DE102006021735A1 - Solenoid valve with flooded anchor space - Google Patents
Solenoid valve with flooded anchor space Download PDFInfo
- Publication number
- DE102006021735A1 DE102006021735A1 DE200610021735 DE102006021735A DE102006021735A1 DE 102006021735 A1 DE102006021735 A1 DE 102006021735A1 DE 200610021735 DE200610021735 DE 200610021735 DE 102006021735 A DE102006021735 A DE 102006021735A DE 102006021735 A1 DE102006021735 A1 DE 102006021735A1
- Authority
- DE
- Germany
- Prior art keywords
- anchor
- front side
- magnetic yoke
- fuel injector
- solenoid valve
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M47/00—Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure
- F02M47/02—Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure of accumulator-injector type, i.e. having fuel pressure of accumulator tending to open, and fuel pressure in other chamber tending to close, injection valves and having means for periodically releasing that closing pressure
- F02M47/027—Electrically actuated valves draining the chamber to release the closing pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M63/00—Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
- F02M63/0012—Valves
- F02M63/0014—Valves characterised by the valve actuating means
- F02M63/0015—Valves characterised by the valve actuating means electrical, e.g. using solenoid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M63/00—Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
- F02M63/0012—Valves
- F02M63/0014—Valves characterised by the valve actuating means
- F02M63/0015—Valves characterised by the valve actuating means electrical, e.g. using solenoid
- F02M63/0017—Valves characterised by the valve actuating means electrical, e.g. using solenoid using electromagnetic operating means
- F02M63/0019—Valves characterised by the valve actuating means electrical, e.g. using solenoid using electromagnetic operating means characterised by the arrangement of electromagnets or fixed armatures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M63/00—Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
- F02M63/0012—Valves
- F02M63/0014—Valves characterised by the valve actuating means
- F02M63/0015—Valves characterised by the valve actuating means electrical, e.g. using solenoid
- F02M63/0017—Valves characterised by the valve actuating means electrical, e.g. using solenoid using electromagnetic operating means
- F02M63/0021—Valves characterised by the valve actuating means electrical, e.g. using solenoid using electromagnetic operating means characterised by the arrangement of mobile armatures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M63/00—Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
- F02M63/0012—Valves
- F02M63/0031—Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M63/00—Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
- F02M63/0012—Valves
- F02M63/007—Details not provided for in, or of interest apart from, the apparatus of the groups F02M63/0014 - F02M63/0059
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M2200/00—Details of fuel-injection apparatus, not otherwise provided for
- F02M2200/30—Fuel-injection apparatus having mechanical parts, the movement of which is damped
- F02M2200/308—Fuel-injection apparatus having mechanical parts, the movement of which is damped using pneumatic means
Abstract
Die Erfindung bezieht sich auf einen Kraftstoffinjektor (10) mit einem Magnetventil (12), welches ein Magnetjoch (16) und eine Magnetspule (18) sowie einen Anker (32, 34) umfasst. Der Anker (32, 34) ist durch eine Schließfeder (26) in Schließrichtung beaufschlagt. Zwischen einer Stirnseite (58) des Magnetjochs (16) und einer Stirnseite (54) des Ankers (32, 34) verläuft ein steuermengenaufnehmender Hohlraum (50). An mindestens einer der Stirnseiten (54, 58) ist eine das Volumen des Hohlraumes (50) vergrößernde Ausnehmung (56, 66) ausgebildet.The invention relates to a fuel injector (10) with a solenoid valve (12) which comprises a magnetic yoke (16) and a magnetic coil (18) as well as an armature (32, 34). The armature (32, 34) is urged in the closing direction by a closing spring (26). Between an end face (58) of the magnet yoke (16) and an end face (54) of the armature (32, 34) runs a cavity (50) which absorbs the taxable amount. A recess (56, 66) which enlarges the volume of the cavity (50) is formed on at least one of the end faces (54, 58).
