Method and apparatus for determining engine exhaust backpressure

Abstract: Apparatus for determining engine exhaust backpressure in a crankcase scavenged two-stroke engine (10) comprises means (48) for determining a period in the engine cycle during which the inlet and exhaust ports (34,26) of a cylinder (14) of the engine are both open and the pressure in an associated crankcase chamber (18) is substantially equal to engine exhaust backpressure due to airflow between the respective crankcase chamber (18) and exhaust port (26) during said period; a pressure sensor (46) and associated processor (50) for deriving a plurality of values (CCP) indicative of the air pressure in the crankcase chamber during the period, the procesor (50) calculating an average crankcase pressure from the plurality of derived values, and thereby obtaining a value (EBP) indicative of the average backpressure at the exhaust port and determining the amount of air trapped in the cylinder therefrom. An accurate measure of engine exhaust backpressure can thereby be obtained without exposing the pressure sensor (46) to the harsh environment of the engine exhaust.

Description: This invention relates to a method and apparatus for determining engine exhaust backpressure and more particularly for determining remotely the average backpressure at a cylinder exhaust port in a crankcase scavenged, two-stroke engine by averaging the pressure of air within a crankcase chamber during a portion of the engine operating cycle. In a direct fuel injected, crankcase scavenged, two-stroke engine, knowledge of the mass of air per cylinder available for combustion is required for the precise control of engine operating parameters such as spark advance, injection timing, and fuel requirements. Conventionally, the mass of air per cylinder inducted into the engine is measured during an engine cycle, by means of a standard mass airflow sensor, and then compensated for by a factor known as the cylinder trapping efficiency to determine the mass of air actually captured within a cylinder. The trapping efficiency is a function of engine design, engine rotational speed, the mass of air per cylinder inducted into the engine, and the exhaust backpressure. In a crankcase scavenged, two-stroke engine, the exhaust backpressure is especially significant with regard to the trapping efficiency because of the absence of engine valves. Instead of valves, this type of engine has inlet and exhaust ports opening into each cylinder wall. During the downstroke of a piston in a cylinder, the exhaust port is first uncovered by the moving piston to release combustion products, followed by the uncovering of the inlet port to enable the entry of a fresh charge of air for the next combustion event. As there is significant overlap in the periods of time during which the inlet and exhaust ports are open, a portion of the fresh air charge escapes out of the open exhaust port, and will not be available for the next combustion event. The larger the backpressure appearing at the exhaust port, the smaller will be the amount of air which escapes, due to the reduced pressure differential between the cylinder and the engine exhaust system. Also, as the backpressure increases, the resistance to airflow from the crankcase into the cylinder increases, thereby reducing the mass of air transferred. Since the average exhaust backpressure is equal to the local barometric pressure plus the pressure drop associated with the engine exhaust system, changes in the exhaust system, in the altitude of engine operation, or in local barometric pressure will affect the amount of fresh air which is available for combustion within a cylinder. For the above reasons, some measure of engine exhaust backpressure, either direct or indirect, is essential for proper engine control. Pressure sensors can be used to measure directly the exhaust backpressure within the exhaust system, however, such sensors are generally expensive and have poor durability due to the hostility of the exhaust system environment. Also, an average value for the exhaust backpressure, near the engine exhaust port, can be obtained indirectly by measuring barometric pressure, and then adding an estimated pressure drop associated with the engine exhaust system. The major disadvantage with this scheme is inaccuracy due to variations in the actual pressure drop across.the exhaust system caused by exhaust gas heating, changes in engine speed, and physical changes in the exhaust system with time. An alternative method for determining