WO2024056227A1 - Method for operating a gas injector - Google Patents
Method for operating a gas injector Download PDFInfo
- Publication number
- WO2024056227A1 WO2024056227A1 PCT/EP2023/067840 EP2023067840W WO2024056227A1 WO 2024056227 A1 WO2024056227 A1 WO 2024056227A1 EP 2023067840 W EP2023067840 W EP 2023067840W WO 2024056227 A1 WO2024056227 A1 WO 2024056227A1
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- WO
- WIPO (PCT)
- Prior art keywords
- gas injector
- phase
- combustion engine
- internal combustion
- magnetic actuator
- Prior art date
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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
- F02D41/20—Output circuits, e.g. for controlling currents in command coils
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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
- F02D19/00—Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
- F02D19/02—Controlling engines characterised by their use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures peculiar to engines working with gaseous fuels
- F02D19/021—Control of components of the fuel supply system
- F02D19/023—Control of components of the fuel supply system to adjust the fuel mass or volume flow
- F02D19/024—Control of components of the fuel supply system to adjust the fuel mass or volume flow by controlling fuel injectors
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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
- F02D41/04—Introducing corrections for particular operating conditions
- F02D41/042—Introducing corrections for particular operating conditions for stopping the engine
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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
- F02D41/20—Output circuits, e.g. for controlling currents in command coils
- F02D2041/2003—Output circuits, e.g. for controlling currents in command coils using means for creating a boost voltage, i.e. generation or use of a voltage higher than the battery voltage, e.g. to speed up injector opening
- F02D2041/2006—Output circuits, e.g. for controlling currents in command coils using means for creating a boost voltage, i.e. generation or use of a voltage higher than the battery voltage, e.g. to speed up injector opening by using a boost capacitor
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/30—Use of alternative fuels, e.g. biofuels
Definitions
- the present invention relates to a method for operating a gas injector of an internal combustion engine when the gas injector is venting before the internal combustion engine is switched off.
- Gas injectors are known from the prior art in different designs.
- One problem with gas injectors that inject a gaseous fuel is that when the internal combustion engine is switched off, despite the gas injector being closed, a leak of the gaseous fuel that is still under high pressure can occur in the gas injector. However, this must be avoided for environmental reasons. Therefore, before the internal combustion engine is finally switched off, the gas injector is operated in a drain function (so-called “purge function”), in which gas that is still under high pressure is released from the gas injector into a combustion chamber of the internal combustion engine and there the internal combustion engine is finally switched off is burned.
- a connection of the gas injector to a gas storage is already interrupted by additional closing elements.
- the gas injector Since the pressure in the gas injector drops during this release function, the gas injector must be designed in such a way that it opens even at low system pressure.
- a magnetic circuit of a magnetic actuator of the gas injector has been dimensioned in such a way that a sufficient magnetic force is present even at a minimum system pressure that can be achieved.
- the method according to the invention for operating a gas injector of an internal combustion engine with a drain function before switching off the internal combustion engine with the features of claim 1 has the advantage that a magnetic actuator for the gas injector can be designed to be significantly smaller. This saves installation space on the gas injector, which is particularly advantageous for gas injectors that inject directly, since there is little installation space available for the gas injector near a combustion chamber of the internal combustion engine. Furthermore, the gas injector can be manufactured more cost-effectively using a smaller magnetic actuator.
- the magnetic actuator is activated in a boost phase takes place in such a way that the current for the magnetic actuator is continuously increased until the end of the boost phase.
- the current for the magnetic actuator is kept constant in a tightening phase, which follows the boost phase. The current is kept constant at a level that corresponds to a maximum current in the boost phase.
- a current level can be increased during the release function in order to compensate for the continuously falling gas pressure during the release function.
- the increased power requirement in the pick-up phase is preferably provided by a DC/DC converter and/or a boost capacitor.
- control in the pick-up current phase is preferably carried out with boost voltage.
- the boost capacitor was charged during normal operation of the internal combustion engine and can therefore provide the increased power requirement for the drain function. More preferably, a length of the tightening phase is reduced in comparison with normal operation of the gas injector, ie, normal injection operation.
- the background is the longer boost current phase due to a higher boost current level.
- a switching point from starting current to holding current is preferably stored in the control unit as a constant value. A longer boost current phase therefore results in a shorter pick-up current phase.
- the current level in the boost phase is increased in comparison to the normal operation of the gas injector.
- a higher current level is achieved than in comparison with normal operation of the gas injector, whereby the current level in the pick-up phase can also be easily maintained at a higher level than in comparison with normal operation.
- the current level in the boost phase is kept the same compared to normal operation of the gas injector. Then the higher current level in the pick-up phase is provided, for example, by using the boost capacitor.
- a length of the boost phase in the drain function is extended in comparison to the normal operation of the gas injector. This means more time is available to achieve a higher absolute current level in the boost phase compared to normal operation.
- a holding phase of the gas injector in which the gas injector is kept open, is preferably extended in comparison to the normal operation of the gas injector.
- the present invention further relates to a control device which is set up to carry out the steps of the method according to the invention.
- the control device preferably carries out the method until a gas pressure in the gas injector corresponds to the ambient pressure.
