The present disclosure generally relates to engine system diagnostics and, more specifically, to systems and methods for detecting combustion gas leaks in a work machine.
Combustion engines rely on the ignition and combustion of fuel and air within a cylinder to generate pressure and kinetic energy to, ultimately, cause rotation of a crankshaft. The gases generated during combustion are typically sealed within the combustion chamber of the engine via a head gasket. Various types of seals and cylinder liners also assist in retaining combustion gases within engine cylinders. Failure of a head gasket, a cracked cylinder liner, or even an eroded seal can easily permit combustion gases to leak into the engine cooling system, causing damage to the engine.
Detecting a combustion gas leak is time consuming and often requires costly testing kits. This is because combustion gas leaks typically manifest as failures of the engine cooling system. For example, as combustion gas leaks into the engine cooling system of a work machine, the gas can aerate the coolant fluid, causing a typical diagnostic system for the work machine to generate a failure code indicating a reduction in coolant flow. The aeration can also cause excessive coolant overflow, causing the diagnostic system to generate a failure code simply indicating the level of coolant is low. In both of these examples, the damage to the engine or engine cooling system may appear benign based on the failure codes generated by the diagnostic systems; however, failure to detect and resolve the underlying combustion gas leak can eventually result in failure of the engine and associated systems.
Prior attempts at diagnosing combustion gas leakage in a combustion engine have been directed to methods of confirming a combustion gas leak after the leak is already suspected. For example, U.S. Pat. No. 4,667,507 discloses a method of testing the sealing integrity of the engine by running the engine until a normal operating temperature is achieved, venting pressure inside the coolant system to atmospheric pressure by opening a valve fluidly connected between the coolant system and atmosphere, closing the valve, and then running the engine again for a predetermined test period while measuring the pressure within the coolant system.
Such systems and methods described above for confirming suspected combustion gas leaks, are both time consuming and costly, requiring the work machine to be out of service during testing. Consequently, there remains a need for an improved combustion leak detection and diagnostic strategy for work machines.
In accordance with one aspect of the present disclosure, a work machine with a remote diagnostic system is disclosed. The work machine may include a combustion engine and a pump driven by the engine. The pump may include an inlet and an outlet. The work machine may also include a coolant temperature sensor and a pressure sensor. The coolant temperature sensor may be configured to monitor and transmit a coolant fluid temperature. The pressure sensor may be coupled to the inlet of the pump, and may monitor and transmit a coolant fluid pressure at the inlet of the pump. A controller, including a processor, may be operatively associated with the engine, the coolant fluid temperature sensor, the pressure sensor and an equipment care advisor module. The equipment care advisor module may also include a processor and may be configured to monitor the coolant fluid temperature during a start-up of the work machine, to monitor the coolant fluid pressure during the start-up of the work machine, to calculate an expected coolant fluid pressure based on the monitored coolant fluid temperature and the monitored coolant fluid pressure, and to generate a failure code indicating a combustion gas leak into a cooling system of the engine when the monitored coolant fluid pressure exceeds the expected coolant fluid pressure.
In accordance with another aspect of the present disclosure, a remote diagnostic system for a plurality of work machines is disclosed. Each work machine may include at least an engine and a controller. The remote diagnostic system may include a display module and an equipment care advisor module. The display module may include at least one display device and at least one user input device. The equipment care advisor module may include a processor, and may be electronically coupled to each controller of each work machine. Furthermore, each controller may be electronically coupled to a coolant temperature sensor and a coolant pressure sensor. For each work machine, the equipment care advisor module may monitor a coolant fluid temperature measured by the coolant temperature sensor during a start-up period, monitor a coolant fluid pressure measured by the coolant pressure sensor during the start-up period, calculate an expected coolant fluid pressure based on the monitored coolant fluid temperature and the monitored coolant fluid pressure, and generate a failure code indicating a combustion gas leak when the monitored coolant fluid pressure exceeds the expected coolant fluid pressure.
