EP3411580B1 - Method for resetting two pressure sensors in an air-intake line of an engine with sensor fault prevention - Google Patents
Method for resetting two pressure sensors in an air-intake line of an engine with sensor fault prevention Download PDFInfo
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- EP3411580B1 EP3411580B1 EP17706560.4A EP17706560A EP3411580B1 EP 3411580 B1 EP3411580 B1 EP 3411580B1 EP 17706560 A EP17706560 A EP 17706560A EP 3411580 B1 EP3411580 B1 EP 3411580B1
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- capsural
- capadmi
- capatm
- sensors
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- 238000000034 method Methods 0.000 title claims description 45
- 230000002265 prevention Effects 0.000 title description 3
- 238000009530 blood pressure measurement Methods 0.000 claims description 19
- 238000002485 combustion reaction Methods 0.000 claims description 16
- 238000012795 verification Methods 0.000 claims description 9
- 230000001427 coherent effect Effects 0.000 claims description 6
- 238000012937 correction Methods 0.000 claims description 5
- 238000005259 measurement Methods 0.000 claims description 5
- 238000003745 diagnosis Methods 0.000 description 31
- 238000001514 detection method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 5
- 238000012790 confirmation Methods 0.000 description 4
- 230000007547 defect Effects 0.000 description 4
- 238000011084 recovery Methods 0.000 description 3
- 230000006866 deterioration Effects 0.000 description 2
- 239000000725 suspension Substances 0.000 description 2
- 238000013475 authorization Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000009529 body temperature measurement Methods 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005764 inhibitory process Effects 0.000 description 1
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Classifications
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- 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
- F02D41/2425—Particular ways of programming the data
- F02D41/2429—Methods of calibrating or learning
- F02D41/2451—Methods of calibrating or learning characterised by what is learned or calibrated
- F02D41/2474—Characteristics of sensors
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- 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
- F02D41/2425—Particular ways of programming the data
- F02D41/2429—Methods of calibrating or learning
- F02D41/2451—Methods of calibrating or learning characterised by what is learned or calibrated
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- 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
- F02D41/1401—Introducing closed-loop corrections characterised by the control or regulation method
- F02D2041/1433—Introducing closed-loop corrections characterised by the control or regulation method using a model or simulation of the system
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2200/00—Input parameters for engine control
- F02D2200/02—Input parameters for engine control the parameters being related to the engine
- F02D2200/04—Engine intake system parameters
- F02D2200/0406—Intake manifold pressure
Definitions
- the present invention relates to a method of readjusting at least two pressure sensors positioned in an air intake line of an internal combustion engine with prevention of a fault in one of the sensors, the detection of a fault in one of the sensors causing the suspension of the implementation of the method.
- the invention lies in the technical field of the command and control system of an internal combustion engine which is preferably with spark ignition.
- three pressure sensors are present, namely an atmospheric pressure sensor, a boost pressure sensor, this when the engine is turbocharged.
- the boost pressure sensor located downstream of a compressor of a turbocharger and an intake pressure sensor positioned in the air distributor. These three sensors are used to measure the pressure existing at certain specific points on the air intake line.
- the adjustment of the pressure sensors consists in compensating for this offset, in order to equalize the values measured on the sensors when the pressure to be measured is the same. This operation is particularly necessary for the correct operation of the piloting of a positive-ignition engine.
- a reference sensor is chosen by calibration. It is in relation to the measurement of this sensor that the other sensors will be readjusted. This reference sensor must be the most accurate sensor. This is frequently the case for an atmospheric pressure sensor which is most often preferred as a reference sensor.
- a timer is started. This delay makes it possible, on the one hand, to ensure that the intake line is at equilibrium of atmospheric pressure, and on the other hand, to ensure that the sensors are in a state allowing them to perform a consistent measure. During this time delay, the differences in measured values between the reference sensor and each sensor to be readjusted are determined.
- the time delay is calibrated very short. Its order of magnitude is 300 milliseconds.
- the readjustment is inhibited because it is considered that the readjustment is not reliable enough, the measured values having been distorted due to the fact that one or more pressure sensors were not in their optimal working condition.
- the figure 1 illustrates a chronogram as a function of time t of the process for resetting the pressure sensors according to the prior art, the resetting process having taken place correctly while the figure 2 illustrates a chronogram as a function of time t of the same process according to the state of the art, the start having been suspended by a failure of the resetting in the determined time before start.
- Capatm the atmospheric pressure, supercharging and air intake sensors are referenced respectively Capatm, Capsural and Capadmi. These sensors are shown in these two figures at the top of the figure on the left not readjusted Capnrecal then at the top of the figure on the right readjusted Caprecal.
- An initial Div divergence between the Capatm, Capsural and Capadmi sensors to be reset is more significant at the figure 2 that at the figure 1 .
- Def defect can be raised by issuing a reconfiguration flag, also known by the Anglo-Saxon name of flag.
- the reconfiguration flag is a Boolean variable in the engine control software representing the state of a diagnosis.
- the reconfiguration flag identifies a failure of a pressure sensor and the engine control functions use this flag to activate recovery strategies in the event of a sensor failure.
- the transmission time of a configuration flag can be of the order of 2 seconds and is to be compared with that of the registration delay and the need for rapid application of registration.
- the sensor failure is not signaled until after the registration has been applied. The diagnosis is therefore not useful. But above all, the registration will be carried out from erroneous values, for example a value 0.
- a pressure sensor has a measurement accuracy which depends on its temperature. Generally, the accuracy is optimal in the temperature range 0 ° C-90 ° C. It becomes much larger when the sensor is very cold ( ⁇ 0 ° C) or very hot (> 90 ° C).
- the figure 3 illustrates the evolution of the error ranges as a function of the temperature respectively for two specific pressure sensors, namely a Capatm atmospheric pressure sensor and a Capsural boost sensor.
- the temperature is indicated on the abscissa with ordinates of error multiplier values.
- a template comprising two curves delimits the range of errors for a succession of temperatures.
- the two dotted curves are associated with the Capsural boost sensor while the two solid lines are associated with the Capatm atmospheric pressure sensor.
- the curves for each sensor are different with a higher margin of error for the values of the Capsural boost sensor than for the Capatm atmospheric pressure sensor.
- a Capatm atmospheric pressure sensor is accurate to +/- 15mb in the 0-85 ° C area
- a Capsural boost pressure sensor is accurate to +/- 25mb in the same area.
- a maximum compensation of Crmax (T1) and Crmax (T) respectively for a temperature T1 or T can be defined between the points furthest from each other by one of the curves of the Capatm atmospheric pressure sensor with a curves of the Capsural boost sensor, between the highest curve of the Capsural boost sensor and the lowest curve of the Capatm atmospheric sensor.
- the figure 3 shows that by keeping the same registration compensation for all temperatures, the accuracy of the pressure measurement is degraded by a specific sensor. This can lead to unacceptable situations, for example of non-starting or loss of performance of the internal combustion engine, for example by the false determination of a target torque of the engine.
- the problem underlying the invention is to optimize a method of readjusting sensors present in an air intake line of an engine with a detection of a sensor failure which is effective while does not prevent the proper functioning of the engine and in particular its starting.
- a method of readjusting at least two pressure sensors positioned in an air intake line of an internal combustion engine in which said at least two sensors pressure are readjusted by a compensation compensation calculated for at least a second sensor with respect to a first pressure sensor serving as a reference sensor between their respective pressure measurements at a temperature known as initial of the sensors during an engine stop, this registration compensation then being applied to said at least one second sensor for correction of its pressure measurements, characterized in that, prior to the application of registration compensation on said at least one second sensor, a step internal diagnostic based on the value of the compensation for shifting consisting in determining if the compensation for shifting exceeds a value of maximum compensation, in which case it is diagnosed that one of said at least two sensors is faulty and in that, in this case, the application of the compensation for registration is suspended.
- the technical effect is to obtain a readjustment process of at least two pressure sensors which is freed from the times necessary for the development of diagnoses, this by carrying out a diagnosis directly internally faster. This eliminates completely the situations of non-start-up or loss of performance caused by a readjustment process according to the state of the art requiring a long time to develop a diagnosis.
- the internal diagnosis finds a fault, then readjustment is prohibited and is not carried out. This allows, on the one hand, not to reset the sensors to inconsistent values when the internal diagnosis indicates a failure and, on the other hand, to reset the sensors more quickly when the internal diagnosis indicates no failure.
- the solution proposed by the present invention is a software solution, simple to implement, since it can immediately be integrated into an engine control. It is also very inexpensive since it does not require additional equipment. This solution is essential because the resetting of the sensors is crucial for the proper functioning of the control of the air flow in the engine which cannot function correctly without this resetting.