- the gas injector can be kept in the closed position without leakage when the internal combustion engine is switched off.
- the invention relates to a computer program with a program code which carries out steps of the method according to the invention when the computer program runs on a computer or a corresponding computing unit, for example on a control device according to the invention.
- a computer program product is proposed with a computer program according to the invention, which is stored on a machine-readable data carrier or storage medium.
- Figure 1 is a schematic diagram showing the voltage and the
- Figure 2 is a schematic diagram showing the voltage and the
- Figure 3 shows a longitudinal section through a gas injector, which is used for
- Figure 3 shows an example of a gas injector 1 with a magnetic actuator.
- the magnetic actuator comprises a magnetic coil 3 for acting on an axially movable armature 2.
- the armature 2 can be brought into contact with a closing element 4, in particular a valve needle, in order to release an injection cross section at a sealing seat 5.
- Reference number 8 designates a restoring element of the gas injector.
- the closing element 4 is held in the closed position shown in Figure 3 by means of a valve spring 7.
- the current supply to the magnetic coil 3 is stopped, so that the restoring element 8 returns the armature 2 to the starting position shown in FIG.
- the valve spring 7 also returns the closing element 4 to the closed position shown in FIG.
- the gas injector 1 is an injector that opens to the outside.
- Hydrogen or methane or the like is preferably used as the gaseous fuel.
- the diagram in Figure 1 shows normal operation of the gas injector 1 for injecting gaseous fuel, in particular hydrogen, directly into a combustion chamber of an internal combustion engine.
- the gas injector and the magnetic actuator basically go through four phases, namely a boost phase A, a tightening phase B, a holding phase C and a closing phase D.
- K1 shows the current curve of the current for the magnetic actuator over time.
- K2 shows the average voltage of the magnetic actuator over time.
- K3 shows the force curve of the anchor over time and K4 shows the stroke of the anchor over time t.
- a closing force K5 is shown in Figures 1 and 2, which represents the subtraction of the pressure force of the system pressure in the gas injector from the spring force of the valve spring. This is increased to F1 in normal operation in FIG. 1 and to F2 by F' in the drain operation shown in FIG.
- a battery voltage K6 is shown in Figures 1 and 2, which is constant both in normal operation and in discharge operation.
- the boost phase A in normal operation of the internal combustion engine ends after time t1
- the tightening phase B ends after time t2 has elapsed
- the hold phase C ends after time t3 has elapsed
- the closing phase D ends after time t4 has elapsed.
- the current curve K1 is such that at the end of the boost phase, the current level drops and is then maintained at a constant level 11 in the pick-up phase.
- the opening process begins, i.e. the closing element is lifted off the sealing seat at the transition between the boost phase A and the tightening phase B.
- the maximum opening stroke is achieved in the tightening phase B (stroke curve K4).
- the current curve K1 is such that a continuous increase in the current up to point IT is achieved in the boost phase A '.
- This current value I is maintained in the let-off function throughout the entire tightening phase B'.
- the current level in the boost phase A 'or in the tightening phase B' in the let-down function is significantly higher than in the boost phase A or in the tightening phase B of Figure 1 in normal operation.
- the absolute value IT is also greater than the value 11 in normal operation at the end of the boost phase.
- This can be achieved by dimensioning a DC/DC converter and/or a boost capacitor.
- the DC/DC converter and the boost capacitor are like this dimensioned so that all relevant operating points of the gas injector can be served in normal operation ( Figure 1). If the internal combustion engine is switched off and the purge function is then required, power reserves are available which are sufficient in the purge function for the few necessary injections, usually at a lower speed than in normal operation.
- the energy reserves from the DC/DC converter and/or the boost capacitor are used for the control shown in FIG. 2 to increase the current level (curve K1 in FIG. 2 in the pick-up phase B').
- the tightening phase B 'in draining operation (t2'-tT) is shorter than the tightening phase B in normal operation (t2-t1).
- the boost phase A' in drain operation is larger than in normal operation due to the higher boost current level, which is shown in Figure 2 by the time tT compared to the time t1 in normal operation.
- the higher current level IT in the draining operation also provides an increased opening force of the magnetic actuator, which can be seen by comparing the force curves K3 between FIG. 1 and FIG. 2. This allows the missing force component of the gas pressure to open the gas injector due to the falling gas pressure in the gas injector to be compensated for.
- all four curves K1, K2, K3 and K4 are the same again.
- control variants are also conceivable in which the current curve in the boost phase A' in the let-off mode is the same as in normal operation and then the compensation is only realized by the magnetic force in the pick-up phase B' with increased current.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Abstract
Description
Beschreibung Description
Titel title
Verfahren zum Betreiben eines Gasinjektors Method for operating a gas injector
Stand der Technik State of the art
Die vorliegende Erfindung betrifft ein Verfahren zum Betreiben eines Gasinjektors einer Brennkraftmaschine bei einer Ablassfunktion des Gasinjektors vor einem Abstellen der Brennkraftmaschine. The present invention relates to a method for operating a gas injector of an internal combustion engine when the gas injector is venting before the internal combustion engine is switched off.
