1. Field of the Invention
The present invention relates to engine control for internal combustion engines and, more particularly, for small internal combustion engines of the type which are used in a variety of applications, such as walk-behind lawnmowers, lawn and garden implements, generators, or in small utility vehicles such as riding lawnmowers, lawn tractors, and the like.
2. Description of the Related Art
Small internal combustion engines generally include an operator-selected command speed setting, for example, a throttle control for utility vehicles or a normal/idle switch for generators. However, driving a variable load may reduce or increase the engine speed from the commanded setting. For example, in a lawnmower powered by an internal combustion engine, it is desired that the commanded speed of the engine remain relatively constant under a variety of loading conditions. Thus, it is desired that whether the lawnmower encounters tall grass or short grass, the engine speed which has been selected by the operator should remain constant. Likewise, in the case of a generator, it is desired that the alternator output frequency, i.e., the engine drive speed, remain constant despite changes in the electrical loads connected to the alternator output.
To regulate engine speed, small internal combustion engines generally include a mechanical speed-regulating governor, such as an air vane mechanism or a centrifugal flyweight mechanism sensitive to engine speed. For engines having a carburetor, the throttle valve is generally mechanically linked to both the governor and the operator throttle control. Therefore, the throttle valve is acted upon by a first force related to the commanded speed setting and a second force corresponding to the governor and related to the actual engine speed.
A disadvantage of known engine control systems for small internal combustion engines is the potential unreliability of cables, springs, and linkages that are used to transmit and combine the inputs from the operator-commanded engine speed and the actual engine speed. Such components might bind, require lubrication, or may fail from mechanical vibrations or loading.
Another disadvantage of known engine control systems for small internal combustion engines is the difficulty of mechanically adjusting the amount of movement of the throttle valve as it relates to the commanded engine speed setting or the actual engine speed and the difficulty of providing dampening of transients due to engine speed changes.
Yet another disadvantage of known speed control mechanisms for small internal combustion engines is that ambient temperature and engine operating conditions are not taken into account to adjust the fuel-to-air ratio for easy starting and optimum efficiency for a range of ambient engine conditions.
What is needed is an engine control system for internal combustion engines that reliably accounts for the commanded engine speed setting and the actual engine speed to drive the throttle and fuel controls, and that accounts for the ambient and engine operating temperatures to provide an efficient fuel-to-air ratio.
The present invention is directed to an engine control system for an internal combustion engine. The engine control system may include a governor assembly, engine speed sensor, control circuit, and fuel system. The governor assembly and sensor are coupled by a coupling member. The coupling member is displaced relative to the governor assembly according to the engine speed. The sensor detects the displacement of the coupling member and outputs an electrical speed signal related to the actual engine speed.
A first and second exemplary engine control system includes a control circuit that provides a speed command signal to control the intake system of the engine, including air flow, fuel flow, and/or air-to-fuel ratio, to correlate the actual engine speed to the operator-commanded speed setting. The speed command signal is a function of both commanded speed and the actual engine speed, which may be detected by the governor assembly and sensor.
A third exemplary engine control system includes a control circuit and may also include a combination of an exhaust temperature sensor cylinder head temperature, an intake temperature sensor, and/or mass air flow for detecting ambient and engine operating conditions. The output of the sensors is used to control one or both of a throttle signal and a fuel flow signal for adjusting the fuel-to-air ratio for a more efficient engine start and efficiency over a range of operating conditions.
The control systems may also include elements of a fuel system. For a first exemplary fuel system, a fuel signal is supplied to control the speed of a fuel pump motor, thereby controlling the fuel flow through a fuel injector. A second exemplary fuel system provides the fuel flow signal to a solenoid which controls the fuel flow through a regulator valve, thereby controlling the fuel flow through the fuel injector.
Small internal combustion engines used in a variety of applications generally include an operator-controlled commanded speed setting. However, as the engine drives a variable load, the engine may slow from the commanded speed when the load is increased, or overshoot the commanded speed when the load is decreased. The invention provides an engine control system that provides constant engine speed under varying loads by determining engine control inputs from both the operator-commanded speed and the actual engine speed.
Advantageously, the present engine control system for internal combustion engines provides operator setting, detection, and adjustment of engine speeds using electrical components and electrical signals in the place of certain mechanical components which had typically been used in known systems. The electrical and other components of the present engine control system reliably transmit engine control signals and provide for simple adjustment of engine control and dampening of the response of the engine control system to changes in the engine speed.
