ENGINE CONTROL SYSTEM AND METHODS

Abstract

Embodiments describe a method of controlling a two-stroke internal combustion engine. A method of controlling a two-stroke internal combustion engine includes determining a base nominal exhaust gas temperature, determining a base barometric pressure correction to base nominal exhaust gas temperature, determining exhaust gas temperature differential, determining exhaust gas temperature injection correction, and utilizing the exhaust gas temperature injection correction to make a final short-term fuel or ignition correction.

Claims

1. A method of controlling a two-stroke internal combustion engine, comprising: determining a base nominal exhaust gas temperature; determining a base barometric pressure correction to base nominal exhaust gas temperature; determining exhaust gas temperature differential; determining exhaust gas temperature injection correction; and utilizing the exhaust gas temperature injection correction to make a final short-term fuel correction.

2. The method of claim 1, wherein before determining a base nominal exhaust gas temperature, the step of implementing an initial short-term fuel correction.

3. The method of claim 1, wherein before determining a base nominal exhaust gas temperature, the step of determining engine hours.

4. The method of claim 3, wherein determining engine hours is used in order to at least determine if an engine hour criteria has been met.

5. The method of claim 1, wherein before determining a base nominal exhaust gas temperature, the step of determining coolant system temperature.

6. The method of claim 5, wherein determining coolant system temperature is used in order to at least determine if a coolant temperature range criteria has been met.

7. The method of claim 1, wherein before determining a base nominal exhaust gas temperature, the step of determining air temperature.

8. The method of claim 7, wherein determining air temperature is used in order to at least determine if an air temperature range criteria has been met.

9. The method of claim 1, wherein before determining a base nominal exhaust gas temperature, the step of confirming completeness of a startup protocol.

10. The method of claim 1, wherein determining a base nominal exhaust gas temperature comprises utilizing the inputs of exhaust valve position, and one or more of engine speed, throttle valve angle, and crankcase pressure.

11. The method of claim 1, wherein determining a base barometric pressure correction to base nominal exhaust gas temperature comprises utilizing the inputs of engine speed and barometric pressure.

12. The method of claim 1, wherein determining exhaust gas temperature differential comprises utilizing exhaust gas temperature as an input.

13. The method of claim 1, wherein a fuel correction comprises adjusting a fuel injection amount.

14. A method of controlling a two-stroke internal combustion engine, comprising: determining a base nominal exhaust gas temperature; determining a base barometric pressure correction to base nominal exhaust gas temperature; determining exhaust gas temperature differential; determining exhaust gas temperature injection correction; and utilizing the exhaust gas temperature ignition correction to make a final short-term ignition correction.

15. The method of claim 14, wherein the final short-term ignition correction comprises adjusting an ignition angle measured in degrees.

16. A method of controlling a two-stroke internal combustion engine, comprising: determining an initial short-term fuel or ignition correction; comparing one or more engine inputs to a long-term correction range criteria; starting long-term fuel or ignition correction criteria once long-term correction range criteria are met; comparing engine hours to an engine hour criteria; comparing one or more engine inputs to a corresponding engine input gradient; utilizing one or more engine inputs to implement a final long-term fuel or ignition correction.

17. The method of claim 16, wherein comparing one more engine inputs to a long-term correction range criteria comprises engine speed, throttle position, and crankcase pressure.

18. The method of claim 16, wherein comparing one or more engine inputs to a corresponding engine input gradient comprises engine speed, engine hours, throttle position, exhaust gas temperature, coolant temperature, and barometric pressure.

19. The method of claim 16, wherein utilizing one or more engine inputs to implement a final long-term fuel or ignition correction comprises engine speed, throttle position, and crankcase pressure.

Description

BRIEF DESCRIPTION OF DRAWINGS

[0008] This written disclosure describes illustrative embodiments that are non-limiting and non-exhaustive. Reference is made to illustrative embodiments that are depicted in the figures, in which:

[0009] FIG. 1 illustrates a flow chart diagram 100 of a method of controlling a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0010] FIGS. 2A-B illustrate flow chart diagrams 200, 202 of a method of controlling a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0011] FIGS. 3A-B illustrate flow chart diagrams 300, 302 of a method of controlling a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0012] FIGS. 4A-B illustrate flow chart diagrams 400, 402 of a method of controlling a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0013] FIGS. 5A-B illustrate flow chart diagrams 500, 502 of a method of controlling a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0014] FIG. 6 illustrates a flow chart diagram 600 of a method of controlling a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0015] FIG. 7 illustrates a flow chart diagram 700 of a method of controlling a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0016] FIG. 8 illustrates a flow chart diagram 800 of a method of controlling a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0017] FIG. 9 illustrates a flow chart diagram 900 of a method of controlling a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0018] FIG. 10 illustrates a flow chart diagram 1000 of a method of controlling a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0019] FIG. 11 illustrates a flow chart diagram 1100 of a method of controlling a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0020] FIG. 12 illustrates a flow chart diagram 1200 of a method of controlling a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0021] FIG. 13 illustrates a graph 1300 of an injector flow in a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0022] FIG. 14 illustrates a cross-sectional view 1400 of a two-stroke internal combustion engine, according to some embodiments of this disclosure.

[0023] FIGS. 15A-B illustrate perspective views 1500, 1502 of a cylinder, according to some embodiments of this disclosure.

[0024] FIGS. 16A-B illustrate a flow chart diagram 1600 of a method of controlling a two-stroke internal combustion engine with a short-term fuel correction, according to some embodiments of this disclosure.

[0025] FIGS. 17A-B illustrate a flow chart diagram 1700 of a method of controlling a two-stroke internal combustion engine with a short-term fuel correction, according to some embodiments of this disclosure.

