METHOD FOR ADJUSTING A FUEL MASS TO BE INJECTED
20230323830 · 2023-10-12
Inventors
Cpc classification
F02D41/1401
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2041/1432
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2200/0616
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/182
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2041/1433
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A method for adjusting a fuel mass to be injected into an internal combustion engine. The internal combustion engine including an intake tract, at least one cylinder, and an exhaust tract. In the method, an air mass introduced into the internal combustion engine is ascertained and a fuel mass to be injected into the internal combustion engine is determined. An air-fuel ratio in the exhaust tract of the internal combustion engine is determined which is adjusted in time. Based on the time-adjusted air-fuel ratio and the calculated fuel mass to be injected, a first wall film fuel mass is calculated and the fuel mass to be injected is adjusted based on the first wall film fuel mass.
Claims
1. A method for adjusting a fuel mass to be injected into an internal combustion engine, the internal combustion engine including an intake tract, at least one cylinder, and an exhaust tract, the method comprising the following steps: ascertaining an air mass introduced into the at least one cylinder of the internal combustion engine; determining a fuel mass to be injected into the at least one cylinder of the internal combustion engine; determining an air-fuel ratio in the exhaust tract of the internal combustion engine; temporally adjusting the determined air-fuel ratio to obtain a time-adjusted air-fuel ratio; determining a first wall film fuel mass based on the time-adjusted air-fuel ratio, the ascertained introduced air mass, and the determined fuel mass to be introduced; and adjusting the fuel mass to be injected based on the calculated first wall film fuel mass.
2. The method as recited in claim 1, wherein the temporal adjustment of the determined air-fuel ratio is ascertained based on a model of the exhaust tract.
3. The method as recited in claim 2, wherein the temporal adjustment of the determined air-fuel ratio includes a dead time caused by the exhaust tract and a time delay caused by the determination.
4. The method as recited in claim 3, wherein the dead time is adjusted using predetermined characteristic data and/or the time delay is adjusted using a filter transfer function.
5. The method as recited in claim 1, wherein the adjusting of the fuel mass to be injected based on the calculated first wall film fuel mass includes a determination of an adaptation factor from the first wall film fuel mass and a second wall film fuel mass.
6. The method as recited in claim 5, wherein the second wall film fuel mass is determined from a wall film model.
7. The method as recited in claim 6, wherein a least squares estimator is used for the ascertaining of the adaptation factor.
8. A computing unit configured to adjust a fuel mass to be injected into an internal combustion engine, the internal combustion engine including an intake tract, at least one cylinder, and an exhaust tract, the computing unit configured to: ascertain an air mass introduced into the at least one cylinder of the internal combustion engine; determine a fuel mass to be injected into the at least one cylinder of the internal combustion engine; determine an air-fuel ratio in the exhaust tract of the internal combustion engine; temporally adjust the determined air-fuel ratio to obtain a time-adjusted air-fuel ratio; determine a first wall film fuel mass based on the time-adjusted air-fuel ratio, the ascertained introduced air mass, and the determined fuel mass to be introduced; and adjust the fuel mass to be injected based on the calculated first wall film fuel mass.
9. An internal combustion engine, comprising: an intake tract; at least one cylinder; an exhaust tract; and a computing unit configured to adjust a fuel mass to be injected into the internal combustion engine, the computing unit configured to: ascertain an air mass introduced into the at least one cylinder of the internal combustion engine; determine a fuel mass to be injected into the at least one cylinder of the internal combustion engine; determine an air-fuel ratio in the exhaust tract of the internal combustion engine; temporally adjust the determined air-fuel ratio to obtain a time-adjusted air-fuel ratio; determine a first wall film fuel mass based on the time-adjusted air-fuel ratio, the ascertained introduced air mass, and the determined fuel mass to be introduced; and adjust the fuel mass to be injected based on the calculated first wall film fuel mass.
10. A non-transitory machine-readable storage medium on which is stored a computer program for adjusting a fuel mass to be injected into an internal combustion engine, the internal combustion engine including an intake tract, at least one cylinder, and an exhaust tract, the computer program, when executed by a processor, causing the processor to perform the following steps: ascertaining an air mass introduced into the at least one cylinder of the internal combustion engine; determining a fuel mass to be injected into the at least one cylinder of the internal combustion engine; determining an air-fuel ratio in the exhaust tract of the internal combustion engine; temporally adjusting the determined air-fuel ratio to obtain a time-adjusted air-fuel ratio; determining a first wall film fuel mass based on the time-adjusted air-fuel ratio, the ascertained introduced air mass, and the determined fuel mass to be introduced; and adjusting the fuel mass to be injected based on the calculated first wall film fuel mass.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0041]
[0042]
[0043]
DETAILED DESCRIPTION OF EXAMPLE EMBODIMENTS
[0044]
[0045] A lambda sensor 8 is situated in exhaust tract 9 of the internal combustion engine shown, which sensor determines the residual oxygen in the exhaust gas of the engine in order to determine the air-fuel ratio of the combusted mixture.
[0046] In addition, the internal combustion engine includes a computing unit 3, which can for example be the engine control device, which is connected to throttle valve 6, injection valve 4, and lambda sensor 8. Computing unit 3 can receive the signals from the sensors of the combustion engine (e.g. lambda sensor 8) and control the actuators of the combustion engine (e.g. throttle valve 6 and injection valve 4).
[0047] Computing unit 3 can, for example, receive the output signal of the lambda probe 8, calculate the first wall film fuel mass based thereon, and adjust the fuel mass to be injected by injection valve 4 accordingly.