Description
Stand der TechnikState of technology
Aus
Bei den aus dem Stand der Technik bekannten Magnetventilen werden zur Realisierung extrem kurzer Schaltzeiten die Restluftspalte der Magnetkreise sehr klein ausgelegt. Als Restluftspalt wird der Abstand zwischen einem Magnetjoch und dem Anker nach dessen Betätigung bezeichnet. Der Kraftstoff, der aufgrund der Druckentlastung eines Steuerraums zum Beispiel in den sich ergebenden Hohlraum zwischen dem Magnetjoch (Magnetkern) und den Anker gelangt, wird durch den sehr schnell ablaufenden Schaltvorgang verdrängt und neigt dazu, bedingt durch die hohe Abfließgeschwindigkeit, zur Dampfblasenbildung, d. h. zur Kavitation. Bei der darauf folgenden Wiederbefüllung des Hohlraums mit Kraftstoff brechen die Dampfblasen zusammen, was zu einer hohen mechanischen Belastung, im Extremfall gar zur Kavitationserosion, der Bauteile führt, die den hohen Drücken aus gesetzt sind, die sich bei der schlagartigen Implosion der Dampfblasen einstellen. Die sich bei der Kavitationserosion ergebenden Beschädigungen der Bauteile führen dazu, dass der eingestellte Hub einer Ankerbaugruppe innerhalb eines Magnetventils beeinträchtigt wird, so dass es zu ungenauen, undefinierten Hüben der Ankerbaugruppe bei Bestromung der Magnetspule des Magnetventils kommt, was wiederum zu Streuungen der in den Brennraum eingespritzten Kraftstoffmenge führt.at the known from the prior art solenoid valves are for Realization of extremely short switching times the residual air gaps of the magnetic circuits designed very small. The residual air gap is the distance between a magnetic yoke and the armature after its operation is called. The fuel that due to the pressure relief of a control room, for example in the resulting cavity between the magnetic yoke (magnetic core) and The anchor gets through the very fast switching process repressed and tends, due to the high discharge rate, for vapor bubble formation, d. H. for cavitation. During the subsequent refilling of the Cavity with fuel break the vapor bubbles together, resulting in a high mechanical load, in extreme cases even cavitation erosion, leads the components, the high pressures are set off by the sudden implosion of the vapor bubbles to adjust. The damage resulting from the cavitation erosion lead the components that the set stroke of an armature assembly within a solenoid valve impaired so that it adds to inaccurate, undefined strokes of the armature assembly Energization of the solenoid of the solenoid valve comes, which in turn to scatter the amount of fuel injected into the combustion chamber leads.
Offenbarung der Erfindungepiphany the invention
Der vorliegenden Erfindung liegt die Aufgabe zugrunde, eine konstruktive Ausgestaltung eines Magnetventils bereitzustellen, welche Beschädigungen der Komponenten eines Magnetventils durch Kavitationserosion vermeidet.Of the present invention is based on the object, a constructive Provide a design of a solenoid valve, which damage the Prevents components of a solenoid valve from cavitation erosion.
Der erfindungsgemäß vorgeschlagenen Lösung folgend, wird die Kontur entweder eines Magnetjochs des Magnetventiles oder die Kontur einer dem Magnetjoch gegenüberliegenden Stirnseite der Ankerbaugruppe so ausgelegt, dass sich ein großes Volumen an kavitationserosionskritischen Stellen und ein kleines Volumen an kavitationserosionsunkritischen Stellen im Hohlraum, d. h. im Luftspalt zwischen dem Anker und dem Magnetjoch des Magnetventils einstellt. Die Auslegung der Konturen entweder an der dem Anker gegenüberliegenden Stirnseite des Magnetjochs oder an der dem Magnetjoch gegenüberliegenden Stirnseite der Ankerbaugruppe, beeinflusst die magnetischen Eigenschaften des Magnetventils, insbesondere den magnetischen Fluss, nicht.Of the proposed according to the invention solution Following, the contour of either a magnetic yoke of the solenoid valve or the contour of a magnetic yoke opposite end of the armature assembly designed to hold a large volume at cavitation-erosion critical sites and a small volume cavitation-erosion-critical sites in the cavity, d. H. in the Air gap between the armature and the magnetic yoke of the solenoid valve established. The design of the contours either on the anchor opposite Front side of the magnetic yoke or at the magnetic yoke opposite Front side of the armature assembly, affects the magnetic properties of the solenoid valve, in particular the magnetic flux, not.