the air mass per cylinder in a crankcase scavenged engine has been previously disclosed in US application serial no. 377,383, (US patent no. 4,920,790) filed on July 10, 1989, by S. D. Stiles et al, and assigned to the applicant, and which corresponds to Australian patent application no. 55966/90; European patent application no. 90305476.5; and Japanese patent application no. 182533/90. Essentially, this alternative technique consists of deriving an estimate for the mass of air inducted and compressed within the crankcase chamber, prior to its transfer into the cylinder. A computer estimates the crankcase chamber air mass by integrating the pressure of the air under compression within crankcase chamber, with respect to change in crankcase volume, and then dividing by a factor containing the temperature of the crankcase air at the start of compression. A standard pressure sensor is used to measure the pressure within the crankcase chamber, and provides the computer with an input signal indicative of crankcase pressure. The temperature of the air within the crankcase chamber at the start of compression is derived from a manifold air temperature signal produced by a manifold absolute temperature sensor. The estimated value for the mass of air is then corrected for any leakage out of the crankcase chamber during compression. The leakage correction is a function of the barometric pressure, and the manifold absolute pressure, as given by the crankcase pressure signal when top dead centre occurs in the cylinder. Finally, this corrected value for the mass of air M', contained within the crankcase, is multiplied by the cylinder trapping efficiency, to obtain the mass of air transferred and captured within the cylinder, after closure of the air inlet port and the exhaust port. In a crankcase scavenged, two-stroke engine such as the above engine, one of the most significant factors affecting the amount of fresh air which enters the cylinder, and is subsequently lost out of the exhaust port, is the engine exhaust backpressure. The larger the backpressure in the exhaust port, the smaller will be the mass of air escaping, due to the reduced pressure differential between the exhaust port and the cylinder, and the smaller the mass of air transferred to the cylinder from the crankcase chamber, due to the corresponding increased resistance to airflow. Since changes in altitude, local barometric pressure, and the engine exhaust system affect the value of exhaust backpressure, the cylinder trapping efficiency can be compensated to account for these changes by including a correction based upon engine exhaust backpressure. Consequently, for proper engine control, an accurate and reliable technique is needed for determining engine exhaust backpressure. Consequently, an alternative, more accurate and dependable technique is sought for determining the exhaust backpressure of a crankcase scavenged two-stroke engine for use in engine control compensation. US-A-4,461,260 discloses a controller for a two-stroke crankcase scavenged engine in which the amount of air transferred to a cylinder from its associated crankcase chamber is determined by sensing, with a sensing device, the maximum pressure in the crankcase chamber immediately prior to opening of the scavenge passage of the cylinder and the minimum pressure immediately subsequent to closing of the scavenge passage. According to an aspect of the present invention, there is provided a method of determining engine exhaust backpressure in a crankcase scavenged two-stroke engine as defined in claim 1. According to another aspect of the present invention, there is provided a crankcase scavenged two-stroke engine as defined in claim 4. According to another aspect of the present invention, there is provided apparatus for determining engine exhaust backpressure in a crankcase scavenged two-stroke engine as defined in claim 7. Thus, exhaust backpressure can be measured remotely in the crankcase, rather than in the harsh environment of the exhaust system. The portion of the overlap interval, where the crankcase pressure substantially equals the exhaust backpressure, preferably excludes an initial portion of the interval associated with the equalization of pressure between the cylinder and its crankcase chamber. At the beginning of the overlap interval when the cylinder inlet port is first uncovered, a large pressure differential exists between the crankcase and the cylinder. Thus, during the initial portion of the interval, crankcase pressure is not indicative of exhaust