1. Field of the Invention
The present application relates to the use of the characteristics of an ion current sensor signal for onboard measurement of in-cylinder variables such as but not limited to soot, engine load, and fuel consumption, and for the control of different engine parameters accordingly.
2. Description of Related Art
One existing technology in quantitative soot measurement utilizes laser techniques in optically accessible engines. These techniques are used in research facilities only and cannot be applied in commercial engines. Another existing technology uses sampling techniques which require very expensive instrumentation and can also only be applied in research labs. Other technologies have provided some results for soot measurement where a sensor is located in the exhaust pipe or within after treatment devices. The problem of this type of sensors is the slow access to the soot measurement data. Furthermore, this type of sensors is unable to predict the amount of soot attributable to each engine cylinder accurately. This brings us to the conclusion that there is no in-cylinder, low cost technology that is capable of quantitatively and adequately predict the amount of soot produced in commercial engines.
As of engine load and fuel flow, there are several methods for which these parameters can be measured, each with their own advantages, disadvantages and applications. One method is to use the engine speed density. The method involves a manifold absolute pressure sensor (MAP) and intake air temperature. Speed density systems are very sensitive to temperature changes which affect load and fuel calculations.
A system and method is provided for an onboard in-cylinder soot measurement in an internal combustion engine. The system can be further used in controlling the engine based on a feedback signal from the soot measured. The system acquires an ion current signal and controls the engine operating parameters based on the characteristics of the ion current signal.
Throughout the application examples will be provided with regard to soot, load, and fuel consumption measurements, however, these principles can be applied to other in-cylinder variables as well and such applications are contemplated herein.
A system and method is provided for onboard engine load such as IMEP (Indicated Mean Effective Pressure), BMEP (Brake Mean Effective Pressure) and fuel consumption (FC) measurement in internal combustion engine based on an acquired ion current signal. ISFC (Indicated Specific Fuel Consumption) and BSFC (Brake Specific Fuel Consumption) can be calculated from the measurements mentioned above. The system can be further used in controlling the engine based on a feedback signal obtained from the measured engine load fuel consumption.
The new technique gives the ion-current sensor, located inside the engine cylinder, the ability to detect and accurately measure the amount of soot (black smoke), and mean effective pressure produced from the combustion process on a cyclic basis. Fuel consumption (FC) is also measured on a cylinder-by-cylinder and cycle-by-cycle basis using the ion current signal. This fast response measuring technique can be applied in all engine cylinders in order to provide an onboard feedback signal to the contribution of each cylinder to soot formation, produced power, and fuel consumed.
The system offers a new cost effective and simple technique to measure soot, load, and fuel consumption (FC) inside the combustion chamber using the ion-current signal. The system also provides a fast cycle-by-cycle soot prediction technique to accommodate the engine transient operation. The feedback signal is sent to the engine ECU for better engine control, thereby producing less soot to comply with the EPA stringent emissions rules with no modification to the engine.
The system is cost effective as the sensor involved is the ion sensor. The system provides a fast response soot, load, and fuel consumption (FC) measuring technique, as it depends on electron speed. The system is able to measure the disclosed parameters inside the combustion chamber and on a cycle-by-cycle basis. Further, the system is able to measure soot, load, fuel consumption (FC) in every engine cylinder with no modifications required to the engine block. Accordingly, the system is well suited as an on-board tool for soot, load, and fuel consumption (FC) measurement and provides an efficient, compact design for integration in production models.
Further objects, features and advantages of this application will become readily apparent to persons skilled in the art after a review of the following description, with reference to the drawings and claims that are appended to and form a part of this specification.
