Method to improve engine synchronization performance

Information

  • Patent Grant
  • 6745118
  • Patent Number
    6,745,118
  • Date Filed
    Thursday, December 6, 2001
    22 years ago
  • Date Issued
    Tuesday, June 1, 2004
    20 years ago
Abstract
A method for determining the angular position of an internal combustion engine throughout an engine cycle, the method includes the steps of providing a crankshaft having a plurality of teeth, the crankshaft completing two revolutions per engine cycle. A camshaft is provided having a plurality of teeth, the camshaft completing one revolution per engine cycle. An engine controller is provided. A sample size of the engine cycle is set in each of two concurrent engine cycles. The teeth of the plurality of teeth are counted on the camshaft found in the sample sizes. The crank position is then determined according to the teeth appearing in the sample sizes.
Description




FIELD OF THE INVENTION




The present invention relates generally to engine synchronization, and more particularly to a method of identifying the crankshaft phase from the camshaft location resulting in engine synchronization at a reduced time.




BACKGROUND




Generally in a conventional four stroke engine, an electric engine controller must determine the angular position of the engine by processing signals from sensors on the cam and crank shafts. The four stroke engine cycle repeats every two revolutions of the crankshaft or 720 degrees of crankshaft rotation. The crankshaft signal however, repeats every 360 degrees of crankshaft rotation. The camshaft rotates at half speed of the crankshaft, therefore the camshaft signal repeats every 720 degrees of engine rotation. Information from the camshaft is required to determine which half (or phase) of the 720 degree cycle the crankshaft is in. Normally the crankshaft signal is used to control the engine because of its higher accuracy and the camshaft is used only as a phase reference.




To start the engine quickly, synchronization must be achieved as soon as possible. The crankshaft has reference points every 180 degrees allowing the crankshaft position to be determined around 210 degrees. However the phase is not known based on the crank alone, therefore the engine position can be x or x+360 degrees. The phase cannot be determined until the engine position is determined uniquely from the camshaft signal. The camshaft has fewer teeth to generate a signal from, therefore more engine rotation is needed to achieve synchronization on the camshaft signal. A method is needed to exploit information available from the camshaft signal in order to reduce the overall synchronization time.




SUMMARY OF THE INVENTION




According to a preferred embodiment of the present invention, a method for determining the angular position of an internal combustion engine throughout an engine cycle is provided. The method includes the steps of providing a crankshaft having a plurality of teeth, the crankshaft completing two revolutions per engine cycle. A camshaft is provided having a plurality of teeth, the camshaft completing one revolution per engine cycle. An engine controller is also provided. A sample size of an engine cycle is designated in each of two concurrent engine cycles. The teeth are counted which appear on the camshaft in the sample sizes. The crankshaft position is determined according to the teeth appearing in the sample sizes.




Further areas of the present invention will become apparent from the detailed description provided hereinafter. It should be understood however that the detailed description and specific examples, while indicating preferred embodiments of the invention, are intended for purposes of illustration only, since various changes and modifications within the spirit and scope of the invention will become apparent to those skilled in the art from this detailed description.











BRIEF DESCRIPTION OF THE DRAWINGS




The present invention will become more fully understood from the detailed description and the accompanying drawings, wherein:





FIG. 1

is a perspective view of an engine block.





FIG. 2

is a perspective view of an engine control unit incorporating the low resolution processor according to a first embodiment of the present invention.





FIG. 3

is a representation of the collection of data groups referred to in the low resolution processor.





FIG. 4

is a representation of a lookup table assigned for each collection of data groups used according to the first embodiment of the present invention.





FIG. 5

is a flow chart representation of the fast lock algorithm employed according to a second embodiment of the present invention.





FIG. 6

is an example of the waveform from the cam and crank sensors.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




The following description of the preferred embodiment(s) is merely exemplary in nature and is in no way intended to limit the invention, its application, or uses.




With initial reference to

FIGS. 1 and 2

, a camshaft


12


and crankshaft


14


are shown operatively associated with engine block


10


. Engine block


10


has been removed from vehicle


20


for illustration. It will be readily appreciated by those skilled in the art that camshaft


12


, crankshaft


14


and engine block


10


are merely exemplary and may comprise other variations within the scope of this invention.