backpressure. By excluding this initial portion from the predetermined portion of the interval, a more accurate indication of the average exhaust backpressure is obtained. Preferably, the crankcase pressure is derived by sampling the output of a conventional pressure sensor disposed within the crankcase chamber. This ability to measure the backpressure remotely, in terms of crankcase pressure, avoids the hostile environment of the exhaust system and improves the reliability and durability of the pressure sensor. Advantageously, the portion of the overlap interval is determined by rotational positions of the engine during the operating cycle. Consequently, the occurrence of that portion of the overlap interval can be derived from any type of sensor commonly used in determining engine rotational angle for other engine control functions. An advantage in determining exhaust backpressure in accordance with the principles of the present invention is that its value will reflect variations in barometric pressure and any changes in the pressure drop across the engine exhaust system. Consequently, correction of engine control based on exhaust backpressure will inherently include compensation for changes in altitude and shifts in local barometric pressure. Also, differences between production exhaust systems and any variations in engine exhaust systems due to damage or ageing will be automatically accounted for, without requiring recalibration of the engine control system. Additionally, other than a crankcase pressure sensor, no additional sensors or transducers are required to implement the preferred embodiment of the present invention, which is applied to a crankcase scavenged engine having a conventional computer control system, including means for sensing engine rotational angle. An embodiment of the present invention is described below, by way of illustration only, with reference to the accompanying drawings, in which: Figure 1 is a schematic diagram illustrating an embodiment of engine control system associated with a cylinder of a crankcase scavenged, two-stroke engine; Figure 2 is a graph of crankcase pressure and exhaust backpressure against engine rotational angle, which also shows the interval of overlap in the opening of cylinder inlet and exhaust ports; and Figure 3 is a flow chart representing program instructions for execution by the system of Figure 1. Referring to Figure 1, there is shown schematically a crankcase scavenged two-stroke engine, generally designated as 10, with a portion of the engine exterior cut away, exposing cylinder 14. Piston 12 resides within the wall of cylinder 14, with rod 16 connecting piston 12 to a rotatable crankshaft (not shown) disposed within crankcase chamber 18. Connected to engine 10 is an air intake manifold 20 with a throttle 22, and an exhaust manifold 24. Cylinder 14 communicates with exhaust manifold 24 and the remainder of the engine exhaust system (not shown), through exhaust port 26. Intake manifold 20 communicates with cylinder 14 and crankcase chamber 18 through a reed valve checking mechanism 28, which opens into a common air transfer passage 30 linking crankcase port 32 with inlet port 34 in the wall of cylinder 14. Cylinder 14 is provided with a spark plug 36 and an electric solenoid-driven fuel injector 38 projecting into combustion chamber 40. The operation of engine 10 will now be briefly described based upon the cycle occurring in cylinder 14. During the,upstroke, piston 12 moves from its lowest position in cylinder 14 toward top dead centre. While moving upwardly, piston 12 covers air inlet port 34 and exhaust port 26, closing them off from the combustion chamber 40, and thereafter, air is inducted into crankcase chamber 18 through reed valve 28. Air in combustion chamber 40, above piston 12, is mixed with fuel from injector 38 and compressed until spark plug 36 ignites the mixture near the top of the stroke. As combustion is initiated, piston 12 begins the downstroke, decreasing the volume of crankcase chamber 18 and compressing the air inducted therein, due to closure of reed valve 28. Toward the end of the downstroke, piston 12 uncovers exhaust port 26, through which combustion products are expelled from engine 10. Shortly thereafter, air inlet port 34 is uncovered, enabling the fresh air trapped within the crankcase chamber 18 to flow into cylinder 14, through the transfer passage 30. Since air inlet port 34 and exhaust port 26 are simultaneously open for a period of time, the entry of fresh air into cylinder 14 aids in