- the registration is done on at least three pressure sensors with a first reference sensor among said at least three sensors and, if the compensation compensation between the first sensor and respectively the second and third sensors both exceed the value of maximum compensation, it is diagnosed that the first sensor has failed, while, if the compensation compensation of the first sensor exceeds the maximum compensation value with one of the second and third sensors then it does not exceed the maximum value with the other of the second or third sensors, it is diagnosed that the second or the third sensor associated with a compensation for adjustment which exceeds the maximum compensation value has failed.
- the maximum compensation value is specific to the pair or to each pair formed by said at least two sensors, the maximum compensation value being greater than 20 or 30 millibars.
- a respective error mask as a function of the temperature of the sensor is developed for each sensor, the error mask of each sensor defining an error range for each temperature, the compensation for registration being calculated from the difference. respective pressure measurements of said at least two sensors at the initial temperature.
- a temperature measurement step is carried out before said registration compensation at the level of said at least two sensors and, if the temperature is not within a predetermined temperature interval, registration compensation is suspended, this interval being from 0 to 85 ° C.
- the compensation compensation after application of the compensation compensation on said at least one second sensor, it is expected for a predetermined time interval sufficient to carry out a verification that the state of said at least two sensors allows them to carry out a coherent pressure measurement and if it is found that a sensor is not in a condition to carry out a coherent pressure measurement, the application of the compensation for registration is canceled, this time interval being approximately two seconds.
- a system for waiting for the reading of the verification made by a diagnosis external to the sensor is set up, in order to confirm or cancel the registration. .
- This verification is essentially based on an external diagnosis which can be done by control elements external to the sensor. This external diagnosis is more complete than the internal diagnosis previously carried out, but takes more time. This is why the invention first of all provides for carrying out an internal diagnosis so as not to have a problem waiting for the internal diagnosis which could lead to a non-start up, this internal diagnosis being verified by the longer external diagnosis Implementation.
- the invention relates to a powertrain comprising an internal combustion engine with an air intake line to the engine, the line comprising a first and at least a second pressure sensor, characterized in that said at least one second sensor pressure is readjusted relative to the first pressure sensor according to a readjustment method as described above.
- the first and said at least one second pressure sensor are selected from an atmospheric pressure sensor, a boost sensor positioned downstream of a turbocharger compressor of a supercharged internal combustion engine and a intake pressure sensor positioned in an intake air distributor.
- the first sensor is the atmospheric pressure sensor.
- the engine is with spark ignition.
- the present invention relates to a readjustment process of at least two Capatm, Capsural, Capadmi pressure sensors positioned in an air intake line of an internal combustion engine.
- said at least two Capatm, Capsural, Capadmi pressure sensors are readjusted by a compensation of Cr (T1) or Cr (T) readjustment calculated for at least a second Capsural, Capadmi sensor compared to a first Capatm sensor of pressure serving as a reference sensor between their respective pressure measurements at a so-called initial temperature of the sensors when the engine is stopped.
- This compensation for registration Cr (T1) or Cr (T) is then applied to said at least one second Capsural sensor, Capadmi for correction of its pressure measurements.
- an internal diagnostic step is carried out prior to the application of the compensation compensation for said at least one second sensor. on the value of the adjustment compensation consisting in determining whether the adjustment compensation exceeds a maximum compensation value.
- the registration compensation exceeds a maximum compensation value, it is diagnosed that one of said at least two sensors is faulty and, in this case, the application of registration compensation is suspended.
- the maximum compensation value Crmax (T), Crmax (T1) can be specific to the pair or to each pair formed by said at least two sensors Capatm, Capsural, Capadmi, the maximum compensation value Crmax (T), Crmax (T1) being greater than 20 or 30 millibars.
- a respective error template as a function of the temperature of the Capatm, Capsural, Capadmi sensor can be produced for each sensor, the error template of each Capatm, Capsural, Capadmi sensor defining an error range for each temperature.
- the compensation compensation Cr (T1) or Cr (T) can then be calculated from the difference of the respective pressure measurements of said at least two Capatm, Capsural, Capadmi sensors at the initial temperature.
- a predetermined time interval may be expected sufficient to carry out a verification that the state of said at least two sensors Capatm, Capsural, Capadmi allows them to perform a consistent pressure measurement.
- the predetermined time interval can be approximately two seconds.
- the invention relates to a powertrain comprising an internal combustion engine with an air intake line to the engine, the line comprising a first and at least a second Capsural, Capadmi pressure sensor.
- said at least one second Capural sensor, Capadmi pressure is reset relative to the first Capatm pressure sensor according to a registration process as described above.
- Capadmi pressure can be selected from a Capatm atmospheric pressure sensor, a Capsural boost sensor positioned downstream of a supercharged internal combustion engine turbocharger compressor and a pressure sensor d Capadmi intake positioned in an intake air distributor.
- Capatm atmospheric pressure sensor may for example have only a Capatm atmospheric pressure sensor and a Capadmi air intake sensor in the case of a non-turbocharged engine.
- Other pressure sensors can also be taken into account.
- the first sensor in the sense of the present invention can be the Capatm atmospheric pressure sensor, this being the most precise and the internal combustion engine can be with spark ignition.
- the figure 4 shows a flow diagram of a method for resetting pressure sensors present in the air intake line of an internal combustion engine, this method being in accordance with the state of the art, while referring to the other figures for references not indicated in this figure.
- This registration process includes the step of turning on or awakening the computer referenced 1 to the figure 4 . This is done as soon as the electrical contact is made for the motor vehicle. From this ignition, a timer T elapses allowing the pressure sensors to readjust as it can be seen in the Figures 1 and 2 .
- the readjustment of the pressure sensors by calculating the differences between the values measured by the various sensors is referenced 2 in the figure 4 .
- Registration compensation, previously referenced Cr (T) or Cr (T1) at the figure 3 is thus calculated for each pressure sensor with respect to a reference sensor which is advantageously the Capatm atmospheric pressure sensor.
- step referenced 3a The registration is then applied during a step referenced 3a. This registration is done without internal diagnosis. Then, if a failure is detected, during the next step referenced 4, the engine start is suspended or if no failure is detected, the engine is started. No updating of the compensation compensation with respect to the temperature of the sensors which may vary is provided for in this registration process according to the state of the art.
- the registration process according to the present invention retains the steps referenced 1 and 2 above mentioned, respectively concerning the ignition of the computer, that is to say its awakening by its power-up, and the recalibration calculations for the pressure sensors relative to a reference sensor.
- the inventive contribution lies in the management of the authorizations for this registration.
- the registration process begins with the power-up of the computer in charge of the process.
- a first so-called delay time T is launched as soon as the computer is powered up.
- this delay time T has the role of ensuring the balance of the pressures in the air line and that the sensors are in the state to carry out a coherent measurement. Starting or starting the engine interrupts this time delay.
- the step referenced 3 of the registration process according to the present invention relates to an internal diagnosis.
- the role of internal diagnostics is to determine whether one of the sensors detects an atmospheric pressure measurement very far from the pressure measurement of the other or the other sensors.
- an internal diagnostic step is based on the value of the compensation compensation consisting in determining whether the compensation compensation Cr (T1) or Cr (T) exceeds a maximum compensation value Crmax (T), Crmax (T1), this internal diagnostic step being referenced 5 at the figure 5 .
- the registration is then done on at least three Capatm, Capsural, Capadmi pressure sensors with a first reference Capatm sensor among said at least three Capatm, Capsural, Capadmi sensors. It is possible to determine which pressure sensor is faulty among the three, the reference sensor being able to be as well as a failed sensor.
- the Cr (T1) or Cr (T) compensation compensation of the first Capatm sensor exceeds the maximum compensation value Crmax (T), Crmax (T1) with one of the second and third Capsural sensors, Capadmi while it does not exceed the maximum value with the other of the second or third sensors, it is diagnosed that the second or the third Capsural sensor, Capadmi associated with a Cr (T1) or Cr (T) registration compensation exceeding the compensation value maximum Crmax (T), Crmax (T1) is faulty.
- Reference 6 to the figure 5 indicates the step for measuring the sensor temperatures. If the temperatures of the sensors go beyond a certain threshold, for example by leaving the temperature interval between 0 and 85 ° C. then the initial compensation compensation Cr (T1) or Cr (T) is suspended.
- the sensor (s) are reset pressure relative to one of the pressure sensors then being the reference sensor. This step is referenced 3 to the figure 5 . Only one of these two temperature or outlier conditions is sufficient to suspend registration.