Gasinjektoren sind aus dem Stand der Technik in unterschiedlichen Ausgestaltungen bekannt. Ein Problemkreis bei Gasinjektoren, welche einen gasförmigen Brennstoff einblasen, liegt darin, dass bei einer abgestellten Brennkraftmaschine trotz geschlossenem Gasinjektor eine Leckage des sich noch unter hohem Druck befindlichen gasförmigen Brennstoffs im Gasinjektor auftreten kann. Dies muss jedoch aus Umweltschutzgründen vermieden werden. Daher wird der Gasinjektor vor einem endgültigen Abstellen der Brennkraftmaschine in einer Ablassfunktion betrieben (sog. „Purge-Funktion“), bei der sich noch unter hohem Druck befindliches Gas aus dem Gasinjektor in einen Brennraum der Brennkraftmaschine abgelassen wird und dort dem endgültigen Abstellen der Brennkraftmaschine verbrannt wird. Eine Verbindung des Gasinjektors zu einem Gasspeicher ist hierbei durch zusätzliche Schließelemente schon unterbrochen. Da während dieser Ablassfunktion der Druck im Gasinjektor sinkt, muss der Gasinjektor derart ausgelegt werden, dass dieser auch bei einem geringen Systemdruck öffnet. Hier wird bisher ein Magnetkreis eines Magnetaktors des Gasinjektors derart dimensioniert, dass eine ausreichende Magnetkraft auch bei einem minimal zu erreichenden Systemdruck vorhanden ist. Dies führt jedoch zu großen Magnetaktoren, welche einen großen Bauraum einnehmen, welcher größer ist als ein für den eigentlichen Injektorbetrieb notwendiger Bauraum. Gas injectors are known from the prior art in different designs. One problem with gas injectors that inject a gaseous fuel is that when the internal combustion engine is switched off, despite the gas injector being closed, a leak of the gaseous fuel that is still under high pressure can occur in the gas injector. However, this must be avoided for environmental reasons. Therefore, before the internal combustion engine is finally switched off, the gas injector is operated in a drain function (so-called “purge function”), in which gas that is still under high pressure is released from the gas injector into a combustion chamber of the internal combustion engine and there the internal combustion engine is finally switched off is burned. A connection of the gas injector to a gas storage is already interrupted by additional closing elements. Since the pressure in the gas injector drops during this release function, the gas injector must be designed in such a way that it opens even at low system pressure. Here, a magnetic circuit of a magnetic actuator of the gas injector has been dimensioned in such a way that a sufficient magnetic force is present even at a minimum system pressure that can be achieved. However, this leads to large magnetic actuators, which take up a large installation space, which is larger than the installation space required for the actual injector operation.
Offenbarung der Erfindung Das erfindungsgemäße Verfahren zum Betreiben eines Gasinjektors einer Brennkraftmaschine bei einer Ablassfunktion vor einem Abstellen der Brennkraftmaschine mit den Merkmalen des Anspruchs 1 weist demgegenüber den Vorteil auf, dass ein Magnetaktor für den Gasinjektor deutlich kleiner ausgelegt werden kann. Hierdurch wird ein Bauraum am Gasinjektor eingespart, was insbesondere bei direkt einblasenden Gasinjektoren sehr vorteilhaft ist, da nahe einem Brennraum der Brennkraftmaschine wenig Bauraum für den Gasinjektor zur Verfügung steht. Ferner kann der Gasinjektor durch einen verkleinerten Magnetaktor kostengünstiger hergestellt werden. Dies wird erfindungsgemäß dadurch erreicht, dass bei der Ablassfunktion, in der gasförmiger Brennstoff aus dem Gasinjektor vor einem endgültigen Abstellen der Brennkraftmaschine in den Brennraum abgelassen wird, um noch in der Brennkraftmaschine verbrannt zu werden, in einem ersten Schritt ein Ansteuern des Magnetaktors in einer Boostphase derart erfolgt, dass bis zum Ende der Boostphase eine kontinuierliche Erhöhung des Stroms für den Magnetaktor ausgeführt wird. In einem weiteren Schritt erfolgt ein Konstanthalten des Stroms für den Magnetaktor in einer Anzugsphase, welche auf die Boostphase folgt. Das Konstanthalten des Stroms wird dabei auf einem Niveau durchgeführt, welches einer maximalen Stromstärke in der Boostphase entspricht. Dadurch kann bei der Ablassfunktion des Gasinjektors trotz des reduzierten Gasdrucks im Gasinjektor eine Öffnung und ein Offenhalten des Gasinjektors ermöglicht werden, da eine erhöhte Aktorkraft den reduzierten Gasdruck während der Ablassfunktion des Gasinjektors ausgleicht. Disclosure of the invention The method according to the invention for operating a gas injector of an internal combustion engine with a drain function before switching off the internal combustion engine with the features of claim 1 has the advantage that a magnetic actuator for the gas injector can be designed to be significantly smaller. This saves installation space on the gas injector, which is particularly advantageous for gas injectors that inject directly, since there is little installation space available for the gas injector near a combustion chamber of the internal combustion engine. Furthermore, the gas injector can be manufactured more cost-effectively using a smaller magnetic actuator. This is achieved according to the invention in that during the drain function, in which gaseous fuel is drained from the gas injector into the combustion chamber before the internal combustion engine is finally switched off in order to be burned in the internal combustion engine, in a first step the magnetic actuator is activated in a boost phase takes place in such a way that the current for the magnetic actuator is continuously increased until the end of the boost phase. In a further step, the current for the magnetic actuator is kept constant in a tightening phase, which follows the boost phase. The current is kept constant at a level that corresponds to a maximum current in the boost phase. This makes it possible to open and keep the gas injector open during the venting function of the gas injector despite the reduced gas pressure in the gas injector, since an increased actuator force compensates for the reduced gas pressure during the venting function of the gas injector.
