Patent Grant
10378501
The present disclosure relates to vehicle powertrain fuel delivery, and more particularly, to prognosis of valves for controlling fuel delivery.
Stricter emission regulations and increasing fuel economy requirements have been among the key driving forces that have led the automotive industry to constantly improve the efficiency of gasoline engines and to innovate to reduce harmful exhaust gas emissions. In prior years, port fuel injection (PFI) engines represented the state-of-the-art for production gasoline engines. In PFI engines, a plurality of fuel injectors deliver gasoline adjacent to each intake valve, and the fuel then mixes with incoming air and gets pulled into each combustion chamber when each intake valve opens. However, increasingly stringent fuel economy and emissions standards have prompted the use of spark ignition direction injection (SIDI) engines. In SIDI engines, fuel is injected directly into each combustion chamber at a high pressure during the compression stroke, reducing wall wetting and hence improving cold start hydrocarbon emissions. Direction injection (SIDI technology) reduces throttling loss of the gas exchange by stratified and homogenous lean operation, enables higher thermal efficiency by stratified operation and increased compression ratio, decreases the fuel consumption and CO2 emissions, lowers heat losses, enables fast heating of the catalyst by injection during the gas expansion phase, increases performance and volumetric efficiency due to cooling of air charge, and enables better cold start performance.
In SIDI engines, however, a carbon and/or dirt build-up may occur in the intake valves that reduces the airflow to the cylinders over time because fuel (containing cleaners) is no longer being sprayed into the intake valves. Breaking off of the built-up dirt or carbon can cause failure. In addition, failure of other SIDI components can cause the system to fail or to operate poorly. It is therefore desirable to diagnose problems with the fuel intake system prior to such failures.
The present disclosure provides a fuel delivery system, prognosis system, and method for conducting fuel pump prognosis that identifies an issue with the fuel pump control valve by monitoring current feedback and making a determination as to the mode of failure based on examining the current feedback. If the current feedback is low, a suspected bad electrical connection is indicated; and if the current feedback has a large peak-to-peak variation, a suspected weakened electromagnetic field is indicated.
In one form, which may be combined with or separate from the other forms disclosed herein, a method of conducting a fuel pump solenoid prognosis is provided. The method includes determining a solenoid current feedback of a fuel pump control solenoid and determining whether the solenoid current feedback is less than a predetermined low current threshold. The method further includes determining a magnitude of variation of the solenoid current feedback and determining whether the magnitude of variation of the solenoid current feedback exceeds a predetermined variation threshold. The method includes indicating a potential solenoid electrical connection fault if the solenoid current feedback is less than the predetermined low current threshold and less than the predetermined variation threshold; and the method includes indicating a potential solenoid weakened electromagnetic field fault if the solenoid current feedback is greater than the predetermined variation threshold.
In another form, which may be combined with or separate from the other forms disclosed herein, a fuel delivery system is provided that includes a fuel pump having a pumping chamber and a closeable inlet valve and a fuel rail configured to communicate pressurized fuel received from the fuel pump to at least one engine cylinder. A control system comprises a memory and an instruction set, where the instruction set is executable to: determine a current feedback of the closeable inlet valve; determine whether the current feedback is less than a predetermined low current threshold; determine a magnitude of variation of the current feedback; determine whether the magnitude of variation of the current feedback exceeds a predetermined variation threshold; indicate a potential valve electrical connection fault if the current feedback is less than the predetermined low current threshold and less than the predetermined variation threshold; and indicate a potential valve weakened electromagnetic field fault if the current feedback is greater than the predetermined variation threshold.