- the verification step is carried out if a diagnostic variable for each sensor reveals a failure of the respective Capatm, Capsural, Capadmi sensor, this by a complete and external diagnosis to the sensors. In this case, the registration carried out in step 3 is canceled.
- This verification and cancellation or confirmation step is referenced 4 to the figure 5 .
- This operation is done after resetting since it cannot be done before due to too long a duration for the completion of the complete diagnosis on the sensors. Given the arrival time of the complete sensor diagnostic variable, incompatible with the need to quickly reset the sensors, the registration takes place before any detection and confirmation of a fault but can be revised later by being canceled.
- the complete diagnosis on the sensors only arrives after a certain period after registration. This period is of the order of 2 seconds. However, if a sensor fault is noted by the complete diagnosis of the sensors, this fault is taken into account to cancel the registration.
- the cancellation step or the confirmation step of registration is referenced 7.
- the sensors keep their original value while the registration is confirmed if no fault on the sensors is found.
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Description
La présente invention concerne un procédé de recalage d'au moins deux capteurs de pression positionnés dans une ligne d'admission d'air d'un moteur à combustion interne avec prévention d'un défaut dans un des capteurs, la détection d'un défaut dans un des capteurs entraînant la suspension de la mise en oeuvre du procédé.The present invention relates to a method of readjusting at least two pressure sensors positioned in an air intake line of an internal combustion engine with prevention of a fault in one of the sensors, the detection of a fault in one of the sensors causing the suspension of the implementation of the method.
L'invention se situe dans le domaine technique du système de contrôle commande d'un moteur à combustion interne qui est de préférence à allumage commandé.The invention lies in the technical field of the command and control system of an internal combustion engine which is preferably with spark ignition.
Il est fréquent que, dans une ligne d'admission d'air d'un moteur à combustion interne, trois capteurs de pression soient présents, à savoir un capteur de pression atmosphérique, un capteur de pression de suralimentation, ceci quand le moteur est turbocompressé, le capteur de pression de suralimentation se trouvant en aval d'un compresseur d'un turbocompresseur et un capteur de pression d'admission positionné dans le répartiteur d'air. Ces trois capteurs servent à la mesure de la pression existante en certains points spécifiques de la ligne d'admission d'air.Frequently, in an air intake line of an internal combustion engine, three pressure sensors are present, namely an atmospheric pressure sensor, a boost pressure sensor, this when the engine is turbocharged. , the boost pressure sensor located downstream of a compressor of a turbocharger and an intake pressure sensor positioned in the air distributor. These three sensors are used to measure the pressure existing at certain specific points on the air intake line.
La mesure d'une même pression par plusieurs capteurs peut donner des valeurs différentes, dû à leur précision intrinsèque et évolutive. Ceci se produit notamment à moteur à l'arrêt pour lequel la pression mesurée par chaque capteur est la pression atmosphérique, ce qui ne sera pas forcément le cas en fonctionnement du moteur.The measurement of the same pressure by several sensors can give different values, due to their intrinsic and evolving precision. This occurs in particular with the engine stopped, for which the pressure measured by each sensor is atmospheric pressure, which will not necessarily be the case in engine operation.
Il est donc nécessaire de recaler ces capteurs de pression avant leur utilisation, ce recalage se faisant lors d'un arrêt du moteur avant démarrage du véhicule. Le recalage des capteurs de pressions consiste à compenser ce décalage, afin d'égaliser les valeurs mesurées sur les capteurs quand la pression à mesurer est la même. Cette opération est particulièrement nécessaire au bon fonctionnement du pilotage d'un moteur à allumage commandé.It is therefore necessary to readjust these pressure sensors before their use, this readjustment being done when the engine stops before starting the vehicle. The adjustment of the pressure sensors consists in compensating for this offset, in order to equalize the values measured on the sensors when the pressure to be measured is the same. This operation is particularly necessary for the correct operation of the piloting of a positive-ignition engine.
Actuellement, il est connu un procédé de recalage des capteurs de pression de la ligne d'admission d'air. Les étapes de ce procédé de recalage sont les suivants. A l'arrêt moteur, les trois capteurs mesurent la même pression : la pression atmosphérique. On profite donc de cette phase de vie pour réaliser le recalage.Currently, a method of readjusting the pressure sensors of the air intake line is known. The steps of this registration process are as follows. When the engine stops, the three sensors measure the same pressure: atmospheric pressure. We therefore take advantage of this phase of life to achieve registration.
Pour ce recalage, un capteur de référence est choisi par calibration. C'est par rapport à la mesure de ce capteur que les autres capteurs seront recalés. Ce capteur de référence doit être le capteur le plus précis. C'est fréquemment le cas pour un capteur de pression atmosphérique qui est le plus souvent privilégié comme capteur de référence.For this readjustment, a reference sensor is chosen by calibration. It is in relation to the measurement of this sensor that the other sensors will be readjusted. This reference sensor must be the most accurate sensor. This is frequently the case for an atmospheric pressure sensor which is most often preferred as a reference sensor.
A l'initialisation d'un calculateur de bord embarqué dans le véhicule automobile et effectuant le contrôle commande du groupe motopropulseur ainsi que de ses éléments auxiliaires, une temporisation est lancée. Cette temporisation permet, d'une part, de s'assurer que la ligne d'admission est à l'équilibre de pression atmosphérique, et d'autre part, de s'assurer que les capteurs sont dans un état leur permettant de réaliser une mesure cohérente. Pendant cette temporisation, on détermine les différences de valeurs mesurées entre le capteur de référence et chaque capteur à recaler.Upon initialization of an on-board computer in the motor vehicle and carrying out the control command of the powertrain as well as of its auxiliary elements, a timer is started. This delay makes it possible, on the one hand, to ensure that the intake line is at equilibrium of atmospheric pressure, and on the other hand, to ensure that the sensors are in a state allowing them to perform a consistent measure. During this time delay, the differences in measured values between the reference sensor and each sensor to be readjusted are determined.
A la fin de cette temporisation, ces différences sont alors ajoutées aux valeurs des capteurs à recaler pour compenser le décalage. Afin d'assurer que le recalage soit bien effectué dans la plupart des cas de démarrage, même des démarrages rapides pour lesquelles le moteur n'a été laissé à l'arrêt que brièvement, la temporisation est calibrée de manière très courte. Son ordre de grandeur est de 300 millisecondes.At the end of this time delay, these differences are then added to the values of the sensors to be readjusted to compensate for the offset. In order to ensure that the resetting is carried out in most starting cases, even rapid starts for which the engine has been left at a standstill only briefly, the time delay is calibrated very short. Its order of magnitude is 300 milliseconds.
Si la mise en action du moteur a lieu avant la fin de la temporisation, alors le recalage est inhibé car on considère que le recalage n'est pas assez fiable, les valeurs mesurées ayant été faussées du fait qu'un ou des capteurs de pression n'étaient pas dans leur état de fonctionnement optimal.If the actuation of the motor takes place before the end of the time delay, then the readjustment is inhibited because it is considered that the readjustment is not reliable enough, the measured values having been distorted due to the fact that one or more pressure sensors were not in their optimal working condition.
La
Aux
A partir de l'établissement d'un contact électrique déclenchant le réveil I d'un calculateur de bord embarqué dans le véhicule automobile, le chronogramme des
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A la
La remontée de défaillance Def peut se faire par émission d'un drapeau de reconfiguration, aussi connu sous la dénomination anglo-saxonne de flag. Le drapeau de reconfiguration est une variable booléenne du logiciel de contrôle moteur représentant l'état d'un diagnostic. Lorsqu'un diagnostic est réalisé, si un défaut est détecté et confirmé, alors le drapeau de reconfiguration associé à ce diagnostic vaut 1. S'il n'y a pas de défaut confirmé, alors il vaut 0.Def defect can be raised by issuing a reconfiguration flag, also known by the Anglo-Saxon name of flag. The reconfiguration flag is a Boolean variable in the engine control software representing the state of a diagnosis. When a diagnosis is carried out, if a fault is detected and confirmed, then the reconfiguration flag associated with this diagnosis is worth 1. If there is no confirmed fault, then it is worth 0.
Le drapeau de reconfiguration permet de repérer une défaillance d'un capteur de pression et les fonctions de pilotage du moteur utilisent ce drapeau afin d'activer des stratégies de recouvrement lors d'une défaillance du capteur.The reconfiguration flag identifies a failure of a pressure sensor and the engine control functions use this flag to activate recovery strategies in the event of a sensor failure.
