The present disclosure relates to vehicle powertrain fuel delivery.
Fuel delivery to an internal combustion engine affects engine performance and may be regulated by one or more fuel pumps to draw fuel from a tank. A number of components arranged between the fuel tank and an engine combustion chamber facilitate precise delivery of fuel to the engine. Failure of any of the intermediate components can affect proper fuel delivery and degrade engine performance.
An engine fuel delivery system includes a fuel pump having a pumping chamber to increase fuel pressure and a closeable inlet valve. The fuel delivery system also includes a fuel rail to communicate pressurized fuel received from the fuel pump to at least one engine cylinder. The engine fuel delivery system further includes a controller programmed to issue a control signal to periodically close the inlet valve to generate a setpoint fuel pressure within the pumping chamber. The controller is also programmed to adjust a control signal gain value in response to deviation in an outlet fuel pressure relative to the setpoint fuel pressure. The controller is further programmed to issue a warning message in response to the control signal gain being adjusted by more than a predetermined threshold from a calibrated gain value.
A method of conducting fuel pump prognosis includes issuing a control signal to periodically actuate a fuel pump solenoid valve based on an engine RPM. The method also includes applying a gain value to the control signal to change a timing of actuation of the fuel pump solenoid based on a fuel output pressure setpoint corresponding to engine fuel demand. The method further includes adjusting the gain value in response to fuel output pressure deviating from the pressure setpoint. The method further includes issuing an imminent failure warning message in response to the gain value being adjusted by more than a predetermined threshold.
A direct-inject fuel pump prognosis system includes a solenoid inlet valve operable to regulate a fuel inlet flow into the fuel pump and a sensor to provide a pressure signal indicative of fuel pressure downstream of the fuel pump. The fuel pump prognosis system also includes a controller programmed to issue a control signal to actuate the solenoid inlet value to create a pressure rise within the fuel pump to satisfy an engine demand. The controller is also programmed to adjust a control signal gain value based on the pressure signal from the sensor. The controller is further programmed to issue a prognosis message indicative of a fuel pump state of health based on the control signal gain value.
Embodiments 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 the present invention. 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 crankshaft 28 to output torque from the engine. According to aspects of the disclosure, pressurized fuel from each injector 24 is directly sprayed into a corresponding cylinder 22 to mix with air once inside of the cylinder as opposed to being pre-mixed before injection. Direct injection of pressurized fuel into the cylinders enhances the ability to send precise amounts of fuel to the cylinders 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. 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 each shaft is related to the rotations per minute (RPM) of the output of 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 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. According to aspects of the present disclosure, fuel outlet pressure is measured by a pressure sensor directly at the outlet of the high-pressure pump 18. The controller may also be in communication with one or more additional pressure sensors 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 as a pressure setpoint.
Referring to
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 solenoid inlet valve 46 is used to control fuel entering into the pumping chamber 36 based on the desired pressure increase, or target pressure setpoint. 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 valve is normally closed when de-energized. In either case, the valve is caused to remain open during the suction stroke to allow fuel to flow into the pumping chamber 36.
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 pump. 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 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 fuel is compressed. Once pressure within the pumping chamber 36 builds to a sufficient level which exceeds a pressure threshold, the fuel flow overcomes a check valve 50 allowing the pressurized fuel to exit the pump 18 and be delivered to the fuel rail 20.
The pressure rise generated within the pumping chamber 36 may be generally described by equation (1) below.
As noted in equation (1), 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. 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 fuel pulses 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 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 rapidly and precisely pulses fuel to the injector to create the most optimal fuel-to-air mixture.
A relief valve 56 is 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 flow connection to 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 may be degraded by a number of factors. Solenoid wear may cause increased mechanical resistance opposing the actuation of the solenoid valve. The controller may be programmed to automatically adjust control signal gain to change the actuation timing of the solenoid valve. In one example, the control signal gain is increased to alter the timing of the solenoid valve to open it sooner to capture a desired amount of fuel within the pumping chamber. However there may be a limit to the timing adjustment that may be applied to the solenoid valve to compensate for wear. At some point, continually opening the solenoid valve sooner no longer improves response time for overcoming wear issues.