In yet another form, which may be combined with or separate from the other forms disclosed herein, a direct-inject fuel pump prognosis system is provided that includes a memory and an instruction set. The instruction set is executable to: determine a current feedback of a closeable inlet valve; determine a mean current based on the current feedback; determine whether the current feedback and/or the mean current is less than a predetermined low current threshold; determine a magnitude of variation of the current feedback; determine whether the magnitude of variation of the current feedback exceeds a predetermined variation threshold; determine whether the mean current is greater than a predetermined high current threshold; indicate a potential valve electrical connection fault if the current feedback is less than the predetermined low current threshold and less than the predetermined variation threshold; and indicate a potential valve weakened electromagnetic field fault if the current feedback is greater than the predetermined variation threshold and/or if the mean current is greater than the predetermined high current threshold.
Further additional features may be provided, including but not limited to the following: the control system, prognosis system, and method being configured to determine the solenoid current feedback by measuring an amount of current flowing through the fuel pump control solenoid (or closeable inlet valve) at a range of operating conditions and normalizing the amount of current flowing through the fuel pump control solenoid (or closeable inlet valve) against the range of operating conditions; the control system, prognosis system, and method being configured to determine a plurality of control signal adjustment gain values applied to a control signal for controlling the fuel pump control solenoid (or closeable inlet valve) and normalize the plurality of control signal adjustment gain values against the range of operating conditions to define a set of normalized control signal adjustment gain values; the control system, prognosis system, and method being configured to indicate a deviating control signal adjustment if any normalized control signal adjustment gain value of the set of normalized control signal adjustment gain values lies outside of a predetermined desired gain range and to indicate a normal control signal adjustment if the set of normalized control signal adjustment gain values lies inside of the predetermined desired gain range; and the control system, prognosis system, and method being configured to indicate a potential bad current sensing fault if the normal control signal adjustment is indicated and at least one of the potential solenoid electrical connection fault and the potential solenoid weakened electromagnetic field fault is indicated.
Further additional features may be included, including but not limited to the following: wherein determining the solenoid current feedback includes calculating a mean and a standard deviation of a difference between an actual solenoid current feedback signal and an expected solenoid current feedback signal; the control system, prognosis system, and method being configured to energize the fuel pump control solenoid (or the closeable inlet valve) to hold the fuel pump control solenoid closed during a hold timeframe and deenergize the fuel pump control solenoid (or the closeable inlet valve) to begin a solenoid off timeframe; and wherein determining the solenoid current feedback is performed at one of the following times: a) at the start of the solenoid off timeframe; and b) during the hold timeframe.
Additional further details may be provided, including but not limited to the following: the control system, prognosis system, and method being configured to issue a potential solenoid electrical connection fault warning message if the potential solenoid electrical connection fault is indicated, issue a potential solenoid weakened electromagnetic field fault warning message if the potential solenoid weakened electromagnetic field fault is indicated, and/or issue a potential bad current sensing fault warning message if the potential bad current sensing fault is indicated; the fuel delivery system further comprising a low-pressure supply pump configured to provide fuel to the (high pressure) fuel pump; the control system, prognosis system, and method being configured to determine whether a mean current is greater than a predetermined high current threshold; and the control system, prognosis system, and method being configured to indicate the potential solenoid weakened electromagnetic field fault if the mean current is greater than the predetermined high current threshold.
Embodiments and examples of the present disclosure are described herein. It is to be understood, however, that the disclosed embodiments are merely examples and other embodiments can take various and alternative forms. The figures are not necessarily to scale; some features could be exaggerated or minimized to show details of particular components. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a representative basis for teaching one skilled in the art to variously employ aspects of the present disclosure. As those of ordinary skill in the art will understand, various features illustrated and described with reference to any one of the figures can be combined with features illustrated in one or more other figures to produce embodiments that are not explicitly illustrated or described. The combinations of features illustrated provide representative embodiments for typical applications. Various combinations and modifications of the features consistent with the teachings of this disclosure, however, could be desired for particular applications or implementations.