Le temps d'émission d'un drapeau de configuration peut être de l'ordre de 2 secondes et est à comparer avec celui de la temporisation de recalage et le besoin d'application rapide du recalage. Ainsi, en cas de défaut du capteur de référence, le plus fréquemment le capteur de pression d'air atmosphérique Capatm, la défaillance du capteur n'est signalée qu'après l'application du recalage. Le diagnostic n'est donc pas utile. Mais surtout, le recalage sera réalisé à partir de valeurs erronées, par exemple une valeur 0.The transmission time of a configuration flag can be of the order of 2 seconds and is to be compared with that of the registration delay and the need for rapid application of registration. Thus, in the event of a defect in the reference sensor, most often the Capatm atmospheric air pressure sensor, the sensor failure is not signaled until after the registration has been applied. The diagnosis is therefore not useful. But above all, the registration will be carried out from erroneous values, for example a value 0.
De plus, dans l'état de la technique le plus proche, il n'y a pas de prise en compte de la température des capteurs de pression pour le calcul du recalage. Ceci peut amener à une dégradation importante de la précision du capteur. La performance en conduite du véhicule est alors dégradée et même il peut y avoir une impossibilité de démarrage.In addition, in the closest prior art, there is no consideration of the temperature of the pressure sensors for the calculation of the registration. This can lead to a significant deterioration in the accuracy of the sensor. The driving performance of the vehicle is then degraded and even it may be impossible to start.
Un capteur de pression a une précision de mesure qui dépend de sa température. Généralement, la précision est optimale dans la plage de température 0°C-90°C. Elle devient bien plus grande dès lors que le capteur est très froid (<0°C) ou très chaud (>90°C).A pressure sensor has a measurement accuracy which depends on its temperature. Generally, the accuracy is optimal in the temperature range 0 ° C-90 ° C. It becomes much larger when the sensor is very cold (<0 ° C) or very hot (> 90 ° C).
La
Pour chaque capteur, un gabarit comportant deux courbes délimite la gamme d'erreurs pour une succession de températures. Les deux courbes en pointillés sont associées au capteur de suralimentation Capsural tandis que les deux courbes en trait plein sont associées au capteur de pression atmosphérique Capatm. Les courbes pour chaque capteur sont différentes avec une marge d'erreur plus élevée pour les valeurs du capteur de suralimentation Capsural que pour le capteur de pression atmosphérique Capatm.For each sensor, a template comprising two curves delimits the range of errors for a succession of temperatures. The two dotted curves are associated with the Capsural boost sensor while the two solid lines are associated with the Capatm atmospheric pressure sensor. The curves for each sensor are different with a higher margin of error for the values of the Capsural boost sensor than for the Capatm atmospheric pressure sensor.
Par exemple, un capteur de pression atmosphérique Capatm est précis à +/-15mb dans la zone 0-85°C, alors qu'un capteur de pression de suralimentation Capsural est précis à +/-25mb dans la même zone. Il en va de même pour un capteur de pression d'admission d'air positionné dans un répartiteur d'air que pour un capteur de pression de suralimentation Capsural, sans que le gabarit de ce capteur de pression d'admission ne soit montré à la
Une compensation de recalage maximale Crmax (T1) et Crmax (T) respective pour une température T1 ou T peut être définie entre les points les plus éloignés l'un de l'autre d'une des courbes du capteur de pression atmosphérique Capatm avec une des courbes du capteur de suralimentation Capsural, entre la courbe la plus haute du capteur de suralimentation Capsural et la courbe la plus basse du capteur atmosphérique Capatm.A maximum compensation of Crmax (T1) and Crmax (T) respectively for a temperature T1 or T can be defined between the points furthest from each other by one of the curves of the Capatm atmospheric pressure sensor with a curves of the Capsural boost sensor, between the highest curve of the Capsural boost sensor and the lowest curve of the Capatm atmospheric sensor.
Par exemple, en prenant comme capteur de référence le capteur de pression atmosphérique Capatm, quand la compensation de recalage maximale Crmax (T1), précédemment prise pour la température T1, est appliquée dans la zone médiane de précision optimale des capteurs pour le capteur de suralimentation Capsural, par exemple à la température T, cela peut faire sortir la précision de ce capteur de suralimentation Capsural en-dehors des bornes de précision intrinsèque de son gabarit.For example, taking as reference sensor the atmospheric pressure sensor Capatm, when the maximum registration compensation Crmax (T1), previously taken for the temperature T1, is applied in the middle zone of Optimal accuracy of the sensors for the Capsural boost sensor, for example at temperature T, this can cause the accuracy of this Capsural boost sensor to go outside the intrinsic precision limits of its size.
La
Le document
Par conséquent, le problème à la base de l'invention est d'optimiser un procédé de recalage de capteurs présents dans une ligne d'admission d'air d'un moteur avec une détection de défaillance d'un capteur qui soit efficace tout en n'empêchant pas le bon fonctionnement du moteur et notamment son démarrage.Consequently, the problem underlying the invention is to optimize a method of readjusting sensors present in an air intake line of an engine with a detection of a sensor failure which is effective while does not prevent the proper functioning of the engine and in particular its starting.
Pour atteindre cet objectif, il est prévu selon l'invention un procédé de recalage d'au moins deux capteurs de pression positionnés dans une ligne d'admission d'air d'un moteur à combustion interne, dans lequel lesdits au moins deux capteurs de pression sont recalés par une compensation de recalage calculée pour au moins un deuxième capteur par rapport à un premier capteur de pression servant de capteur de référence entre leurs mesures de pression respectives à une température dite initiale des capteurs lors d'un arrêt du moteur, cette compensation de recalage étant ensuite appliquée sur ledit au moins un deuxième capteur pour correction de ses mesures de pression, caractérisé en ce qu'il est effectué, préalablement à l'application de la compensation de recalage sur ledit au moins un deuxième capteur, une étape de diagnostic interne basé sur la valeur de la compensation de recalage consistant à déterminer si la compensation de recalage dépasse une valeur de compensation maximale, auquel cas il est diagnostiqué qu'un desdits au moins deux capteurs est défaillant et en ce que, dans ce cas, l'application de la compensation de recalage est suspendue.To achieve this objective, there is provided according to the invention a method of readjusting at least two pressure sensors positioned in an air intake line of an internal combustion engine, in which said at least two sensors pressure are readjusted by a compensation compensation calculated for at least a second sensor with respect to a first pressure sensor serving as a reference sensor between their respective pressure measurements at a temperature known as initial of the sensors during an engine stop, this registration compensation then being applied to said at least one second sensor for correction of its pressure measurements, characterized in that, prior to the application of registration compensation on said at least one second sensor, a step internal diagnostic based on the value of the compensation for shifting consisting in determining if the compensation for shifting exceeds a value of maximum compensation, in which case it is diagnosed that one of said at least two sensors is faulty and in that, in this case, the application of the compensation for registration is suspended.
L'effet technique est d'obtenir un procédé de recalage d'au moins deux capteurs de pression qui soit affranchi des temps nécessaires pour l'élaboration de diagnostics, ceci en réalisant un diagnostic directement en interne plus rapide. On élimine ainsi complètement les situations de non démarrage ou de perte de performance causées par un procédé de recalage selon l'état de la technique nécessitant un temps d'élaboration important de diagnostic.The technical effect is to obtain a readjustment process of at least two pressure sensors which is freed from the times necessary for the development of diagnoses, this by carrying out a diagnosis directly internally faster. This eliminates completely the situations of non-start-up or loss of performance caused by a readjustment process according to the state of the art requiring a long time to develop a diagnosis.
Si le diagnostic interne constate une défaillance, alors le recalage est interdit et n'est pas réalisé. Ceci permet, d'une part, de ne pas recaler les capteurs à des valeurs incohérentes quand le diagnostic interne indique une défaillance et, d'autre part, de recaler plus vite les capteurs quand le diagnostic interne n'indique aucune défaillance.If the internal diagnosis finds a fault, then readjustment is prohibited and is not carried out. This allows, on the one hand, not to reset the sensors to inconsistent values when the internal diagnosis indicates a failure and, on the other hand, to reset the sensors more quickly when the internal diagnosis indicates no failure.
La solution proposée par la présente invention est une solution logicielle, simple à implémenter, car immédiatement intégrable dans un contrôle moteur. Elle est également très peu coûteuse puisqu'elle ne demande pas d'équipement supplémentaire. Cette solution s'impose car le recalage des capteurs est crucial pour le bon fonctionnement du contrôle du débit d'air dans le moteur qui ne peut fonctionner correctement sans ce recalage.The solution proposed by the present invention is a software solution, simple to implement, since it can immediately be integrated into an engine control. It is also very inexpensive since it does not require additional equipment. This solution is essential because the resetting of the sensors is crucial for the proper functioning of the control of the air flow in the engine which cannot function correctly without this resetting.