In accordance with yet another aspect of the present disclosure, method of detecting a combustion gas leak in an engine of a work machine is disclosed. The work machine may include an engine and a coolant pump. The method may include starting the engine. The engine may have a start-up period corresponding to a predetermined period of time. The method may further include monitoring, for the duration of the start-up period, a coolant fluid temperature and a coolant fluid pressure. The method further includes calculating an expected coolant fluid pressure based on the monitored coolant fluid temperature and the monitored coolant fluid pressure, and comparing the monitored coolant fluid pressure to the expected coolant fluid pressure. Finally, the method includes generating a failure code when the monitored coolant fluid pressure exceeds the expected coolant fluid pressure, the failure code indicating combustion gas created in the engine is leaking out of the engine.
These and other aspects and features of the present disclosure will be better understood upon reading the following detailed description, when taken in conjunction with the accompanying drawings.
Reference will now be made in detail to specific embodiments or features, examples of which are illustrated in the accompanying drawings. Wherever possible, corresponding or similar reference numbers will be used throughout the drawings to refer to the same or corresponding parts.
The undercarriage 12 may support a main frame 18. The main frame 18 may support various components of the work machine 10, including an implement system 20, an operator cab 22 and a combustion engine 24. The implement system 20 may include a work implement 26, one or more push arms 28, one or more hydraulic lift cylinders 30, and one or more hydraulic tilt cylinders 32. While the present work implement 26 is illustrated as a blade, the work implement may include any suitable tool or attachment, such as, for example, a bucket, a ripper, a compactor, forks, a plow, a trencher, or any other known implement configured to collect, hold and transport material and/or heavy objects at the worksite. The work implement 26 may be connected to the main frame 18 and/or the undercarriage 12 by at least one of the push arms 28, the lift cylinders 30, and/or the tilt cylinders 32. Alternatively, the work implement 26 may be connected to the main frame 18 by a power angle tilt (or “PAT”) arrangement (not shown). The push arms 28 may be coupled at one end to a roller frame 34 of the undercarriage 12, and coupled at an opposite end to the work implement 26 to stabilize the work implement as the work machine 10 travels in the X direction. The hydraulic lift cylinders 30 may configured to move the work implement in the Z direction, and the hydraulic tilt cylinders 32 may be configured to move the work implement in the Y direction. The push arms 28, lift cylinders 30 and tilt cylinders 32 may be configured to effectuate the movement of the work implement 26 based on operator commands received through various input devices (not shown) disposed within the operator cab 22. Further, the engine 24 may provide power to the ground engaging mechanisms 14, the implement system 20, a cooling system 100 (
The engine may be, for example, a diesel engine, a gasoline engine, a gaseous fuel engine, or any other type of combustion engine. The engine may be enclosed and protected by an engine hood 36 of the work machine 10. The engine 24 may also be coupled to the cooling system 100 (
Combustion of the fuel or air-fuel mixture generates heat within the engine 24. Consequently, the engine cooling system 100 may be configured to dissipate the heat generated within the engine 24 by circulating a coolant fluid within the engine 24. The coolant may be a liquid, and may include, for example, water, ethylene glycol, and other suitable solutions. To facilitate coolant flow within the engine 24, the engine 24 may include an engine cooling jacket 106 with a plurality of fluid passageways. While illustrated schematically in
The engine cooling system 100 may also include a coolant pump 108, a thermostat valve 110, and a radiator 112. The coolant pump 108 may be driven by the engine 24 to circulate the coolant through the engine cooling system 100. Generally, the coolant may flow from the pump 108 through the engine cooling jacket 106 of the engine 24, and subsequently through various conduits that circulate the coolant back to the pump. The direction of coolant flow is illustrated in
The pump 108 may further include an inlet pressure sensor 128 associated with the pump inlet 124 and configured to monitor a pressure P1 of the coolant as it enters the pump via the pump inlet conduit 126. An outlet pressure sensor 130 may be associated with the pump outlet 122 and configured to monitor a pressure P2 of the coolant as it exits the pump via the pump outlet conduit 114. The inlet pressure sensor 128 and outlet pressure sensor 130 may consist of any conventionally known pressure sensors capable of measuring fluid pressure.
