EP2786003A1 - Verfahren und vorrichtung zur regelung eines luft-kraftstoff-verhältnisses eines verbrennungsmotors - Google Patents
Verfahren und vorrichtung zur regelung eines luft-kraftstoff-verhältnisses eines verbrennungsmotorsInfo
- Publication number
- EP2786003A1 EP2786003A1 EP12795783.5A EP12795783A EP2786003A1 EP 2786003 A1 EP2786003 A1 EP 2786003A1 EP 12795783 A EP12795783 A EP 12795783A EP 2786003 A1 EP2786003 A1 EP 2786003A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- probe
- determined
- exhaust gas
- lambda
- internal combustion
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 46
- 239000000446 fuel Substances 0.000 title claims abstract description 36
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 33
- 230000001105 regulatory effect Effects 0.000 title abstract description 6
- 239000000523 sample Substances 0.000 claims abstract description 109
- 239000000203 mixture Substances 0.000 claims abstract description 29
- 238000011156 evaluation Methods 0.000 claims abstract description 11
- 230000001419 dependent effect Effects 0.000 claims abstract description 8
- 238000004364 calculation method Methods 0.000 claims abstract description 7
- 230000032683 aging Effects 0.000 claims description 11
- 238000013021 overheating Methods 0.000 claims description 6
- 238000001514 detection method Methods 0.000 claims description 5
- 206010008428 Chemical poisoning Diseases 0.000 claims description 2
- 230000001143 conditioned effect Effects 0.000 claims 1
- 239000007789 gas Substances 0.000 description 30
- 238000012937 correction Methods 0.000 description 12
- 230000001276 controlling effect Effects 0.000 description 6
- 238000002347 injection Methods 0.000 description 6
- 239000007924 injection Substances 0.000 description 6
- 230000003197 catalytic effect Effects 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 239000003054 catalyst Substances 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- 208000005374 Poisoning Diseases 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000003679 aging effect Effects 0.000 description 1
- 238000009529 body temperature measurement Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000011133 lead Substances 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 231100000572 poisoning Toxicity 0.000 description 1
- 230000000607 poisoning effect Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/24—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means
- F02D41/2406—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using essentially read only memories
- F02D41/2409—Addressing techniques specially adapted therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1438—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor
- F02D41/1444—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the characteristics of the combustion gases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1438—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor
- F02D41/1444—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the characteristics of the combustion gases
- F02D41/1454—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the characteristics of the combustion gases the characteristics being an oxygen content or concentration or the air-fuel ratio
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1438—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor
- F02D41/1477—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the regulation circuit or part of it,(e.g. comparator, PI regulator, output)
- F02D41/1479—Using a comparator with variable reference
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1438—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor
- F02D41/1486—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor with correction for particular operating conditions
- F02D41/1487—Correcting the instantaneous control value
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1438—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor
- F02D41/1439—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the position of the sensor
- F02D41/1441—Plural sensors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1438—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor
- F02D41/1493—Details
- F02D41/1496—Measurement of the conductivity of a sensor
Definitions
- the invention relates to a method for controlling an air-fuel ratio of an internal combustion engine as a function of a composition of its exhaust gas and a correspondingly configured control device.
- Lambda probe is measured in the exhaust system. This procedure is generally referred to as lambda control.
- the lambda probe provides an actual probe signal which is dependent on the oxygen content of the exhaust gas and which is usually a probe voltage.
- This probe signal is converted by means of a stored characteristic or a corresponding calculation rule into the lambda value and this is used for the control.
- the probe signal not only depends on the exhaust gas composition but is also influenced by additional disturbing influences which cause the characteristic curve not to be constant under all conditions.
- the probe temperature that is to say the temperature of the measuring element of the probe
- This has an effect especially in the rich lambda range, ie at lambda values ⁇ 1.
- changes in the characteristic curve resulting from increasing aging of the measuring element of the probe over the operating time can cause progressive poisoning of the measuring element and thus to a change in the characteristic curve.
