METHOD FOR OPERATING A REAGENT METERING SYSTEM, DEVICE FOR CARRYING OUT THE METHOD, COMPUTER PROGRAM AND COMPUTER PROGRAM PRODUCT

Abstract

A method for operating a reagent metering system which meters a reagent into an exhaust duct of an internal combustion engine upstream of an SCR catalytic converter, in which, after the metering operation is ended, at least part of the reagent metering system is emptied by back-suction by means of a reciprocating pump. The procedure according to the invention is distinguished in that during the back-suction, a stop determination determines the flight time of a reciprocating piston of the reciprocating pump from a starting time as far as the stop time, in that a comparator compares the flight time determined with a flight time threshold value, and in that the activation power of the reciprocating pump is reduced if the flight time determined is less than the flight time threshold value.

Claims

1. A method of operating a reagent metering system (10) which meters a reagent (14) into an exhaust duct (16) of an internal combustion engine (18) upstream of an SCR catalytic converter (20), the method comprising: emptying at least part of the reagent metering system (10) by back-suction by a reciprocating pump after the metering operation has ended; determining a flight time (TZ) of a reciprocating piston of a reciprocating pump from a starting time (TS) as far as a stop time (TA) during the back-suction; comparing the flight time (TZ), by a comparator (50), with a flight time threshold value (52); and reducing an activation power of the reciprocating pump (30) if the flight time (TZ) is less than the flight time threshold value (52).

2. The method according to claim 1, characterized in that a stop determination (48) determines the stop time (TA) of the reciprocating piston of the reciprocating pump (30) on the basis of an assessment of the temporal characteristic of the current (i) flowing through the reciprocating pump (30).

3. The method according to claim 1, characterized in that the average activation power of the reciprocating pump (30) is controlled by a pulse-width-modulated signal.

4. The method according to claim 1, characterized in that, after the average activation power of the reciprocating pump (30) is reduced, the flight time (TZ) of the piston of the reciprocating pump (30) is furthermore determined, in that a comparison of the flight time (TZ) with the flight time threshold value (52) is furthermore undertaken, and in that, whenever the flight time (TZ) exceeds the flight time threshold value (52), the reduction in the average activation power is ended.

5. A device for operating a reagent metering system (10), wherein a specially designed control device (26) is provided for carrying out the method according to claim 1.

6. A control device program which executes all of the steps of a method according to claim 1 when it runs on a control device (26).

7. A non-transitory machine-readable storage medium having program code for a control device program, the control device program carrying out the method according to claim 1 when the control device program is executed on a control device (26).

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0025] An exemplary embodiment of the invention is illustrated in the drawing and explained in more detail in the description below.

[0026] FIG. 1 shows a technical environment in which a method according to the invention runs, and

[0027] FIGS. 2 and 3 show signal variations as a function of the time.

DETAILED DESCRIPTION

[0028] FIG. 1 shows a reagent metering system 10 which meters a reagent 14 stored in a tank 12 into an exhaust duct 16 of an internal combustion engine 18 upstream of an SCR catalytic converter 20. The reagent 14 is preferably a urea-water solution which is a precursor of the reagent ammonia required in the SCR catalytic converter 20. Only the term reagent 14 is used below.

[0029] The reagent 14 is brought by a pump 22 to an operating pressure which lies, for example, within a range of 3-9 bar. The metering rate of the reagent 14 is defined by a metering valve 24 which is activated with a metering signal 28 by a control device 26.

[0030] Depending on the configuration of the reagent 14, the reagent 14 may freeze below a certain temperature. If a urea-water solution is provided as the reagent 14, freezing below 11 C. has to be anticipated. In order to avoid damage in the reagent metering system 10, back-suction of the reagent 14 is therefore provided, at least whenever a dropping of the ambient temperature below the freezing temperature of the reagent 14 should be anticipated.

[0031] The reagent metering system 10 is intended to be emptied in the overrunning of the control device 26, in which the control device 26 is still supplied with current for carrying out further tasks after the internal combustion engine 18 is shut down and after the metering operation is ended. For the back-suction of the reagent, a reciprocating pump 30 is provided. In the exemplary embodiment shown, the reciprocating pump 30 is provided as a separate pump which is present in addition to the pump 22. Alternatively, a single reciprocating pump can be provided, wherein, in this case, valves have to be provided so that a switch can be made between metering operation and back-suction operation. In the exemplary embodiment shown in FIG. 1, the pump 22 is activated by a pump signal 32 which the control device 26 provides.

[0032] If the internal combustion engine 18 is intended to be switched off, a switching-off signal 40 which is made available to an activation means 42 occurs within the context of overrunning of the control device 26, within which the control device 26 is still supplied with energy. The activation means 42 provides an activation signal 44 which is made available to the reciprocating pump 30. The activation signal 44 is preferably a pulse-width-modulated signal, and therefore simple power control of the reciprocating pump 30 is possible.