Both the inlet pressure sensor 128 and outlet pressure sensor 130 may be in electronic communication with a controller 136, and may transmit data signals, readings, and/or sensed measurements electronically for processing at the controller. The controller 136 may also be in electronic communication with an engine speed sensor 138 associated with the engine 24 and configured to measure a speed of the engine, a coolant temperature sensor 140 positioned in the engine outlet conduit 116 and configured to measure a temperature of the coolant, as well as the thermostat valve 110. Like the inlet pressure sensor 128 and the outlet pressure sensor 130, the engine speed sensor 138 and coolant temperature sensor 140 may also transmit data signals, readings, and/or sensed measurements electronically for processing at the controller.
More specifically, the coolant temperature sensor 140 may include any type of device(s) or any type of component(s) that may sense (or detect) a temperature of the coolant. While a single coolant temperature sensor 140 is illustrated in
The controller 136 may include any type of device or any type of component that may interpret and/or execute information and/or instructions stored within a memory to perform one or more functions. The memory may include a random access memory (“RAM”), a read only memory (“ROM”), and/or another type of dynamic or static storage device (e.g., a flash, magnetic, or optical memory) that stores information and/or instructions for use by the controller 136. Additionally, or alternatively, the memory may include non-transitory computer-readable medium or memory, such as a disc drive, flash drive, optical memory, read-only memory (ROM), or the like. The memory may store the information and/or the instructions in one or more data structures, such as one or more databases, tables, lists, trees, etc. The controller 136 may also include a processor (e.g., a central processing unit, a graphics processing unit, an accelerated processing unit), a microprocessor, and/or any processing logic (e.g., a field-programmable gate array (“FPGA”), an application-specific integrated circuit (“ASIC”), etc.), and/or any other hardware and/or software. The controller 136 may transmit data via a network (not shown). For example, the controller 136 may be configured to provide output to one or more display units (not shown) that may be visible by the operator of the work machine 10, but may also be configured to provide output to external system, such as a remote diagnostic system 200, which may be electronically coupled to a plurality of controllers associated with a plurality of work machines and other vehicles. In this regard, data associated with each work machine may be stored in a central location and may be accessible by machine operators, technicians, data analysts, and others, as needed.
As mentioned above, the engine cooling system 100 may include a thermostat valve 110 positioned at a junction of the engine outlet conduit 116, a bypass conduit 132 and a radiator inlet conduit 134. The thermostat valve 110 may be configured to regulate the flow of the coolant from the engine 24 toward either or both of the bypass flow path 118 and the radiator flow path 120 based on one or more engine parameters. The engine parameters may include, for example, the speed of the engine 24, as measured by the engine speed sensor 138, and the temperature of the coolant, as measured by the coolant temperature sensor 140. The thermostat valve 110 may be any conventionally known thermostat that includes an electrically assisted valve element (not shown) having a thermally sensitive element, such as wax. The controller 136 may thus cause the valve element of the thermostat valve 110 to open or close based on the one or more engine parameters. The valve position of the thermostat valve 110 may vary between a fully open position, a fully closed position, and a myriad of intermediate partially open or partially closed positions to finely tune the distribution of coolant to the bypass flow path 118 and the radiator flow path 120, as explained more specifically below.
At low coolant temperatures, for example, such as upon startup of the work machine 10, the thermostat valve 110 may direct coolant through the bypass flow path 118, which, as illustrated in
Conversely, at higher coolant temperatures, for example, the thermostat valve 110 may direct coolant through the radiator flow path 120, which as illustrated in
Furthermore, the controller 136 is configured to shift the thermostat valve 110 into various partially open or partially closed positions when the controller determines the coolant temperature, as measured by the coolant temperature sensor 140, is greater than or equal to the first threshold temperature T1 and less than or equal to the second threshold temperature T2. In this situation, for example, coolant may flow through both the bypass flow path 118 and the radiator flow path 120, thereby creating a parallel flow path, as illustrated in
The radiator 112 includes a radiator inlet 146 configured to be fluidly connected to the engine outlet conduit 116 and the thermostat valve 110 via the radiator inlet conduit 134. The radiator 112 further includes a radiator outlet 148 configured to be fluidly connected to the pump inlet conduit 126 via the radiator outlet conduit 144. In operation, the heated coolant exits the engine 24 and is directed by the thermostat valve 110 toward the radiator 112. As the coolant flows through the radiator, the temperature of the coolant is reduced or cooled. The cooled coolant exits the radiator through the radiator outlet 148, and is directed back toward the pump 108 via the radiator outlet conduit 144 and the pump inlet conduit 126.
