EP2596230A1 - Injection device having improved spray preparation - Google Patents

Injection device having improved spray preparation

Info

Publication number
EP2596230A1
EP2596230A1 EP11724597.7A EP11724597A EP2596230A1 EP 2596230 A1 EP2596230 A1 EP 2596230A1 EP 11724597 A EP11724597 A EP 11724597A EP 2596230 A1 EP2596230 A1 EP 2596230A1
Authority
EP
European Patent Office
Prior art keywords
injection
hole
spray
holes
injection hole
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP11724597.7A
Other languages
German (de)
French (fr)
Other versions
EP2596230B1 (en
Inventor
Guenter Dantes
Bernd Krauss
Andreas Krause
Anja Melsheimer
Harald Lang
Martin Stahl
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of EP2596230A1 publication Critical patent/EP2596230A1/en
Application granted granted Critical
Publication of EP2596230B1 publication Critical patent/EP2596230B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1806Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
    • F02M61/1833Discharge orifices having changing cross sections, e.g. being divergent
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1806Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
    • F02M61/1813Discharge orifices having different orientations with respect to valve member direction of movement, e.g. orientations being such that fuel jets emerging from discharge orifices collide with each other
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1806Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
    • F02M61/1846Dimensional characteristics of discharge orifices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1853Orifice plates