[0033] After the occurrence of the switching-off signal 40, the activation signal 44 is provided at a starting time TS, shown in FIGS. 2 and 3, and the back-suction operation begins. The reciprocating piston (not shown specifically) of the reciprocating pump 30, which reciprocating piston is connected to an armature (not shown specifically) of the reciprocating pump 30, executes a stroke movement because of the energizing of the solenoid of the reciprocating pump with the current i. On account of the inductance of the solenoid, which depends on the solenoid itself, but also on the entire magnetic circuit consisting of armature and piston of the reciprocating pump 30, the current i cannot increase abruptly, but rather at least approximately has a characteristic as shown in FIGS. 2 and 3.

[0034] If the reciprocating pump 30 is filled with the reagent 14 during the back-suction, a normal operating noise occurs which is caused in particular by the reciprocating piston of the reciprocating pump 30 striking against an end stop. However, this noise greatly increases if air bubbles or no reagent 14 at all are or is present in the reciprocating pump 30. In this case, the counterforce due to the reagent 14 is missing, and therefore, when the power supply to the reciprocating pump 30 is unchanged, the stroke movement becomes more rapid and the striking noise becomes correspondingly louder. In particular, the increase in the noise is unpleasant for a user of the reagent metering system 10 since, at the time of the back-suction of the reagent 14, the internal combustion engine 18 is already switched off, and therefore the general noise level is reduced and the annoying noise caused by the reciprocating pump 30 is more noticeable.

[0035] According to the invention, it is therefore provided to reduce the average power made available to the reciprocating pump 30 if the load is reduced because of the formation of bubbles in the reciprocating pump 30. The flight time TZ of the reciprocating piston of the reciprocating pump 30 is used as a measure for the reduction in the mechanical load of the reciprocating pump 30. The determination of the flight time TZ of the reciprocating piston of the reciprocating pump 30 is provided, beginning at a starting time TS until the end stop is reached at the stop time TA. The flight time TZ is subsequently compared with a flight time threshold value.

[0036] If the flight time TZ is less than the flight time threshold value, the activation power of the reciprocating pump 30 is reduced. The reduced power ensures that the reciprocating piston moves more slowly, and therefore the striking of the reciprocating piston of the reciprocating pump 30 against the end stop also takes place with less noise.

[0037] According to a refinement, the flight time TZ of the armature or of the reciprocating piston of the reciprocating pump 30 is determined on the basis of an assessment of the current i during the back-suction, which current is detected by a current sensor 46. For this purpose, a stop determination 48 assesses the current i by forming, for example, the first and/or second time derivative i, i of the current i. As soon as the armature or the reciprocating piston of the reciprocating pump 30 reaches the end stop, a great change in the inductance of the inductive circuit described further above occurs in a short time. The great increase in the inductance leads to a characteristic dip in the current i at the stop time TA. The change in the current i can lead to the passage through zero of the first derivative i of the current i. The change in the current i can also take place in such a manner that a turning point in the current characteristic occurs, which turning point can be identified on the basis of an assessment of the second derivative i of the temporal current characteristic.

[0038] As soon as the stop determination 48 has identified the reaching of the end stop at the stop time TA the flight time TZ is determined from the time difference between the starting time TS and the stop time TA and made available to a comparator 50. The comparator 50 compares the flight time TZ with the flight time threshold value 52. If the flight time TZ determined is less than the flight time threshold value 52, the comparator 50 provides a switching signal 54 which triggers the activation means 42 to change the activation signal 44 of the reciprocating pump 30 in such a manner that a lower average power is made available to the reciprocating pump 30.

[0039] If the refinement, already described, of the activation signal 44 is provided as a pulse-width-modulated activation signal, the average power can be reduced in a simple manner by changing a characteristic variable of the pulse-width-modulated signal, for example a reduction in the pulse duration.

[0040] The reduction in the average power made available to the reciprocating pump 30 causes the movement of the armature or the reciprocating piston of the reciprocating pump 30 to slow down. The reduction in the power has to be pursued in such a manner that the reciprocating piston of the reciprocating pump 30 continues to reach the end stop, wherein, however, the generation of noise is reduced. The reduced power is preferably determined experimentally.

[0041] As soon as the reciprocating pump 30 is filled again with the reagent 14, a return can be made to the normal back-suction operation with full power. The return to the normal back-suction operation with the normal power of the reciprocating pump 30 can be initiated by the simple measure that the stop identification 48 furthermore determines the flight time TZ and makes the latter available to the comparator 50. The comparator 50 furthermore compares the current flight time TZ with the flight time threshold value 52. The flight time TZ is slowed down on account of the increase in the load of the reciprocating pump 30 by the reagent 14 which is present. If it is now established that the flight time TZ is increased and exceeds the flight time threshold value 52, the comparator 50 withdraws the switching signal 54, whereupon the activation means 42 again provides the normal activation signal 44 without reducing the average power.