a single integral element.
Needle valve element 58 may have multiple driving hydraulic surfaces. For example, needle valve element 58 may include a hydraulic surface 112 tending to drive needle valve element 58, with the bias of return spring 90, toward a first or orifice-blocking position when acted upon by pressurized fuel. Needle valve element 58 may also include a hydraulic surface 114 that opposes the bias of return spring 90 to drive needle valve element 58 in the opposite direction toward a second or orifice-opening position when acted upon by pressurized fuel.
Solenoid actuator 59 may be disposed opposite nozzle member 56 to control the forces on needle valve element 58. In particular solenoid actuator 59 may include windings 116 of a suitable shape through which current may flow to establish a magnetic field. Solenoid actuator 59 may also include an armature 118 fixedly connected to a two-position control valve element 120. When energized, the magnetic field established by windings 116 may urge armature 118 and connected control valve element 120 against the bias of a return spring 123 from a first or non-injecting position to a second or injecting position. For example, control valve element 120 may be moved between a lower seat 122 and an upper seat 124. In the non-injecting position, fuel may flow from fuel inlet 102 through control passageway 108 into control chamber 106. As pressurized fuel builds within control chamber 106, the downward force generated at hydraulic surface 112 combined with the force of return spring 90 may overcome the upward force at hydraulic surface 114, thereby closing orifices 80 and terminating fuel injection. In the injecting position, fuel may flow from control chamber 106 to tank 28 via a restricted orifice 121, central bore 100, and fuel outlet 104. As fuel from control chamber 106 drains to tank 28, the upward force at hydraulic surface 114 may urge needle valve element 58 against return spring 90, thereby opening orifices 80 and initiating fuel injection into combustion chambers 22. When de-energized, return spring 123 may return armature 118 and control valve element 120 to the non-injecting position.
The timing and level of the induced current within windings 116 may be controlled to affect fuel injection. For example, as illustrated in the control diagrams of
A current waveform associated with an exemplary injection event may also include dampening current levels. In particular, controller 53 may induce a fifth current level within windings 116 at time T7 to dampen or slow the movement of control valve element 120 prior to control valve element 120 reaching the injecting position (e.g., prior to time T8). The induced current may be of an appropriate level between zero and the current level at time T2. Dampening the closing movement of control valve element 120 just prior to time T8 may reduce the likelihood of control valve element 120 bouncing off of a lower seat 124. It is contemplated that instead of controller 53 inducing a fifth current, control valve element 120 may alternatively enter a freewheeling mode of operation where the kinetic energy of control valve element 120 is converted to electrical energy directed away from solenoid actuator 59 (freewheeling induced current indicated with a dashed line in
The current levels induced within windings 116 may be adjusted to dampen the movement of control valve element 120 toward the non-injecting position between time T3 and T4. In particular, the current level induced within windings 116 may be reduced just prior to control valve element 120 reaching upper seat 122 to decrease the likelihood of control valve element 120 bouncing away from upper seat 122 and to lessen the effects of the associated hydraulic inertia. The current level immediately following time T3 may be reduced to an amount sufficient to dampen the movement of control valve element 120 while allowing adequate time to induce the third current level at time T4 (referring to the dashed line in
In addition to dampening the movement of control valve element 120, operation of control valve element 120 in the freewheeling mode may provide an indication of the relative positions between control valve element 120 and lower seat 124. In particular, the time during which the current generated from the movement of control valve element 120 toward the non-injecting position may be measured during each movement cycle of control valve element 120. These time measurements may then be averaged to determine an approximate amount of time that it takes for control valve element 120 to move from the injecting position to the non-injecting position. It is noted that this average time may change depending on the previous injection duration, the time before the next injection, the injected amounts, and any other injection-related characteristics. An elapsed time may then be compared with the average amount of time to determine a distance remaining between control valve element 120 and lower seat 124 or a time remaining before control valve element 120 engages lower seat 124.