A second cause of degraded response time of the solenoid valve may be leakage of the high-pressure fuel pump. As discussed above, loss in fuel pressure may be caused by degradation in the seals between the plunger and the pumping chamber. As fuel leaks past the plunger and escapes the high-pressure pump, a pressure drop is caused in the pumping chamber. Due to the leakage, the solenoid valve may need to be held open longer to allow more fuel to accumulate within the chamber. Referring back to equation (1) above, Qin may be increased in order to compensate and maintain the same pressure rise in the pumping chamber in spite of a fuel pump leak. The controller may be programmed to automatically adjust the control signal gain to modify the open time of the solenoid valve 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.
Referring back to
In one example, if fuel pump output fuel pressure deviates from the pressure setpoint 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 valve 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 engine 14 performance is reduced.
If a deviation in the pressure rise created by the high-pressure pump 18 deviates from the pressure setpoint by less than the shutdown threshold, the controller 32 may operate the pump 18 utilizing modified control gains to adjust solenoid 46 timing to maintain the fuel outlet pressure as close to the pressure setpoint as possible. However, such deviations may be an indication of degrading performance of the high-pressure fuel pump 18 and ultimately pump failure. According to aspects of the present disclosure, the control gains applied to the high-pressure fuel pump 18 to optimize operation may be used to conduct a prognosis of the operational life of the fuel pump. The controller 32 may be further programmed to provide an owner and/or service technician with any of a number of messages about the operational life of the high-pressure pump 18. Further, the type of gain adjustment may correspond to a particular type of failure mode and enhance the available specificity of the message generated.
Referring to
As discussed above, the controller is programmed to adjust the gain value of the control signal based on the output pressure of the high-pressure fuel pump deviating from the pressure setpoint. The adjustment compensates for changes in pump performance over time in order to deliver necessary fuel output to match the pressure setpoint. In the example of
The controller may be programmed to issue a fuel delivery system state of health message based on the value of the control signal gain k applied to the solenoid valve. When the applied control system gain is within a nominal region such as gain region 106, the message may be indicative of a properly functioning fuel delivery system. The state of health message may include information about the remaining useful life of various fuel system components. The state of health message may be provided to a driver via a user display in the vehicle. Alternatively, the state of health message may be provided by an external processor portion of the controller and sent to a user's mobile device, a user's computer, a vehicle service sever, or any number of different external processors.
The controller is also programmed to issue a first warning message in response to the control signal gain k being adjusted by more than a predetermined threshold amount from the calibrated gain value k0. With continued reference to the example of
If repair service is not performed and the solenoid response time continues to increase, a more severe message is issued that is indicative of an imminent failure. The controller is programmed to issue an imminent failure warning message in response to the gain value deviating from the calibrated gain value by a predetermined threshold amount. In the example of
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 becomes inoperable. At operating conditions at about location 114, the fuel pump may fail due to requiring gain values outside of the authority of the controller. In one example the controller may deactivate the high-pressure fuel pump and enter limp home mode as discussed above, delivering fuel by the supply fuel pump only.
Although the plot of
While a first warning message is discussed as preceding an imminent failure message, it is contemplated that any number of varying degree severity messages may be generated based on the trends of control signal gains applied to the fuel delivery system. 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.
Referring to
Curve 206 represents the control signal gain applied to a healthy fuel pump where the gain value is insensitive to changes in engine RPM. That is, the control system gain value of the high-pressure fuel pump remains relatively constant at a calibrated gain value k0 across a range of engine RPM values when the fuel pump is operating properly.
Curve 208 reflects an adjustment trend of the control signal gain values in the case of a worn solenoid exhibiting a response time increase of about 50%. As demonstrated by the shape of curve 208, the control system gain value increases as engine RPM increases when the solenoid is degraded from wear. As engine speed increases and more fuel is demanded, the gain value is more sensitive to a slower operating solenoid—thus the controller increases the gain value to compensate. This trend may be used by the controller to generate a more detailed prognosis message. In one example, the prognosis message is indicative of solenoid degradation or imminent failure when the control gain value increases to satisfy engine demand as engine RPM increases.