Aspects of this application will be described by way of examples with reference to the accompanying drawings. They serve to illustrate several aspects of the present application, and together with the description provide explanation of the system principles. In the drawings:
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The engine control unit 150 includes a combustion controller 152, a fuel delivery controller 156 and other engine controllers 158. The combustion controller 152 may act as a master module that provides a control signal to different engine components such as the glow plug 124 heater, the fuel delivery system 162, or the injector 122. The fuel delivery controller 156 provides a fuel delivery control signal 160 to an engine fuel delivery system 162. The engine fuel delivery system controls the delivery of fuel to the injector 122. The fuel from the tank 166 is delivered by the fuel pump 164 to the fuel delivery system 162. The fuel delivery system 162 distributes the supplied fuel based on a signal 160 from the ECU 150. The fuel is further supplied to the injector 122 through a fuel line 168. In addition, the fuel delivery controller 156 is in communication electronically with the fuel injector 122 to control different injection parameters such as number of injection events, injection duration and timing as noted by line 170. In addition, the other engine controllers 158 control other engine parameters such as engine speed, load, amount of exhaust gas recirculation, variable geometry turbocharger, or other units installed to the engine. Further, an output sensor 180 may be in communication with the crankshaft 130 to measure crank shaft position, and engine speed, torque of the crankshaft, or vibration of the crank shaft, and provide the feedback signal to the engine control unit 150 as denoted by line 182.
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In one example, the relationship used to come up with measured parameters may be expressed as predicted parameter (SOOT, IMEP, BMEP, FC)=(A1, A2, A3, A4)*Fn (SOI)+(B1, B2, B3, B4)*Fn (m)+(C1, C2, C3, C4)*Fn (I)+(L1, . . . , L4)*Fn (P)+(E1, . . . , E4)*Fn (ICD)+(F1, . . . , F4)*Fn (Ar)+(H1, . . . , H4)*Fn (EOI)+(K1, . . . , K4)*Fn(D)+(Y1, . . . , Y4)*Fn (SOI,m)+(X1, . . . , X4)*Fn (SOI, m, I)+ . . . etc. While the forgoing equation is exemplary, additional variables may be readily introduced. Such variables may include peak to peak, peak to end, peak to start, peak to start of injection, peak to top dead center, peak to end of injection, peak to start of combustion, peak amplitudes for each peak, and each of those variable may have their own weighting as indicated above. Each weighting factor An, Bn, Cn, Ln, En, Fn, Hn, Kn, . . . , Yn, and Xn may be different based on the in-cylinder variable being measured. Hence, A1, B1, C1, . . . X1 may be used for soot, while A2, B2, C2, . . . , X2 may be used for IMEP as illustrated in Table 1. In addition, weighting factors such as An, Bn, Cn, Ln, En, Fn, Hn, Kn, Yn, . . . , Xn may constants or may vary according to a look up table based on other parameters such as ion current sensor location inside the combustion chamber. Further, it is anticipated that other relationship functions may be developed including linear, quadratic, root, trigonometric, exponential or logarithmic components or any combination thereof. Also note that the correlation between the constants mentioned above and the predicted parameters can be expressed as follows:
In one particular example in accordance with the general equation provided above, soot could be predicted according to a function:
soot=A0+A1(Par1)+A2(Par2)+A3(Par3)+A4(Par4)+A5(Par1*Par2)+A6(Par1*Par3)+A7(Par1*Par4)+A8(Par2*Par3)+A9(Par2*Par4)+A10(Par1*Par2*Par3)+A11(Par1*Par3*Par4)+A12(Par1^2*Par2^2*Par3^2*Par4^2)
where (Par) stands for an ion current parameter and (A) is a coefficient or weighting.
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From the graph, it is clear that a good correlation between the measured soot and the predicted soot is achieved. The test was conducted based on a transient engine operating condition where engine speed and load were varying. The engine was operated in transient test via an open ECU. The engine speed varied between 1150 and 2000 RPM, load varied between 70 and 220 Nm, injection pressure was kept constant at 400 bar, the engine intake pressure (MAP) varied between 1 and 1.3 bar due to an activated VGT (Variable Geometry Turbocharger).
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The original manufacturer ECU used for this test was calibrated by the manufacturer to produce soot emissions within the EPA standards. The test was developed to see if the predicted soot using the new technique is sensitive enough to capture the very low soot levels emitted. The engine speed was kept constant at 1800 RPM, load (IMEP) varied between 12 and 18 bar, injection pressure varied between 950 and 1150 bar, and intake pressure (MAP) varied between 2.4 and 2.8 bar. The results showed a good match between the measured and predicted soot ranging between 0.05% and 0.6%. The ability to capture the very low soot levels reflects high accuracy and high sensitivity of the described technique.
