The present disclosure relates to a fuel sensing system and method of operation, and more particularly, a fuel sensing system and process for monitoring fuel levels in outdoor power equipment.
Fuel sensors coupled to indicator displays or fuel gauges are frequently used in outdoor power equipment. Outdoor power equipment includes, but is not limited to, riding lawn mowers, lawn and agricultural tractors, snowmobiles, snowblowers, jet skis, boats, all terrain vehicles, bulldozers, generators, and the like. Fuel sensors indicate to the operator of the power equipment how much fuel remains in the fuel supply or tank.
The fuel sensors indicator displays in a riding mower or tractor is frequently mounted to the dash panel, typically in view with the operator while operating the lawn mower. Further discussion relating to developments in indicator displays are discussed in U.S. Pat. No. 7,777,639 that issued on Aug. 17, 2010. The '639 patent is owned by the assignee of the present application and is incorporated herein by reference in their entirety.
One example embodiment of the present disclosure includes a fuel sensing system and method of measuring and monitoring an amount of fuel in a storage tank for power operated equipment. The method comprises the steps of positioning a fuel sensor assembly within a storage tank that supports fuel provided to the power operated equipment during operation and generating a pulse width modulated output signal with a pulse width modulation generating circuit. The pulse width modulated output signal provides a signal width proportional to the fuel level in the storage tank. The method also comprises processing the pulse with modulated output signal with non-transient computer readable medium by one or more processors internal to a microcontroller to form an output value indicating the amount of fuel in the storage tank and displaying the output value on an indicator display mounted on the power equipment.
Another example embodiment of the present disclosure includes a system measuring and monitoring an amount of fuel in a storage tank for power operated equipment comprising a control circuit having a non-transitory computer readable medium storing machine executable instructions executable by a processor coupled to and in communication with the control circuit for reading and processing a pulse width modulated signal to form a non-transitory output value indicating the amount of fuel in a storage tank. The system further comprises a display for displaying the non-transitory output value for viewing by a user of the system.
While another example embodiment of the present disclosure includes an apparatus for measuring and monitoring an amount of fuel in a storage tank comprising a fuel sensor assembly to be positioned during use within a storage tank that supports fuel provided to power operated equipment during operation, the fuel sensor assembly having a pulse width modulation circuit for generating a pulse width modulated signal wherein the pulse width modulated signal has a signal width proportional to the fuel level in a storage tank and a control circuit remotely located from fuel sensor assembly, the control circuit having a non-transitory computer readable medium storing machine executable instructions executable by a processor coupled to and in communication with said control circuit for reading said pulse width modulated signal to form a non-transitory output value indicating the amount of fuel in a storage tank.
The foregoing and other features and advantages of the present disclosure will become apparent to one skilled in the art to which the present invention relates upon consideration of the following description of the invention with reference to the accompanying drawings, wherein like reference numerals refer to like parts unless described otherwise throughout the drawings and in which:
Referring now to the figures generally wherein like numbered features shown therein refer to like elements throughout unless otherwise noted. The present disclosure relates to a fuel sensing system and method of operation, and more particularly, a fuel sensing system and process for monitoring fuel level in outdoor power equipment with heightened accuracy.
As stated above, the power equipment 10 uses a fuel sensing system 12 that comprises an indicator display 20, located typically on the dash 14 of the riding mower as illustrated in
As illustrated in
The float 38 moves up and down the stem 34 in the directions of arrows A as the level of the fuel (F) moves up and down in the tank 26, indicated by arrows B. As the float 38 moves up and down the stem 34, supply power 40 from, for example, a battery passing through a voltage regulator (not shown) provides a direct current DC signal 42A, in which the signal's magnitude is altered magnetically based on the location of the float corresponding to the fuel level within the tank. Thus, the magnitude of the DC signal 42A is proportional to the level of the fuel in the tank 26 of the power equipment 10.
While
Unlike conventional fuel sensors that use an analog signal from a rotary potentiometer to generate a signal as an indication the fuel level in the tank, the fuel sensor assembly 18 includes a pulse width modulator circuit 44. The PWM circuit 44, in one example embodiment includes a PWM signal generator constructed from an analog circuit, a digital circuit, a discrete integrated circuit IC, microcontroller, or any combination thereof as would be appreciated by those skilled in the art.
The PWM circuit 44 alters the DC signal 42A to a PWM signal 42B shown in
If noise or wiring in the power equipment 10 induces in this conventional system 0.0195V of signal onto an existing half full tank signal of 2.5 VDC, a new signal of 2.5195V is received. This error by the count amount of 0.0195V represents a different and inaccurate fuel level to the sensing and display system of the power equipment.
Advantageously, the PWM signal 42B of the present disclosure generated by PWM circuit 44 as part of the fuel sensor assembly 18 and shown in
Referring now to
Input power to the control circuit 16 is supplied by connector pin 46 and ground by connector pin 48. Capacitor 50 filters power from any noise or transients exposed to the circuit 16. The control circuit 16 employs a rectifier 52 that provides reverse polarity protection for the incoming power supply. In one example embodiment, the power supply is a 12V DC battery.
The control circuit 16 further comprises a voltage regulator circuit 54 consisting of resistors 54A and 54B, transistor 54C, zener diode 54D and capacitor 54E. The voltage regulator circuit 54 provides power to integrated circuits 56, 58. Resistor 54A is a current limiting resistor that protects transistor 54C in case of a short to ground occurs. Resistor 54B supplies zener current to zener diode 54D. The zener diode 54D supplies 5.6V to transistor 54C. In the voltage regulator circuit 54, the emitter lead of transistor 54C is regulated at approximately 5 VDC. A capacitor 54E acts as an output filter for 5V load transients.