[0026] FIGS. 18A-B illustrate a flow chart diagram 1800 of a method of controlling a two-stroke internal combustion engine with a short-term ignition correction, according to some embodiments of this disclosure.

[0027] FIGS. 19A-B illustrate a flow chart diagram 1900 of a method of controlling a two-stroke internal combustion engine with a short-term ignition correction, according to some embodiments of this disclosure.

[0028] FIGS. 20A-C illustrate a flow chart diagram 2000 of a method of controlling a two-stroke internal combustion engine with a long-term fuel correction, according to some embodiments of this disclosure.

[0029] FIGS. 21A-C illustrate a flow chart diagram 2100 of a method of controlling a two-stroke internal combustion engine with a long-term fuel correction, according to some embodiments of this disclosure.

[0030] FIGS. 22A-C illustrate a flow chart diagram 2200 of a method of controlling a two-stroke internal combustion engine with a long-term ignition correction, according to some embodiments of this disclosure.

[0031] FIGS. 23A-C illustrate a flow chart diagram 2300 of a method of controlling a two-stroke internal combustion engine with a long-term ignition correction, according to some embodiments of this disclosure.

DETAILED DESCRIPTION

[0032] Embodiments of the present disclosure describe methods of controlling a two-stroke internal combustion engine, in either forward or reverse crankshaft rotation direction. Embodiments herein adapt an engine to environmental and manufacturing variations to optimize engine operations. On a crankcase scavenged two-stroke engine all air mass entering the engine must travel through the crankcase, therefore by measuring the crankcase pressure of the engine, the engine load can more accurately be determined. In some embodiments, the crankcase pressure may be used as a direct measure of engine load instead of as correction factor to an indirect measure of engine load (i.e. throttle position). This is especially important for applications in which boosted air is entering the crankcase (i.e., turbocharged). The additional airflow created by the boost renders traditional measurements inaccurate or delayed. If inaccurate or delayed information is communicated to an engine control unit, the engine run less efficiently and with less performance A direct pressure measurement can be combined with additional inputs, such as a pre-throttle pressure measurement, to enable boost pressure control via wastegate valve and air bypass valve control. Even in naturally aspirated applications, the measurement analysis herein creates greater engine efficiencies.

[0033] Embodiments of this disclosure additionally discuss optimizing engine performance based on utilizing the temperature of the expansion chamber within an exhaust system to calibrate and optimize the engine throughout all operating conditions. This calibration method utilizes nominal exhaust gas temperature and changes the calibration based on the difference from the nominal temperature to optimize engine outputs and performance. Short-term corrections can be generated and implemented as well as long-term corrections that account for manufacturing variances, or any factors that uniquely affect that specific engine. If exhaust gas temperatures (such as expansion chamber temperatures) are used as an input in a lookup or reference table, they are referenced as large temperature ranges. This creates stepped adjustments across only a handful of different temperature ranges, as opposed to a near continuous short and long-term adjustments discussed herein. The system will smooth out any stepped adjustments over smaller time increments, but also have safety criteria, such that adjustments will have maximum possible changes over the existing state. This prevents erroneous readings from making quick and large engine parameter adjustments that could be dangerous.

[0034] Referring to FIG. 1, flow chart diagram 100 of a method of controlling a two-stroke internal combustion engine is shown, according to some embodiments of this disclosure. One set of two or more sets of engine parameter inputs or a weighted value of two or more sets of engine parameter inputs are selected 102. From the selection, an engine output parameter is determined 104. The determined engine output parameter is utilized 106 to control one or more engine operations. Engine parameter inputs include one or more of engine speed, barometric pressure, crankcase pressure, exhaust valve position, air temperature, engine coolant temperature (e.g., water temperature), exhaust temperature (e.g., expansion chamber temperature), boost pressure, crankshaft position and direction of rotation, humidity, fuel pressure, fuel temperature, detonation sensor level, exhaust oxygen content, and throttle valve angle. Engine speed may be measured via a crankshaft position sensor, for example. Barometric pressure measures atmospheric pressure and may be measured via a pressure sensor located outside the crankcase, or located outside of the air intake passage, for example. Crankcase pressure may be measured within the crankcase with an absolute pressure sensor, for example. Exhaust valve position and throttle valve angle include measurements of the valve's position as open, closed or in some position in between open or closed. The throttle valve position may be mechanically or electrically controlled, for example. Inlet air temperature may be measured via a temperature sensor located within the air intake passage. Engine coolant temperature may be measured via a temperature sensor located within the engine coolant system. Exhaust temperature may be measured via a temperature sensor located within the exhaust passage or within the expansion chamber. Boost pressure may be measured via an absolute pressure sensor located within the pressurized portion of the air intake passage, for example. Crankshaft position and direction of rotation may be measured by one or more crankshaft position sensors. Humidity may be measured by a humidity sensor located within the air intake passage. Fuel pressure may be measure by a pressure located within the pressurized portion of the fuel system. A set of engine parameter inputs includes two or more of the engine parameter inputs. In one embodiment, a set of engine parameter inputs includes a measurement of engine speed and one or more of barometric pressure, crankcase pressure, exhaust valve position, air temperature, engine coolant temperature, exhaust temperature, boost pressure, crankshaft position and direction of rotation, humidity, fuel pressure, fuel temperature, detonation sensor level, exhaust oxygen content, and throttle valve angle. Sets of engine parameter inputs can be determined prior to engine operation and programmed into the ECU. Each set of engine parameter inputs may be optimal to utilize under different engine conditions, environmental conditions, or in response to user input. Each set of inputs can be selected 102 individually or a weighted combination of two or more sets of measurements can be considered. The selection 102 can be done by an engine control unit (ECU), for example. Selecting 102 can be in response to pre-programmed reference values, such as engine speed. Alternatively, selecting 102 can be in response to an analysis of collected data points over a time period.