Comparatively, curve 210 represents an adjustment trend of the control signal gain value in the case of a leaking plunger sleeve seal. Assuming a steady state rate of leakage from the fuel pump, the gain becomes less sensitive to the leakage as the speed of pulsation of the pump increases. Said another way, there is less time between each cycle for fuel to leak from the pumping chamber 36. In effect the gain value decreases as engine RPM increases, as shown by curve 210. In this case the controller may issue a prognosis message indicative of pump leakage corresponding to seal degradation and/or imminent failure when the control gain value decreases to satisfy engine demand as engine RPM increases.
The degraded performance scenarios corresponding to example curve 208 and example curve 210 each have adjusted gain values to about 0.7 at 1500 RPM, however the gain values trend differently as a function of engine RPM. While increasing and decreasing trends are depicted by way of example, control signal gain trends may have a number of different characteristic forms depending to the particular cause of degraded performance. The controller may include one or more algorithms to monitor adjustment trends of control signal gain across ranges of different engine operation parameters to distinguish between causal factors of degraded fuel pump performance.
Referring to
At step 304 the controller normalizes the control signal gains and fuel delivery timing over the range of operating conditions. The normalized values establish baseline operation to which deviations are compared to generate component prognosis.
At step 306 the controller considers whether data provided from the fuel injectors indicates that the injectors are causing a rich fuel-air mix. If the injectors are causing the less than desirable fuel-to-air ratio, additional prognosis of the high-pressure fuel pump may not be required. The controller may continue to collect, normalize, and monitor fuel delivery data concerning the fuel pump.
If at step 306, the fuel injectors are not indicated to be the cause of a rich fuel-air mix, the controller considers whether control signal gains applied to the high-pressure fuel pump are changing. If these data are not changing at step 308, the controller continues the collect, normalize, and monitor data loop.
If at step 308 there is a change over time in control signal gains applied to the high-pressure fuel pump, the controller considers at step 310 whether the control signal gain value has been adjusted by more than a predetermined threshold from the calibrated gain value. If the control signal gains applied to the high-pressure fuel pump are within the threshold at step 310, the controller continues the collect, normalize, and monitor data loop.
If the control signal gains are beyond the threshold at step 310, the controller may collect data regarding the fuel delivery rate of the low-pressure supply pump at step 312. At step 314 the controller considers whether the supply fuel pump is delivering more fuel than an amount corresponding to a normalized rate of delivery. If the rate is increase to exceed a rate delivery threshold at step 314, the condition may be indicative of fuel pump leakage. The increase in the fuel supply rate may be a symptom of increased demand to compensate for pressure loss due to pump leakage. In this way, the controller may use outputs from both of the low-pressure supply fuel pump as well as the high-pressure fuel pump in order to conduct a prognosis of the high-pressure fuel pump. At step 316 the controller issues a prognosis warning message indicative of fuel pump leakage.
If at step 314 the low-pressure supply fuel pump is delivering fuel at a rate within the rate delivery threshold the controller may consider other data pertaining to the fuel pump to generate a prognosis. At step 318, the controller collects data regarding solenoid inlet valve feedback current. If at step 320 the solenoid feedback current is increasing relative to normalized values, it may be indicative of solenoid wear. If the feedback current is increased from the normalized value beyond a feedback current threshold, the controller issues at step 322 a prognosis message indicative of solenoid wear.
If at step 320 the solenoid feedback current is within the feedback current threshold, the elevated gain value may be a symptom of degradation of other fuel delivery components. If the solenoid feedback current is not increasing, the solenoid may not be the cause of the increased control signal gains. The condition may indicate a fuel flow restriction within the high-pressure fuel pump. For example, either the pressure relief valve or the check valve may be fully or partially stuck causing the controller to increase control signal gain value to compensate. At step 324 the controller issues a prognosis warning message indicative of a flow restriction of the check valve or pressure relief valve.
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 on-board 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.