Additionally, the second exemplary speed control system may provide a combination of intake air temperature sensing, intake mass airflow sensing, exhaust gas temperature sensing, and cylinder head temperature sensing to adjust the fuel flow for optimal cold start, hot start, and performance over a range of operating temperatures and other conditions.
In one form thereof, the present invention provides an engine control system for an internal combustion engine, including a governor assembly mounted to and driven by the engine and responsive to engine speed; a coupling member associated with the governor assembly, the coupling member displaceable by the governor assembly according to engine speed; and a position sensor controlled by the coupling member, the position sensor detecting the displacement of the coupling member and outputting an electrical speed signal corresponding to the displacement and to engine speed.
In another form thereof, the present invention provides an internal combustion engine, including an engine housing; an engine control device connected to the housing; a governor assembly connected to the housing and responsive to engine speed; a coupling member coupled with the governor assembly and movably displaced by the governor assembly in response to engine speed; and a position sensor mounted to the housing and detecting the position of the coupling member, the position sensor outputting an electrical speed signal, the speed signal acting upon the engine control device to adjust the engine speed.
In a further form thereof, the present invention provides an engine control system for an internal combustion engine, including a governor assembly driven by the engine, the governor assembly having a spool capable of translating axially in response to the engine speed; a rotary shaft associated with the spool such that the rotary shaft is rotationally displaced upon translation of the spool; a spring coupled between the engine and the rotary shaft, the spring resisting rotational displacement of the rotary shaft; and a rotary position sensor capable of detecting the rotational position of the rotary shaft and outputting an electrical speed signal corresponding to the position.
In another form thereof, the present invention provides a method of controlling the speed of an internal combustion engine having a mechanical governor and at least one of an intake throttle and a fuel injector, including the steps of driving the governor to produce an output proportional to engine speed; sensing the governor output; determining an actual engine speed from the governor output; supplying a commanded engine speed signal; and controlling at least one of the intake throttle and fuel injector based on the actual engine speed signal and the commanded engine speed signal.
In yet a further form thereof, the present invention provides an engine control system for a small internal combustion engine, the system including at least one of a voltage supply and a current supply, a governor sensor having an input and an output, the governor input coupled to the at least one of a voltage supply and current supply, an operator control sensor having an input and an output, the operator control sensor input coupled to the governor sensor output, and at least one of an intake throttle actuator and a fuel flow controller coupled to the operator control sensor output.
In a further form, the present invention provides an engine control system for a small internal combustion engine, the system including at least one of a voltage supply and a current supply; an operator control sensor having an input and an output, the operator control sensor input coupled with the at least one of a voltage supply and a current supply; a governor sensor having an input and an output, the governor sensor input coupled to the operator control sensor output; and at least one of an intake throttle actuator and a fuel flow controller coupled to the governor sensor output.
In yet another form, the present invention provides an engine control system for a small internal combustion engine, the system including an operator control sensor providing a command signal; an engine speed sensor providing a speed signal; a control circuit receiving the command signal and the speed signal and providing a fuel control signal; and a fuel flow device having an actuator adapted for adjusting the fuel flow through the fuel flow device, the actuator receiving the fuel control signal.
The above-mentioned and other features and advantages of this invention, and the manner of attaining them, will become more apparent and the invention itself will be better understood by reference to the following description of exemplary embodiments of the invention taken in conjunction with the accompanying drawings, wherein:
Corresponding reference characters indicate corresponding parts throughout the several views. The exemplifications set out herein illustrate preferred embodiments of the invention, and such exemplifications are not to be construed as limiting the scope of the invention in any manner.
Referring to
Referring again to
Referring to
Sensor assembly 44 generally includes rotary shaft 62, coil spring 64, spring housing 66, and rotary sensor 68. Rotary shaft 62 transmits the engine speed from flyweight governor 34 to sensor 68, and includes first end 70 having radially extending rotary lever 72, and second end 74 which extends through engine housing 22 to rotary sensor 68. Rotary shaft 62 is rotationally supported by bushing 76 within housing 22. Lever 72 is positioned in contact with spool 56 so that axial translation of spool 56 displaces lever 72 to rotate rotary shaft 62. Thus, as governor assembly 34 is driven above a predetermined speed, rotary shaft 62 and sensor 68 are rotated proportionally to the speed of engine 20.