- the probe temperature is determined as a function of the internal resistance of the probe from a stored characteristic curve.
- the current correction voltage which is added to the current probe actual voltage is then determined in order to obtain a corrected probe voltage.
- DE 199 19 427 A describes a method for correcting a characteristic curve of a broadband lambda probe which is installed upstream of an exhaust gas catalytic converter, the sensor signal of the lambda probe being evaluated in a fuel cut-off phase of the internal combustion engine and the signal level thus determined being used for the correction of the slope of the characteristic curve becomes.
- DE 10 2007 015 362 A discloses a method for calibrating a stepping lambda probe arranged upstream of a catalytic converter. For this purpose, a correction signal is determined from a measurement signal provided by a downstream reference lambda probe and used for the characteristic adaptation of the jump lambda probe.
- a disadvantage of all known methods is that even the corrections have only a limited accuracy and therefore deviations of the corrected characteristic of the exact characteristic can remain. This circumstance is taken into account in the prior art in that lambda desired values or lambda threshold values to be regulated, the achievement of which trigger a change in the air-fuel mixture, are determined with a safety margin taking into account the uncertainty. This safety distance is usually dimensioned so that the largest assumed inaccuracy of the characteristic is taken into account.
- a typical example of this procedure is the enrichment of a motor, which is made to protect components from overheating.
- the combustion and thus the exhaust gas temperature is lowered by additional addition of fuel and thus prevents overheating example of turbochargers or catalysts.
- the Gemischanfettung for component protection usually takes place when reaching a permissible limit temperature, for example, of 900 ° C, with a target lambda value of, for example, 0.9 is set by additional fuel addition, which ensures an effective cooling effect. If, for example, a maximum tolerance band of 2% is calculated for the lambda probe used, the lambda threshold of 0.88 is conventionally set for the engine in order to remain safely below the necessary limit of lambda 0.9 under all conditions.
- the object of the present invention is therefore to provide a method and a device for controlling an air-fuel ratio of an internal combustion engine and in which the safety distance to be maintained by threshold values for the exhaust gas composition, in particular lambda threshold values, is determined according to actual requirements and thus the fuel consumption is reduced.
- the method according to the invention comprises the steps:
- Determination of the exhaust gas composition by detecting an actual probe signal dependent on the exhaust gas composition by means of an exhaust gas probe and determining the exhaust gas composition as a function of the actual probe signal by means of a characteristic curve or a calculation rule,
- a safety margin is determined for taking into account at least one disturbance variable on the actual probe signal, which is applied to the characteristic or calculation rule, to the actual probe signal or to the setpoint or threshold value, and
- an assessment of a current accuracy of the at least one disturbance variable and / or an actual influence of the at least one disturbance variable on the probe signal is undertaken and the safety distance caused by the at least one disturbance variable is established as a function of the result of the evaluation.
- the safety margin is thus always set constant and in the amount of its highest possible value in the sense of a worst-case scenario, according to the invention, its variable definition.
- the method thus not only allows a higher accuracy of the regulation of a desired value, but also a fuel economy.
- the disturbance value evaluated in the context of the invention comprises a temperature of the exhaust gas probe and / or an aging of the exhaust gas probe and / or a chemical poisoning of the exhaust gas probe.
- the influence of these disturbances on the probe signal, in particular of lambda probes, is known in the prior art. As already described above, according to the invention, however, it is not assumed that their greatest possible uncertainty or their greatest possible influence on the probe signal for these disturbances, but this / this is currently evaluated.
- a spread is determined for the evaluation of the current accuracy of the at least one disturbance, within which values of this disturbance lie, which were detected in a past period.
- the safety distance is then determined as a function of the spread, it being understood that the safety level is chosen the greater, the greater the spread. For example, if the disturbance is the temperature of the probe, then for a predetermined past period of time it is determined what variance the sensed temperature values had from the true value. If only a small variance of the determined temperature has been found in the past, the safety distance can be set correspondingly small.