driving combusted fuel products out the exhaust port 26. Also, a portion of the fresh air flowing into cylinder 14 escapes out the exhaust port, and will not be available for the next combustion event. The cycle begins anew when piston 12 reaches the lowest point in cylinder 14. The operation of engine 10 is controlled by computer 56, which is a conventional digital computer, and includes in this embodiment a central processing unit, random access memory, read only memory, an analogue-to-digital converter, input/output circuitry, and clock circuitry. Using input signals from various sensors, which will be described subsequently, computer 56 performs the standard computations required for engine control, and provides a pulsed output FUEL SIGNAL to fuel injector 38 and an output SPARK ADVANCE signal to ignition system 58. Ignition system 58 generates a high voltage SPARK signal, which is applied to spark plug 36 at the appropriate time, as determined by the SPARK ADVANCE signal supplied by computer 56, and the rotational position of engine 10. Ignition system 58 may include a standard distributor or any other appropriate device. Associated with engine 10 are various conventional sensors which provide input signals to computer 56. Located within the air intake manifold 20 is a temperature sensor 44 for measuring manifold air temperature (MAT). The input signal BARO represents the atmospheric barometric pressure near engine 10, and it may be obtained by employing a standard barometric pressure sensor, or derived by any other known means. Electromagnetic sensors 48 and 50 provide pulsed signals indicative of crankshaft rotational angle (ANGLE) and of the top dead centre (TDC) position for cylinder 14, by respectively sensing movement of the teeth on ring gear 52 and disk 54, which are attached to the end of the engine crankshaft. The pulsed TDC and ANGLE signals act as inputs to computer 56 and ignition system 58 and give the rotational position of the engine, which is needed for the timing of the SPARK and FUEL SIGNAL outputs. The crankshaft rotational angle ϑ from top dead centre in cylinder 14 may be obtained by counting the number of pulses occurring in ANGLE, after the TDC pulse, then multiplying the number of counted pulses by the angular spacing of the teeth on ring gear 52. Also, the engine speed in revolutions per minute (RPM) may be obtained by counting the number of TDC pulses which occur in a specified period of time, then multiplying by an appropriate conversion constant. Referring now to Figure 2, there is shown a typical plot of the crankcase pressure and exhaust gas backpressure, during one complete cycle within cylinder 14 of engine 10. The data represented by Figure 2 was measured using a 3 cylinder, 1.2 litre, two-stroke engine operating at 1000 revolutions per minute (RPM), under control of an embodiment of apparatus of the present invention. The design of the engine was such that the inlet port 34 and exhaust port 26 are simultaneously open during the interval of rotation from 120 to 240 degrees after top dead centre (ATDC) in cylinder 14. At the start of the interval of port opening overlap (120 degrees), inlet port 34 is opened, allowing the compressed air in crankcase chamber 18 to flow into cylinder 14. At approximately 140 degrees ATDC, the pressure equalizes between cylinder 14 and crankcase chamber 18, and the pressure in the crankcase then approximates the exhaust backpressure over the remainder of the port opening overlap interval (up to 240 degrees ATDC). As engine speed increases, the related number of rotational degrees required for the pressure equalization will also increase, although the applicants have found that such equalization will take place prior to 160 degrees ATDC for all expected speeds and loads within the normal operating range of the engine to which this embodiment has been applied. Of course, other engines may have different intervals of port opening overlap, which may be accounted for accordingly. The embodiment described takes advantage of the operating characteristics of engine 10, as depicted in Figure 2, and determines the backpressure appearing at exhaust port 26, by averaging samples of the crankcase pressure signal CCP provided by pressure sensor 46, during a predetermined portion of the port opening overlap interval. The occurrence of the overlap interval is derived from the ANGLE and TDC inputs to computer 56, which indicate the rotational position of engine 10. The cylinder trapping efficiency for engine 10 is then corrected, based