Coil spring 64 is coupled between rotary shaft 62 and engine housing 22 and provides resistance to rotation of rotary shaft 62. Thus, as the engine speed slows and weights 54 of flyweight governor 34 pivot inwardly, allowing spool 56 to translate toward governor gear 32, coil spring 64 rotates rotary shaft 62 such that rotary lever 72 remains in operational contact with spool 56, thereby returning rotary shaft 62 to its undisplaced, low speed rotational position.
Although located external to engine housing 22 in the exemplary embodiment, coil spring 64, spring housing 66, and/or sensor 68 may alternatively be positioned within the interior of engine housing 22, and flyweight governor assembly 44 may be alternatively positioned exteriorly of engine housing 22. Additionally, although the exemplary embodiment includes rotary shaft 62 which is rotationally displaced by flyweight governor 34, other means of sensing engine speed and providing an input to sensor 68 may be used, for example, flyweight governor 20 may actuate a linear member, the position of which is sensed by a position sensor.
Referring to
For adjustment of the rotational tension applied on rotary shaft 62 by coil spring 64, spring housing 66 may be coarsely rotationally adjusted by aligning selected slots 88 with selected mounting holes 90 defined in engine housing 22, and then inserting fasteners 86 through slots 88 into mounting holes 90. The tension of coil spring 64 may then be finely adjusted by further rotating spring housing 66 with fasteners 86 extending through arcuate slots 88, followed by tightening fasteners 86 to secure spring housing 66 relative to engine housing 22. Similarly, the tension of coil spring 64 may be adjusted after initial assembly of sensor assembly 44 by loosening fasteners 86, rotating spring housing 66 to a selected position, and re-tightening fasteners 86.
In the embodiment shown in
Mechanical calibration adjustment of speed signal 48 may be provided by rotating sensor housing 92 relative to engine housing 22. Specifically, as shown in
Cable 106 supplies an electric signal or voltage to one end of resistor 100 and a ground connection to another end of resistor 100. In the exemplary embodiment, the supplied signal is command signal 108 provided by operator control 46, as shown in FIG. 3. Wiper 110 is mounted on rotary shaft 62 at second end 74 thereof. Wiper 110 contacts resistor 100 and rotates relative to potentiometer disk 96 as rotary shaft 62 is rotated. Thus, resistor 100 and wiper 110 act as a variable voltage divider, with wiper 110 providing speed control signal 48 as a variable potential having a value between operator command signal 108 and ground, which varies according to the displacement of rotary shaft 62 and thus according to the speed of engine 20. Rotary sensor 68 receives second end 74 of rotary shaft 62 and detects the rotational displacement of rotary shaft 62. Based on the rotational displacement of rotary shaft 62, rotary sensor 68 outputs engine control signal 48 (
Referring to
Speed command signal 108 is provided to potentiometer 98 of rotary sensor 68. Rotary sensor 68 is driven by mechanical governor 34 such that speed control signal 48 output at wiper 110 is proportionally equal to or relatively close to command signal 108 for a low speed or under speed condition, and proportionally less than command signal 108 for a high or over speed engine condition, as shown graphically in FIG. 5. This arrangement provides for control of the engine speed under variable engine load conditions as the engine speed may tend to decrease or increase from the commanded speed with changing engine loading. Although command signal 108 is provided for controlling engine speed, modification of command signal 108 is modified by rotary sensor 68 to produce speed control signal 48; therefore, control signal 48 is a function of both commanded and actual engine speed. Alternatively, the output of rotary sensor 48 may supply operator control 46 and the output of operator control 46 providing control signal 48, also a function of both commanded and actual engine speed.
Referring to
As shown in
Engine control system 50 may also control an engine having fuel injector 116. Referring still to
Second exemplary engine control system 120, shown in
Third exemplary engine control system 130, shown in
Advantageously, flyweight governor 34 and sensor 68 of engine control systems 50, 120, 130 provide control signal 48 which may be related to actual and commanded engine speed, which may be used to control the intake system of an engine, and which may be easily electrically or electronically filtered, buffered, amplified, limited, or attenuated to better control the magnitude and oscillation of transient speed adjustments generally associated with known engine control systems which only include mechanical components. It is also advantageous in many applications related to small internal combustion engines to provide electrically transmitted signals, rather than signals transmitted by cables or other mechanical conduits.