Referring to
Each cylinder 22 receives pressurized fuel from the fuel rail 20 and the fuel is dispersed into the cylinder by a fuel injector 24. Air is also supplied to each cylinder 22 through an air valve (not shown) to be mixed with the pressurized fuel to create a desirable fuel-to-air ratio to facilitate optimal fuel combustion. The combustion within each cylinder 22 drives a piston 26 which in turn rotates a crankshaft 28 to output torque from the engine 14.
In the illustrated example, the engine 14 is a spark ignition direction injection (SIDI) engine. Pressurized fuel from each injector 24 is directly sprayed into a corresponding cylinder 22 to mix with air once inside of the cylinder 22 as opposed to being pre-mixed before injection. Direct injection of pressurized fuel into the cylinders 22 enhances the ability to send precise amounts of fuel to the cylinders 22 at exact timing intervals.
The high-pressure pump 18 may generate fuel pressure delivered to the fuel rail 20 at up to about 2,500 psi (in some examples, the pressure may be in a range of 1 to 20 MPa). The high-pressure fuel pump 18 is driven by a camshaft 34 and is operable to vary the fuel output to satisfy engine demand. The camshaft 34 is mechanically linked to the crankshaft 28 such that the rotational speed of the camshaft 34 is related to the rotations per minute (RPM) of the output of the crankshaft 28 of the engine 14.
The various fuel delivery components discussed herein may have one or more associated controllers to control and monitor operation. Controller 32, although represented as a single controller, may be implemented as one controller, or as system of controllers in cooperation to collectively manage fuel delivery. Multiple controllers may be in communication via a serial bus (e.g., Controller Area Network (CAN)) or via discrete conductors. In further examples, at least a portion of the control function is performed by an off-board processing element which is external to the vehicle. The controller 32 is programmed to coordinate the operation of the various fuel delivery components. The fuel demand of the engine 14 required to output torque varies based at least on driver demand indicated by input at an accelerator pedal 30. An accelerator pedal sensor provides a pedal position signal to the controller 32. In addition, or in the alternative, such as in the case of an autonomous or self-driving vehicle, throttle position information may be provided to the controller 32 in lieu of a pedal position influenced by a driver. The controller 32 also monitors operating conditions of the low-pressure supply fuel pump 16, the high-pressure fuel pump 18, fuel rail 20, fuel injectors 24, and/or the cylinders 22. The low-pressure fuel supply pump 16 may include sensors to provide the controller 32 with information regarding the amount of fuel supplied to the high-pressure fuel pump 18. The high-pressure fuel pump 18 includes one or more sensors, discussed in more detail below, which provide feedback information to the controller 32 regarding pump operation. Fuel outlet pressure may be measured by a pressure sensor directly at the outlet of the high-pressure pump 18. The controller 32 may also be in communication with one or more additional pressure sensors 60 along the fuel rail 20 to monitor fuel pressure at other locations in the fuel delivery system 10. In addition, the controller 32 may determine the desired fuel pressure for delivery to the engine 14 as a pressure set point.
The high-pressure pump 18 may be a standalone unit that is mechanically actuated. The high-pressure fuel pump 18 includes a pumping chamber 36 configured to accumulate a pressure rise in fuel within the chamber 36. The high-pressure pump 18 may be directly or indirectly driven by engine output (e.g., crankshaft 28). In the illustrated example, the camshaft 34 drives the high-pressure pump 18, which is operatively coupled to the output rotation (e.g., crankshaft 28) of the engine 14. A plunger 38 is biased against the camshaft 34 by a spring 40. The rotation of the camshaft 34 actuates the high-pressure fuel pump 18 when one or more lobes 42 of the camshaft 34 reciprocally actuate the plunger 38 along an actuation direction depicted by arrow 44. In one example, the camshaft 34 defines a three-lobe cam such that the high-pressure fuel pump 18 cycles at a proportionally higher rate relative to output RPM of the engine crankshaft 28. As the plunger 38 moves, the available volume within the pumping chamber 36 changes, either allowing fuel to be drawn in, or forcing fuel to be expelled following the pressure rise. In alternate examples, the high-pressure pump 18 may be driven by gears or toothed belts. Additionally, the high-pressure pump 18 may be hydraulically actuated using fluid flow of engine oil or fuel.