Generally in a conventional four stroke engine, an electric engine controller or engine control unit must determine the angular position of the engine


10


by processing signals from sensors (not shown) on the camshaft


12


and crankshaft


14


. The four stroke engine cycle repeats every two revolutions of the crankshaft


14


or 720 degrees of crankshaft


14


rotation. The crankshaft signal however, repeats every 360 degrees of crankshaft


14


rotation. The camshaft


12


rotates at half the speed of the crankshaft


14


, therefore the camshaft signal repeats every 720 degrees of engine rotation. Information from the camshaft


12


is required to determine which half (or phase) of the 720 degree cycle the crankshaft


14


is in.




Turning now to

FIG. 2

, an engine control unit (ECU)


16


is shown. Wiring assembly


18


connects the ECU to engine


10


. A power relay


22


and fuel pump relay


24


extend from the wiring assembly


18


and attach to the ECU


16


. The ECU


16


performs various functions such as timing requirements, fuel concentration, emission control among others. Those skilled in the art will recognize that ECU


16


configuration is merely exemplary and may comprise other configurations which incorporate additional or fewer electrical connectors.




With continued reference to FIG.


2


and additional reference to

FIGS. 3 and 4

, ECU


16


incorporates a logic operator


30


having a low resolution processor


32


including a multi-bit lookup table


38


(FIG.


4


). Each multi-bit entry in the table


38


corresponds to one specific engine position and defines those operations that are to take place at that point in the engine cycle. The logic operator


30


also contains other circuitry that tracks the engine angular position.




The operation of the engine control using the lookup table


38


will now be described in greater detail. Conventionally, engine position may be extrapolated to a resolution such as 0.1 degrees of crankshaft rotation. According to this invention, the engine position is determined at a lower resolution such as, for example, 10 degrees of crankshaft rotation. According to this example, each 10 degrees of crankshaft rotation comprises a data group


36


, the data groups collectively illustrated as data groups


40


. It will be appreciated that any resolution which evenly divides into 720 degrees may alternatively be used.




Referencing now

FIGS. 1-4

, as the crankshaft position reaches 0 degrees, 10 degrees, 20 degrees etc., the logic operator


30


reads the corresponding low resolution processor


32


register from the table


38


. In the exemplary 11 bit table


38


shown, each bit represents a specific task to be performed. For each 10 degrees of crankshaft rotation, a table


38


is referenced and the corresponding task is determined from the categories of operations in each bit.




Turning now to

FIG. 4

, the bits assigned to each table


38


will be described. When the accumulate period data bit


50


is set, the time period over the last ten degrees of crankshaft


14


rotation is accumulated to a working register. When the first zero is read after a string of one or more one's, the working register is transferred to a readable register. A two bit accumulate data field


54


,


56


is used to accumulate the time period over the last 10 degrees of engine rotation to one of 3 working registers. When the transfer working register bit


52


is set, the working registers are transferred to a readable register and then cleared. Two generate pulse bits


58


,


60


are used to generate a pulse on an external pin (not shown), each producing a pulse of 0.1 degrees or 10 degrees respectively. When the period capture bit


62


is set, the elapsed time between the current and prior time the bit was set is stored. Interrupt bits


64


,


66


,


68


and


70


generate an interrupt to a microprocessor (not shown) when set. It will be readily understood by those in the art that the order and content of the bits arranged in table


38


is merely exemplary. Likewise, table


38


may also be configured to have a greater or lesser amount of bits.




According to a second aspect of the present invention, a fast lock method employed through the logic operator


30


of the ECU


16


will now be described. Once the crankshaft signal is synchronized or locked, it is not necessary to know the exact position of the engine


10


from the camshaft


12


signal, but only which phase the crankshaft


14


is in. As more edges of the camshaft


12


are read by the logic operator


30


, the number of possible engine positions goes down until eventually only one remains and lock is achieved. When there are several possibilities remaining it is possible to determine the engine phase by comparing the few possible camshaft locations with the position of the crankshaft position.




Allowing for build tolerances, chain stretch and other tolerances, the engine position as found independently from the camshaft


12


and crankshaft


14


signals should agree fairly closely. Therefore, when crankshaft


14


lock is reached and the camshaft


12


is still unlocked, the camshaft


12


position should be within the range y±χ or (y+360)±χ; where y is the position determined using the crankshaft and χ is the tolerance. Once the camshaft


12


position has been narrowed down to the point where there is a potential position in one of the ranges but not the other, the crankshaft


14


phase is then known even though the camshaft


12


position has not been determined yet. The logic operator


30


waits until there are 3 or less possible marked camshaft


12


locations. If exactly one of the marked locations falls within the ranges described above, then the crankshaft


14


phase is known and the camshaft


12


is simultaneously locked using the fast lock method.