[0035] In one embodiment, and prior to the selecting 102 one set of two or more sets, the step of selecting driving fuel control or idle fuel control may be determined. Selecting driving fuel control or idle fuel control can include determining one or more initial input values, comparing the one or more initial input values to one or more reference values, sufficient to determine whether the engine is in a drive mode or idle mode, and then selecting driving fuel control or idle fuel control. The one or more initial input values may include throttle valve angle, for example. The one or more reference value may include reference throttle valve positions. Selecting includes communicating with an engine control unit that the engine is either in idle mode or in drive mode. Whether the engine is in idle mode or driving mode may influence the selection 102 of which set or weight of sets of engine parameter inputs. Whether the engine is in idle mode or driving mode may affect which measurement module the ECU follows.

[0036] After selecting 102, the ECU may re-select one set of two or more sets of engine parameter inputs or a weighted value of two or more sets of engine parameter inputs during engine operation and then utilize the reselected output parameters to adjust or control one or more engine operations. The reselection may use the same inputs as originally selected if the parameters have not changed such that a change in analysis is warranted. A change in parameters during engine operation may trigger a reselection of inputs, or adjust the weight of inputs or switch control methods.

[0037] The engine output parameter may include one or more of fuel injection amount, fuel injection angle, ignition angle, and exhaust valve position. Additional engine output parameters may include boost pressure (e.g., from a turbocharger or supercharger application), wastegate duty, air bypass valve, fuel pressure, target torque, and throttle position. The fuel injection amount includes a mass of fuel to be injected into the combustion chamber, cylinder, crankcase and/or air inlet passage. The fuel injection angle refers to the timing of the fuel injection into the combustion chamber, cylinder, crankcase and or air inlet passage in relation to crankshaft position. The ignition angle includes timing of the firing of the spark plug in relation to the crankshaft position, in order to optimize the combustion cycle. Exhaust valve position, as an output, controls the position of the exhaust valve to increase performance and reduce emissions in optimizing the amount or timing of exhaust air released and unspent fuel/air mixture retained in the combustion chamber.

[0038] The engine operations that may ultimately be adjusted and controlled by the ECU may include one or more of injecting fuel mass, adjusting injection fuel angle, adjusting exhaust valve position, firing spark plug, fuel pressure, boost pressure, wastegate position, bypass valve position, and adjusting exhaust valve position. For example, from a determined 104 fuel injection amount, this information is utilized to control 106 fuel injection into the engine.

[0039] Referring to FIG. 2A, a flow chart diagram 200 of a method of controlling a two-stroke internal combustion engine is shown, according to some embodiments of this disclosure. An initial input value, such as throttle valve angle 204 can be measured. The initial input is compared 202 by the ECU to a reference position. In this example, current throttle valve angle or position 204 is compared to the reference throttle valve angle to determine if the engine is in drive mode or idle mode. If in drive mode, the ECU follows the analysis of the driving fuel control module 206. If in idle mode, the ECU follows the analysis of the idle fuel control module 208. In this embodiment, the ECU selects between one of two sets 201, 203 of engine parameter inputs. The selection of one set over the other set can be based on a current, pre-determined input value, such as engine speed or throttle valve angle, or based on an analysis of collected data points over a time period. The selection between sets 201, 203 can be a binary choice based on a certain condition, can utilize a weighted combination of the two, or switch from one set to the other set based on pre-determined or real time parameters. The time period could be 0.1-10 seconds, 5 seconds to 30 seconds, 10 seconds to 2 minutes, for example. In one embodiment, the ECU may analyze both set one and set two over a time period and compare results for consistency, variance from expected reference values, or in response to user input and then make a selection. For example, a binary choice between sets is shown in Table 1. As engine speed increases, the control method switches at 4000 RPM in this example.

TABLE-US-00001 TABLE 1 Column 1 Engine Speed Column 2 Weighting Factor 1000 0 Weighting factor between control 2000 0 methods by RPM 2500 0 3000 0 4000 1 4500 1 5000 1 5200 1 5400 1 5600 1 5800 1 6000 1 6200 1 6400 1 6600 1 6800 1 7000 1 7200 1 7400 1 7600 1 7800 1 8000 1 8200 1 8400 1

[0040] In Table 2, weighting factors between control methods by throttle valve angle versus engine speed is show in an example. Table 3 shows weighting factors between control methods by crankcase pressure and engine speed.

TABLE-US-00002 TABLE 2 Crankcase Pressure (mmHg) X-Axis Engine Speed Weighing factor between control Y-Axis Weighting Factor methods by crankcase pressure Z-Axis 200 300 400 500 600 800 1000 1200 1400 1000 0 0 0 0 0 0 0 0 0 2000 0 0 0 0 0 0 0 0 0 2500 0 0 0.8 0 0 0 0 0 0 3000 0 0 0.8 0.8 0.8 0.8 0.8 0.8 0.8 4000 0 0 0.8 1 1 1 1 1 1 4500 0 0 0.8 1 1 1 1 1 1 5000 0 0 0.8 1 1 1 1 1 1 5200 0 0 0.8 1 1 1 1 1 1 5400 0 0.8 0.8 1 1 1 1 1 1 5600 0 0.8 0.8 1 1 1 1 1 1 5800 0 0.8 0.8 1 1 1 1 1 1 6000 0 0.8 0.8 1 1 1 1 1 1 6200 0 0.8 0.8 1 1 1 1 1 1 6400 0 0.8 0.8 1 1 1 1 1 1 6600 0 0.8 0.8 1 1 1 1 1 1 6800 0 0.8 0.8 1 1 1 1 1 1 7000 0 0 0 1 1 1 1 1 1 7200 0 0 0 1 1 1 1 1 1 7400 0 0 0 1 1 1 1 1 1 7600 0 0 0 0.8 1 1 1 1 1 7800 0 0 0 0.8 1 1 1 1 1 8000 0 0 0 0.8 1 1 1 1 1 8200 0 0 0 0.8 1 1 1 1 1 8400 0 0 0 0.8 1 1 1 1 1