There are generally two operation states for the high-pressure fuel pump 18. First, a suction stroke causes low-pressure fuel to be drawn into the pumping chamber 36 from the supply pump 16. A fuel pump control solenoid 46, which is a closeable inlet valve, is used to control fuel entering into the pumping chamber 36 based on the desired pressure increase, or target pressure set point. In one example, the solenoid valve 46 is configured to be normally open when de-energized. However it is contemplated that the reverse configuration of a solenoid valve may be used where the solenoid valve is normally closed when de-energized. In either case, the solenoid valve 46 is caused to remain open during the suction stroke to allow fuel to flow into the pumping chamber 36. Conversely, fuel may flow back toward the low-pressure pump 16 and the sump 12 when the solenoid valve 46 is open and the plunger 38 rises.
As the camshaft 34 rotates, the plunger 38 is actuated to compress the fuel within the pumping chamber 36 to increase fuel pressure. Specifically, as the camshaft lobe 42 rotates to cause the plunger 38 to rise to a maximum position, the plunger 38 reduces the volume within the pumping chamber 36, compressing fuel present inside the pumping chamber 36. The plunger 38 is sealed to an opening 47 through a portion of the pumping chamber 36 by one or more seals 48. In one example, the seal 48 is arranged as a sleeve surrounding the plunger 38. In alternative examples, the seal 48 may be configured as an O-ring seal.
In order to facilitate the pressure rise, the solenoid valve 46 is energized (or conversely de-energized) to close off fuel flow between the low-pressure fuel pump 16 and the pumping chamber 36. When the solenoid valve 46 is closed, pressure rises as the plunger 38 moves upward (in the orientation of
The pressure rise generated within the pumping chamber 36 may be generally described by equation (1) below:
where dP/dt represents the pressure rise or change; V(t) is the volume of the pumping chamber 36 as a function of time; B is the bulk modulus of the fuel within the pump 18; Qin is the flow rate into the pump through inlet fuel line 52; Qout is the outlet flow rate through the check valve 50 and outlet fuel line 54; and Qleak is the loss flow rate due to fuel pump leakage, for example from a degraded seal (e.g., seal 48).
The timing of the closing of the inlet solenoid valve 46 has a significant effect upon the amount of pressure rise developed within the pumping chamber 36. That is, there is a relationship between pump pressure, position of camshaft 34, and the state of the inlet solenoid valve 46. These elements influence opening time of the injectors 24 and can be calibrated to provide optimal performance and component life. Controller 32 is programmed to issue control signals to periodically close the inlet solenoid valve 46 at the exact time required to build desired pressure corresponding to demand of the engine 14. By precisely controlling the inlet solenoid valve 46 timing, the controller 32 may influence both of the volume and fuel outlet pressure for each pulse. When direct injection is operating properly, the high-pressure fuel pump 18 rapidly and precisely pulses fuel to the injector 24 to create the most optimal fuel-to-air mixture.
A relief valve 56 may be provided as an internal return line to compensate for excessive pressure created by the high-pressure fuel pump 18. The relief valve 56 is in fluid communication with the outlet fuel line 54 downstream of the check valve 50. In response to pressure in the outlet fuel line 54 exceeding a pressure limit threshold, the relief valve 56 opens and returns fuel to the inlet fuel line 52.
The response time of the actuation of the solenoid valve 46 may be degraded by a number of factors. Solenoid wear may cause increased mechanical resistance opposing the actuation of the solenoid valve 46. The controller 32 may be programmed to automatically adjust control signal gain to change the actuation timing of the solenoid valve 46. In one example, the control signal gain is increased to alter the timing of the solenoid valve 46 to open it sooner to capture a desired amount of fuel within the pumping chamber 36. However, there may be a limit to the timing adjustment that may be applied to the solenoid valve 46 to compensate for wear. At some point, continually opening the solenoid valve 46 sooner no longer improves response time for overcoming wear issues.