Avantageusement, le recalage se fait sur au moins trois capteurs de pression avec un premier capteur de référence parmi lesdits au moins trois capteurs et, si les compensations de recalage entre le premier capteur et respectivement les deuxième et troisième capteurs dépassent toutes les deux la valeur de compensation maximale, il est diagnostiqué que le premier capteur est défaillant, tandis que, si la compensation de recalage du premier capteur dépasse la valeur de compensation maximale avec l'un des deuxième et troisième capteurs alors qu'elle ne dépasse pas la valeur maximale avec l'autre des deuxième ou troisième capteurs, il est diagnostiqué que le deuxième ou le troisième capteur associé à une compensation de recalage dépassant la valeur de compensation maximale est défaillant.Advantageously, the registration is done on at least three pressure sensors with a first reference sensor among said at least three sensors and, if the compensation compensation between the first sensor and respectively the second and third sensors both exceed the value of maximum compensation, it is diagnosed that the first sensor has failed, while, if the compensation compensation of the first sensor exceeds the maximum compensation value with one of the second and third sensors then it does not exceed the maximum value with the other of the second or third sensors, it is diagnosed that the second or the third sensor associated with a compensation for adjustment which exceeds the maximum compensation value has failed.
Ainsi, il peut facilement être déterminé quel capteur des trois capteurs présents est défaillant, la probabilité que deux capteurs soient simultanément défaillants étant très faible.Thus, it can easily be determined which sensor of the three sensors present is faulty, the probability that two sensors are simultaneously faulty being very low.
Avantageusement, la valeur de compensation maximale est spécifique à la paire ou à chaque paire formée par lesdits au moins deux capteurs, la valeur de compensation maximale étant supérieure à 20 ou 30 millibars.Advantageously, the maximum compensation value is specific to the pair or to each pair formed by said at least two sensors, the maximum compensation value being greater than 20 or 30 millibars.
Avantageusement, un gabarit d'erreur respectif en fonction de la température du capteur est élaboré pour chaque capteur, le gabarit d'erreur de chaque capteur définissant une plage d'erreur pour chaque température, la compensation de recalage étant calculée à partir de la différence des mesures de pression respectives desdits au moins deux capteurs à la température initiale.Advantageously, a respective error mask as a function of the temperature of the sensor is developed for each sensor, the error mask of each sensor defining an error range for each temperature, the compensation for registration being calculated from the difference. respective pressure measurements of said at least two sensors at the initial temperature.
Avantageusement, il est effectué, préalablement à la compensation de recalage, une étape de mesure de température au niveau desdits au moins deux capteurs et si la température n'est pas à l'intérieur d'un intervalle de température prédéterminé, la compensation de recalage est suspendue, cet intervalle étant de 0 à 85°C.Advantageously, a temperature measurement step is carried out before said registration compensation at the level of said at least two sensors and, if the temperature is not within a predetermined temperature interval, registration compensation is suspended, this interval being from 0 to 85 ° C.
Ceci permet de ne pas tomber dans la situation où la performance des capteurs est dégradée à cause d'un recalage réalisé à chaud ou à froid, c'est-à-dire en dessous de 0°C et au-dessus de 85°C en mettant en place un système d'inhibition du recalage.This avoids falling into the situation where the performance of the sensors is degraded due to a registration carried out hot or cold, that is to say below 0 ° C and above 85 ° C by setting up a readjustment inhibition system.
Ceci permet de travailler avec des capteurs recalés dans une zone de précision optimale des capteurs. En dehors de cette zone de précision, il y aurait une possibilité de dégradation de la précision des capteurs due à une trop grande compensation de recalage maximale. En prenant en compte la température des capteurs, on élimine complètement les situations de non démarrage ou de perte de performance causées par le procédé selon l'état de la technique le plus proche.This makes it possible to work with sensors reset in an area of optimal sensor accuracy. Outside this precision zone, there would be a possibility of deterioration of the precision of the sensors due to too great a maximum compensation of registration. By taking into account the temperature of the sensors, the situations of non-starting or loss of performance caused by the process are completely eliminated according to the closest prior art.
Avantageusement, après application de la compensation de recalage sur ledit au moins un deuxième capteur, il est attendu pendant un intervalle de temps prédéterminé suffisant pour effectuer une vérification que l'état desdits au moins deux capteurs leur permet de réaliser une mesure de pression cohérente et s'il est constaté qu'un capteur n'est pas en état de réaliser une mesure de pression cohérente, l'application de la compensation de recalage est annulée, cet intervalle de temps étant environ de deux secondes. Ainsi, après le diagnostic interne permettant de s'affranchir du temps de diagnostic capteur, il est mis en place un système d'attente de la lecture de la vérification faite par un diagnostic externe au capteur, afin de confirmer ou d'annuler le recalage.Advantageously, after application of the compensation compensation on said at least one second sensor, it is expected for a predetermined time interval sufficient to carry out a verification that the state of said at least two sensors allows them to carry out a coherent pressure measurement and if it is found that a sensor is not in a condition to carry out a coherent pressure measurement, the application of the compensation for registration is canceled, this time interval being approximately two seconds. Thus, after the internal diagnosis enabling the sensor diagnostic time to be dispensed with, a system for waiting for the reading of the verification made by a diagnosis external to the sensor is set up, in order to confirm or cancel the registration. .
Cette vérification est basée essentiellement sur un diagnostic externe pouvant être fait par des éléments de contrôle externes au capteur. Ce diagnostic externe est plus complet que le diagnostic interne précédemment effectué mais prend plus de temps. C'est pour cela que l'invention prévoit tout d'abord d'effectuer un diagnostic interne pour ne pas avoir de problème d'attente du diagnostic interne pouvant entraîner un non démarrage, ce diagnostic interne étant vérifié par le diagnostic externe plus long de mise en oeuvre.This verification is essentially based on an external diagnosis which can be done by control elements external to the sensor. This external diagnosis is more complete than the internal diagnosis previously carried out, but takes more time. This is why the invention first of all provides for carrying out an internal diagnosis so as not to have a problem waiting for the internal diagnosis which could lead to a non-start up, this internal diagnosis being verified by the longer external diagnosis Implementation.
Il est ainsi prévu de compléter ce diagnostic interne qui peut être faux ou incomplet par une vérification plus complète mais requérant plus de temps tout en mettant en oeuvre quand même le procédé de recalage par défaut, cela au moins provisoirement.It is thus planned to complete this internal diagnosis which may be false or incomplete by a more complete verification but requiring more time while still implementing the default registration process, at least temporarily.
En effet, si cette vérification indique une défaillance d'un ou de capteurs, le procédé de recalage est annulé car il est considéré comme faussant la précision des capteurs. Le procédé de recalage n'aura alors été appliqué que pour une durée réduite n'entraînant pas ou peu de conséquence sur le fonctionnement optimal du moteur.Indeed, if this verification indicates a failure of one or more sensors, the registration process is canceled because it is considered to distort the accuracy of the sensors. The readjustment process will then have been applied only for a reduced duration which has little or no consequence on the optimal operation of the engine.
L'invention concerne un groupe motopropulseur comprenant un moteur à combustion interne avec une ligne d'admission d'air au moteur, la ligne comprenant un premier et au moins un deuxième capteur de pression, caractérisé en ce que ledit au moins un deuxième capteur de pression est recalé par rapport au premier capteur de pression conformément à un procédé de recalage tel que décrit précédemment.The invention relates to a powertrain comprising an internal combustion engine with an air intake line to the engine, the line comprising a first and at least a second pressure sensor, characterized in that said at least one second sensor pressure is readjusted relative to the first pressure sensor according to a readjustment method as described above.
Avantageusement, le premier et ledit au moins un deuxième capteur de pression sont sélectionnés parmi un capteur de pression atmosphérique, un capteur de suralimentation positionné en aval d'un compresseur de turbocompresseur de moteur à combustion interne suralimenté et un capteur de pression d'admission positionné dans un répartiteur d'air en admission.Advantageously, the first and said at least one second pressure sensor are selected from an atmospheric pressure sensor, a boost sensor positioned downstream of a turbocharger compressor of a supercharged internal combustion engine and a intake pressure sensor positioned in an intake air distributor.
Avantageusement, le premier capteur est le capteur de pression atmosphérique.Advantageously, the first sensor is the atmospheric pressure sensor.
Avantageusement, le moteur est à allumage commandé.Advantageously, the engine is with spark ignition.