Other linear operations adjusting the actual engine speed to the commanded engine speed, including increasing or decreasing the engine speed, filtering engine speed transients, and other control operations known in the art, may also be incorporated into engine control system 50, 120, and 130. For example, the outputs of operator control 46 and governor sensor 68 to adjust throttle signal 126 and fuel control signal 128, based on a fixed proportion determined by discrete analog circuit elements, or based on a stored schedule or function.
Third exemplary engine control system 130 may also include other sensors in order to provide for easy starting and optimum efficiency over a range of ambient and engine operating temperatures and conditions. Throttle control signal 126 is provided by adjusting the output of operator control 46 according to the actual engine speed sensed by governor sensor 68. Engine crankshaft 26 drives flyweight governor 34 in accordance with the engine speed, as described above for the first exemplary embodiment. Rotary governor shaft 62 couples flyweight governor 34 to sensor 68, and tension spring 64 is coupled with rotary shaft 62 so that displacement of rotary shaft 62 is normally biased to provide a higher signal output TO1 from sensor 68 for a lower engine speed, as shown in FIG. 8A.
Operator control 46 provides an operator-commanded speed signal having a higher signal output TO2 from operator control 46 for a higher commanded speed, as shown in FIG. 8B. Throttle signal 126 is determined by ECM 124 as a function of TO1 and TO2. Zero calibration 132 (
As shown in
Third exemplary engine control system 130 also provides engine control in response to ambient and engine operating conditions. Specifically, exhaust temperature sensor 136, shown mounted in exhaust passage 40, which is coupled to muffler 138 in
Additional sensors used to determine throttle control signal 126 and/or fuel control signal 128 may also be included and coupled to ECM 124, for example, mass air sensor 144 and cylinder head temperature sensor 142.
In the case of starting a cold engine in cold conditions, it is desirable to provide a rich fuel-to-air mixture, and thus a higher fuel control signal 128 for increased fuel flow. Therefore, as shown in
As exhaust gas temperatures are directly related to a rich or lean mixture, as shown in
Depending on the implementing circuit configuration, the output of intake temperature sensor 140 may inversely relate to intake temperature, and the output of exhaust temperature sensor 136 may proportionally relate to exhaust temperature, as shown in
In order to limit the leaning effect that exhaust temperature sensor 136 would have during a cold-start operating condition, exhaust temperature sensor 136 may be disabled under cold-start conditions, such as by intake temperature sensor 140 sensing a temperature below a preset level.
Intake mass airflow sensor 144 may be implemented, for example, as shown in FIG. 10. Throttle 114 includes intake opening 146, narrowing venturi 148, and intake pipe connection 150. As throttle actuator 112 adjusts throttle plate 152, thereby restricting the airflow through throttle 114, the pressure differential generated at narrowing venturi 148 varies proportionally with the mass airflow into engine 20. Throttle actuator 112 may be biased by an internal spring to a position that closes throttle plate 152, thereby restricting airflow into the cylinder of engine 20. Venturi tube 154 conducts vacuum to cylinder 156, in which piston 158 translates against spring 160 in accordance with a differential between ambient air pressure 162 and the lower pressure present in venturi tube 89. As piston 158 translates, connecting member 164 actuates intake mass airflow sensor 144 and fuel pump cutoff switch 166, which supplies power to fuel pump 168 (FIG. 9).
Intake mass airflow sensor 144 may be a variable resistor, such as a potentiometer, that is mechanically driven by connecting member 164. Alternatively, intake mass airflow sensor 144 may be another sensor type capable of measuring pressure or the displacement of connecting member 164. Thus, intake mass airflow sensor 144 provides a variable voltage or current signal proportional to the mass airflow through throttle 114. Additionally, fuel pump cutoff switch 166 provides a safety shutoff for fuel pump 168 when insufficient airflow is present through throttle 114, i.e., engine 20 is not running or drawing air through throttle 114.
Referring to
Referring to
The output signal of variable resistor R1 is provided to variable resistor R4, which is coupled in series with variable resistor R5 and throttle actuator 112. Rotary governor sensor 68 comprises variable resistor R4 and, as shown in
Exhaust temperature sensor 136 comprises thermistor R6, or a similar temperature-sensing device, such as a resistance temperature detector (RTD). Intake mass airflow sensor 144 comprises variable resistor R8. Third exemplary engine control system 130 includes only one of exhaust temperature sensor 136 and intake mass airflow sensor 144. Intake temperature sensor 140 comprises thermistor R7, or a similar temperature-sensing device such as an RTD.