Somit kann in der Anzugsphase ein Stromniveau bei der Ablassfunktion angehoben werden, um den bei der Ablassfunktion kontinuierlich sinkenden Gasdruck auszugleichen. Thus, in the tightening phase, a current level can be increased during the release function in order to compensate for the continuously falling gas pressure during the release function.
Die Unteransprüche zeigen bevorzugte Weiterbildungen der Erfindung. The subclaims show preferred developments of the invention.
Vorzugsweise wird der erhöhte Strombedarf in der Anzugsphase durch einen DC/DC-Wandler und/oder einen Boostkondensator bereitgestellt. Hierbei erfolgt eine Ansteuerung in der Anzugsstromphase vorzugsweise mit Boostspannung. Der Boostkondensator wurde im normalen Betrieb der Brennkraftmaschine aufgeladen und kann somit den erhöhten Strombedarf bei der Ablassfunktion bereitstellen. Weiter bevorzugt wird eine Länge der Anzugsphase im Vergleich mit einem Normalbetrieb des Gasinjektors, d.h., einem normalen Einblasbetrieb, reduziert. Hintergrund ist die längere Booststromphase bedingt durch ein höheres Booststromniveau. Vorzugsweise ist ein Umschaltzeitpunkt von Anzugsstrom auf Haltestrom im Steuergerät als konstanter Wert hinterlegt. Somit hat eine längere Booststromphase eine kürzere Anzugsstromphase zur Folge. The increased power requirement in the pick-up phase is preferably provided by a DC/DC converter and/or a boost capacitor. Here, control in the pick-up current phase is preferably carried out with boost voltage. The boost capacitor was charged during normal operation of the internal combustion engine and can therefore provide the increased power requirement for the drain function. More preferably, a length of the tightening phase is reduced in comparison with normal operation of the gas injector, ie, normal injection operation. The background is the longer boost current phase due to a higher boost current level. A switching point from starting current to holding current is preferably stored in the control unit as a constant value. A longer boost current phase therefore results in a shorter pick-up current phase.
Weiter bevorzugt wird das Stromniveau in der Boostphase im Vergleich mit dem Normalbetrieb des Gasinjektors erhöht. Somit wird am Ende der Boostphase ein höheres Stromniveau als im Vergleich mit dem Normalbetrieb des Gasinjektors erreicht, wodurch auf einfache Weise das Stromniveau in der Anzugsphase ebenfalls auf einem höheren Niveau als im Vergleich mit dem Normalbetrieb gehalten werden kann. More preferably, the current level in the boost phase is increased in comparison to the normal operation of the gas injector. Thus, at the end of the boost phase, a higher current level is achieved than in comparison with normal operation of the gas injector, whereby the current level in the pick-up phase can also be easily maintained at a higher level than in comparison with normal operation.
Alternativ wird das Stromniveau in der Boostphase im Vergleich mit dem Normalbetrieb des Gasinjektors gleich gehalten. Dann wird das in der Anzugsphase höhere Stromniveau beispielsweise durch Nutzung des Boostkondensators bereitgestellt. Alternatively, the current level in the boost phase is kept the same compared to normal operation of the gas injector. Then the higher current level in the pick-up phase is provided, for example, by using the boost capacitor.
Weiter bevorzugt ist eine Länge der Boostphase bei der Ablassfunktion im Vergleich mit dem Normalbetrieb des Gasinjektors verlängert. Hierdurch steht mehr Zeit zur Verfügung, um in der Boostphase einen im Vergleich mit dem Normalbetrieb höheres absolutes Stromniveau zu erreichen. Further preferably, a length of the boost phase in the drain function is extended in comparison to the normal operation of the gas injector. This means more time is available to achieve a higher absolute current level in the boost phase compared to normal operation.
Um möglichst viel gasförmigen Brennstoff während der Ablassfunktion des Gasinjektors in den Brennraum einblasen zu können, wird vorzugsweise eine Haltephase des Gasinjektors, in welcher der Gasinjektor offengehalten wird, im Vergleich mit dem Normalbetrieb des Gasinjektors verlängert. In order to be able to blow as much gaseous fuel as possible into the combustion chamber during the exhaust function of the gas injector, a holding phase of the gas injector, in which the gas injector is kept open, is preferably extended in comparison to the normal operation of the gas injector.