Durch die vorgeschlagene Konturierung entweder des Magnetjochs oder der Stirnseite der Ankerbaugruppe werden innerhalb des vergrößerten Volumens sich einstellende Kavitationsblasen zur Implosion gebracht, wodurch die Oberflächenbeanspruchung sowohl der Stirnseite des Magnetjochs als auch insbesondere der Stirnseite der Ankerbaugruppe erheblich herabgesetzt wird.By the proposed contouring of either the magnetic yoke or the Face of the anchor assembly become within the enlarged volume resulting cavitation bubbles brought to implosion, causing the surface stress both the end face of the magnetic yoke and in particular the Front side of the armature assembly is significantly reduced.
In einer vorteilhaften Ausgestaltung der Konturierung entweder der Stirnseite des Magnetjochs oder der Stirnseite der Ankerbaugruppen, kann der Restluftspalt, der sich im bestromten Zustand des Magnetjoches zwischen dessen Stirnseite und der Stirnseite der Ankerbaugruppe einstellt, am Rande der Stirnseite der Ankerbaugruppe oder am Rand des Magnetjoches kleiner ausgelegt werden als in der Mitte. Dadurch stellt sich eine kleinere Spaltweite innerhalb des Randbereiches zwischen der Stirnseite des Magnetjoches und der Stirnseite der Ankerbaugruppe ein, wodurch die Abfließgeschwindigkeit des Kraftstoffes aus dem Hohlraum zwischen Magnetjoch und Anker am Ende der Ankerhubbewegung gedrosselt, d. h. verlangsamt wird und die Kavitationsneigung erheblich herabgesetzt wird.In an advantageous embodiment of the contouring either the End face of the magnetic yoke or the face of the anchor assemblies, can the residual air gap, which is in the energized state of the magnetic yoke between the front side and the front side of the armature assembly adjusts, on the edge of the face of the anchor assembly or on the edge of Magnet yoke be designed smaller than in the middle. Thereby turns a smaller gap width within the edge area between the end face of the magnetic yoke and the front side of the Anchor assembly, whereby the flow rate of the fuel off the cavity between magnetic yoke and armature at the end of Ankerhubbewegung throttled, d. H. slows down and the cavitation tendency considerably is lowered.
Ein weiterer durch die erfindungsgemäß vorgeschlagene Lösung erzielbarer Vorteil ist darin zu erblicken, dass eine gedämpfte Bewegungsbegrenzung der Ankerbaugruppe mit einer geringeren mechanischen Beanspruchung der Bauteile des Magnetventils erfolgt, was die Lebensdauer des vorgeschlagenen Magnetventiles erheblich erhöht.One further proposed by the invention solution achievable advantage is to be seen in that a damped movement limitation the armature assembly with a lower mechanical stress the components of the solenoid valve takes place, which the life of the proposed solenoid valve significantly increased.
Zeichnungdrawing
Anhand der Zeichnung wird die Erfindung nachstehend eingehender beschrieben.Based In the drawings, the invention will be described below in more detail.
Es zeigt:It shows:
Detail Z eine vergrößerte Darstellung des Hohlraumes zwischen einer Stirnseite des Magnetjochs und der Stirnseite des dem Magnetjoches gegenüberliegenden Ankers,detail Z is an enlarged view the cavity between an end face of the magnetic yoke and the Front side of the magnet yoke opposite armature,
Ausführungsvariantenvariants
Aus
der Darstellung gemäß
In
einem Kraftstoffinjektor
Das
Magnetventil
Im
Magnetjoch
Die
eine Ankerscheibe
Über die
in
Detail Z zeigt den sich zwischen dem Magnetjoch und der Ankerscheibe der Ankerbaugruppe einstellenden Hohlraum in vergrößerter Darstellung.detail Z shows the between the magnetic yoke and the armature disc of Anchor assembly adjusting cavity in an enlarged view.