A second cause of degraded response time of the solenoid valve 46 may be leakage of the high-pressure fuel pump 18. As discussed above, loss in fuel pressure may be caused by degradation in the seal(s) 48 between the plunger 38 and the pumping chamber 36. As fuel leaks past the plunger 38 and escapes the high-pressure pump 18, a pressure drop is caused in the pumping chamber 36. Due to the leakage, the solenoid valve 46 may need to be held open longer to allow more fuel to accumulate within the chamber 36. Referring back to equation (1) above, Qin may be increased in order to compensate and maintain the same pressure rise in the pumping chamber 36 in spite of a fuel pump leak. The controller 32 may be programmed to automatically adjust the control signal gain to modify the open time of the solenoid valve 46 to compensate for leakage. In this case the control signal gain may be adjusted in order to increase the solenoid valve open time duration during a cycle.
The controller 32 may be programmed to receive a pressure signal from a sensor 58 that is indicative of fuel pressure downstream of the fuel pump 18. In one example, the sensor 58 is arranged to read pressure of the fuel outlet flow through the outlet fuel line 54. In other examples, the pressure of the flow through the fuel rail 20 may be sensed to provide the controller 32 with information about performance of the fuel pump 18. The controller 32 may be further programmed to adjust a control signal gain value based on the pressure signal from the sensor 58. The controller 32 may adjust the control signal gain value in response to deviation in the outlet fuel pressure relative to the fuel pressure set point.
In one example, if fuel pump output fuel pressure deviates from the pressure set point by a shutdown threshold value, the controller 32 may recognize a severe fault and cause a deactivation of the high-pressure fuel pump 18. In this case, the powertrain may operate in a low-pressure “limp” mode where the inlet solenoid valve 46 is caused to remain open such that fuel is provided to the fuel rail 20 under pressures as delivered by the low-pressure supply pump 16. As discussed above, the solenoid valve 46 may be configured to remain open while de-energized or alternatively require energy to remain in the open state. In the limp mode, the powertrain remains operable, but performance of the engine 14 is reduced.
If a deviation in the pressure rise created by the high-pressure pump 18 deviates from the pressure set point by less than the shutdown threshold, the controller 32 may operate the pump 18 utilizing modified control gains to adjust the solenoid valve 46 timing to maintain the fuel outlet pressure as close to the pressure set point as possible. However, such deviations may be an indication of degrading performance of the high-pressure fuel pump 18 and a precursor to ultimate pump failure.
Referring now to
As discussed above, the controller 32 is programmed to adjust the gain value of the control signal if the output pressure of the high-pressure fuel pump 18 deviates from the pressure set point. The adjustment compensates for changes in pump performance over time in order to deliver necessary fuel output to match the pressure set point. In the example of
In the illustrated example, when the applied control system gain is within a nominal region, such as gain region 106, the fuel delivery system 10 is functioning properly. If the control signal is adjusted by the controller 32 to a value greater than a gain value k1, which is outside of a threshold gain region 106, this could be indicative of an issue with the pump 18 and/or the solenoid valve 46. The gain value k1 corresponds to a degraded solenoid response time T2. A region 110 (between k1 and k2) may indicate a need to service one or more components of the fuel delivery system 10 soon. If repair service is not performed and the solenoid response time continues to increase, a failure may be imminent, such as when the control gain signal exceeds k2 at response time T3. The gain value within the range indicated by gain region 112 (between k2 and k3) represents an operating band in which failure is imminent. In the continued absence of service, the gain value k may continue to be adjusted corresponding to a degraded solenoid response time. However there is an upper limit to which the gain value may be adjusted and maintain solenoid valve operation. For example, a critical gain value k3 is the failure threshold where the solenoid valve 46 becomes inoperable. At operating conditions at about location 114, the fuel pump 18 may fail due to requiring gain values outside of the authority of the controller 32. In one example, the controller 32 may deactivate the high-pressure fuel pump 18 and enter limp home mode as discussed above, delivering fuel by the low-pressure supply fuel pump 16 only. A series of warning messages may be sent to a vehicle operator, system, or technician when each of the gain thresholds k1, k2, k3 are crossed.