As noted above, the controller 136 is configured to determine the one or more engine parameters, such as engine speed and coolant temperature. In this regard, measurements taken by the engine speed sensor 138 and coolant temperature sensor 140 may be communicated to, and received by, the electronic controller 136. Further, the controller 136 may be configured to determine a pressure difference between the pump inlet pressure P1 and the pump outlet pressure P2. In this regard, measurements taken by the pump inlet pressure sensor 128 and pump outlet pressure sensor 130 may be communicated to, and received by, the electronic controller 136. Upon receipt of the pressure values P1 and P2, the controller 136 may calculate the pressure difference between P1 and P2 to determine the pressure difference. Moreover, the controller 136 may be configured to determine a change in pump inlet pressure over a period of time (ΔPin).
Monitoring the engine parameters as well as the coolant fluid pressure is not only essential in maintaining optimal performance of the engine 24, but is also crucial to diagnose a combustion gas leak and prevent damage to the engine or work machine 10. When improperly monitored, an undetected combustion gas leak may critically damage the engine 24 and other associated components of the work machine 10. To prevent such damage, the controller 136 of the work machine 10 may be in electronic communication via a network (not shown) with a remote diagnostic system 200, which may be configured to monitor at least the coolant temperature, the pump inlet pressure P1, the pump outlet pressure P2, the pump inlet pressure differential ΔPin, and the speed of the engine 24 to determine, before damage can occur, whether combustion gas may be leaking into the cooling system 100.
As illustrated in
The display module 204 may include at least a display (not shown) and at least one input device (not shown), such as a keyboard and mouse. Other types of displays, such as, for example, a hand held computing device, voice recognition means, a touch screen, or the like, are also contemplated. Accordingly, the equipment care advisor module 202 may also transmit received data, as well as calculated values (such as the rate of change in pump pressure and coolant temperature) to the display module 204 for viewing by those with access to the remote diagnostic system 200. While not shown, the remote diagnostic system 200 may also include at least one data storage device (e.g., a database), and may be electronically coupled to a plurality of controllers associated with a plurality of work machines and other vehicles, such that data associated with each work machine may be stored in a central location and may be accessible by machine operators, technicians, data analysts, and others, as needed.
As discussed above and further discussed herein, the remote diagnostic system 200, and the included and/or associated components thereof, including, in part, the equipment care advisor module 202, is configured to continuously monitor, process, and determine, in part, the performance, operating condition, and/or failure of components of the work machine 10. The remote diagnostic system 200 is therefore configured to provide a failure code, in real time, to a user of the remote diagnostic system, when a combustion gas leak is detected, as determined by the equipment care advisor module 202. In providing such failure code, the remote diagnostic system 200, and equipment care advisor module 202 thereof, can provide an operator and/or technicians accessing the work machine 10 with the opportunity to take appropriate responsive actions, including, but not limited to, actions relating to the operation of the work machine. Responsive actions may be necessary to prevent damage to the engine 24, as well as any associated components of the cooling system 100 and the work machine 10. Providing such failure code from the remote diagnostic system 200 may further provide the operator and/or user of user of the remote diagnostic system with the opportunity to coordinate, plan, and/or schedule timely procurement and deployment of maintenance services and/or personnel to ensure replacement of defective or damaged components as necessary to prevent any machine downtime or loss in productivity.