- a duration is determined for the assessment of the current accuracy of the at least one disturbance, which has elapsed since a past calibration of a detection system of this disturbance.
- the safety distance is then determined as a function of the duration determined in this way, the safety distance being chosen to be greater with increasing duration, since an increasingly imprecise disturbance variable detection can be assumed.
- an absolute height of the currently detected disturbance variable is determined for the evaluation of the current influence of the at least one disturbance variable on the probe signal, and the safety distance is established as a function of the absolute altitude. For example, if the absolute value of the internal resistance of the measuring element of the probe in a range in which a temperature determination can be very inaccurate, for example at resistance values close to zero, is assumed by a relatively high error of the temperature determination and set a correspondingly high safety margin.
- the safety distance is also determined depending on an operating point of the internal combustion engine, in particular as a function of an engine speed and / or an engine load.
- a map can be used which represents the safety distance as a function of the speed and / or the load. In this way influences can be taken into account which can not be quantified in the evaluation.
- the method can be used particularly advantageously in connection with the performance of a mixture enrichment for component protection of the internal combustion engine and / or the exhaust system against overheating.
- the lambda input provided for the mixture enrichment is preferably determined according to the method.
- the method makes it possible to set the lambda input for component protection as lean as possible, that is to say with the smallest possible safety distance to the target value, thereby minimizing the additional fuel consumption required for component protection.
- Lambda control of the internal combustion engine are used, wherein the deliberatelyregelnde lambda setpoint is set in the inventive manner.
- the invention enables a particularly precise lambda control.
- the invention further relates to a control device for controlling an air-fuel ratio of an internal combustion engine, which for carrying out the invention
- FIG. 2 shows a flow chart of a method sequence for carrying out a
- FIG. 3 shows characteristic curves of a jump lambda probe for different temperatures.
- FIG. 1 shows an internal combustion engine 10 whose fuel supply takes place via a fuel injection system 12.
- the injection system 12 may be a port injection or a cylinder direct injection.
- the internal combustion engine 10 is also supplied via an intake manifold 14 with combustion air.
- the amount of air supplied via a arranged in the intake manifold 14 controllable actuator 16, such as a throttle valve, are regulated.
- An exhaust gas generated by the internal combustion engine 10 is released into the environment via an exhaust passage 18, whereby environmentally relevant exhaust gas constituents are converted by a catalyst 20.
- an exhaust gas probe 22 is arranged at a position close to the engine, which is in particular a lambda probe, typically a jump lambda probe.
- a further exhaust gas probe 24 may be arranged downstream of the catalytic converter 20, which may likewise be a lambda probe, in particular a broadband lambda probe, or an NO x sensor.
- the signals of the exhaust probes 22 and 24 are transmitted to a motor controller 26. Other signals not shown sensors also go into the engine control 26.
- the engine controller 26 controls in dependence on the incoming signals in a known manner to various components of the internal combustion engine 10.
- the engine control 26 regulates a fuel quantity to be supplied via the fuel injection system 12 and / or an air quantity to be supplied via the intake system 14.
- the engine controller 26 includes a control device 28, which for carrying out the method according to the invention for controlling the Air-fuel ratio of the internal combustion engine 10 is set up.
- the control device 28 includes a corresponding algorithm in computer-readable form and suitable characteristics and maps.
- the method illustrated in FIG. 2 is based on a state in which the temperature T M (see FIG. 1) of a component, for example intake or exhaust valves of the engine 10 or an exhaust-gas turbocharger or the catalytic converter 20, is an admissible temperature
- the method starts in step 100, where, for the purpose of detecting the temperature of the lambda probe 22, the internal resistance R 1 of the measuring element of the probe 22 is read.
- the sensor temperature T s of the probe 22 is determined as a function of the internal resistance R i.