Ferner betrifft die vorliegende Erfindung ein Steuergerät, welches eingerichtet ist, die Schritte des erfindungsgemäßen Verfahrens auszuführen. Vorzugsweise führt das Steuergerät dabei das Verfahren derart aus, bis ein Gasdruck im Gasinjektor dem Umgebungsdruck entspricht. Dadurch kann bei abgestellter Brennkraftmaschine der Gasinjektor ohne Leckage in der geschlossenen Stellung gehalten werden. Weiterhin betrifft die Erfindung ein Computerprogramm mit einem Programmcode, welcher Schritte des erfindungsgemäßen Verfahrens ausführt, wenn das Computerprogramm auf einem Computer oder einer entsprechenden Recheneinheit, beispielsweise auf einem erfindungsgemäßen Steuergerät, abläuft. The present invention further relates to a control device which is set up to carry out the steps of the method according to the invention. The control device preferably carries out the method until a gas pressure in the gas injector corresponds to the ambient pressure. As a result, the gas injector can be kept in the closed position without leakage when the internal combustion engine is switched off. Furthermore, the invention relates to a computer program with a program code which carries out steps of the method according to the invention when the computer program runs on a computer or a corresponding computing unit, for example on a control device according to the invention.
Ferner wird ein Computerprogrammprodukt mit einem erfindungsgemäßen Computerprogramm vorgeschlagen, das auf einem maschinenlesbaren Datenträger oder Speichermedium gespeichert ist. Furthermore, a computer program product is proposed with a computer program according to the invention, which is stored on a machine-readable data carrier or storage medium.
Kurze Beschreibung der Zeichnung Short description of the drawing
Nachfolgend wird die vorliegende Erfindung unter Bezugnahme auf die begleitende Zeichnung im Detail beschrieben. In der Zeichnung ist: The present invention will be described in detail below with reference to the accompanying drawings. In the drawing is:
Figur 1 ein schematisches Diagramm, welches die Spannung und denFigure 1 is a schematic diagram showing the voltage and the
Strom eines erfindungsgemäßen Magnetaktors und einen Kraftverlauf und einen Hub eines Ankers des Magnetaktors über der Zeit bei einem Normalbetrieb einer Brennkraftmaschine darstellt, Current of a magnetic actuator according to the invention and a force curve and a stroke of an armature of the magnetic actuator over time during normal operation of an internal combustion engine,
Figur 2 ein schematisches Diagramm, welches die Spannung und denFigure 2 is a schematic diagram showing the voltage and the
Strom eines erfindungsgemäßen Magnetaktors und einen Kraftverlauf und einen Hub eines Ankers des Magnetaktors über der Zeit bei einer Ablassfunktion einer Brennkraftmaschine darstellt, und Current of a magnetic actuator according to the invention and a force curve and a stroke of an armature of the magnetic actuator over time during a drain function of an internal combustion engine, and
Figur 3 einen Längsschnitt durch einen Gasinjektor, welcher zurFigure 3 shows a longitudinal section through a gas injector, which is used for
Durchführung des erfindungsgemäßen Verfahrens eingerichtet ist. Implementation of the method according to the invention is set up.
Bevorzugte Ausführungsform der Erfindung Preferred embodiment of the invention
Nachfolgend wird unter Bezugnahme auf die Figuren 1 bis 3 ein bevorzugtes Ausführungsbeispiel der Erfindung im Detail beschrieben. Figur 3 zeigt beispielhaft einen Gasinjektor 1 mit einem Magnetaktor. Der Magnetaktor umfasst eine Magnetspule 3 zur Einwirkung auf einen axial beweglichen Anker 2. Der Anker 2 ist mit einem Schließelement 4, insbesondere einer Ventilnadel, in Kontakt bringbar, um an einem Dichtsitz 5 einen Einblasquerschnitt freizugeben. Das Bezugszeichen 8 bezeichnet ein Rückstellelement des Gasinjektors. Das Schließelement 4 ist mittels einer Ventilfeder 7 in der in Figur 3 gezeigten, geschlossenen Position, gehalten. A preferred exemplary embodiment of the invention is described in detail below with reference to FIGS. 1 to 3. Figure 3 shows an example of a gas injector 1 with a magnetic actuator. The magnetic actuator comprises a magnetic coil 3 for acting on an axially movable armature 2. The armature 2 can be brought into contact with a closing element 4, in particular a valve needle, in order to release an injection cross section at a sealing seat 5. Reference number 8 designates a restoring element of the gas injector. The closing element 4 is held in the closed position shown in Figure 3 by means of a valve spring 7.
Wenn die Magnetspule 3 bestromt wird, bildet sich ein Magnetfeld aus, dessen Magnetkraft den Anker 2 in Richtung des Schließelements 4 bewegt (Pfeil 11). Dabei gelangt ein mit dem Anker 2 verbundener Ankerbolzen 9 zur Anlage mit dem Schließelement 4, so dass das Schließelement 4 entgegen der Federkraft der Ventilfeder 7 am Dichtsitz 5 geöffnet wird. Der Anker 2 wird dabei bis zu einem Hubanschlag 6 für den Anker bewegt, was den vollständigen Öffnungszustand des Gasinjektors darstellt. When the magnetic coil 3 is energized, a magnetic field is formed, the magnetic force of which moves the armature 2 in the direction of the closing element 4 (arrow 11). An anchor bolt 9 connected to the anchor 2 comes into contact with the closing element 4, so that the closing element 4 is opened against the spring force of the valve spring 7 on the sealing seat 5. The armature 2 is moved up to a stroke stop 6 for the armature, which represents the complete opening state of the gas injector.