In practice, the present disclosure finds utility in various industrial applications, including, but not limited to, construction, paving, transportation, mining, industrial, earthmoving, agricultural, and forestry machines and equipment. For example, the present disclosure may be applied to compacting machines, paving machines, dump trucks, mining vehicles, on-highway vehicles, off-highway vehicles, earth-moving vehicles, agricultural equipment, material handling equipment, and/or any work machine including an electronically controlled combustion engine. More particularly, the present disclosure provides a remote diagnostic system 200 with an equipment care advisor module 202 to ultimately detect a combustion gas leak into a cooling system.
A series of steps 300 involved in detecting a combustion gas leak into the cooling system 100 of the work machine 10 is illustrated in flowchart format in
At step 304, while the work machine 10 remains idling, the coolant temperature, the engine 24 speed, the pump inlet pressure P1 and the pump outlet pressure P2 may be monitored by the remote diagnostic system 200. More specifically, the coolant temperature sensor 140, the engine speed sensor 138, the pump inlet pressure sensor 128 and the pump outlet pressure sensor 130 may transmit the sensed data to the controller 136 associated with the work machine 10. The controller 136 may then transmit the data to the remote diagnostic system 200. While the present disclosure utilizes coolant pressures and temperatures and engine speed, it should be noted and appreciated that additional data, such as air temperature, engine load, fuel temperatures and other data may also be monitored and analyzed in the same manner described herein. The coolant temperature, the engine 24 speed, the pump inlet pressure P1 and the pump outlet pressure P2 may ultimately be received by the equipment care advisor module 202 and stored in the memory 206 associated therewith. Alternatively, this data may be stored in a storage unit not illustrated in
If, at a next step 306, the equipment care advisor module 202 determines that not enough time has elapsed with respect to the predetermined period of time for engine start-up, steps 304 and 306 will repeatedly execute until the equipment care advisor module determines that the start-up period has elapsed. Once the predetermined period of time for engine start-up has fully elapsed, a step 308 may be executed.
At step 308, a change in coolant temperature over the engine start-up period, hereinafter ΔT, may be calculated. Specifically, the equipment care advisor module 202 may retrieve both the coolant temperature T1 as it was sensed by the coolant temperature sensor 140 at the end of the start-up period and the coolant temperature T0 as it was sensed by the coolant temperature sensor at the time the engine 24 was started from its memory 206. The final coolant temperature T1 may be subtracted from the initial coolant temperature T0 to calculate the ΔT value, which indicates by how many degrees the coolant temperature rose or fell during the engine start-up period.
At step 310, a change in pump inlet pressure, hereinafter ΔPin may be calculated. Specifically, the equipment care advisor module 202 may retrieve both the pump inlet pressure P11 as it was sensed by the pump inlet pressure sensor 128 at the end of the start-up period and the pump inlet pressure P10 as it was sensed by the pump inlet pressure sensor at the time the engine 24 was started from its memory 206. The equipment care advisor module 202 may subtract the final pump inlet pressure P11 from the initial pump inlet pressure P10 to determine the ΔPin value, which indicates by how many kilopascals (kPa) the pump inlet pressure rose or fell during the engine start-up period.
Using the change in coolant temperature ΔT value calculated at step 308, the equipment care advisor module 202 may then (at step 312) calculate an expected change in coolant pressure value, hereinafter E[ΔPin]. Using volumetric thermal expansion principals known in the art, the equipment care advisor module 202 may calculate E[ΔPin] using the initial pump inlet pressure P10, the initial coolant temperature T0 and the final coolant temperature T1 values, as well as the predetermined period of time given for the start-up period.
At step 314, the equipment care advisor module 202 may compare the actual change in pump inlet pressure ΔPin with the calculated expected change in pump inlet pressure E[ΔPin] to determine whether the coolant pressure is increasing too quickly in relation to the change in coolant temperature. For example, assume an initial coolant temperature T0 of approximately 83° C., a final coolant temperature T1 of approximately 93° C., an initial pump inlet pressure P10 of approximately 20 kPa, a final pump inlet pressure P11 of approximately 120 kPa, and a predetermined engine start-up period of approximately 6 minutes. The change in coolant temperature ΔT would be approximately 10° C., while the change in pump inlet pressure ΔPin would be approximately 100 kPa. The expected change in pump inlet pressure E[ΔPin] over that predetermined engine start-up period of 6 minutes, with a 10° C. increase in coolant temperature should have been approximate 20 kPa. In this example, the work machine should be parked immediately, as the expected change in pump inlet pressure E[ΔPin] is far lower than the actual change in pump inlet pressure ΔPin, indicating a combustion gas leak into the engine cooling system.