An additional voltage regulator circuit 62 consists of resistors 62A and 62B, transistor 62C, zener diode 62D, and capacitor 62E. The voltage regulator circuit 62 provides power to two remote fuel sensor assemblies 18. Resistor 62A is a current limiting resistor that protects transistor 62C in case of a short to ground occurs. Resistor 62B supplies zener current to zener diode 62D. The zener diode 62D supplies 6.2V to the transistor 62C. In the voltage regulator circuit 62, the emitter lead of transistor 62C is regulated at approximately 5 VDC. The capacitor 62E acts as an output filter for 5V load transients of the fuel sensor assemblies 18.
A diode 66 provides reverse polarity protection for the output 5 VDC at connector 68. A capacitor 70 provides a high frequency filter for output 68.
The fuel sensor assembly 18 and particularly the PWM circuit 44, for a left “L” and right “R” fuel tank receive their respective supply power from output 68 as illustrated in the example embodiment of
The PWM signal 42B of
A low-pass filter is formed with resistor 74 and capacitor 76 for the PWM signal 42B. Diode 78 provides a clamp to 5 VDC for the PWM signal 42B. Diode 80 provides a clamp to ground for the PWM signal 42B. Resistor 82 is a pull-up resister for the PWM generator 44 and provides current to an internal output transistor of the generator. A Schmitt trigger inverter 84 reduces the noise influence on the measurement of the PWM 42B signal at pins 1 and 2 in the right fuel tank circuit at pins 3 and 4 in the left fuel tank. Capacitor 86 is a noise decoupling capacitor for the Schmitt trigger inverter 84A. Output pin 2 of Schmitt trigger 84A is the input into microcontroller 56 at pin 22 for measurement and averaging of the PWM signal 42B. Output pin 3 of the Schmitt trigger 84B is the input to the microcontroller 56 at pin 23 for measurement and averaging of the PWM signal 42B.
In the illustrated example embodiment, microcontroller 56 is a PIC chip. In particular, the PIC chip is identified under part number 16F1933T, which the specification data sheet is incorporated herein by reference. The microcontroller 56 measures the pulse width and period of the pulse width modulated signal 42B at input pins 22 and 23 for respective left L and right R tanks having respective fuel sensor assemblies 18. The measurement by the microcontroller 56 of the PWM signal 42B of both the width and period are then translated to percent duty cycle via a formula represented by percentage duty cycle is equal to the pulse width divided by the period. The percentage duty cycle that is then translated for display by illuminating the corresponding bars of the LCD in the gage 20 for respective tanks as illustrated in
The microcontroller 56 includes one or more processors, such as one or more microprocessors, digital signal processors (DSPs), combinations thereof or such other devices known to those having ordinary skill in the art. Each processor is coupled to an at least one memory device (also referred to herein as “a memory”), such as random access memory (RAM), dynamic random access memory (DRAM), and/or read only memory (ROM) or equivalents thereof, that maintains data and programs/instructions that may be executed by the one or more processors. Unless otherwise specified herein, all functions described as being performed herein by the microcontroller 56 is performed by their respective one or more processors, which are configured to perform such functionality based on the data and programs/instructions maintained in the corresponding memory.
Illustrated in
Illustrated in
The main loop of the operation 200 shown in
At 210, a master timer used to count time and/or store time associated with the PWM signal 42B in EEPROM and RAM. At 212, the time from the PWM signal 42 is decoded, by for example an A/D converter internal to the microcontroller 56 stored in RAM.
At 214, the microcontroller 56 reads eight (8) separate signals from the PWM generator from the fuel sensor assemblies 18. Each reading is collected by the microcontroller 56 at an average rate of 1 reading or PWM 42B signal every 18 seconds. These eight (8) readings are then averaged by processors internal to the microcontroller 56 to create a final value 230A/230B, relating to fuel level for each fuel sensor assembly 18 for display on the liquid crystal display (LCD) as shown in
The fuel tank 26 level readings used by the main loop 210-216 are generated by two separate interrupt routines, 218 and 220. Each interrupt routine waits for the sensor 18 value to go high in the PWM signal 42B, and then processors within the microcontroller 56 measure the amount of time it is high for the width measurement. Then the interrupts 218 and 220 wait until the sensor 18 value of the PWM signal 42B goes high again to generate the period measurement. With these two measurements, relating to time and period, the operation 200 computes the pulse width value based on the following formula PWM value=pulse width/pulse period written as instructions from software or firmware forming the operation 200 internal to the microcontroller 56.
This operation 200 also indicates to the operator that a fuel sensor assembly 18 is not connected by detecting the loss of the PWM signal 42B. Upon loss of signal 42B, blinking occurs in corresponding left or right tank bars. This is useful for troubleshooting and for the operator to ensure the system is working properly.
When the fuel gauge 20 powers up, a power up routine, which measures each fuel tank eight (8) times to fill up the running average buffer, as indicated by the timing interrupt 222. The timing interrupt permits the operator to fill up the tank and not have to wait for 8×18 seconds, or 144 seconds before indicating the value of the fuel level.
What have been described above are examples of the present disclosure. It is, of course, not possible to describe every conceivable combination of components or methodologies for purposes of describing the present disclosure, but one of ordinary skill in the art will recognize that many further combinations and permutations of the present disclosure are possible. Accordingly, the present disclosure is intended to embrace all such alterations, modifications, and variations that fall within the spirit and scope of the appended claims.
The following application is a Nonprovisional patent application that claims priority to co-pending U.S. Provisional Patent Application Ser. No. 61/707,149 filed Sep. 28, 2012 entitled FUEL SENSING SYSTEM AND METHOD OF OPERATION. The above-identified application is incorporated herein by reference in its entirety for all purposes.
Number | Date | Country | |
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61707149 | Sep 2012 | US |