D'autres caractéristiques, buts et avantages de la présente invention apparaîtront à la lecture de la description détaillée qui va suivre et au regard des dessins annexés donnés à titre d'exemples non limitatifs et sur lesquels :
- la
figure 1 est une représentation schématique d'un chronogramme du déroulement d'un procédé de recalage selon l'état de la technique, le démarrage ayant réussi, les capteurs de pression étant montrés au-dessus de ce chronogramme tout d'abord selon un premier graphique dans un état non recalé et ensuite selon un second graphique dans un état recalé, - la
figure 2 est une représentation schématique d'un chronogramme du déroulement d'un procédé de recalage selon l'état de la technique, les capteurs de pression étant montrés au-dessus de ce chronogramme tout d'abord selon un premier graphique dans un état non recalé et ensuite selon un second graphique dans un état recalé, le recalage n'ayant pas pu se faire avant le démarrage et le démarrage ayant été suspendu, - la
figure 3 est une représentation schématique de deux gabarits d'erreur pour respectivement un capteur de pression atmosphérique et un capteur de suralimentation, la compensation de recalage n'étant pas ajustée en fonction de la température, - la
figure 4 illustre un logigramme du procédé de recalage selon l'état de la technique tandis que lafigure 5 illustre un logigramme du procédé de recalage selon la présente invention.
- the
figure 1 is a schematic representation of a timing diagram of the progress of a registration process according to the state of the art, the start having been successful, the pressure sensors being shown above this timing diagram firstly according to a first graph in a non-readjusted state and then according to a second graph in a readjusted state, - the
figure 2 is a schematic representation of a chronogram of the progress of a registration process according to the state of the art, the pressure sensors being shown above this chronogram first of all according to a first graph in a non-readjusted state and then according to a second graph in a state failed, resetting could not be done before starting and starting having been suspended, - the
figure 3 is a schematic representation of two error templates for an atmospheric pressure sensor and a supercharging sensor, respectively, the compensation for adjustment is not adjusted as a function of the temperature, - the
figure 4 illustrates a flow diagram of the registration process according to the state of the art while thefigure 5 illustrates a flow diagram of the registration method according to the present invention.
Il est à garder à l'esprit que les figures sont données à titre d'exemples et ne sont pas limitatives de l'invention. Elles constituent des représentations schématiques de principe destinées à faciliter la compréhension de l'invention.It should be borne in mind that the figures are given by way of examples and are not limitative of the invention. They constitute schematic representations of principle intended to facilitate understanding of the invention.
Dans ce qui va suivre, il est fait référence à toutes les figures prises en combinaison. Quand il est fait référence à une ou des figures spécifiques, ces figures sont à prendre en combinaison avec les autres figures pour la reconnaissance des références numériques désignées.In what follows, reference is made to all the figures taken in combination. When reference is made to one or more specific figures, these figures are to be taken in combination with the other figures for the recognition of the designated numerical references.
Les
En se référant aux figures, et notamment à la
Dans ce procédé, lesdits au moins deux capteurs Capatm, Capsural, Capadmi de pression sont recalés par une compensation de recalage Cr(T1) ou Cr(T) calculée pour au moins un deuxième capteur Capsural, Capadmi par rapport à un premier capteur Capatm de pression servant de capteur de référence entre leurs mesures de pression respectives à une température dite initiale des capteurs lors d'un arrêt du moteur.In this method, said at least two Capatm, Capsural, Capadmi pressure sensors are readjusted by a compensation of Cr (T1) or Cr (T) readjustment calculated for at least a second Capsural, Capadmi sensor compared to a first Capatm sensor of pressure serving as a reference sensor between their respective pressure measurements at a so-called initial temperature of the sensors when the engine is stopped.
Cette compensation de recalage Cr(T1) ou Cr(T) est ensuite appliquée sur ledit au moins un deuxième capteur Capsural, Capadmi pour correction de ses mesures de pression.This compensation for registration Cr (T1) or Cr (T) is then applied to said at least one second Capsural sensor, Capadmi for correction of its pressure measurements.
Selon l'invention, il est effectué, préalablement à l'application de la compensation de recalage sur ledit au moins un deuxième capteur, une étape de diagnostic interne basé sur la valeur de la compensation de recalage consistant à déterminer si la compensation de recalage dépasse une valeur de compensation maximale.According to the invention, an internal diagnostic step is carried out prior to the application of the compensation compensation for said at least one second sensor. on the value of the adjustment compensation consisting in determining whether the adjustment compensation exceeds a maximum compensation value.
Si la compensation de recalage dépasse une valeur de compensation maximale, il est diagnostiqué qu'un desdits au moins deux capteurs est défaillant et, dans ce cas, l'application de la compensation de recalage est suspendue.If the registration compensation exceeds a maximum compensation value, it is diagnosed that one of said at least two sensors is faulty and, in this case, the application of registration compensation is suspended.
Avantageusement, la valeur de compensation maximale Crmax(T), Crmax(T1) peut être spécifique à la paire ou à chaque paire formée par lesdits aux moins deux capteurs Capatm, Capsural, Capadmi, la valeur de compensation maximale Crmax(T), Crmax(T1) étant supérieure à 20 ou 30 millibars.Advantageously, the maximum compensation value Crmax (T), Crmax (T1) can be specific to the pair or to each pair formed by said at least two sensors Capatm, Capsural, Capadmi, the maximum compensation value Crmax (T), Crmax (T1) being greater than 20 or 30 millibars.
Avantageusement, un gabarit d'erreur respectif en fonction de la température du capteur Capatm, Capsural, Capadmi peut être élaboré pour chaque capteur, le gabarit d'erreur de chaque capteur Capatm, Capsural, Capadmi définissant une plage d'erreur pour chaque température. La compensation de recalage Cr(T1) ou Cr(T) peut être alors calculée à partir de la différence des mesures de pression respectives desdits au moins deux capteurs Capatm, Capsural, Capadmi à la température initiale.Advantageously, a respective error template as a function of the temperature of the Capatm, Capsural, Capadmi sensor can be produced for each sensor, the error template of each Capatm, Capsural, Capadmi sensor defining an error range for each temperature. The compensation compensation Cr (T1) or Cr (T) can then be calculated from the difference of the respective pressure measurements of said at least two Capatm, Capsural, Capadmi sensors at the initial temperature.
Après application de la compensation de recalage Cr(T1) ou Cr(T) sur ledit au moins un deuxième capteur Capsural, Capadmi, il peut être attendu un intervalle de temps prédéterminé suffisant pour effectuer une vérification que l'état desdits au moins deux capteurs Capatm, Capsural, Capadmi leur permet de réaliser une mesure de pression cohérente.After application of the Cr (T1) or Cr (T) registration compensation on said at least one second Capsural sensor, Capadmi, a predetermined time interval may be expected sufficient to carry out a verification that the state of said at least two sensors Capatm, Capsural, Capadmi allows them to perform a consistent pressure measurement.
S'il est constaté qu'un capteur Capatm, Capsural, Capadmi n'est pas en état de réaliser une mesure de pression cohérente, l'application de la compensation de recalage Cr(T1) ou Cr(T) peut être annulée. L'intervalle de temps prédéterminé peut être environ de deux secondes.If it is found that a Capatm, Capsural, Capadmi sensor is not in a position to carry out a coherent pressure measurement, the application of the compensation of registration Cr (T1) or Cr (T) can be canceled. The predetermined time interval can be approximately two seconds.
L'invention concerne un groupe motopropulseur comprenant un moteur à combustion interne avec une ligne d'admission d'air au moteur, la ligne comprenant un premier et au moins un deuxième capteur Capsural, Capadmi de pression. Dans ce groupe motopropulseur, ledit au moins un deuxième capteur Capsural, Capadmi de pression est recalé par rapport au premier capteur Capatm de pression conformément à un procédé de recalage tel que décrit précédemment.The invention relates to a powertrain comprising an internal combustion engine with an air intake line to the engine, the line comprising a first and at least a second Capsural, Capadmi pressure sensor. In this powertrain, said at least one second Capural sensor, Capadmi pressure is reset relative to the first Capatm pressure sensor according to a registration process as described above.
Comme généralement présents dans une ligne d'admission d'air à un moteur à combustion interne turbocompressé avec un répartiteur d'air en admission, le premier capatm et ledit au moins un deuxième capteur Capsural, Capadmi de pression peuvent être sélectionnés parmi un capteur de pression atmosphérique Capatm, un capteur de suralimentation Capsural positionné en aval d'un compresseur de turbocompresseur de moteur à combustion interne suralimenté et un capteur de pression d'admission Capadmi positionné dans un répartiteur d'air en admission.As generally present in an air intake line to a turbocharged internal combustion engine with an intake air distributor, the first capatm and said at least one second Capsural pressure sensor, Capadmi pressure can be selected from a Capatm atmospheric pressure sensor, a Capsural boost sensor positioned downstream of a supercharged internal combustion engine turbocharger compressor and a pressure sensor d Capadmi intake positioned in an intake air distributor.