[0048] From
[0049]
[0050] The wall film model is standardly adjusted to a limited number of vehicles during the application of the engine controlling. In order to correctly take into account wall film effects over the life of a vehicle and for different vehicles, the advantageous specific embodiment of the present invention described herein includes an adaptation of the wall film fuel mass flow rate calculated using the wall film model {dot over (m)}.sub.wf,2, which is described below in connection with
[0051] The adaptation makes use of a measured air-fuel ratio λ.sub.sens to determine the real fuel mass entering the cylinder. Because the measured signal of the lambda probe λ.sub.sens reflects the air-fuel ratio λ in the cylinder with a time delay, this time delay has to be taken into account in the adaptation.
[0052]
[0053]
[0054] In function block 21, the air-fuel ratio λ prevailing in cylinder 1 is calculated based on the input variables air mass flow {dot over (m)}.sub.air, fuel mass flow {dot over (m)}.sub.fuel and stoichiometric air requirement L.sub.st. The fuel mass flow {dot over (m)}.sub.fuel entering cylinder 1 is here made up of the fuel mass flow {dot over (m)}.sub.direct, which enters the cylinder from the current injection, and the wall film fuel mass flow {dot over (m)}.sub.wf,2.
[0055] The delayed behavior of the air-fuel ratio λ.fwdarw.λ.sub.sens is mapped here by a PT1 element with the time constant τ.sub.exh in function block 22. Because the dead time is considered separately (via a simple shift of the values on the time scale) and is not included in the transfer function 23 for the adaptation model 30, it is not shown in the present block diagram.
[0056] Function blocks 10 to 14 show the wall film model for dynamic feedforward control of the wall film fuel mass flow {dot over (m)}.sub.wf,1. The fuel mass situated in wall film 10 is preferably stored in the engine control unit in a corresponding map 10 as a function of the engine rotational speed n.sub.eng and the engine temperature t.sub.mot. The input variables of map 10 are not limited to the variables shown; additional or other boundary conditions, such as pressure and/or temperature in intake tract 2 of the engine, can be taken into account.
[0057] Function block 11 describes a filter transfer function with a filter time constant π.sub.wf, that calculates the wall film fuel mass flow using the time derivative of the wall film fuel mass. The wall film fuel mass flow calculated in this way is subsequently divided into a portion that flows into the cylinder quickly and a portion that flows into the cylinder with a significant delay. This is realized by two function blocks 12 and 13 connected in parallel, which have filter transfer functions with a slow time constant τ.sub.slow and a fast time constant τ.sub.fast.
[0058] Because, in addition to the above-described functional dependence of the wall film behavior on the engine rotational speed and the engine temperature, there may be other dependencies in the fuel mass flow (e.g. a directional dependence of the mass flow entering or exiting the wall film), the fuel mass flow resulting from function blocks 12 and 13 is advantageously multiplied again here by a correction factor f.sub.corr, by a multiplier 14.
[0059] This block 10 to 14 is usually not individually parameterized for the specific engine, so that the determined second wall film fuel mass flow {dot over (m)}.sub.wf,2 is not (always) optimal.
[0060] Therefore, advantageously, the determined second wall film fuel mass flow {dot over (m)}.sub.wf,2 is now subsequently multiplied by the adaptation factor f.sub.corr,adp, which is ascertained in function block 30 from, inter alia, the measured and time-adjusted air-fuel ratio λ.sub.corr. This multiplication at the multiplier 15 results in the first (positive or negative) wall film fuel mass flow {dot over (m)}.sub.wf,1, which is added to the fuel mass flow {dot over (m)}.sub.direct at the addition point 20.
[0061] In function block 30, the calculation of the adaptation factor f.sub.corr,adp, inter alia, is carried out also using the first wall film fuel mass flow rate {dot over (m)}.sub.wf,1, which however is calculated differently than in 15. The first wall film mass flow rate {dot over (m)}.sub.wf,1 can be calculated for example according to equation (2), and the adaptation factor f.sub.corr,adp can be calculated therefrom, for example according to equation (4). The adaptation factor f.sub.corr,adp can preferably also be determined using a recursive least squares estimator, which increases the numerical stability of the calculation.
[0062] In order to perform the calculation steps according to equations (2) and (4), function block 30 receives the measured and time-adjusted air ratio λ.sub.corr, the air mass flow {dot over (m)}.sub.air, the fuel mass flow {dot over (m)}.sub.direct, and the filtered wall film mass flow {dot over (m)}.sub.wf,2flt, ascertained from the wall film model, as input variables.
[0063] For the temporal adjustment of the measured air-fuel ratio λ.sub.sens to the air ratio λ present in the cylinder, the filter transfer function shown in function block 23 and described in equation (3) is used. This produces the time-adjusted air ratio λ.sub.corr, which is used in function block 30 to calculate the first wall film fuel mass flow {dot over (m)}.sub.wf,1 according to equation (2).
[0064] From a comparison of function blocks 22 and 23, it can be seen that the filter transfer function shown in function block 23 is the inverse of the time delay of the measured air-fuel ratio λ.sub.sens shown in function block 22. In addition, the transfer function 23 has in the denominator a further filter function with the predetermined time constant τ.sub.flt.
[0065] The time constant τ.sub.flt is used in the same way to filter the first wall film fuel mass flow {dot over (m)}.sub.wf,2 in function block 16, so that the input variables {dot over (m)}.sub.wf,2flt and λ.sub.corr enter function block 30 synchronously in time, which block has the adaptation factor f.sub.corr,adp as output variable.
[0066] With the help of the adaptation factor calculated in function block 30, for example on the basis of equations (2) and (4), the wall film fuel mass flow can be continuously adjusted to the real engine conditions during vehicle operation. In this way, the stoichiometric air-fuel ratio can be reliably maintained even during load change processes, and transient mixture deviations can thus be reliably minimized.