Definitions

  • the present invention relates to an injection device for injecting fluid, in particular fuel, with an improved spray treatment.
  • Fuel injection devices are known in the prior art in various configurations. Frequently be here
  • Spray hole disc is arranged.
  • the injection holes provided in the spray perforated disk define u.a. the spray treatment during the injection of fuel.
  • Such spray perforated disks have basically proven, but there is a continuing desire to further reduce fuel consumption through an improved spray conditioning and the
  • an injection is carried out in such a way that the injected fluid is torn open at the outlet from the spray holes as wide as possible and in particular forms a partial hollow blade in order to achieve a very good spray distribution.
  • This is inventively achieved in that at least a first and a second injection hole in a
  • the opening edge distance is the distance which, when a straight line is formed at the inflow opening, has the maximum distance between two edge points of the inflow opening.
  • Further spray hole axes of the injection holes according to the invention are arranged in mutually different directions. As a result, a spray treatment in different directions is achieved at the outlet from the first and second spray hole, so that a relatively wide space area is covered with injected fluid.
  • the inflow at the two injection holes is positively influenced by the main inflows influencing each other in the two injection holes and causing a strong deflection on the inflow side of the injection holes.
  • the injection holes are thus intentionally not arranged at equal intervals along the circumference, but preferably in pairs with a small distance, so that a positive mutual
  • the first and second spray holes of different sizes must be satisfied, that is, the distance is defined by the largest opening edge distance of one of the injection holes.
  • the distance between the first and second injection hole is 0.5 times to 1.5 times the maximum opening edge distance of
  • Spray holes and particularly preferably the distance between the two spray holes corresponds approximately to the maximum opening edge distance of the spray holes.
  • the spray hole axes of the first and second spray hole in
  • Spray hole axis extends through a plane comprising the inlet opening.
  • the inclination angle of the injection hole axes are preferably in a range from 5 ° to 85 °, preferably 20 ° to 60 °, and the angles of inclination are more preferably approximately up to 40 °, and preferably approximately 40 °.
  • the spray holes of a spray hole pair each have one
  • Spray hole axis which have the same angle of inclination, but are directed in different directions. As a result, essentially the same shape spray cone per injection hole can be achieved.
  • an even number of spray holes is provided, wherein in each case two of the spray holes are arranged in pairs, corresponding to the arrangement of the first and second spray holes. This allows a particularly good spray treatment, in particular a spray pattern with two
  • Spray jets can be generated in each case in the form of cones, wherein each spray jet is generated by a plurality of spray holes. Alternatively, an odd number of spray holes are provided, which preferably produce a spray pattern with only a single jet of spray in cone shape.
  • At least one of the injection holes has a widening shape, in particular a conically widening shape.
  • the spray-hole shape expands particularly preferably in the direction of flow.
  • Injection holes have an expanding shape, wherein the expanding shapes may be the same or different.
  • an inflow opening of a spray hole is circular or oval.
  • the maximum corresponds
  • the maximum opening edge distance of a largest axis corresponds to one of the oval-shaped openings, in particular a main axis of an ellipse.
  • the first and second spray holes are arranged on a circumference and the injection hole axes are arranged at a hole pitch angle of 20 ° to 60 °, preferably 20 ° to 30 °, and preferably about 25 °.
  • the injection device further comprises a funnel-shaped inflow space, which is arranged on the inflow side of the injection holes. Through this funnel-shaped inflow a relatively sharp deflection of the
  • Inflow fluid reaches the injection holes, which entails an increased turbulence of the fluid and contributes to improved spray conditioning.
  • a main flow of the fluid is supplied to each spray hole in an inflow angle, so that a sum of the inflow angle and an angle of the spray hole axis is less than or equal to 90 °.
  • the inflow angle is between 40 ° and 60 °.
  • the injection device further comprises a third and a fourth injection hole, which are arranged at a distance which is less than or equal to a double maximum opening edge distance at the
  • Inflow side of the injection holes is and whose injection hole axes are arranged in mutually different directions. Furthermore, the third and fourth injection hole are arranged opposite the first and second injection hole.
  • the injection device comprises a fifth and a sixth injection hole, which are arranged opposite to each other and whose spray hole axes are arranged in different directions.
  • the fifth and sixth spray holes are at a greater distance from
  • the injection holes are preferably arranged in a spray perforated disk.
  • Spray hole disc can then be easily attached to the injector.
  • Figure 1 is a plan view of a spray hole geometry of a