upon the value of exhaust backpressure determined in this fashion. This compensated value for the cylinder trapping efficiency is then used by computer 56 in computing the proper fuel pulse width, injector timing, and spark advance for the control of engine 10. Referring now to Figure 3, there is illustrated a flow diagram of a routine executed by computer 56. The routine is entered at point 60, for each occurrence of top dead centre in cylinder 14, as initiated by a pulse in the TDC signal provided by sensor 50. At this point in time, the engine rotational angle ϑ is zero degrees. Computer 56 determines the value of ϑ based upon the input signals TDC and ANGLE as described previously. The program begins at step 62, where computer 56 samples the signal CCP to obtain the value of the pressure in crankcase chamber 18 at top dead centre within cylinder 14. Next in step 64, the variable MAP, representing the manifold absolute pressure, is assigned the value of the crankcase pressure found in step 62. Applicants have found that the crankcase pressure, at top dead centre, represents the pressure in the intake manifold 20, since the reed valve 28 has not yet closed and piston 12 is not yet compressing the air in crankcase chamber 18. At step 66, the variables N and SUM are both set equal to zero. N represents the number of samples of crankcase pressure CCP which will be averaged in determining exhaust backpressure, while SUM is used to accumulate the sum of the sampled crankcase pressure values. In addition, the variable ϑs is set to the value represented by ϑf. The variable ϑs represents a rotational angle of the engine where crankcase pressure is to be sampled for later averaging, while ϑf represents the rotational angle where the first sample of crankcase pressure is to be taken. In the preferred embodiment of the present invention, ϑf is set equal to 160 degrees ATDC. As mentioned previously, the interval of port opening overlap in engine 10 occurs for rotational angles ranging from 120 to 240 degrees ATDC. Applicants have found that by delaying the start of sampling of crankcase pressure until ϑf = 160 degrees ATDC, sufficient time is allowed after intake port 34 is uncovered for pressure equalization in the crankcase chamber 18 and cylinder 14. Of course, this value will vary for another engine having a substantially different porting structure. Next at step 68, the value for the mass of air M' trapped within crankcase chamber 18, is computed by integrating the crankcase pressure as indicated previously. In the next series of steps from 70 to 82, the average value for the exhaust backpressure EBP is determined by averaging samples of crankcase pressure CCP which have been sampled during the predetermined portion of the overlap interval. At step 70, a decision is made as to whether the engine rotational angle ϑ is equal to the sampling angle ϑs, where a sample of crankcase pressure is to be taken. The first time step 70 is encountered after top dead centre, ϑs will equal 160 degrees, as set in step 66 above. Thus, if engine 10 has not yet rotated to where ϑ = 160 degrees, step 70 is repeated until ϑ = 160 degrees, at which time the program proceeds to step 72. At step 72, a sample of crankcase pressure is obtained by sampling the signal CCP provided by pressure sensor 46. The value of sampled crankcase pressure is assigned to the program variable CCP. At step 74, a value for the variable SUM is computed by adding its previous value, represented by SUM₋₁, and the sampled value of crankcase pressure CCP. The first time step 74 is executed after top dead centre, SUM₋₁ will equal zero as set in step 66 above. Thereafter, SUM will represent the accumulated sum of crankcase pressure samples taken at the sampling angles defined by ϑs. At step 76, the value of N is incremented by 1 to account for the crankcase pressure sample added to SUM at step 74. N represents the total number of crankcase pressure samples that have been added at step 74. Next at step 78, a new value for the rotational sampling angle ϑs is computed by adding its previous value ϑs₋₁ and the sampling angle increment ϑ. In the preferred embodiment, ϑ is equal to 20 degrees, however, other embodiments are possible using different values for the sampling angle increment. In general, smaller values of ϑ will provide a more accurate numerical estimate for the average value of the crankcase pressure, during the predetermined portion of the overlap interval, limited of course by the data processing speed of computer 56, if no