Either exhaust temperature sensing device 136 or intake mass airflow sensor 144 and intake temperature sensor 140 are coupled in series between variable resistor R1 and battery B1 ground. Fuel control device 118 is coupled to the node between the two sensors. The signal reference IOref for fuel control device 118 may be coupled to resistor R3 of zero adjust circuit 132, or to another node in engine control system 130, for example, battery B1 ground.
As shown in
Referring to
The fuel pressure, and therefore the fuel flow, at fuel injector 116 is controlled by a combination of the flow restriction provided by restricting orifice 182 and the fuel pressure created by fuel pump 176. To control the resulting fuel flow through fuel injector 116, fuel pump 176 is driven by variable speed motor 118a, which serves as the fuel control device discussed above. Thus, variable speed motor 118a may be driven by fuel control signal 128 in order to provide a desired fuel flow to engine 20. By adjusting the range of fuel control signal 128, for example, by adjusting output calibration 134 and zero calibration 132 in third exemplary engine control system 130, the fuel pressure can be controlled between 0 psi and a value approaching the deadhead pressure of pump 176.
The fuel pressure for second exemplary fuel system 188 and therefore the fuel flow through fuel injector 116 is determined by the constant speed of and therefore fuel flow through fuel pump 176 and the variable fuel flow through return line 182, which is controlled by fuel bypass regulator 192. To achieve a constant fuel flow at pump 176, motor 190 is driven by a fixed power source, such as battery B1. To control the return line 182 flow and therefore the fuel flow through fuel injector 116, fuel bypass regulator 192 is actuated by solenoid 118b. Solenoid 118b may be driven by fuel control signal 128. Solenoid 118b and fuel bypass regulator 192 provide the fuel control device discussed above and provide linear fuel flow control of fuel system 188.
Fuel bypass regulator 192, which may be, for example, a device such as the one disclosed by U.S. patent application Ser. No. 10/641,556, entitled “Bypass Pressure Regulator,” by Rado, filed Aug. 15, 2003, the assignee of which is the assignee of the present application, the disclosure of which is hereby incorporated herein. While the referenced disclosed bypass regulator includes a valve and spring to provide fuel flow when the fuel pressure exceeds a certain preset level, fuel bypass regulator 192 provides a variable fuel flow and therefore a variable fuel pressure by adding linear solenoid 118b which adjusts the pressure that spring 194 applies to valve shuttle 196 of regulator 192. The inventive arrangement of fuel bypass regulator 192 and solenoid 118b allows fuel control signal 128 to regulate the fuel flow through fuel return line 182, thereby providing for linear control of fuel flow through fuel injector 116.
While this invention has been described as having exemplary embodiments, the present invention can be further modified within the spirit and scope of this disclosure. This application is therefore intended to cover any variations, uses, or adaptations of the invention using its general principles. Further, this application is intended to cover such departures from the present disclosure as come within known or customary practice in the art to which this invention pertains and which fall within the limits of the appended claims.
This application claims the benefit of U.S. Provisional Application No. 60/416,859 filed Oct. 8, 2002 and claims the benefit of U.S. Provisional Application No. 60/448,263 filed Feb. 17, 2003.
Number | Name | Date | Kind |
---|---|---|---|
2883975 | Spetner | Apr 1959 | A |
2971596 | Davis et al. | Feb 1961 | A |
4409940 | Gaus | Oct 1983 | A |
4422420 | Cromas et al. | Dec 1983 | A |
4430975 | Ishida et al. | Feb 1984 | A |
4867261 | King | Sep 1989 | A |
4884541 | Marriott | Dec 1989 | A |
4887684 | King | Dec 1989 | A |
5103125 | Ogden | Apr 1992 | A |
5141070 | Hickmann et al. | Aug 1992 | A |
5558062 | De Minco et al. | Sep 1996 | A |
5672818 | Schaefer et al. | Sep 1997 | A |
5901683 | Patel | May 1999 | A |
Number | Date | Country | |
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20040123837 A1 | Jul 2004 | US |
Number | Date | Country | |
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60448263 | Feb 2003 | US | |
60416859 | Oct 2002 | US |