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The engine system 700 includes an engine 710 with four cylinders 712. Pistons reciprocate in the cylinders 712 to drive the crankshaft 716. The crankshaft 716 may be connected to a dynamometer 718. The dynamometer provides a load signal 720 to a processor 714 for combustion analyzing and data recording. Fuel is provided to the engine through a fuel rail 722, pressure may be monitored in the fuel rail by a fuel sensor which may provide a fuel pressure signal 724 to the processor 714. The fuel may be provided from the fuel rail 722 to the cylinder 712 through a fuel line 726. The fuel may be provided through a fuel needle 728. As such a needle lift signal 730 may be provided to the processor 714 for further analysis in conjunction with the other engine operating parameters. Further, a fuel flow meter is embedded within the fuel line 726 and is used to measure the fuel flow representing engine fuel consumption. It is understood that different fuel measurement devices could be used in this scenario.
The engine may also include a glow plug 732, however, it is readily understood that a spark plug may have been used for other combustion engines. Further, an ion current sensor 734 may be located within the cylinder 712 to measure ion current. The ion current signal 736 may be provided to the processor 714 from the ion current sensor 734. In addition, an inlet cylinder pressure sensor 742 may be located within the cylinder to measure cylinder pressure. The cylinder pressure signal 744 may be provided to the processor 714 by the pressure sensor 742. The processor 714 uses the cylinder pressure signal 744 to calculate the Indicated Mean Effective Pressure (IMEP) for each engine cylinder. BMEP is also calculated. It is understood that IMEP, BMEP are forms of representation of engine load and accordingly can be predicted using the ion current signal. Further, crank position sensor 738 may be connected to the crankshaft to provide an encoder signal 740 to the processor 714, to track the various engine parameters based on the engine crank angle. In addition, a soot measurement device 746 may be provided in an exhaust outlet 748 for each cylinder 712. A soot measurement signal 750 may be provided to the processor 714 by the soot measurement device 746. In one example, the soot measurement device 746 may be an opacity measurement device to optically determine the amount of soot in the exhaust based on opacity. However, it is understood that other soot measurement devices could be used in this scenario.
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In other embodiments, dedicated hardware implementations, such as application specific integrated circuits, programmable logic arrays and other hardware devices, can be constructed to implement one or more of the methods described herein. Applications that may include the apparatus and systems of various embodiments can broadly include a variety of electronic and computer systems. One or more embodiments described herein may implement functions using two or more specific interconnected hardware modules or devices with related control and data signals that can be communicated between and through the modules, or as portions of an application-specific integrated circuit. Accordingly, the present system encompasses software, firmware, and hardware implementations.
In accordance with various embodiments of the present disclosure, the methods described herein may be implemented by software programs executable by a computer system. Further, in an exemplary, non-limited embodiment, implementations can include distributed processing, component/object distributed processing, and parallel processing. Alternatively, virtual computer system processing can be constructed to implement one or more of the methods or functionality as described herein.
Further, the methods described herein may be embodied in a computer-readable medium. The term “computer-readable medium” includes a single medium or multiple media, such as a centralized or distributed database, and/or associated caches and servers that store one or more sets of instructions. The term “computer-readable medium” shall also include any medium that is capable of storing, encoding or carrying a set of instructions for execution by a processor or that cause a computer system to perform any one or more of the methods or operations disclosed herein.
As a person skilled in the art will readily appreciate, the above description is meant as an illustration of the principles of this invention. This description is not intended to limit the scope or application of this invention in that the invention is susceptible to modification, variation and change, without departing from spirit of this invention, as defined in the following claims.
The present application is a 371 national stage application of PCT Application No. PCT/US2012/026873, filed Feb. 28, 2012, which application claims the benefit of U.S. Provisional Application No. 61/447,163 filed on Feb. 28, 2011 which is incorporated herein by reference in its entirety.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/US2012/026873 | 2/28/2012 | WO | 00 | 12/3/2013 |
Publishing Document | Publishing Date | Country | Kind |
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WO2012/118781 | 9/7/2012 | WO | A |
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Entry |
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International Search Report, Serial No. PCT/US2012/026873, Dated Jun. 7, 2012. |
Number | Date | Country | |
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20140081556 A1 | Mar 2014 | US |
Number | Date | Country | |
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61447163 | Feb 2011 | US |