adjustment for this is made. At step 80, the decision is made as to whether the rotational angle ϑ is greater than ϑe, the end of the interval of port opening overlap, where the averaging of crankcase pressure ceases. For engine 10, ϑe is equal to 240 degrees ATDC, where intake port 34 is covered by the upstroke of piston 12. If ϑ is not yet greater than ϑe, the program proceeds to repeat steps 70 through 80 and take the next sample of crankcase pressure as defined by the new rotational sampling angle ϑs determined at step 78. If, however, ϑ is greater than ϑe, sampling ceases and the program proceeds to the next step 82. At step 82, the average value for the exhaust backpressure EBP is computed by dividing the sum of the crankcase pressure samples SUM by N, the number of samples taken. Thus, in the preferred embodiment, the average exhaust backpressure is assigned a value equal to the numerical average of samples of crankcase pressure taken over a portion of the interval of port opening overlap defined by rotational angles ranging from 160 to 240 degrees ATDC. Crankcase pressure is sampled at the specified engine rotational positions of 160, 180, 200, 220, and 240 degrees ATDC, for a total of five samples, which are then averaged to obtain the exhaust backpressure. At step 84, the program looks up a value for trapping efficiency TE in a look-up table stored in memory, as a function of values for M', calculated previously at step 68, and the current engine speed in RPM, which is related to the time available for air to pass through inlet port 34 or be lost out of exhaust port 26. The trapping efficiency TE represents that percentage of the mass air M' within crankcase chamber 18, which is transferred and captured within combustion chamber 40, after closure of air inlet port 34 and exhaust port 26. Values for trapping efficiency are determined first using standard engine dynamometer procedures, as are the other look-up tables that will be referred to subsequently. Next at step 86, a trapping efficiency correction factor TEC is looked up in a table stored in memory and is a function of the difference between the exhaust backpressure EBP, found at step 82, and the manifold absolute pressure MAP, found at step 64. This correction factor is required to adjust the value for the trapping efficiency TE to take into account any changes in exhaust backpressure EBP and manifold absolute pressure MAP from their nominal values at the time the trapping efficiency values were experimentally determined on the dynamometer. At step 88, a new corrected value for the trapping efficiency TE is obtained by multiplying the previous value for the trapping efficiency TE₋₁ by the trapping efficiency correction factor TEC. Thus, this new value for TE will be automatically compensated when changes occur in the engine exhaust system, in the altitude of engine operation, or in the local barometric pressure due to variations in weather. Next at step 90, the appropriate air-fuel ratio A/F for cylinder 14 is looked up in a stored table, using values for the crankcase air mass M' determined at step 68 and the engine speed in RPM. At step 92, the mass of air CMA, which is available for combustion within cylinder 14, is computed by multiplying the crankcase air mass M' by the corrected trapping efficiency TE, found at step 88, according to the equation CMA = M'*TE. In the remaining steps 94 to 98, the combustion chamber mass air CMA, found at step 92, is used to compute standard engine control parameters. At step 94, the injector fuel pulse width FPW is computed according to the following: FPW = K*CMA*[1/(A/F)], where K is a predetermined units scaling constant stored in memory, CMA was found in step 92, and A/F was determined in step 90. Next, at step 96, the proper timing for the output fuel injector pulse is looked up in the appropriate table stored in memory, based upon the value of the engine speed in RPM and the combustion chamber mass air CMA. Using the computed values for fuel pulse width FPW and the injector pulse timing, computer 56 provides the appropriate FUEL SIGNAL (see Figure 1) to injector 38. Finally, at step 98, the correct spark advance for cylinder 14 is found in a stored look up table as a function of engine speed in RPM and combustion chamber mass air CMA. Computer 56 then provides ignition system 58 with the SPARK ADVANCE signal so that spark plug 36 can be fired at the proper time in advance of top dead centre for cylinder 14. After the above steps have been executed, the routine is exited at 100.