- a characteristic curve which maps the probe temperature T s as a function of the internal resistance R.
- Such a method for determining the probe temperature is known, for example, from DE 100 36 129 A1.
- other methods for determining the probe temperature can be used in the context of the present invention.
- St the lambda probe 22 read.
- the determination of the exhaust gas composition, in particular of the actual lambda value ⁇ 1 takes place as a function of the probe signal U 1 S t and the probe temperature T s determined in step 102.
- a stored characteristic map which maps the lambda value as a function of the probe signal Uist and the probe temperature T s .
- FIG. 3 shows by way of example such a map in which the characteristic curves of the jump lambda probe for three different probe temperatures T s are shown. It can be seen that, in particular for rich lambda values ⁇ 1, the
- a step 104 following step 102 an evaluation of a current accuracy of the disturbing probe temperature AT S or an actual influence of this disturbance variable on the probe signal U
- the range of the measured resistance value 5R, or the derived probe temperature 5T S are determined in a predetermined past period. Further embodiments of the evaluation carried out in step 104 have already been explained above.
- the safety distance AS is determined in a subsequent step 106, the safety distance AS being selected to be greater, the greater the spread 5T S of the probe temperature.
- a linear relationship can be used.
- step 108 a setpoint for the lambda input ⁇ ⁇ 0 ⁇ is set for the Gemischanfettung for the purpose of component protection.
- the previously determined safety distance AS is subtracted from the lambda target value ⁇ ⁇ 1 to be maintained for the component protection. If the target ⁇ for the component protection is, for example, 0.9 and, in step 106, a safety distance AS of 0.02 has been determined, the lambda setpoint ⁇ ⁇ 0 ⁇ is 0.88.
- the lambda deviation AS can also be a factor which is multiplied by the lambda target.
- step 1 14 a control of the engine 10 to be supplied to the air-fuel mixture according to the determined in step 108 lambda target specification ⁇ ⁇ 0 ⁇ occurs, as is well known in the art.
- a query takes place in step 1 14, in which the actual lambda value determined in step 1 12 is compared with the desired lambda value ⁇ ⁇ 0 ⁇ determined in step 108.
- it can be checked in step 1 14 whether the difference - ⁇ ⁇ 0 ⁇ > 0.
- step 1 16 an amount of fuel m K s supplied to the internal combustion engine 10 is increased by a predetermined increment of the fuel quantity AKS, to enrichment of the air-fuel mixture. If the query in step 1 14 is negated otherwise, that is, the actual lambda value is smaller (fatter) than the desired lambda value ⁇ ⁇ 0 ⁇ , the method goes to step 1 18, where the fuel quantity m K s to a corresponding increment AKS is lowered in order to achieve a leaning of the engine. In step 120, the supply of the fuel to the internal combustion engine 10 takes place in accordance with the fuel quantity m K s determined in step 1 16 or 1 18.
- step 1 10 The method then goes back to step 1 10, to detect the probe signal U again, to determine the actual lambda value in step 1 12 as a function of the probe signal U. and in step 1 14 again to compare the actual lambda value with the target specification ⁇ ⁇ 0 ⁇ .
- This cycle is repeated during the entire component protection measure until the component temperature T M has reached a permissible value.
- the query cycle for checking the component temperature T M is not shown in FIG.
- steps 104 to 108 are performed during each passage, since a change in the safety distance AS and thus the desired lambda value ⁇ ⁇ 0 ⁇ usually does not change in the short term.
- steps 100 and 102 for determining the probe temperature T s in each interrogation cycle makes sense, especially in the case of the mixture enrichment for component protection, since a sinking temperature of the sensor is also to be expected here.
- the safety distance AS is applied to the target lambda value ⁇ ⁇ ⁇ , so as to set the desired lambda value ⁇ ⁇ 0 ⁇ for the lambda control.