Aus
dem Detail z geht hervor, dass der Hohlraum
Aus
der Darstellung gemäß
In
bestromten Zustand der von dem Magnetjoch
In
der
In
dem durch den innenliegenden Luftspalt
Der
Darstellung gemäß
Der
Darstellung gemäß
In
Abwandlung der in
Der
Darstellung gemäß
Die
Darstellung gemäß
Claims (8)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200610021735 DE102006021735A1 (en) | 2006-05-10 | 2006-05-10 | Solenoid valve with flooded anchor space |
EP07726781A EP2021616B1 (en) | 2006-05-10 | 2007-03-12 | Solenoid valve with flooded armature chamber |
PCT/EP2007/052266 WO2007128607A1 (en) | 2006-05-10 | 2007-03-12 | Solenoid valve with flooded armature chamber |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200610021735 DE102006021735A1 (en) | 2006-05-10 | 2006-05-10 | Solenoid valve with flooded anchor space |
Publications (1)
Publication Number | Publication Date |
---|---|
DE102006021735A1 true DE102006021735A1 (en) | 2007-11-15 |
Family
ID=38283523
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE200610021735 Withdrawn DE102006021735A1 (en) | 2006-05-10 | 2006-05-10 | Solenoid valve with flooded anchor space |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP2021616B1 (en) |
DE (1) | DE102006021735A1 (en) |
WO (1) | WO2007128607A1 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009124789A1 (en) * | 2008-04-10 | 2009-10-15 | Robert Bosch Gmbh | Solenoid valve without a residual air gap disk |
WO2010000507A1 (en) * | 2008-06-30 | 2010-01-07 | Robert Bosch Gmbh | Solenoid valve, fuel injector, and method for the production thereof |
DE102009045728A1 (en) | 2009-10-15 | 2011-04-21 | Robert Bosch Gmbh | Magnetic valve for use in common-rail injector, has valve housing actuated by armatures in uncontrolled state of magnetic coil, where movement of housing is delayed using damping elements in direction of valve seat |
EP2653712A1 (en) * | 2012-04-16 | 2013-10-23 | Robert Bosch GmbH | Fuel injector with a solenoid valve |
WO2019206657A1 (en) * | 2018-04-26 | 2019-10-31 | Robert Bosch Gmbh | Fuel injector |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT227711Y1 (en) * | 1992-12-29 | 1997-12-15 | Elasis Sistema Ricerca Fiat | ELECTROMAGNETIC CONTROLLED METERING VALVE FOR A FUEL INJECTOR |
DE19832826C2 (en) * | 1998-07-21 | 2000-08-17 | Bosch Gmbh Robert | Assembly procedure for fuel injector and pilot valve and fuel injector |
DE10018304A1 (en) * | 2000-04-13 | 2001-10-25 | Bosch Gmbh Robert | Armature plate of a switching magnet, in particular for diesel fuel injectors, and method for producing such an armature plate |
DE10131199A1 (en) * | 2001-06-28 | 2003-01-16 | Bosch Gmbh Robert | Solenoid valve for controlling an injection valve of an internal combustion engine |
DE10305985A1 (en) * | 2002-12-13 | 2004-07-15 | Robert Bosch Gmbh | No-bounce magnetic actuator for injectors |
-
2006
- 2006-05-10 DE DE200610021735 patent/DE102006021735A1/en not_active Withdrawn
-
2007
- 2007-03-12 EP EP07726781A patent/EP2021616B1/en active Active
- 2007-03-12 WO PCT/EP2007/052266 patent/WO2007128607A1/en active Application Filing
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009124789A1 (en) * | 2008-04-10 | 2009-10-15 | Robert Bosch Gmbh | Solenoid valve without a residual air gap disk |
WO2010000507A1 (en) * | 2008-06-30 | 2010-01-07 | Robert Bosch Gmbh | Solenoid valve, fuel injector, and method for the production thereof |
DE102009045728A1 (en) | 2009-10-15 | 2011-04-21 | Robert Bosch Gmbh | Magnetic valve for use in common-rail injector, has valve housing actuated by armatures in uncontrolled state of magnetic coil, where movement of housing is delayed using damping elements in direction of valve seat |
EP2653712A1 (en) * | 2012-04-16 | 2013-10-23 | Robert Bosch GmbH | Fuel injector with a solenoid valve |
WO2019206657A1 (en) * | 2018-04-26 | 2019-10-31 | Robert Bosch Gmbh | Fuel injector |
CN112352096A (en) * | 2018-04-26 | 2021-02-09 | 罗伯特·博世有限公司 | Fuel injector |
Also Published As
Publication number | Publication date |
---|---|
EP2021616A1 (en) | 2009-02-11 |
EP2021616B1 (en) | 2011-05-18 |
WO2007128607A1 (en) | 2007-11-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
R119 | Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee |
Effective date: 20111201 |