Il peut par exemple n'avoir qu'un capteur de pression atmosphérique Capatm et un capteur d'admission Capadmi d'air dans le cas d'un moteur non turbocompressé. D'autres capteurs de pression peuvent aussi être pris en compte.It may for example have only a Capatm atmospheric pressure sensor and a Capadmi air intake sensor in the case of a non-turbocharged engine. Other pressure sensors can also be taken into account.
Le premier capteur au sens de la présente invention peut être le capteur de pression atmosphérique Capatm, celui-ci étant le plus précis et le moteur à combustion interne peut être à allumage commandé.The first sensor in the sense of the present invention can be the Capatm atmospheric pressure sensor, this being the most precise and the internal combustion engine can be with spark ignition.
La
Ce procédé de recalage comprend l'étape d'allumage ou de mise en éveil du calculateur référencée 1 à la
Le recalage des capteurs de pression par calcul des différences entre les valeurs relevées de pression par les différents capteurs est référencé 2 à la
Il est ensuite procédé à l'application du recalage lors d'une étape référencée 3a. Ce recalage se fait sans diagnostic interne. Ensuite, si une défaillance est détectée, lors de l'étape suivante référencée 4, il est procédé à la suspension du démarrage du moteur ou si aucune défaillance n'est détectée, il est procédé au démarrage du moteur. Aucune actualisation de la compensation de recalage par rapport à la température des capteurs pouvant varier n'est prévue dans ce procédé de recalage selon l'état de la technique.The registration is then applied during a step referenced 3a. This registration is done without internal diagnosis. Then, if a failure is detected, during the next step referenced 4, the engine start is suspended or if no failure is detected, the engine is started. No updating of the compensation compensation with respect to the temperature of the sensors which may vary is provided for in this registration process according to the state of the art.
En se référant aux figures et notamment à la
Le procédé de recalage selon l'invention débute avec la mise sous tension du calculateur en charge du procédé. Une première durée dite de temporisation T est lancée dès la mise sous tension du calculateur. Comme pour l'état de la technique montré à la
Lors de cette temporisation, il est procédé à l'étape référencée 2 à la
L'étape référencée 3 du procédé de recalage selon la présente invention concerne un diagnostic interne. Le diagnostic interne a pour rôle de déterminer si un des capteurs relève une mesure de pression atmosphérique très éloignée de la mesure de pression de l'autre ou des autres capteurs.The step referenced 3 of the registration process according to the present invention relates to an internal diagnosis. The role of internal diagnostics is to determine whether one of the sensors detects an atmospheric pressure measurement very far from the pressure measurement of the other or the other sensors.
Pour ce faire, on utilise les valeurs de compensation de décalage Cr(T1) ou Cr(T) précédemment calculées et on les compare à un seuil. Si ces valeurs sont au-delà d'un seuil, alors cela signifie qu'un des capteurs est défaillant. Cette étape se fait avec un moteur arrêté.To do this, we use the offset compensation values Cr (T1) or Cr (T) previously calculated and compare them to a threshold. If these values are above a threshold, then it means that one of the sensors has failed. This step is done with the engine stopped.
Ainsi, il est effectué, préalablement à l'application de la compensation de recalage sur un capteur de pression, une étape de diagnostic interne basé sur la valeur de la compensation de recalage consistant à déterminer si la compensation de recalage Cr(T1) ou Cr(T) dépasse une valeur de compensation maximale Crmax(T), Crmax(T1), cette étape de diagnostic interne étant référencée 5 à la
Dans ce cas, il est diagnostiqué que le capteur est défaillant et, dans ce cas, l'application de la compensation de recalage est suspendue. Cela permet de ne pas recaler les capteurs à des valeurs incohérentes.In this case, it is diagnosed that the sensor is faulty and, in this case, the application of the compensation for registration is suspended. This makes it possible not to readjust the sensors to inconsistent values.
Dans le mode préféré de réalisation de la présente invention, il peut y avoir trois capteurs de pression dans la ligne d'admission d'air au moteur. Le recalage se fait alors sur au moins trois capteurs Capatm, Capsural, Capadmi de pression avec un premier capteur Capatm de référence parmi lesdits au moins trois capteurs Capatm, Capsural, Capadmi. Il est possible de déterminer quel capteur de pression est défaillant parmi les trois, le capteur de référence pouvant l'être aussi bien qu'un capteur recalé.In the preferred embodiment of the present invention, there may be three pressure sensors in the air intake line to the engine. The registration is then done on at least three Capatm, Capsural, Capadmi pressure sensors with a first reference Capatm sensor among said at least three Capatm, Capsural, Capadmi sensors. It is possible to determine which pressure sensor is faulty among the three, the reference sensor being able to be as well as a failed sensor.
Si les compensations de recalage Cr(T1) ou Cr(T) entre le premier capteur Capatm, c'est-à-dire le capteur de référence et respectivement les deuxième et troisième capteurs Capsural, Capadmi dépassent toutes les deux la valeur de compensation maximale Crmax(T), Crmax(T1), il est diagnostiqué que le premier capteur Capatm est défaillant.If the Cr (T1) or Cr (T) readjustment compensations between the first Capatm sensor, i.e. the reference sensor and the second and third Capsural sensors respectively, Capadmi both exceed the maximum compensation value Crmax (T), Crmax (T1), it is diagnosed that the first Capatm sensor has failed.
Inversement, si la compensation de recalage Cr(T1) ou Cr(T) du premier capteur Capatm dépasse la valeur de compensation maximale Crmax(T), Crmax(T1) avec l'un des deuxième et troisième capteurs Capsural, Capadmi alors qu'elle ne dépasse pas la valeur maximale avec l'autre des deuxième ou troisième capteurs, il est diagnostiqué que le deuxième ou le troisième capteur Capsural, Capadmi associé à une compensation de recalage Cr(T1) ou Cr(T) dépassant la valeur de compensation maximale Crmax(T), Crmax(T1) est défaillant.Conversely, if the Cr (T1) or Cr (T) compensation compensation of the first Capatm sensor exceeds the maximum compensation value Crmax (T), Crmax (T1) with one of the second and third Capsural sensors, Capadmi while it does not exceed the maximum value with the other of the second or third sensors, it is diagnosed that the second or the third Capsural sensor, Capadmi associated with a Cr (T1) or Cr (T) registration compensation exceeding the compensation value maximum Crmax (T), Crmax (T1) is faulty.
La référence 6 à la
Il peut en effet être constaté au regard de la
Si toutes les conditions sont remplies, à savoir principalement une température de prise de mesure de pression dans l'intervalle et aucune valeur aberrante donnée par au moins un capteur, à la fin de la temporisation T, il est procédé au recalage du ou des capteurs de pression par rapport à un des capteurs de pression étant alors le capteur de référence. Cette étape est référencée 3 à la
Il est cependant attendu une variable d'un diagnostic complet pour chaque capteur Capatm, Capsural, Capadmi pendant une période de temps suivant le recalage référencé 3 à la
De ce fait, des défaillances peuvent ne pas avoir été diagnostiquées lors de l'étape de diagnostic interne 5 alors que ces défaillances peuvent être signalées par un diagnostic capteur complet. Ainsi, pendant une période après recalage, d'environ deux secondes, il est procédé à l'étape de vérification si une variable de diagnostic pour chaque capteur révèle une défaillance du capteur Capatm, Capsural, Capadmi respectif, ceci par un diagnostic complet et externe aux capteurs. Dans ce cas, le recalage réalisé à l'étape 3 est annulé. Cette étape de vérification et d'annulation ou de confirmation est référencée 4 à la
Cette opération est faite après recalage étant donné qu'elle ne peut pas se faire avant due à une trop grande durée pour l'accomplissement du diagnostic complet sur les capteurs. Etant donné le temps d'arrivée de la variable de diagnostic complet des capteurs, incompatible avec le besoin de recaler rapidement les capteurs, le recalage a lieu avant toute détection et confirmation d'un défaut mais peut être révisé par la suite en étant annulé.This operation is done after resetting since it cannot be done before due to too long a duration for the completion of the complete diagnosis on the sensors. Given the arrival time of the complete sensor diagnostic variable, incompatible with the need to quickly reset the sensors, the registration takes place before any detection and confirmation of a fault but can be revised later by being canceled.