Zum Schließen des Gasinjektors 1 wird die Bestromung der Magnetspule 3 beendet, so dass das Rückstellelement 8 den Anker 2 wieder in die in Figur 3 gezeigte Ausgangsposition zurückstellt. Gleichzeitig stellt auch die Ventilfeder 7 das Schließelement 4 in die in Figur 1 gezeigte, geschlossene Position zurück. To close the gas injector 1, the current supply to the magnetic coil 3 is stopped, so that the restoring element 8 returns the armature 2 to the starting position shown in FIG. At the same time, the valve spring 7 also returns the closing element 4 to the closed position shown in FIG.
Der Gasinjektor 1 ist ein nach außen öffnender Injektor. The gas injector 1 is an injector that opens to the outside.
Als gasförmiger Brennstoff wird vorzugsweise Wasserstoff oder Methan oder dgl. verwendet. Hydrogen or methane or the like is preferably used as the gaseous fuel.
Das Diagramm in Figur 1 zeigt einen Normalbetrieb des Gasinjektors 1 zum Einblasen von gasförmigem Brennstoff, insbesondere Wasserstoff, direkt in einen Brennraum einer Brennkraftmaschine. Hierbei durchlaufen der Gasinjektor und der Magnetaktor grundsätzlich vier Phasen, nämlich eine Boostphase A, eine Anzugsphase B, eine Haltephase C und eine Schließphase D. The diagram in Figure 1 shows normal operation of the gas injector 1 for injecting gaseous fuel, in particular hydrogen, directly into a combustion chamber of an internal combustion engine. The gas injector and the magnetic actuator basically go through four phases, namely a boost phase A, a tightening phase B, a holding phase C and a closing phase D.
In Figur 1 und 2 sind hierbei vier Kurven über der Zeit t in den vier Phasen dargestellt. K1 zeigt dabei den Stromverlauf des Stroms für den Magnetaktor über der Zeit. K2 zeigt die mittlere Spannung des Magnetaktors über der Zeit. K3 zeigt den Kraftverlauf des Ankers über der Zeit und K4 zeigt den Hub des Ankers über der Zeit t. Weiterhin ist in den Figuren 1 und 2 eine schließende Kraft K5 dargestellt, welche die Subtraktion der Druckkraft des Systemdrucks im Gasinjektor von der Federkraft der Ventilfeder darstellt. Diese ist im Normalbetrieb in Figur 1 bei F1 und um F‘ bei dem in Figur 2 gezeigten Ablassbetrieb auf F2 erhöht, da im Ablassbetrieb der unterstützende Öffnungsdruck durch das Druckniveau des gasförmigen, einzublasenden Brennstoffs fehlt. In Figures 1 and 2, four curves are shown over time t in the four phases. K1 shows the current curve of the current for the magnetic actuator over time. K2 shows the average voltage of the magnetic actuator over time. K3 shows the force curve of the anchor over time and K4 shows the stroke of the anchor over time t. Furthermore, a closing force K5 is shown in Figures 1 and 2, which represents the subtraction of the pressure force of the system pressure in the gas injector from the spring force of the valve spring. This is increased to F1 in normal operation in FIG. 1 and to F2 by F' in the drain operation shown in FIG.
Ferner ist in den Figuren 1 und 2 noch eine Batteriespannung K6 eingezeichnet, welche sowohl im Normalbetrieb als auch im Ablassbetrieb konstant ist. Furthermore, a battery voltage K6 is shown in Figures 1 and 2, which is constant both in normal operation and in discharge operation.
Wie aus Figur 1 ersichtlich ist, endet die Boostphase A im Normalbetrieb der Brennkraftmaschine nach der Zeit t1 , die Anzugsphase B endet nach Zeitablauf der Zeit t2, die Haltephase C endet nach Zeitablauf der Zeit t3 und die Schließphase D endet nach Zeitablauf der Zeit t4. As can be seen from Figure 1, the boost phase A in normal operation of the internal combustion engine ends after time t1, the tightening phase B ends after time t2 has elapsed, the hold phase C ends after time t3 has elapsed and the closing phase D ends after time t4 has elapsed.
Weiterhin ist im Normalbetrieb in Figur 1 der Stromverlauf K1 derart, dass am Ende der Boostphase das Stromniveau absinkt und in der Anzugsphase dann auf einem konstanten Niveau 11 gehalten wird. Wie weiter aus Figur 1 ersichtlich ist, beginnt der Öffnungsvorgang, d.h., ein Abheben des Schließelements vom Dichtsitz am Übergang zwischen der Boostphase A und der Anzugsphase B. Der maximale Öffnungshub wird dabei in der Anzugsphase B erreicht (Hubkurve K4). Furthermore, in normal operation in Figure 1, the current curve K1 is such that at the end of the boost phase, the current level drops and is then maintained at a constant level 11 in the pick-up phase. As can be seen from Figure 1, the opening process begins, i.e. the closing element is lifted off the sealing seat at the transition between the boost phase A and the tightening phase B. The maximum opening stroke is achieved in the tightening phase B (stroke curve K4).