TABLE-US-00003 TABLE 3 Throttle Valve Angle Percent X-Axis Engine Speed Weighing factor between control Y-Axis Weighting Factor methods by throttle valve angle Z-Axis 0 10 20 30 40 50 60 70 80 90 100 1000 0 0 0 0 0 0 0 0 0 0 0 2000 0 0 0 0 0 0 0 0 0 0 0 2500 0 0 0.8 0 0 0 0 0 0 0 0 3000 0 0 0.8 0.8 0.8 0.8 0.8 0.8 0.8 0.8 0.8 4000 0 0 0.8 1 1 1 1 1 1 1 1 4500 0 0 0.8 1 1 1 1 1 1 1 1 5000 0 0 0.8 1 1 1 1 1 1 1 1 5200 0 0 0.8 1 1 1 1 1 1 1 1 5400 0 0.8 0.8 1 1 1 1 1 1 1 1 5600 0 0.8 0.8 1 1 1 1 1 1 1 1 5800 0 0.8 0.8 1 1 1 1 1 1 1 1 6000 0 0.8 0.8 1 1 1 1 1 1 1 1 6200 0 0.8 0.8 1 1 1 1 1 1 1 1 6400 0 0.8 0.8 1 1 1 1 1 1 1 1 6600 0 0.8 0.8 1 1 1 1 1 1 1 1 6800 0 0.8 0.8 1 1 1 1 1 1 1 1 7000 0 0 0 1 1 1 1 1 1 1 1 7200 0 0 0 1 1 1 1 1 1 1 1 7400 0 0 0 1 1 1 1 1 1 1 1 7600 0 0 0 0.8 1 1 1 1 1 1 1 7800 0 0 0 0.8 1 1 1 1 1 1 1 8000 0 0 0 0.8 1 1 1 1 1 1 1 8200 0 0 0 0.8 1 1 1 1 1 1 1 8400 0 0 0 0.8 1 1 1 1 1 1 1

[0041] For set 201, engine speed 212 is utilized with barometric pressure 220 in order to calculate a base idle fuel amount 214 and then subsequently a fuel injection amount 218. For set 203, a crankcase pressure 216 is compared to engine speed 212 in order to calculate a base idle fuel amount 214 and then subsequently a fuel injection amount 218.

[0042] In the embodiment shown in FIG. 2B, further possible inputs and outputs related to fuel injection system are shown (see 202). After determining a base idle fuel amount 214, some combination of fuel temperature 252 and fuel pressure 250 is utilized to determine the fuel specific density 260 on a reference table. The fuel specific density 260 is then compared to the injector characterization 254 to calculate fuel injection volume amount 218 and then subsequently the fuel injector pulse width 256. Injector characterization 254 refers to pre-modeling or pre-testing of an injector system. The ratio of fuel to oil can be more precisely controlled in this method, for example. The purpose of fuel pressure control is to broaden the effective fuel flow range of a fuel injector. In a load situation, when a fuel injector is operated below 1.6 msec the injector flowrate versus injector pulse width is nonlinear (see 1300 of FIG. 13). This makes modeling fuel injector operation difficult. By decreasing the fuel pressure, the fuel flow is decreased. In order to match the desired fuel flowrate, the fuel pulse width is increased potentially into a linear region where the fuel injector performance can be more easily modeled. Conversely, in a high load situation where a fuel injector is operated near maximum duty, when the fuel pressure is increased, the fuel flow is increased. To match the desired fuel flowrate the injector pulse width is decreased, reducing the injector duty allowing for long fuel atomization time. Therefore, in this embodiment fuel pressure is actively controlled (versus simply monitoring).

[0043] Referring to FIG. 3A, a flow chart diagram 300 of a method of controlling a two-stroke internal combustion engine is shown, according to some embodiments of this disclosure. An initial input value, such as throttle valve angle 204 can be measured. The initial input is compared 302 by the ECU to a reference position. Engine speed 212 can also be used as an initial input in this example, before the ECU selects set 301 or set 303. In this example, current throttle valve angle or position 204 is compared to the reference throttle valve angle to determine if the engine is in drive mode or idle mode. If in drive mode, the ECU follows the analysis of the driving fuel control module 206. If in idle mode, the ECU follows the analysis of the idle fuel control module 208. In this embodiment, the ECU selects between one of two sets 301, 303 of engine parameter inputs in drive mode.

[0044] Set 301 utilizes engine speed 212 with throttle valve angle 204 to determine an exhaust valve position 304. The exhaust valve position 304 is then used as input in consideration with throttle valve angle 204 and engine speed 212 to determine fuel injection amount 218. For set 303, crankcase pressure 216 measurement is substituted for throttle valve angle 204 only after the exhaust valve positioning in 304, within the engine parameter inputs. In FIG. 3B, view 302 additionally utilizes throttle valve angle 204 and engine speed 212 to calculate fuel mass injection amount 350. This can then be utilized to find the fuel specific density 260 with fuel temperature 252 and fuel pressure 250 as inputs. Using injector characterization 254, a fuel volume injection amount 218 and fuel injector pulse width 256 are calculated. Another embodiment in drive mode is illustrated in FIG. 4A (see view 400). Both sets 401, 403 utilize engine speed 212 and throttle angle 204 to determine exhaust valve position 304. To finalize the injection amount measurement 214, set 401 utilizes engine speed 212, throttle valve angle 204, and exhaust valve position to output the fuel injection amount 218. Set 403 differs in that crankcase pressure 216 is utilized with engine speed 212 and exhaust valve position 304 to determine fuel amount 214 and final injection amount output 218. An example injection fuel amount 218 table is shown in Table 4 below.