- a corresponding safety distance AS can also be applied to the characteristic curve applied in step 1 12 in order to adapt it so that a lambda scattering reflecting the uncertainty of the temperature determination is taken into account.
- the safety distance AS is additionally made dependent on which absolute value the current desired lambda value of the engine assumes. This can take into account that some disturbances gain influence in certain areas. For example, the probe temperature T s influences the characteristic curve at rich lambda values much more strongly than lean ones (see FIG. 3). Thus, the function used in step 106 in FIG. 2 for determining the safety distance AS can take into account the current lambda value in such a way that, as the lambda values decrease, the safety distance AS is increased.
- the aging of the lambda probe 22 for example by means of the downstream lambda probe 24 (see FIG. 1), which here acts as a reference probe.
- a deviation from the average mixture value can be determined via the signal of the Breibandlambdasonde 24 and the characteristic curve of the lambda probe 22 are corrected accordingly.
- Corresponding methods for taking account of such aging effects and for correcting the characteristic are known in the prior art. Other methods for determining an aging correction value may also be used within the scope of the present invention.
- the inaccuracies in the aging of the exhaust gas probe are evaluated on the basis of the thus determined aging correction value, despite the characteristic curve correction in the conversion of the probe signal U
- an aging correction value will result on aging of the lambda probe 22 and concomitant correction of the probe characteristic. From the extent of this correction value is now inventively evaluated, for example, which tolerance in the determined actual lambda value despite characteristic correction can still remain. Depending on this, the safety distance AS, that is the additionally necessary enrichment for the component protection is determined.
- influences which can not be quantified explicitly with evaluation variables but nevertheless can disturb the lambda determination are taken into account.
- the influence of the operating point of the internal combustion engine 10 can be evaluated here, for example by determining an additional safety distance operating point-dependent from a speed-load characteristic map.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102011087213A DE102011087213A1 (de) | 2011-11-28 | 2011-11-28 | Verfahren und Vorrichtung zur Regelung eines Luft-Kraftstoff-Verhältnisses eines Verbrennungsmotors |
PCT/EP2012/073690 WO2013079468A1 (de) | 2011-11-28 | 2012-11-27 | Verfahren und vorrichtung zur regelung eines luft-kraftstoff-verhältnisses eines verbrennungsmotors |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2786003A1 true EP2786003A1 (de) | 2014-10-08 |
EP2786003B1 EP2786003B1 (de) | 2019-09-18 |
Family
ID=47294875
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP12795783.5A Active EP2786003B1 (de) | 2011-11-28 | 2012-11-27 | Verfahren und vorrichtung zur regelung eines luft-kraftstoff-verhältnisses eines verbrennungsmotors |
Country Status (5)
Country | Link |
---|---|
US (1) | US9714623B2 (de) |
EP (1) | EP2786003B1 (de) |
CN (1) | CN103958867B (de) |
DE (1) | DE102011087213A1 (de) |
WO (1) | WO2013079468A1 (de) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108240268B (zh) * | 2016-12-27 | 2020-07-14 | 上海汽车集团股份有限公司 | 车辆中的电子执行器及其控制方法 |
CN113217210B (zh) * | 2021-04-16 | 2023-05-12 | 联合汽车电子有限公司 | 氧传感器低温闭环控制的优化方法和系统、发动机闭环控制系统和可读存储介质 |
FR3123089A1 (fr) * | 2021-05-20 | 2022-11-25 | Psa Automobiles Sa | Procede d'amelioration d'un signal de mesure d'une sonde a oxygene |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19629552C1 (de) * | 1996-07-22 | 1997-12-18 | Siemens Ag | Vorrichtung zum Kompensieren der Temperaturdrift einer Abgassonde |