Bei der in Figur 2 dargestellten Ablassfunktion des Gasinjektors vor einem endgültigen Abstellen der Brennkraftmaschine ist der Stromverlauf K1 derart, dass in der Boostphase A‘ eine kontinuierliche Erhöhung des Stroms bis zum Punkt IT erreicht wird. Dieser Stromwert I wird in der kompletten Anzugsphase B‘ in der Ablassfunktion beibehalten. Wie ein Vergleich zwischen Figur 1 und Figur 2 zeigt, ist somit in der Boostphase A‘ bzw. in der Anzugsphase B‘ in der Ablassfunktion das Stromniveau deutlich höher als in der Boostphase A bzw. in der Anzugsphase B von Figur 1 im Normalbetrieb. In the exhaust function of the gas injector shown in Figure 2 before the internal combustion engine is finally switched off, the current curve K1 is such that a continuous increase in the current up to point IT is achieved in the boost phase A '. This current value I is maintained in the let-off function throughout the entire tightening phase B'. As a comparison between Figure 1 and Figure 2 shows, the current level in the boost phase A 'or in the tightening phase B' in the let-down function is significantly higher than in the boost phase A or in the tightening phase B of Figure 1 in normal operation.
Insbesondere findet keine Absenkung des Stromniveaus in der Anzugsphase B‘ in der Ablassfunktion des Gasinjektors statt. Auch ist der absolute Wert IT größer als der Wert 11 im Normalbetrieb am Ende der Boostphase. Dies kann durch Dimension eines DC/DC-Wandlers und/oder eines Boostkondensators erreicht werden. Der DC/DC-Wandler und der Boostkondensator sind derart dimensioniert, dass im Normalbetrieb (Figur 1) alle relevanten Betriebspunkte des Gasinjektors bedient werden können. Im Falle des Abstellens der Brennkraftmaschine und der dann notwendigen Ablassfunktion (Purge-Funktion) sind Leistungsreserven vorhanden, welche in der Ablassfunktion für die wenigen notwendigen Einspritzungen, üblicherweise bei geringerer Drehzahl als im Normalbetrieb, ausreichen. In particular, there is no reduction in the current level in the pick-up phase B 'in the exhaust function of the gas injector. The absolute value IT is also greater than the value 11 in normal operation at the end of the boost phase. This can be achieved by dimensioning a DC/DC converter and/or a boost capacitor. The DC/DC converter and the boost capacitor are like this dimensioned so that all relevant operating points of the gas injector can be served in normal operation (Figure 1). If the internal combustion engine is switched off and the purge function is then required, power reserves are available which are sufficient in the purge function for the few necessary injections, usually at a lower speed than in normal operation.
Somit werden die Energiereserven aus dem DC/DC-Wandler und/oder dem Boostkondensator für die in Figur 2 dargestellte Ansteuerung zur Anhebung des Stromniveaus (Kurve K1 in Figur 2 in der Anzugsphase B‘) genutzt. Thus, the energy reserves from the DC/DC converter and/or the boost capacitor are used for the control shown in FIG. 2 to increase the current level (curve K1 in FIG. 2 in the pick-up phase B').
Wie weiterhin aus dem Vergleich zwischen Figur 1 und Figur 2 ersichtlich ist, ist die Anzugsphase B‘ im Ablassbetrieb (t2‘-tT) kürzer als die Anzugsphase B im Normalbetrieb (t2-t1). Hingegen ist die Boostphase A‘ im Ablassbetrieb bedingt durch das höhere Booststromniveau größer als im Normalbetrieb, was in Figur 2 durch den Zeitpunkt tT im Vergleich zum Zeitpunkt t1 im Normalbetrieb gezeigt ist. As can also be seen from the comparison between FIG. 1 and FIG. 2, the tightening phase B 'in draining operation (t2'-tT) is shorter than the tightening phase B in normal operation (t2-t1). On the other hand, the boost phase A' in drain operation is larger than in normal operation due to the higher boost current level, which is shown in Figure 2 by the time tT compared to the time t1 in normal operation.
Durch das höhere Stromniveau IT im Ablassbetrieb wird ferner eine erhöhte Öffnungskraft des Magnetaktors bereitgestellt, was durch einen Vergleich der Kraftverläufe K3 zwischen Figur 1 und Figur 2 ersichtlich ist. Dadurch kann der aufgrund des absinkenden Gasdrucks im Gasinjektor fehlende Kraftanteil des Gasdrucks zum Öffnen des Gasinjektors ausgeglichen werden. In der Haltephase C, C‘ und der Schließphase D, D‘ im Ablassbetrieb und im Normalbetrieb sind alle vier Kurven K1 , K2, K3 und K4 wieder gleich. The higher current level IT in the draining operation also provides an increased opening force of the magnetic actuator, which can be seen by comparing the force curves K3 between FIG. 1 and FIG. 2. This allows the missing force component of the gas pressure to open the gas injector due to the falling gas pressure in the gas injector to be compensated for. In the holding phase C, C' and the closing phase D, D' in the draining operation and in normal operation, all four curves K1, K2, K3 and K4 are the same again.