TABLE-US-00004 RPM X-Axis Crankcase Pressure Y-Axis Amount of fuel Z-Axis 300 400 500 600 700 800 900 1000 1100 1200 1400 1000 2 4 6 8 10 12 14 16 18 20 22 2000 4 6 8 10 12 14 16 18 20 22 24 2500 6 8 10 12 14 16 18 20 22 24 26 3000 8 10 12 14 16 18 20 22 24 26 28 4000 10 12 14 16 18 20 22 24 26 28 30 4500 12 14 16 18 20 22 24 26 28 30 32 5000 14 16 18 20 22 24 26 28 30 32 34 5200 16 18 20 22 24 26 28 30 32 34 36 5400 18 20 22 24 26 28 30 32 34 36 38 5600 20 22 24 26 28 30 32 34 36 38 40 5800 22 24 26 28 30 32 34 36 38 40 42 6000 24 26 28 30 32 34 36 38 40 42 44 6200 26 28 30 32 34 36 38 40 42 44 46 6400 28 30 32 34 36 38 40 42 44 46 48 6600 30 32 34 36 38 40 42 44 46 48 50 6800 32 34 36 38 40 42 44 46 48 50 52 7000 34 36 38 40 42 44 46 48 50 52 54 7200 36 38 40 42 44 46 48 50 52 54 56 7400 38 40 42 44 46 48 50 52 54 56 58 7600 40 42 44 46 48 50 52 54 56 58 60 7800 42 44 46 48 50 52 54 56 58 60 62 8000 44 46 48 50 52 54 56 58 60 62 64 8200 46 48 50 52 54 56 58 60 62 64 66 8400 30 34 38 42 46 50 54 58 62 66 70

[0045] FIG. 4B (view 402) includes a further calculation of fuel specific density 260, from fuel temperature 252 and fuel pressure 250. The fuel volume injection amount 218 can then be calculated using injector characterization 254 and then ultimately, a fuel injector pulse width 256 determined.

[0046] Referring to FIG. 5A, a flow chart diagram 500 of a method of controlling a two-stroke internal combustion engine is shown, according to some embodiments of this disclosure. Sets 501, 503 are similar to previously discussed drive mode sets in FIG. 3. In this embodiment, the decision 502 on which set to choose is a weighted combination of the two sets 501, 503. The example shows a 0.3 weight given to set 501, and a 0.7 weight value given to set 503. The final fuel injection amount 504 reflects the weighted consideration of the injection amount calculated 218 in each set. The weighting may be any increments between 0.01 and 0.99 for one set and 0.99 and 0.01 for the other set, for example. If more than two sets of engine parameter inputs are utilized, the weighting may include any distribution of values between 0 and 1 across the plurality of sets, such that the total of the weights equal 1. FIG. 5B (view 502) includes a further calculation of fuel specific density 260, from fuel temperature 252 and fuel pressure 250. The fuel volume injection amount 218 can then be calculated using injector characterization 254 and then ultimately, a fuel injector pulse width 256 determined. The combined pulse width 510 can also be determined using a weighted combination of methods.

[0047] Referring to FIG. 6, a flow chart diagram 600 of a method of controlling a two-stroke internal combustion engine is shown, according to some embodiments of this disclosure. In this embodiment, a final fuel injection angle 606 is calculated as the engine output parameter from a weighted analysis of sets 601, 603 of engine parameter inputs. Engine speed 212 is measured and inputted for analysis 602 by the ECU. Either one of sets 601, 603 may be selected, but in this example, a weighted consideration is utilized. Set 601 utilizes engine speed 212 and throttle valve angle 204 to determine an exhaust valve position 304, which is then used as an input with engine speed 212 and throttle valve position 204 to determine fuel injection angle 604. For set 603, a crankcase pressure measurement 216 is substituted for the throttle valve angle input 204. The injection angle outputs 604 from each set are used to determine a final injection angle 606. In FIG. 7 (see view 700), similar measurements are used for sets 701, 703, but with the goal of ignition angle 705 table being referenced to produce final ignition angle 704 as the engine output parameter. The analysis or control unit 702 selects between sets 701, 703. In FIG. 8 (see view 800), ignition angle 704 is the engine output parameter, but sets 801, 803 differ from sets 701, 703 in that crankcase pressure 216 is only measured once in set 803 as an input for the ignition angle 705 and final ignition angle output 704. FIG. 9 (see view 900), shows a similar approach to FIG. 8, in which sets 901, 903 output ignition angle 704. In this example, analysis 902 uses weighting between sets 901, 903 to calculate a final ignition angle 904.

[0048] Additional examples of lookup or reference tables that can be used for engine control calculations include Table 5 in which fuel pressure can be controlled based on crankcase pressure. Table 6 shows fuel pressure control based on barometric pressure. Table 7 shows an example of ignition timing based on crankcase pressure. Table 8 displays the start of injection angle versus crankcase pressure.