DE19919427C2 (de) * | 1999-04-28 | 2001-09-20 | Siemens Ag | Verfahren zur Korrektur der Kennlinie einer Breitband-Lambda-Sonde |
DE10036129B4 (de) | 2000-07-25 | 2009-12-17 | Volkswagen Ag | Verfahren zum Messen einer Abgaszusammensetzung |
DE10133524A1 (de) * | 2001-07-11 | 2003-01-30 | Bosch Gmbh Robert | Verfahren und Vorrichtung zur Korrektur des Dynamikfehlers eines Sensors |
DE102006053110B3 (de) * | 2006-11-10 | 2008-04-03 | Audi Ag | Verfahren zur Überprüfung des von einer binären Lambdasonde angezeigten Lambdawertes |
DE102007015362A1 (de) | 2007-03-30 | 2008-10-02 | Volkswagen Ag | Verfahren zur Lambda-Regelung mit Kennlinienanpassung |
DE102007038478A1 (de) * | 2007-08-14 | 2009-02-19 | Volkswagen Ag | Verfahren zur λ-Regelung in Betriebsbereichen mit Kraftstoff-Mangel oder Kraftstoff-Überschuss bei einer Nernst-Sonde |
DE102007038487A1 (de) | 2007-08-14 | 2009-02-19 | Basf Coatings Ag | Wässriger Beschichtungsstoff, Verfahren zu seiner Herstellung und seine Verwendung |
EP2360365B1 (de) * | 2008-12-05 | 2013-11-13 | Toyota Jidosha Kabushiki Kaisha | Vorrichtung zur beurteilung des ungleichgewichts eines luft-/kraftstoffverhältnisses zwischen zylindern eines mehrzylinderverbrennungsmotors |
DE102009053411A1 (de) * | 2009-11-14 | 2011-05-19 | Volkswagen Ag | Verfahren zum Verarbeiten eines gemessenen, ohmschen Widerstandes R(t) eines Messelementes mit temperaturabhängigem, ohmschen Widerstand |
DE102010003143B4 (de) * | 2010-03-23 | 2014-08-28 | Ford Global Technologies, Llc | Verfahren zum Betreiben einer fremdgezündeten Brennkraftmaschine und Brennkraftmaschine zur Durchführung eines derartigen Verfahrens |
-
2011
- 2011-11-28 DE DE102011087213A patent/DE102011087213A1/de not_active Withdrawn
-
2012
- 2012-11-27 EP EP12795783.5A patent/EP2786003B1/de active Active
- 2012-11-27 CN CN201280058511.8A patent/CN103958867B/zh active Active
- 2012-11-27 WO PCT/EP2012/073690 patent/WO2013079468A1/de active Application Filing
- 2012-11-27 US US14/360,749 patent/US9714623B2/en active Active
Non-Patent Citations (1)
Title |
---|
See references of WO2013079468A1 * |
Also Published As
Publication number | Publication date |
---|---|
DE102011087213A1 (de) | 2013-05-29 |
US9714623B2 (en) | 2017-07-25 |
CN103958867A (zh) | 2014-07-30 |
US20150096544A1 (en) | 2015-04-09 |
WO2013079468A1 (de) | 2013-06-06 |
CN103958867B (zh) | 2017-08-15 |
EP2786003B1 (de) | 2019-09-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE102008001244B4 (de) | Sauerstoffsensorausgangssignalkorrekturgerät für eine Brennkraftmaschine | |
DE102011085115B4 (de) | Verfahren und Vorrichtung zur Adaption einer Lambdaregelung | |
DE4324312C2 (de) | Verfahren zum Betreiben einer Brennkraftmaschine in einem Magergemisch-Verbrennungsbereich | |
DE102012211687B4 (de) | Verfahren und Steuereinheit zur Erkennung eines Spannungsoffsets einer Spannungs-Lambda-Kennlinie | |
DE102012211683B4 (de) | Verfahren und Vorrichtung zur Korrektur einer Kennlinie einer Zweipunkt-Lambdasonde | |
DE102016222418A1 (de) | Verfahren zur Regelung einer Füllung eines Speichers eines Katalysators für eine Abgaskomponente | |
DE102013202989A1 (de) | Dynamische katalysator steuerung und regelung | |
DE112015004509B4 (de) | Steuervorrichtung für eine Verbrennungsmaschine | |
DE102012208092B4 (de) | Verfahren und Steuereinheit zur Kompensation eines Spannungsoffsets einer Zweipunkt-Lambdasonde | |
EP1317616A1 (de) | VERFAHREN ZUR NOx-MASSENSTROMBESTIMMUNG AUS KENNFELDDATEN BEI VARIABLER LUFTEINLASS-UND MOTORTEMPERATUR | |
EP2786003B1 (de) | Verfahren und vorrichtung zur regelung eines luft-kraftstoff-verhältnisses eines verbrennungsmotors | |
DE102013216024B4 (de) | Verfahren zur Lambda-Regelung einer Verbrennungskraftmaschine und Regelvorrichtung | |
DE102010000506A1 (de) | Verbrennungsmotorsteuersystem | |