  • FIG. 2 shows a sectional view along the line II-II of FIG. 1,
  • Figure 3 is a schematic sectional view taken along the line III-III.
  • Figures 4 to 10 are plan views of injection hole geometries according to further
  • Fuel injection valve with a spray perforated disk 2 according to a first embodiment of the invention described in detail.
  • the injection valve 1 comprises a spray perforated disk 2, which is arranged on a valve seat 4. Fuel is supplied for injection through an opening 4a in the valve seat 4 in a funnel-shaped, expanding inflow space 5 and guided there to the spray holes.
  • the flow of the fuel to the spray holes indicated by the arrows A, B, C.
  • the spray perforated disk 2 comprises a total of six injection holes, namely a first injection hole 1 1, a second injection hole 12, a third injection hole 13, a fourth injection hole 14, a fifth injection hole 15 and a sixth injection hole 16. It is first and the second injection hole 1 1, 12 and the third and the fourth injection hole 13, 14 arranged as a spray hole pair each relatively close to each other.
  • the injection holes 1 1, 12, 13, 14, 15, 16 are cylindrical and all each have the same diameter. In FIG. 1, for reasons of clarity, only the first diameter D1 of the first is shown Plotted injection hole and the diameter D2 of the second injection hole, the cylindrical injection holes of each plan view of Figure 1 appear oval-shaped.
  • a distance 3 between the first injection hole 1 1 and the second injection hole 12 corresponds to the diameter D1 or D2 of the two
  • the first injection hole 1 1 and the second injection hole 12 are arranged relatively close to each other, whereby the flow on one inflow side 2 a of the spray orifice plate 2 mutually influenced.
  • the spray holes can conically widen or taper or also have different diameters in the flow direction, wherein any combinations are possible.
  • Figure 3 shows a sectional view through the first and second injection hole 1 1 and 12.
  • the reference numeral 1 1 a designates a spray hole axis of the first injection hole 1 1 and the reference numeral 12a denotes a second
  • the first injection hole 1 1 and the second injection hole 12 are arranged in different directions and also have different angles of inclination.
  • the angle of inclination of the injection holes is in each case the one angle which forms the smallest angle on the inflow side 2a with a plane comprising the injection hole opening.
  • the inclination angle of the first injection hole is denoted by and
  • Inclination angle of the second injection hole 12 with ß which is about 45 ° and ß about 70 °.
  • a sum of the inclination angle and the inflow angle ⁇ at the first injection hole 1 1 is about 85 ° and thus smaller than 90 °.
  • Spray hole 12 is about 85 °. Because the sum of the angle of inclination and the inflow angle at each injection hole is less than 90 °, a relatively flat flow of the injection holes can be achieved. Further, as is apparent from Figure 1, is achieved by the close arrangement of the first and second spray hole 1 1, 12 a reinforced one-sided Lochanstromung for each injection hole.
  • the flow of the individual injection holes are indicated by the arrows, wherein the length of the arrows corresponds to the magnitude of the flow.
  • the main flow to the spray holes is marked with the letter C.
  • Lower inflowing fuel quantities are indicated by the arrows D and E.
  • a hole spacing angle ⁇ between the first injection hole 11 and the second injection hole 12 is approximately 25 °.
  • Hole distance angle ⁇ is defined by a center M of the spray hole 2 from. All spray holes 1 1, 12, 13, 14, 15 and 16 lie on a common circumference K. Alternatively, the injection holes can not lie on a common circumference.
  • the paired arrangement of spray holes with a relatively small distance thus allows an increased one-sided spray hole flow.
  • this flow is contrary to a direction of inclination of the
  • injection hole axes of the injection holes are arranged such that the spray jets generated do not meet in the injection space. This ensures the widest possible spread of the fuel droplets in the injection space without overlaps.
  • a thickness of the spray perforated disk 2 corresponds approximately to a diameter of the injection holes.
  • the main flow of the fifth and sixth spray holes 15, 16 is mainly due to the inclination of the injection hole axes 15a and 16a inwardly and the shape of the inflow space 5 mainly from the outside.
  • the main flow is in the paired spray holes 1 1, 12 and 13, 14 substantially in a central region from the outside of the injection hole pair.
  • a relatively small flow is present at the inner areas of the injection holes a relatively small flow is present.
  • the angle of the injection hole axis is different to Hauptanströmwinkel, resulting in an additional impact in the spray hole. As a result, the jet generated by the injection hole is deformed more to a hollow cone, which the
  • the Spray hole angle at the first injection hole about 45 ° and the main flow angle ⁇ is about 35 °.
  • the difference between the main flow angle ⁇ and the tilt angle is preferably equal to or greater than 10 °.
  • FIGS. 4 to 10 further exemplary embodiments are described in detail with reference to FIGS. 4 to 10, wherein identical or functionally identical parts are designated by the same reference numerals as in the first exemplary embodiment.
  • the arrows on the spray holes shown in FIGS. 4 to 10 indicate the directions of inclination of the spray holes, wherein FIGS. 4 to 10 each show a plan view of the inflow sides 2 a of the spray perforated disks 2.