The relative position between control valve element 120 and lower seat 124 may be used to trigger the current induced within windings 116 that dampen the movement of control valve element 120 toward the injecting position. In particular, controller 53 may be configured to initiate and terminate the induced current intended to dampen the movement of control valve element 120 toward the injecting position before control valve element 120 reaches lower seat 124 in order to minimize the likelihood of a return bounce caused by the dampening current. For example, if the previously averaged time required for control valve element 120 to move from the injecting position to the non-injecting position is 350 μs and the desired dampening duration is 100 μs, controller 53 may induce the dampening current at 250 μs or earlier after control valve element 120 has left the non-injecting position to prevent control valve element 120 from return bouncing away from lower seat 124 as a result of the dampening current.
The fuel injector control system of the present disclosure has wide applications in a variety of engine types including, for example, diesel engines, gasoline engines, and gaseous fuel-powered engines. The disclosed fuel injector control system may be implemented into any engine where consistent fuel injector performance and efficiency are important. The operation of control system 35 will now be explained.
As indicated in a flow chart 200 of
Following the first injection, controller 53 may determine if a second injection event in a series of injection events is close-coupled (e.g., the time duration between the end of the first injection event and the start of the second injection event is less than a predetermined amount) (step 210). If the second injection event in a series of injection events is not close-coupled, the second injection event may be implemented in an identical manner to the first injection event by applying the first waveform to solenoid actuator 59.
However, if the second injection event is close-coupled, controller 53 may instead apply a second waveform to solenoid actuator 59. Specifically, in order to overcome the inertial effects of control valve element 120 returning to the non-injecting position and any associated bouncing, the first and/or second current levels of the second waveform may be increased from the current levels of the first waveform. In addition, because of the lack of time between the first injection event and the desired second close-coupled injection event, the application duration of the first one and/or two current levels of the second waveform may be reduced from the first waveform (step 220).
Following the second injection event in the series of injection events, controller 53 may again determine if a subsequent injection event is close-coupled (step 230). If the subsequent injection event is not close-coupled, controller 53 may return to injection using the first waveform. However, if the subsequent injection event is close-coupled, controller 53 may inject using the second waveform (step 240).
As illustrated in a flow chart 300 of
Because control system 35 can implement waveforms having multiple hold-in current levels, the tendency of control valve element 120 to bounce and the energy consumed during an injection event may be reduced. Specifically, because control system 35 can implement the third current level after time T4 when control valve element 120 has reached the injecting position, the likelihood of control valve element 120 bouncing away from upper seat 122 may be reduced. In addition, because control system 35 may reduce the current level induced within windings 116 to the fourth current level after time T5, when the likelihood of bouncing has been reduced, the amount of energy consumed during the injection event may be less than if the current level had remained at the higher third current level.
Further, because control system 35 can modify the waveforms when sequential injection events are close-coupled, the performance of fuel injectors 32 may be increased. In particular, because close-coupled injection events have different current level and duration requirements than injection events that are not close-coupled, these differences must be accommodated to produce consistent injections of fuel. Controller 53 may accommodate these differences by increasing the current level and decreasing the current duration of the subsequent close-coupled injection event.
In addition, because control system 35 implements dampening of control valve element 120, the components of fuel injector 32 may experience less wear and the performance of fuel injectors 32 may be improved. Dampening of the movement of control valve element 120 prior to impact with upper or lower seats 122, 124 may reduce the force of the impact and the likelihood of bouncing away from the seat. The reduction in force may result in increased component life. Further, reducing the likelihood of bouncing can improve injector consistency.
It will be apparent to those skilled in the art that various modifications and variations can be made to the control system of the present disclosure without departing from the scope of the disclosure. Other embodiments will be apparent to those skilled in the art from consideration of the specification and practice of the control system disclosed herein. It is intended that the specification and examples be considered as exemplary only, with a true scope of the disclosure being indicated by the following claims and their equivalents.
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