Turning now to

FIGS. 5 and 6

, the fast lock algorithm


100


will be described. At block


110


the algorithm is started. A cam edge is read at block


112


and the cam locking ratio tests are performed at block


114


. At decision block


116


it is determined if the crankshaft


14


is locked. If the crankshaft


14


is not locked, the process returns to block


112


. If the crankshaft


14


is locked, the process proceeds to decision block


118


. At decision block


118


it is determined if there are 3 or less marked cam positions remaining. If not, the process returns to block


112


. If there are 3 or less cam positions remaining, the process proceeds to block


120


wherein for crankshaft


14


position


1


, the possible camshaft


14


positions possible within χ degrees are counted; χ degrees referring to the width or sample size of the fast lock or reference window


104


. The process then proceeds to block


122


wherein the number of possible camshaft


12


positions determined from block


120


is stored as “A”. Next, the possible camshaft


12


positions for crankshaft


14


position


2


within χ degrees are counted at block


124


and the answer is stored as “B” at block


126


. The process then proceeds to decision block


128


wherein it is determined if “A” is 1 and “B” is 0. If so, then at block


130


it is determined that crankshaft


14


position


1


is correct and the camshaft


12


position is also known and locked. If not, then at decision block


132


it is determined if “A” is 0 and “B” is 1. If not, the process returns to block


112


. If so, then at block


134


it is determined that crankshaft


14


position


2


is the correct one and camshaft


12


position is also known and locked.




The invention being thus described, it will be obvious that the same may be varied in many ways. Such variations are not to be regarded as a departure from the spirit and scope of the invention, and all such modifications as would be obvious to one skilled in the art are intended to be included within the scope of the following claims.



Claims
  • 1. A method for determining an angular position, at startup, of an internal combustion engine having a crankshaft and a camshaft each including a plurality of position indicating teeth, said method comprising the steps of:determining a crankshaft position by sensing the plurality of position indicating teeth on said crankshaft; and determining a crankshaft phase position, comprising the steps of: setting a sample size of the engine cycle in each of two concurrent engine cycles; assigning a predetermined amount of said plurality of teeth of said camshaft as marked teeth; counting the marked teeth of said plurality of teeth on said camshaft found in said sample sizes; and determining said crankshaft phase position according to the marked teeth appearing in said sample sizes.
  • 2. The method according to claim 1, wherein said predetermined amount of marked teeth is 3.
  • 3. The method according to claim 2, wherein the step of determining the crank position includes the step of identifying a single marked cam tooth within said sample sizes.
  • 4. A method for determining an angular position of an internal combustion engine having a rotating crankshaft and a rotating camshaft each including a plurality of position indicating teeth, said method comprising the steps of:assigning a portion of a first and second concurrent engine cycle as a first and second reference window; assigning a predetermined amount of said plurality of teeth as marked teeth; identifying an amount of said plurality of marked teeth of said rotating camshaft within said first and second reference window; and determining the position of said rotating crankshaft based on the amount of marked teeth identified within said first and second reference windows.
  • 5. The method for determining the position of a rotating crankshaft relative to a rotating camshaft throughout an engine cycle of an internal combustion engine of claim 6, wherein said predetermined amount of marked teeth is 3.
  • 6. The method for determining the position of a rotating crankshaft relative to a rotating camshaft throughout an engine cycle of an internal combustion engine of claim 5, wherein the step of determining the position of said rotating crankshaft includes the step of identifying a single marked tooth of said rotating camshaft in said first and second reference windows.
US Referenced Citations (15)
Number Name Date Kind
4338813 Hunninghaus et al. Jul 1982 A
5387253 Remboski et al. Feb 1995 A
5447143 Ott et al. Sep 1995 A
5497748 Ott et al. Mar 1996 A
5577475 De Backer et al. Nov 1996 A
5604304 Kokubo et al. Feb 1997 A
5736633 Magner et al. Apr 1998 A
5823166 Entenmann et al. Oct 1998 A
5862507 Wu et al. Jan 1999 A
6041647 Matsuoka Mar 2000 A
6202611 Regueiro Mar 2001 B1
6212467 Guzella et al. Apr 2001 B1
6253145 Garrard et al. Jun 2001 B1
6278932 Baumel et al. Aug 2001 B1
6283093 Lautenschuetz et al. Sep 2001 B1