If the equipment care advisor module 202 determines the actual change in pump inlet pressure ΔPin is greater than the expected change in pump inlet pressure E[ΔPin], then the work machine 10 may be operating with an active combustion gas leak. Upon making this determination, the equipment care advisor module 202 may transmit a failure code to the display module 204 (step 316). More specifically, the equipment care advisor module 202 may command the display module 204 to communicate via prominent visual and/or audial indication to a user of the remote diagnostic system 200 that the work machine 10 has a combustion gas leak into its engine cooling system 100. An audial indicator or warning may include an alarm, buzzing, and similar sounds optimized to gain the attention of the user of the remote diagnostic system 200. Visual warnings may include simply illuminating a light on the display of the display module 204, or may include displaying symbols, graphics or text that not only informs the user of the warning, but also instructs the user to take specific actions.
In an alternative embodiment, the equipment care advisor module 202 may only transmit the failure code to the display module 204 when the actual change in pump inlet pressure ΔPin exceeds the expected change in pump inlet pressure E[ΔPin] by a predetermined threshold amount, for example, 50 kPa. Returning to the example provided above, the actual change in pump inlet pressure ΔPin exceeded the expected change in pump inlet pressure E[ΔPin] by approximately 100 kPa. As such, in that case, a failure code would still be transmitted to the display module 204 as it exceeds the predetermined 50 kPa threshold amount.
If the equipment care advisor module 202 determines the actual change in pump inlet pressure ΔPin is less than or equal to the expected change in pump inlet pressure E[ΔPin], then the work machine 10 may continue to be operated normally. At step 318, therefore, no action may be taken by the equipment care advisor module 202, and the work machine 10 may simply be allowed to proceed under its normal operating conditions.
While a series of steps and operation have been described herein, those skilled in the art will recognize that these steps and operations may be re-arranged, replaced, eliminated, performed simultaneously and/or performed continuously without departing from the spirit and scope of the present disclosure as set forth in the claims.
With implementation of the present disclosure, service technicians and operators of work machines may be alerted to a combustion gas leak before a catastrophic failure occurs, not in response to it. With early warning and an automated system designed to protect the engine and other components of the work machine, service technicians and operators of a given work machine may be able to use that warning to plan maintenance, overhaul, and/or other service routines on the engine or work machine in a timely manner with little or no obstruction to an ongoing job on a worksite.
While aspects of the present disclosure have been particularly shown and described with reference to the embodiments above, it will be understood by those skilled in the art that various additional embodiments may be contemplated by the modification of the disclosed machines, systems and assemblies without departing from the scope of what is disclosed. Such embodiments should be understood to fall within the scope of the present disclosure as determined based upon the claims and any equivalents thereof.
Number | Name | Date | Kind |
---|---|---|---|
4667507 | Eriksson | May 1987 | A |
5381762 | Evans | Jan 1995 | A |
5868105 | Evans | Feb 1999 | A |
7918129 | Coppola et al. | Apr 2011 | B2 |
9790842 | Dudar et al. | Oct 2017 | B2 |
10151233 | Martin et al. | Dec 2018 | B2 |
10648397 | Rollinger et al. | May 2020 | B2 |
20140303838 | Nam | Oct 2014 | A1 |
20190040815 | Nishida | Feb 2019 | A1 |
20190284986 | Gonze | Sep 2019 | A1 |
20200063653 | Sugimoto | Feb 2020 | A1 |
20200362800 | Keblusek | Nov 2020 | A1 |
Number | Date | Country |
---|---|---|
2007057312 | May 2007 | WO |