Although the plot 100 of
The solenoid valve 46 is energized by a control signal from the controller 32, which may be in the form of a pulse width modulation (PWM) signal. A typical voltage profile to energize the solenoid valve 46 is illustrated in
As will be described in further detail below, a solenoid current feedback may be measured or detected and used to diagnose the solenoid valve 46. For example, the solenoid current feedback may be used to conduct a prognosis of certain failure modes of the solenoid valve 46. The controller 32 may be further programmed to provide an owner and/or service technician with any of a number of messages about the suspected failure mode of the solenoid valve 46.
Referring back to
Referring now to
With reference to
Bad Electrical Connection
Corrosion of the solenoid valve 46 connectors, or a generally loose connection, can cause electrical resistance to increase in the electrical pathway to the solenoid valve 46 in the pump circuit. Such a phenomenon is referred to herein as a bad electrical connection. Referring to
Referring now to
As can be seen in
Referring now to
Weakened Electromagnetic Field
Electric current through the electromagnetic coil 62 of the solenoid valve 46 results in joule heating of the coil 62. Joule heating causes expansion of the electromagnetic coil 62 and induces relative motion from layer to layer (in the radial direction) and turn to turn (in the axial direction). The sheer stress on the insulator film of the electromagnetic coil 62, due to relative motion from thermal expansion and contraction, can gradually wear down the insulation film and eventually result in short circuiting of the electromagnetic windings 64 (shown in
When the electromagnetic field is weakened, the charging and discharging occurs at a faster rate. Within a fixed charging and discharging time window, faster response results in larger peak-to-peak variation in the current feedback signal. Referring to
As can be seen in
In addition, a mean current 650 of the plot 604 of the circuit having the weakened electromagnetic field is greater than a mean current 652 of the plot 602 of the normally functioning solenoid. Therefore, if the mean current has increased beyond a nominal threshold, a solenoid fault can be identified as a short circuiting of the electromagnetic coil windings 64, which may also be referred to as a weakened electromagnetic field fault herein.
In some cases, when the electromagnetic coil windings 64 are shorted, a short circuit inductance loop may occur. In that case, the current feedback may not have a significant amount of peak-to-peak variation, but the mean 650 will still be above a predetermined threshold. Accordingly, if the solenoid current does not have a large peak-to-peak variation in current, but it does have a mean 650 exceeding a predetermined high current threshold, a solenoid fault could be identified as a shorted coil fault or a weakened electromagnetic field fault.
Referring now to
Referring now to
In step 802, the method 800 includes a step or control logic configured to determine a solenoid current feedback of a fuel pump control solenoid, such as the solenoid valve 46. The current feedback may be collected across various operating conditions, which may include temperature, engine speed, injector pulse width, and desired fuel pressure, by way of example. As explained above, the current feedback may be collected by measuring or detecting an amount of current flowing through the solenoid valve 46, at a range of operating conditions including engine speeds. The current feedback may then be normalized against the range of operating conditions, if desired. In some cases, the current feedback may be determined by calculating an average and a standard deviation of a difference between an actual solenoid current feedback signal and an expected solenoid current feedback signal. The current feedback may be collected at the beginning of the solenoid off timeframe, such as in window w shown in
In step 804, the method 800 includes a step or control logic configured to determine a magnitude of variation of the solenoid current feedback. To determine the magnitude, the current feedback may be collected across various operating conditions, which may include temperature, engine speed, injector pulse width, and desired fuel pressure, by way of example. The magnitude of the current feedback may then be normalized against the range of operating conditions, if desired.