DE102008009034B3 (de) | Verfahren und Vorrichtung zum Betreiben einer Brennkraftmaschine | |
DE102008011833B4 (de) | Verfahren zum Steuern einer lambdageregelten Abgasanlage einer Brennkraftmaschine | |
EP1241336B1 (de) | Verfahren und Vorrichtung zur Regelung einer externen Abgasrückführrate | |
DE102012204332A1 (de) | Vorrichtung zum Betreiben einer Brennkraftmaschine | |
DE102009047898A1 (de) | Steuerung zur Kraftstoffeinspritzung | |
DE102011087312B4 (de) | Verfahren und Vorrichtung zur Ermittlung eines Lambdawertes oder einer Sauerstoffkonzentration eines Gasgemischs | |
WO2016083232A1 (de) | Verfahren zur erkennung eines spannungsoffsets zumindest in einem bereich bei einer spannungs-lambda-kennlinie | |
DE19810523B4 (de) | Vorrichtung zur Erfassung ionalen Stroms für eine Brennkraftmaschine | |
EP1363008B1 (de) | Verfahren und Vorrichtung zur Steuerung der einzuspritzenden Kraftstoffmenge einer selbstzündenden Brennkraftmaschine | |
DE102021201323A1 (de) | Verfahren und Vorrichtung zum Betreiben eines Verbrennungsmotors mit einem vorgegebenen Luft-Kraftstoff-Gemisch | |
EP0925433A1 (de) | Verfahren zur regelung des kraftstoff-luft-verhältnisses einer brennkraftmaschine | |
DE102013217013A1 (de) | Verfahren und Vorrichtung zur Korrektur einer Kennlinie einer Zweipunkt-Lambdasonde |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20140611 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: HAHN, HERMANN |
|
DAX | Request for extension of the european patent (deleted) | ||
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
17Q | First examination report despatched |
Effective date: 20180503 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
INTG | Intention to grant announced |
Effective date: 20190509 |
|
GRAJ | Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted |
Free format text: ORIGINAL CODE: EPIDOSDIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
INTC | Intention to grant announced (deleted) | ||
INTG | Intention to grant announced |
Effective date: 20190729 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502012015311 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 1181583 Country of ref document: AT Kind code of ref document: T Effective date: 20191015 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20190918 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20191218 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20191218 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20191219 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200120 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200224 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502012015311 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG2D | Information on lapse in contracting state deleted |
Ref country code: IS |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20191127 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20191130 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20191130 Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200119 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20191130 |
|
26N | No opposition filed |
Effective date: 20200619 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20191127 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20191130 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 1181583 Country of ref document: AT Kind code of ref document: T Effective date: 20191127 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20191127 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20121127 Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20190918 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230523 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20231121 Year of fee payment: 12 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20231123 Year of fee payment: 12 Ref country code: DE Payment date: 20231130 Year of fee payment: 12 |