TABLE-US-00005 TABLE 5 Crankcase pressure (mmHg) X-Axis Engine Speed Fuel Pressure control based on Y-Axis Target Fuel Pressue crankcase pressure Z-Axis 300 400 500 600 700 800 1000 1200 1000 400 400 400 400 450 450 450 450 2000 400 400 400 400 450 450 450 450 3000 400 400 400 400 450 450 450 450 4000 400 400 400 400 450 450 450 450 5000 400 400 400 400 500 500 500 500 6000 400 400 400 400 500 500 500 500 7000 400 400 400 400 500 500 500 500 8000 400 400 400 400 500 500 500 500 9000 400 400 400 400 500 500 500 500

TABLE-US-00006 TABLE 6 Barometric Pressure (mmHg) Fuel X-Axis Engine Speed Pressure control based Y-Axis Target Fuel Pressue on barometric pressure Z-Axis 300 400 500 600 700 700 800 900 1000 400 400 400 400 450 450 450 450 2000 400 400 400 400 450 450 450 450 3000 400 400 400 400 450 450 450 450 4000 400 400 400 400 450 450 450 450 5000 400 400 400 400 500 500 500 500 6000 400 400 400 400 500 500 500 500 7000 400 400 400 400 500 500 500 500 8000 400 400 400 400 500 500 500 500 9000 400 400 400 400 500 500 500 500

TABLE-US-00007 TABLE 7 Crankcase Pressure (mmHg) X-Axis Engine Speed Ignition timing based on Y-Axis Ignition timing crankcase pressure Z-Axis 300 400 500 600 700 800 900 1000 1100 1200 1400 1000 25 25 25 25 25 25 25 25 25 25 25 2000 25 25 25 25 25 25 25 25 25 25 25 2500 25 25 25 25 25 25 25 25 25 25 25 3000 25 25 25 25 25 25 25 25 25 25 25 4000 25 25 25 25 25 25 25 25 25 25 25 4500 25 25 25 25 25 25 25 25 25 25 25 5000 25 25 25 25 25 25 25 25 25 25 25 5200 25 25 25 25 25 25 25 25 25 25 25 5400 25 25 25 25 25 25 25 25 25 25 25 5600 22 22 22 22 22 24 24 24 22 22 22 5800 20 20 20 20 20 22 22 22 20 20 20 6000 20 20 20 20 20 22 22 22 20 20 20 6200 18 18 18 18 18 20 20 20 18 18 18 6400 18 18 18 18 18 20 20 20 18 18 18 6600 18 18 18 18 18 20 20 20 18 18 18 6800 16 16 16 16 16 17 17 17 16 16 16 7000 16 16 16 16 16 17 17 17 16 16 16 7200 15 15 15 15 15 16 16 16 15 15 15 7400 14 14 14 14 14 15 15 15 14 14 14 7600 14 14 14 14 14 15 15 15 14 14 14 7800 14 14 14 14 14 15 15 15 14 14 14 8000 13 13 13 13 13 14 14 14 13 13 13 8200 12 12 12 12 12 13 13 13 12 12 12 8400 12 12 12 12 12 13 13 13 12 12 12

TABLE-US-00008 TABLE 8 Crankcase Pressure (mmHg) X-Axis Engine Speed Start of Ignition Angle Y-Axis Ignition Angle based on crankcase Z-Axis 300 400 500 600 700 800 900 1000 1100 1200 1400 1000 250 250 250 250 250 250 250 250 250 250 250 2000 250 250 250 250 250 250 250 250 250 250 250 2500 250 250 250 250 250 250 250 250 250 250 250 3000 250 250 250 250 250 250 250 250 250 250 250 4000 250 250 250 250 250 250 250 300 300 300 300 4500 250 250 250 250 250 250 250 300 300 300 300 5000 250 250 250 250 250 250 250 300 300 300 300 5200 250 250 250 250 250 250 330 330 330 330 330 5400 250 250 250 250 250 250 330 330 330 330 330 5600 250 250 250 250 250 250 330 330 330 330 330 5800 250 250 250 250 250 250 330 330 330 330 330 6000 250 250 250 250 250 250 330 330 330 330 330 6200 250 250 250 330 330 330 360 360 360 360 360 6400 250 250 250 330 330 330 360 360 360 360 360 6600 250 250 250 330 360 330 400 400 400 400 400 6800 250 250 250 330 360 360 400 400 400 400 400 7000 250 250 250 330 360 360 400 400 400 400 400 7200 250 250 250 330 360 360 400 400 400 400 400 7400 250 250 250 330 360 360 400 400 400 400 400 7600 250 250 250 330 360 360 400 400 400 400 400 7800 250 250 250 330 360 360 400 400 400 400 400 8000 250 250 250 330 360 360 400 400 400 400 400 8200 250 250 250 330 360 360 400 400 400 400 400 8400 250 250 250 330 360 360 400 400 400 400 400

[0049] Referring to FIG. 11, a flow chart diagram 1100 of a method of controlling a two-stroke internal combustion engine, according to some embodiments of this disclosure. Engine parameter input sets 1101, 1103 are selected by analysis 1102, in which engine speed 212 is an input, to obtain final injection angle 604. Set 1101 utilizes engine speed 212 and throttle valve angle 204 to determine exhaust valve position 304. The exhaust valve position 304 is then used in combination with engine speed 212 and throttle valve angle 204 to produce an injection angle 214 and final injection angle output 604. Set 1103 utilizes crankcase pressure 216 in place of throttle valve angle 204. FIG. 12 (see view 1200) uses similar inputs for set 1201 as set 1101, but with set 1203 in relation to 1103, a throttle valve angle 204 measurement is utilized in place of the crankcase pressure 204 to determine exhaust valve position 304. Analysis 1202 selects between the sets 1201, 1203 by relying on engine speed 212 as an input.

[0050] Referring to FIG. 10, a flow chart diagram 1000 of a method of controlling a two-stroke internal combustion engine is shown, according to some embodiments of this disclosure. Engine speed 212 is used as an input for analysis 1002 between sets 1001 and 1003 for determining exhaust valve position 304. In set 1001, engine speed 212 and throttle valve position 204 are used as inputs. In set 1003, engine speed 212 and crankcase pressure 216 are utilized to determine exhaust valve position 304, and exhaust valve output 1004.