The method 800 then includes a step or control logic 806 configured to determine whether the magnitude of variation of the solenoid current feedback exceeds a predetermined variation threshold. For example, with reference to
Furthermore, in step 806, a determination may be made as to whether a solenoid current feedback mean or average has increased above a predetermined high current threshold. For example, with reference to
In step 808, the method 800 and/or prognosis system are configured to determine whether the solenoid current feedback is less than a predetermined low current threshold. For example, with reference to
In step 810, the method 800 and/or prognosis system are configured to indicate a potential solenoid weakened electromagnetic field fault (if the solenoid current feedback is greater than the predetermined variation threshold and/or the mean exceeds the predetermined high current threshold, as indicated along path 809). In step 814, the method 800 and/or prognosis system are configured to indicate a potential solenoid electrical connection fault if the solenoid current feedback is less than the predetermined current threshold and less than the predetermined variation threshold (as indicated along paths 807 and 813).
Referring now to
In step 902, the method 900 includes a step or control logic configured to determine a solenoid current feedback of a fuel pump control solenoid, such as the solenoid valve 46. The current feedback may be collected across various operating conditions, which may include temperature, engine speed, injector pulse width, and desired fuel pressure, by way of example. As explained above, the current feedback may be collected by measuring or detecting an amount of current flowing through the solenoid valve 46, at a range of operating conditions including engine speeds. In some cases, the current feedback may be determined by calculating an average and a standard deviation of a difference between an actual solenoid current feedback signal and an expected solenoid current feedback signal. The current feedback may be collected at the beginning of the solenoid off timeframe, such as in w shown in
In a step 904, the collected current feedback may then be normalized against the range of operating conditions, if desired.
In step 906, the method 900 is configured to determine whether the current feedback is deviating from nominal or normal. To determine deviation, the current feedback may be compared against the predetermined current threshold and the predetermined variation threshold, by way of example. If the current feedback is not deviating from normal, the method 900 is configured to proceed along path 907 back to step 902 to monitor current feedback. If, however, the current feedback is deviating from normal, the method 900 proceeds along path 909 to step 910.
In step 910, the method 900 and/or control/prognosis system is configured to determine whether the control adjustment is deviating from nominal or normal. The control adjustment may be considered to deviate from normal or nominal if the adjustment k is greater than expected, such as shown in
If the control adjustment k is not deviating from normal (i.e., is normal), as determined in step 910, but the current feedback is deviating from normal, as determined in step 906, the control logic arrives at step 912. In step 912, it is determined or indicated that bad current sensing is suspected, which could be a possible ECU fault.
If in step 910 it is determined that the control adjustment is deviating from normal, the method 900 proceeds from step 910 along path 913 to step 914. In step 914, the method 900 includes a step or control logic configured to determine whether the solenoid current feedback has a large variation and/or whether the mean of the feedback current has increased beyond a predetermined high current threshold.
This may be determined, for example, by first determining a magnitude of variation of the solenoid current feedback and then determining whether the magnitude of variation of the solenoid current feedback exceeds a predetermined variation threshold. For example, with reference to
Furthermore, in step 914, the method 900 and/or control/prognosis system may be configured to determine whether a solenoid current feedback mean or average has increased above a predetermined high current threshold. For example, with reference to
If the magnitude does exceed the predetermined variation threshold or the mean of the current feedback is indeed greater than the predetermined high current threshold, the method 900 proceeds along path 915 to step 916.
Although the step 914 may make a determination about whether the current exceeds the predetermined variation threshold and whether the mean current exceeds the predetermined high current threshold, it should be understood that in some variations, only one or the other may be compared against, or these comparisons may be broken out into separate steps.
In step 916, the method 900 and/or control/prognosis system are configured to indicate a potential solenoid weakened electromagnetic field fault. This could mean that the solenoid coil 62 is short circuiting.