Claims: A method of determining engine exhaust backpressure in a crankcase scavenged two-stroke engine (10), which engine comprises a plurality of cylinders (14); an individual crankcase chamber (18) associated with each engine cylinder (14); inlet and exhaust ports (34,26) in the wall of each cylinder, which ports are both open during an overlap interval in each engine cycle; and an engine control system (56) adapted to determine the amount of air trapped in each cylinder during an engine cycle by the amount of air inducted into the respective cylinder in an engine cycle; the method comprising the steps of determining whether the engine cycle is within a portion of the overlap interval of the inlet and exhaust ports (34,26) of a cylinder, the portion of the overlap interval excluding an initial period of the overlap interval during which pressure between the cylinder and its respective crankcase chamber becomes substantially equalised and falling substantially within a period in which the air pressure in the respective crankcase chamber (18) is substantially equal to the backpressure at the exhaust port (26) due to airflow between the respective crankcase chamber and exhaust port during the overlap interval; deriving a plurality of values (CCP) indicative of the air pressure in the crankcase chamber during the portion of the overlap interval; calculating an average indicated crankcase pressure from the plurality of derived values, and thereby to obtain a value (EBP) indicative of the average backpressure at the exhaust port; and determining therefrom the amount of air trapped in the cylinder. A method according to claim 1, wherein the portion of the overlap interval is derived from rotational positions of the engine. A method according to claim 2, wherein the values indicative of crankcase pressure are obtained from a pressure sensor (46) arranged to measure pressure within the crankcase chamber at predetermined engine rotational positions. A crankcase scavenged two-stroke engine (10) comprising a plurality of engine cylinders (14); an individual crankcase chamber (18) associated with each engine cylinder (14); inlet and exhaust ports (34,26) in the wall of each cylinder, which ports are both open during an overlap interval in each engine cycle; an engine control system (56) adapted to determine the amount of air trapped in each cylinder during an engine cycle by the amount of air inducted into the respective cylinder in an engine cycle; determining means (48) for determining whether the engine cycle is within a portion of the overlap interval of the inlet and exhaust ports (34,26) of a cylinder, the portion of the overlap interval excluding an initial period of the overlap interval during which pressure between the cylinder and its respective crankcase chamber becomes substantially equalised and falls substantially within a period in which the air pressure in the respective crankcase chamber is substantially equal to the backpressure at the exhaust port due to airflow between the respective crankcase chamber and exhaust port during the overlap interval; means (46,50) for deriving a plurality of values (CCP) indicative of the air pressure in the crankcase chamber during the portion of the overlap interval; and means (50) for calculating an average crankcase pressure from the plurality of derived values, and thereby to obtain a value (EBP) indicative of the average backpressure at the exhaust port and for use in determining the amount of air trapped in the cylinder therefrom. An engine according to claim 4, wherein the portion of the overlap interval is derived from rotational positions of the engine. An engine according to claim 5, comprising a pressure sensor (46) arranged to measure pressure within the crankcase chamber at predetermined engine rotational positions and thereby to obtain the values indicative of crankcase pressure. Apparatus for determining engine exhaust backpressure in a crankcase scavenged two-stroke engine comprising determining means (48) for determining whether an engine cycle is within a portion of an overlap interval during which the inlet and exhaust ports of a cylinder of the engine are open, the portion of the overlap interval excluding an initial period of the overlap interval during which pressure between the cylinder and its respective crankcase chamber becomes substantially equalised and falls substantially within a period in which the air pressure in the respective crankcase chamber is substantially equal to engine exhaust backpressure at the exhaust port due to airflow between the respective crankcase chamber and exhaust port during said portion of the overlap interval; means (46; 50) for deriving a plurality of values (CCP) indicative of the air pressure in the crankcase chamber during said portion of the overlap interval; and means (50) for calculating an average crankcase pressure from the plurality of derived values, and thereby to obtain a value (EBP) indicative of the average backpressure at the exhaust port and for determining therefrom the amount of air trapped in the cylinder.

Inventors: GOMEZ APARICIO JOSE, MONTVILLE DENNIS WAYNE, TROMBLEY DOUGLAS EDWARD, GOMEZ, APARICIO JOSE, MONTVILLE, DENNIS WAYNE, TROMBLEY, DOUGLAS EDWARD
Applicants: GEN MOTORS CORP, GENERAL MOTORS CORPORATION
Application year: 1990
Main classification: F02D35
IPC codes: F02D45, G01F9, F02D41, G01F1, G01F3