[0051] Referring to FIG. 14, a cross-sectional view 1400 of a two-stroke internal combustion engine is shown, according to some embodiments of this disclosure. A crankcase 1302 holds a crankshaft 1304 which rotatably connects to piston 1322. An air intake passage 1308 receives air, such as from a turbocharger and fills crankcase volume 1306 (shown in black shading). An air intake valve 1327 may be positioned within the passage 1308. Transfer ports 1318 allow for air from the crankcase to move into the combustion chamber 1320 with fuel injected from fuel injection system 1316. The injection system 1316 may located in the cylinder or air intake passage and fluidly connected to the combustion chamber. In an alternative embodiment, the fuel injection system 1316 may be a direct injection into the combustion chamber. One or more spark plugs 1314, as part of an ignition system, ignite the fuel/air mixture in combustion chamber 1320 to force the piston 1322 downward, moving the crankshaft 1304. After combustion, air or air/fuel mixture or exhaust gases may exit via exhaust passage 1310 and if a boosted system, to the turbocharger. In an alternative embodiment, a supercharger is utilized in a boosted application. An exhaust valve 1312 is positioned in the exhaust passage 1310 to assist in controlling fluid flow out of the combustion chamber 1320. One or more air pressure sensors 1325 may be positioned in the crankcase 1302.

[0052] The intake valve 1327 may be a reed valve, for example. A throttle system, including a throttle valve, is mechanically and fluidly coupled to the air intake passage 1308. A turbocharger may be mechanically and fluidly couple to the air intake passage for compressing air entering the crankcase 1302. The position (i.e., angle) of the throttle valve can be used as an input as discussed above. The throttle valve is typically controlled by the user's input and measuring the position of the throttle valve assists in determining initial inputs to the engine analysis and also to the two or more sets of engine input parameters. The throttle valve may be positioned in 3 (i.e. open, partially open, and closed) positions, 4 positions, 5 positions, or a plurality of positions between fully open and fully closed.

[0053] The exhaust valve 1312 may be a guillotine valve, for example. The position of the exhaust valve 1312 can be utilized as both an input and output as discussed above. Measuring and controlling the position of the exhaust valve 1312 not only increases performance of the engine, but also assists in emission control by retaining some portion of unspent fuel within the combustion chamber. The exhaust valve 1312 may be positioned in 2 (i.e. open and closed) positions, 3 positions, 4 positions, or a plurality of positions between fully open and fully closed.

[0054] The one or more pressure sensors 1325 may be absolute pressure sensors, fluidly connected the two-stroke engine crankcase. The sensors 1325 may be located within the crankcase and either attached to or integrated with one or more walls of the crankcase area (see views 1500, 1502 of FIGS. 15A-B). The pressure sensor or sensors 1325 must be located such that they measure pressure within crankcase volume 1306. In some embodiments the pressure sensor is fluidly connected a transfer port passage 1318. The crankcase area may be defined as the area between the intake valve and the transfer port exits into the cylinder. In some embodiments, crankcase pressure is measured during the compression phase, or cycle, of the crankcase and further can be measured at one specific crankshaft position or at multiple crankshaft positions. The crankshaft positions at which measurements may be taken is defined by variables in the engine control unit. If multiple pressure measurements are taken per cycle, the measurements may be processed into an average and/or slope as a method of load determination. Pressure measurement(s) and/or processed measurement(s) may then become a reference value for determining: injection duration or amount, injection timing, ignition timing, exhaust valve position, electronic throttle valve position, engine indicated torque, fuel pressure control, or other engine parameter. The combination of crankcase and a pressure measurement upstream of the throttle, for example between the turbocharger compressor and engine throttle body, becomes a reference value for determining: wastegate valve position, air bypass valve position. In some embodiments this reference value is a ratio of crankcase pressure to upstream pressure. In some embodiments this reference value is the difference between crankcase pressure and upstream pressure.

[0055] Referring to FIGS. 16A-B a flow chart diagram 1600 of a method of controlling a two-stroke internal combustion engine with a short-term fuel correction is shown, according to some embodiments of this disclosure. An initial or baseline short-term fuel correction 1602 can be used as starting parameter in which to analyze and implement an engine adjustment or correction. The initial short-term fuel correction 1602 may be no adjustment or in another embodiment, could be generated from production testing, or data from other engines for example. As the engine runs and the system generates short-term fuel correction data after the startup and initial startup criteria is met, an initial short-term fuel correction 1602 may be generated. Short-term may be in the range of making engine readings, adjustments/corrections, or both every 1 to 10 milliseconds, every 2 to 7 milliseconds, every 5 to 15 milliseconds, or every 20 milliseconds to 50 milliseconds, for example. The system can interpolate between any of these time ranges as well. The short-term is only limited by the speed of any given sensor reading and can approach a continuous reading and adjustments depending on how fast the sensors read and the ECU analyzes and adjusts. Engine hours 1612 may be read and compared to an engine hour criteria 1604, such as an initial break-in period for a new engine. For example, any adjustments may be paused until a new engine reaches 10 running hours for example. Additionally or alternatively, the method includes the step of completion of startup protocol 1606. The analysis and adjustments may be paused until the engine startup protocol 1606 completes and then is ready for further analysis and adjustment.

[0056] In this example, a water or engine coolant temperature 1610 is measured and compared to a reference table or criteria 1608 for adjustment. Similarly, air temperature can be measured before, with, or after coolant temperature and also compared to reference criteria for adjustment. A base nominal exhaust gas temperature 1614 can be calculated from exhaust valve position 304, throttle valve angle 204, and engine speed 212, for example. Subsequently or simultaneously, barometric pressure 220 and engine speed 212 can be utilized to calculate a barometric pressure correction to nominal exhaust gas temperature 1616. An exhaust gas temperature reading 1620 is then used to generate an exhaust gas temperature differential calculation 1618. This exhaust gas temperature differential 1618 can be calculated by subtracting the nominal exhaust gas temperature 1614 from the current exhaust gas temperature 1620, for example. The current exhaust valve position 304 and engine speed 212 may be read and used to calculate the exhaust gas temperature injection correction 1622, which is then used to adjust the final short-term fuel correction 1624. Given that this calculation is generated in the short-term, the cycle repeats itself using the final short-term fuel correction 1624 as the new initial short-term fuel correction 1602 input.