If, however, in step 914, it is determined that the magnitude, or variation in peak-to-peak current, does not exceed the predetermined variation threshold and/or does not have a large variation and/or has not increased, the method 900 may proceed from step 914 along path 917 to step 918.
In step 918, the method 900 and/or control/prognosis system are configured to determine whether the solenoid current feedback has decreased below a predetermined low current threshold. For example, with reference to
In step 920, the method 900 and/or control/prognosis system are configured to indicate a potential solenoid electrical connection fault if the solenoid current feedback is less than the predetermined low current threshold, as indicated along path 919. If in step 918, however, it is determined that the current feedback is not less than the predetermined low current threshold, the method 900 may proceed along path 921 to step 922.
In step 922, the method 900 or control/prognosis indicates a fault or malfunction due to an unknown failure mode, which could be an ECU malfunction. The method 900 may then proceed along path 923 back to step 902. The method 900 may also proceed back to step 902 from any of the other final steps 912, 916, 920.
Warning messages based on the particular faults may be sent to the driver, the vehicle computer/controller, and/or to any other vehicle health management system, tools, or persons (such as a service technician). Any number of varying degree severity messages may be generated based on the solenoid feedback current detected. For example, multiple levels of warnings may be provided prior to generating an imminent failure message, where each level may include a different severity indicator. Further, different severity warning messages may have a specific combination of one or more recipients such as a driver, service technician, vehicle fleet operator, or vehicle manufacturer for example. The warning messages may include what type of fault is indicated, such as a potential weakened electromagnetic field fault, a potential solenoid electrical connection fault, a bad current sensing fault, and/or an unknown failure mode. For example, the method and/or control/prognosis system may be configured to: issue a potential solenoid electrical connection fault warning message if the potential solenoid electrical connection fault is indicated, issue a potential solenoid weakened electromagnetic field fault warning message if the potential solenoid weakened electromagnetic field fault is indicated, and/or issue a potential bad current sensing fault warning message if the potential bad current sensing fault is indicated.
The processes, methods, or algorithms disclosed herein can be deliverable to, and/or implemented by a processing device, controller, or computer, which can include any existing programmable electronic control unit or dedicated electronic control unit. Similarly, the processes, methods, or algorithms can be stored as data and instructions executable by a controller or computer in many forms including, but not limited to, information permanently stored on non-writable storage media such as ROM devices and information alterably stored on writeable storage media such as floppy disks, magnetic tapes, CDs, RAM devices, and other magnetic and optical media. The processes, methods, or algorithms can also be implemented in a software executable object. Alternatively, the processes, methods, or algorithms can be embodied in whole or in part using suitable hardware components, such as Application Specific Integrated Circuits (ASICs), Field-Programmable Gate Arrays (FPGAs), state machines, controllers or other hardware components or devices, or a combination of hardware, software and firmware components. Such example devices may be onboard as part of a vehicle computing system or be located off-board and conduct remote communication with devices on one or more vehicles.
While exemplary embodiments are described above, it is not intended that these embodiments describe all possible forms encompassed by the claims. The words used in the specification are words of description rather than limitation, and it is understood that various changes can be made without departing from the spirit and scope of the disclosure. As previously described, the features of various embodiments can be combined to form further embodiments of the invention that may not be explicitly described or illustrated. While various embodiments could have been described as providing advantages or being preferred over other embodiments or prior art implementations with respect to one or more desired characteristics, those of ordinary skill in the art recognize that one or more features or characteristics can be compromised to achieve desired overall system attributes, which depend on the specific application and implementation. These attributes can include, but are not limited to cost, strength, durability, life cycle cost, marketability, appearance, packaging, size, serviceability, weight, manufacturability, ease of assembly, etc. As such, embodiments described as less desirable than other embodiments or prior art implementations with respect to one or more characteristics are not outside the scope of the disclosure and can be desirable for particular applications.
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