Somit kann durch die Nutzung der Boostspannung für die Anzugsstromregelung in der Anzugsphase B eine höhere mittlere Spannung und damit auch ein höherer Anzugsstrom IT ermöglicht werden. Somit sind höhere Magnetkräfte durch den Magnetaktor möglich, welche die reduzierten öffnenden Druckkräfte des einzublasenden gasförmigen Brennstoffs ausgleichen. Thus, by using the boost voltage for the starting current control in the starting phase B, a higher average voltage and thus also a higher starting current IT can be made possible. This means that higher magnetic forces are possible through the magnetic actuator, which compensate for the reduced opening pressure forces of the gaseous fuel to be injected.
Im beschriebenen Ausführungsbeispiel ist eine Ansteuervariante mit erhöhtem Booststrom am Ende der Boostphase A‘ dargestellt. Es sind jedoch auch Ansteuervarianten denkbar, bei denen der Stromverlauf in der Boostphase A‘ im Ablassbetrieb gleich wie im Normalbetrieb ist und dann der Ausgleich durch die Magnetkraft nur in der Anzugsphase B‘ mit erhöhtem Strom realisiert wird. In the exemplary embodiment described, a control variant with increased boost current is shown at the end of the boost phase A'. However, control variants are also conceivable in which the current curve in the boost phase A' in the let-off mode is the same as in normal operation and then the compensation is only realized by the magnetic force in the pick-up phase B' with increased current.
Claims
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202380066160.3A CN119895134A (en) | 2022-09-14 | 2023-06-29 | Method for operating a gas injector |
| EP23736315.5A EP4587690A1 (en) | 2022-09-14 | 2023-06-29 | Method for operating a gas injector |
| KR1020257011922A KR20250065906A (en) | 2022-09-14 | 2023-06-29 | How a gas injector works |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102022209617.7A DE102022209617A1 (en) | 2022-09-14 | 2022-09-14 | Method for operating a gas injector |
| DE102022209617.7 | 2022-09-14 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2024056227A1 true WO2024056227A1 (en) | 2024-03-21 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/EP2023/067840 Ceased WO2024056227A1 (en) | 2022-09-14 | 2023-06-29 | Method for operating a gas injector |
Country Status (5)
| Country | Link |
|---|---|
| EP (1) | EP4587690A1 (en) |
| KR (1) | KR20250065906A (en) |
| CN (1) | CN119895134A (en) |
| DE (1) | DE102022209617A1 (en) |
| WO (1) | WO2024056227A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN119062481A (en) * | 2024-09-26 | 2024-12-03 | 北京理工大学 | A structure and method for improving the sealing performance of a hydrogen injector |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20010032612A1 (en) * | 1999-10-15 | 2001-10-25 | Welch Alan B. | Directly actuated injection valve |
| US7013876B1 (en) * | 2005-03-31 | 2006-03-21 | Caterpillar Inc. | Fuel injector control system |
| US8166953B2 (en) * | 2006-02-06 | 2012-05-01 | Orbital Australia Pty Limited | Fuel injection apparatus |
| EP2873842A1 (en) * | 2013-11-14 | 2015-05-20 | Delphi Automotive Systems Luxembourg SA | Control of Actuation of Fuel Injector |
| US20160319763A1 (en) * | 2015-04-29 | 2016-11-03 | General Electric Company | Engine system and method |
| DE102015210756A1 (en) * | 2015-06-12 | 2016-12-15 | Robert Bosch Gmbh | Gas injector arrangement, operating method for a gas injector arrangement and internal combustion engine |
-
2022
- 2022-09-14 DE DE102022209617.7A patent/DE102022209617A1/en active Pending
-
2023
- 2023-06-29 WO PCT/EP2023/067840 patent/WO2024056227A1/en not_active Ceased
- 2023-06-29 KR KR1020257011922A patent/KR20250065906A/en active Pending
- 2023-06-29 EP EP23736315.5A patent/EP4587690A1/en active Pending
- 2023-06-29 CN CN202380066160.3A patent/CN119895134A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20010032612A1 (en) * | 1999-10-15 | 2001-10-25 | Welch Alan B. | Directly actuated injection valve |
| US7013876B1 (en) * | 2005-03-31 | 2006-03-21 | Caterpillar Inc. | Fuel injector control system |
| US8166953B2 (en) * | 2006-02-06 | 2012-05-01 | Orbital Australia Pty Limited | Fuel injection apparatus |
| EP2873842A1 (en) * | 2013-11-14 | 2015-05-20 | Delphi Automotive Systems Luxembourg SA | Control of Actuation of Fuel Injector |
| US20160319763A1 (en) * | 2015-04-29 | 2016-11-03 | General Electric Company | Engine system and method |
| DE102015210756A1 (en) * | 2015-06-12 | 2016-12-15 | Robert Bosch Gmbh | Gas injector arrangement, operating method for a gas injector arrangement and internal combustion engine |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN119062481A (en) * | 2024-09-26 | 2024-12-03 | 北京理工大学 | A structure and method for improving the sealing performance of a hydrogen injector |
Also Published As
| Publication number | Publication date |
|---|---|
| CN119895134A (en) | 2025-04-25 |
| EP4587690A1 (en) | 2025-07-23 |
| KR20250065906A (en) | 2025-05-13 |
| DE102022209617A1 (en) | 2024-03-14 |
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