Le diagnostic complet sur les capteurs n'arrive qu'après une certaine période après recalage. Cette période est de l'ordre de 2 secondes. Néanmoins, si un défaut d'un capteur est constaté par le diagnostic complet des capteurs, ce défaut est pris en compte pour annuler le recalage.The complete diagnosis on the sensors only arrives after a certain period after registration. This period is of the order of 2 seconds. However, if a sensor fault is noted by the complete diagnosis of the sensors, this fault is taken into account to cancel the registration.
A la
Claims (10)
- A method for resetting at least two pressure sensors (Capatm, Capsural, Capadmi) positioned in an air-intake line of an internal combustion engine, in which said at least two pressure sensors (Capatm, Capsural, Capadmi) are reset by a resetting compensation (Cr(T1) or Cr(T)) calculated for at least one second sensor (Capsural, Capadmi) with respect to a first pressure sensor (Capatm) serving as reference sensor between their respective pressure measurements at a temperature designated as initial temperature of the sensors when the engine is stopped, this resetting compensation (Cr(T1) or Cr(T)) being then applied to said at least one second sensor (Capsural, Capadmi) for correction of its pressure measurements, characterized in that there is carried out, prior to the application of the resetting compensation (Cr(T1) or Cr(T)) to said at least one second sensor (Capsural, Capadmi), an internal diagnostic step based on the value of the resetting compensation (Cr(T1) or CrT)) consisting of determining whether the resetting compensation (Cr(T1) or Cr(T)) exceeds a maximum compensation value (Crmax(T), Crmax(T1)), in which case it is diagnosed that one of said at least two sensors (Capatm, Capsural, Capadmi) is faulty and in that, in this case, the application of the resetting compensation (Cr(T1) or Cr(T)) is suspended.
- The method according to Claim 1, in which the resetting is carried out to at least three pressure sensors (Capatm, Capsural, Capadmi) with a first reference sensor (Capatm) among said at least three sensors (Capatm, Capsural, Capadmi) and, if the resetting compensations between the first sensor (Capatm) and respectively the second and third sensors (Capsural, Capadmi) both exceed the maximum compensation value (Crmax(T), Crmax/(T1)), it is diagnosed that the first sensor (Capatm) is faulty, whereas, if the resetting compensation (Cr(T1) or Cr(T)) of the first sensor (Capatm) exceeds the maximum compensation value (CrMax(T), Crmax(T1)) with one of the second and third sensors (Capsural, Capadmi), although it does not exceed the maximum value with the other of the second or third sensors (Capsural, Capadmi), it is diagnosed that the second or the third sensor (Capsural, Capadmi) associated with a resetting compensation (Cr(T1) or Cr(T)) exceeding the maximum compensation value (Crmax(T), Crmax(T1)) is faulty.
- The method according to any one of Claims 1 or 2, in which the maximum compensation value (Crmax(T), Crmax(T1)) is specific to a pair or to each pair formed by said at least two sensors (Capatm, Capsural, Capadmi), the maximum compensation value (Cmax(T), Crmax(T1)) being greater than 20 or 30 millibars.
- The method according to any one of the preceding claims, in which a respective error template is developed as a function of the temperature of the sensor (Capatm, Capsural, Capadmi) for each sensor (Capatm, Capsural, Capadmi), the error template of each sensor (Capatm, Capsural, Capadmi) defining a range of error for each temperature, the resetting compensation (Cr(T1) or Cr(T)) being calculated from the difference of the respective pressure measurements of said at least two sensors (Capatm, Capsural, Capadmi) at the initial temperature.
- The method according to any one of the preceding claims, in which there is carried out, prior to the resetting compensation (Cr), a measurement step of temperature at the level of said at least two sensors (Capatm, Capsural, Capadmi) and if the temperature is not within a predetermined temperature interval, the resetting compensation (Cr(T1) or Cr(T)) is suspended, this interval being from 0 to 85 °C.
- The resetting method according to any one of the preceding claims, in which , after application of the resetting compensation (Cr(T1) or Cr(T)) to said at least one second sensor (Capsural, Capadmi), there is a wait during a predetermined time interval sufficient to carry out a verification that the status of said at least two sensors (Capatm, Capsural, Capadmi) allows them to carry out a coherent pressure measurement and that if it is found that a sensor (Capatm, Capsural, Capadmi) is not in a state to carry out a coherent pressure measurement, the application of the resetting compensation (Cr(T1) or Cr(T)) is cancelled, this time interval being approximately two seconds.
- A powertrain including an internal combustion engine with an air-intake line to the engine, the line including a first (Capatm) and at least one second pressure sensor (Capsural, Capadmi), characterized in that said at least one second pressure sensor (Capsural, Capadmi) is reset with respect to the first pressure sensor (Capatm) in accordance with a resetting method according to any one of the preceding claims.
- The powertrain according to Claim 7, in which the first (Capatm) and said at least one second pressure sensor (Capsural, Capadmi) are selected from an atmospheric pressure sensor (Capatm), a supercharging sensor (Capsural) positioned downstream of a turbocharger compressor of a supercharged internal combustion engine, and an intake pressure sensor (Capadmi) positioned in an intake air distributor.
- The powertrain according to any one of Claims 7 or 8, in which the first sensor is the atmospheric pressure sensor (Capatm).
- The powertrain according to any one of Claims 7 to 9, in which the engine is a spark ignition engine.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1650882A FR3047518B1 (en) | 2016-02-04 | 2016-02-04 | METHOD FOR REPLACING TWO PRESSURE SENSORS IN AN AIR INTAKE LINE OF AN ENGINE WITH PREVENTION OF A SENSOR FAULT |
PCT/FR2017/050140 WO2017134363A1 (en) | 2016-02-04 | 2017-01-24 | Method for resetting two pressure sensors in an air-intake line of an engine with sensor fault prevention |
Publications (2)
Publication Number | Publication Date |
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EP3411580A1 EP3411580A1 (en) | 2018-12-12 |
EP3411580B1 true EP3411580B1 (en) | 2020-03-25 |
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Application Number | Title | Priority Date | Filing Date |
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EP17706560.4A Active EP3411580B1 (en) | 2016-02-04 | 2017-01-24 | Method for resetting two pressure sensors in an air-intake line of an engine with sensor fault prevention |
Country Status (4)
Country | Link |
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EP (1) | EP3411580B1 (en) |
CN (1) | CN108474314B (en) |
FR (1) | FR3047518B1 (en) |
WO (1) | WO2017134363A1 (en) |
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JP6710670B2 (en) * | 2017-10-30 | 2020-06-17 | ヤンマーパワーテクノロジー株式会社 | Control device for internal combustion engine |
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Publication number | Priority date | Publication date | Assignee | Title |
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DE10047811A1 (en) * | 2000-09-27 | 2002-04-18 | Volkswagen Ag | Method and device for regulating an internal combustion engine |
JP3788290B2 (en) * | 2001-08-22 | 2006-06-21 | 国産電機株式会社 | Method and apparatus for detecting atmospheric pressure for internal combustion engine control |
DE10261382B4 (en) * | 2002-12-30 | 2012-09-13 | Robert Bosch Gmbh | Method for adapting the characteristic of an intake manifold pressure sensor of an internal combustion engine |
JP4291624B2 (en) * | 2003-05-27 | 2009-07-08 | トヨタ自動車株式会社 | Control of internal combustion engine |
FR2933137B1 (en) * | 2008-06-30 | 2010-08-20 | Renault Sas | SYSTEM AND METHOD FOR CORRECTING THE MEASUREMENT OF A TURBINE FRONT PRESSURE SENSOR |
DE102011088296A1 (en) * | 2011-12-12 | 2013-06-13 | Robert Bosch Gmbh | Method and device for monitoring the dynamics of gas sensors |
JP5462390B1 (en) * | 2013-04-23 | 2014-04-02 | 三菱電機株式会社 | Control device for internal combustion engine |
US9810171B2 (en) * | 2013-12-03 | 2017-11-07 | Ford Global Technologies, Llc | Method for determining an offset of a manifold pressure sensor |
-
2016
- 2016-02-04 FR FR1650882A patent/FR3047518B1/en not_active Expired - Fee Related
-
2017
- 2017-01-24 EP EP17706560.4A patent/EP3411580B1/en active Active
- 2017-01-24 CN CN201780007473.6A patent/CN108474314B/en active Active
- 2017-01-24 WO PCT/FR2017/050140 patent/WO2017134363A1/en active Application Filing
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Also Published As
Publication number | Publication date |
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CN108474314B (en) | 2021-04-02 |
FR3047518A1 (en) | 2017-08-11 |
CN108474314A (en) | 2018-08-31 |
EP3411580A1 (en) | 2018-12-12 |
FR3047518B1 (en) | 2018-03-23 |
WO2017134363A1 (en) | 2017-08-10 |
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