[0057] Referring to FIGS. 17A-B a flow chart diagram 1700 of a method of controlling a two-stroke internal combustion engine with a short-term fuel correction is shown, according to some embodiments of this disclosure. Similar to FIGS. 16 A-B, but after adjusting for coolant temperature, this method uses crankcase pressure 204 in combination with exhausts valve position 304 and engine speed 212 to generate a base nominal exhaust gas temperature 1614. FIGS. 18A-B mimic the steps of FIGS. 16A-B, but for an initial short-term fuel correction 1602 is replaced with an initial short-term ignition correction 1802. Similarly, the adjustment of final short-term fuel correction 1624 is replaced with a final short-term ignition correction 1626. A fuel correction generally is a percentage of the base fuel injection mass or fuel injection amount, for example. An ignition correction is an angle measured in degrees.

[0058] FIGS. 19A-B mimic the steps of FIGS. 17A-B, but for an initial short-term fuel correction 1602 is replaced with an initial short-term ignition correction 1802. Similarly, the adjustment of final short-term fuel correction 1624 is replaced with a final short-term ignition correction 1626.

[0059] Referring to FIGS. 20A-C, a flow chart diagram 2000 of a method of controlling a two-stroke internal combustion engine with a long-term fuel correction, according to some embodiments of this disclosure. A long-term correction may be adjustments made from two or more short-term corrections, or generally corrections made over a longer period of time than short-term corrections and adjustments. A long-term correction could be made after 5 seconds, after 15 seconds, after 30 seconds, or after 1 minute, for example. Long-term corrections create an adaption system, such that the systems learn each individual engine and how the engine performance needs change over time.

[0060] An initial short term fuel correction 1602 may be used as a baseline. Engine speed 212 may then be compared to a reference of engine speed range for long-term correction 2002. Throttle position 204 may also be compared to throttle position range for long-term correction 2004. A long-term criteria time counter 2006 may be initialized to set time parameters on when to make adjustments and how much data is collected before making a further adjustment. Long-term fuel correction criteria 2008 is generated and compared to. Engine parameter gradients may be used to compare inputs to a stabilizing range of data within calibrated limits. This prevents an incorrect long-term correction from being made and causing the engine to operate incorrectly or inefficiently. The method then reads engine speed 212 and compares to an engine speed gradient 2010 to analyze if the inputs are within the long-term criteria and if adjustments need to be made. Similarly, engine hours 1612 are compared to engine hour criteria 1604, throttle position 204 is compared to throttle position gradient 2012, exhaust gas temperature 1620 is compared to exhaust gas temperature (EGT) gradient 2014, water temperature 1610 compared to water temperature range 1608, and barometric pressure 220 compared to barometric pressure range 2016. Air temperature may also be utilized as an input. The system checks against the time in the correction zone criteria 2018 and then checks the engine speed 212 again to compare to an engine speed range to apply a long-term correction 2020. The throttle position 204 is checked again to compare to a throttle position range to apply long-term correction 2004 and then final long term fuel corrections 2024 are implemented. This process can be repeated and continual adjustments made within a single riding session and over the life of the engine.

[0061] FIGS. 21A-C utilize an initial crankcase pressure 216 and comparison to crankcase pressure range 2102 in lieu of initial throttle position, as in FIGS. 20A-C.

[0062] FIGS. 22A-C mimic the steps of FIGS. 20A-C and FIGS. 23A-C mimic the steps of FIGS. 21A-C, but fuel corrections are replaced with ignition corrections in these examples.

[0063] Other embodiments of the present disclosure are possible. Although the description above contains much specificity, these should not be construed as limiting the scope of the disclosure, but as merely providing illustrations of some of the presently preferred embodiments of this disclosure. It is also contemplated that various combinations or sub-combinations of the specific features and aspects of the embodiments may be made and still fall within the scope of this disclosure. It should be understood that various features and aspects of the disclosed embodiments can be combined with or substituted for one another in order to form various embodiments. Thus, it is intended that the scope of at least some of the present disclosure should not be limited by the particular disclosed embodiments described above.

[0064] Thus the scope of this disclosure should be determined by the appended claims and their legal equivalents. Therefore, it will be appreciated that the scope of the present disclosure fully encompasses other embodiments which may become obvious to those skilled in the art, and that the scope of the present disclosure is accordingly to be limited by nothing other than the appended claims, in which reference to an element in the singular is not intended to mean “one and only one” unless explicitly so stated, but rather “one or more.” All structural, chemical, and functional equivalents to the elements of the above-described preferred embodiment that are known to those of ordinary skill in the art are expressly incorporated herein by reference and are intended to be encompassed by the present claims. Moreover, it is not necessary for a device or method to address each and every problem sought to be solved by the present disclosure, for it to be encompassed by the present claims. Furthermore, no element, component, or method step in the present disclosure is intended to be dedicated to the public regardless of whether the element, component, or method step is explicitly recited in the claims.

[0065] The foregoing description of various preferred embodiments of the disclosure have been presented for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure to the precise embodiments, and obviously many modifications and variations are possible in light of the above teaching. The example embodiments, as described above, were chosen and described in order to best explain the principles of the disclosure and its practical application to thereby enable others skilled in the art to best utilize the disclosure in various embodiments and with various modifications as are suited to the particular use contemplated. It is intended that the scope of the disclosure be defined by the claims appended hereto

[0066] Various examples have been described. These and other examples are within the scope of the following claims.