  • a total of eight spray holes 1 1 to 18 are provided, wherein two pairs of spray holes 1 1, 12 and 13, 14 are arranged at a distance 3, which corresponds to a maximum opening edge distance of the injection holes on the inflow side.
  • the injection holes in this exemplary embodiment are cylindrical, and because of the inclination, the cylindrical injection holes on the surface of the spray perforated disc form ovals, so that the distance 3 corresponds to a longitudinal axis of the oval.
  • the centers of the injection holes 1 1 to 18 are all on a common circumference K. Further, the injection directions of the injection holes are chosen such that only two directions are present. Here, in the paired spray holes 1 1 and 12 and 13 and 14, the injection directions are chosen such that they are opposite to each other (see Figure 4).
  • a total of six injection holes 1 1 to 16 are provided, wherein the injection holes are also formed cylindrically.
  • the centers of the injection holes lie on a common
  • Circumference K The injection holes are inclined in mutually different directions, so that at the downstream side, as indicated by the arrows, fuel exits in various directions.
  • injection holes 1 1 to 14 are arranged.
  • the injection holes are again on a circumference K and the opening directions of the injection holes are selected so that the
  • Spray hole axes of the pairwise injection holes are directed by an angle ⁇ by about 140 ° opposite to each other.
  • Embodiment all existing spray holes arranged in pairs, resulting in a particularly good fuel processing.
  • the fifth embodiment shown in Figure 7 substantially corresponds to the third embodiment of Figure 5, in contrast to the injection directions of the injection holes are directed in each case only in two directions. These directions are opposite to each other by 180 °, of the six arranged spray holes four are arranged in two spray-hole pairs and the spray holes 1 1, 12 and 13, 14 are directed in opposite directions.
  • the sixth embodiment shown in Figure 8 also has a total of six injection holes 1 1 to 16, wherein the injection holes 1 1 and 12 and 13 and 14 are each arranged at a distance 3 to each other. In this
  • the distance 3 is equal to twice the maximum opening edge distance of the injection holes 1 1, 12, 13, 14. Since the cylindrical injection holes are inclined in this embodiment again to the axial direction, the maximum opening edge distance is the major axis of the ovals of the injection holes.
  • the injection direction of all injection holes 1 1 to 16 is directed inwards, so that a high fuel concentration is obtained in a central region of an injection space.
  • the seventh embodiment shown in FIG. 9 substantially corresponds to the exemplary embodiment shown in FIG. 8, wherein the injection directions of the injection holes 11 to 16 are different.
  • the injection direction of the injection holes 1 1 and 12 is directed to the outside.
  • FIG. 10 shows an eighth embodiment of the invention, which is shown in FIG.
  • a distance 3 between the first and second injection hole 1 1, 12 and the third and fourth injection hole 13, 14 equal to a double opening edge distance of the injection holes 1 1, 12 and 13, 14.
  • the two injection hole pairs each other arranged opposite and also the injection directions of the respective injection holes go substantially inward.
  • At least two spray holes form a spray hole pair, which is arranged at a maximum distance 3 of a double opening edge distance from each other.
  • a positive mutual influence of the flow behavior is achieved on the inflow side 2a, resulting in an improved spray conditioning.
  • the shape (circular shape, ellipse, etc.), the direction of the injection hole axis, the inclination angle of the injection hole axis, the inner shape (cylindrical, conical, tapered, etc.) of the injection holes can be chosen differently, wherein for the injection holes of
  • Spray hole pair the condition is that the distance 3 between the two spray holes is smaller than twice the maximum opening edge distance on the inflow side and the injection hole axes of the two injection holes are arranged in mutually different directions, to avoid that the generated fuel sprays overlap.

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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)

Abstract

The invention relates to an injection device having at least one first injection hole (11) and a second injection hole (12) forming an injection hole pair, wherein the first and second injection holes (11, 12) are disposed such that a distance (3) between the two injection holes (11, 12) is less than or equal to two times the maximum opening edge distance (D1, D2) at an inflow side (2a) of the two injection holes (11, 12), and wherein injection hole axes (11a, 12a) of the first and second injection holes (11, 12) are disposed in different directions.

Description

Beschreibung  description
Titel title
Einspritzvorrichtung mit verbesserter Spray-Aufbereitung Stand der Technik  Injection device with improved spray treatment state of the art
Die vorliegende Erfindung betrifft eine Einspritzvorrichtung zur Einspritzung von Fluid, insbesondere von Kraftstoff, mit einer verbesserten Spray-Aufbereitung. Einspritzvorrichtungen für Kraftstoff sind aus dem Stand der Technik in unterschiedlichen Ausgestaltungen bekannt. Häufig werden hierbei The present invention relates to an injection device for injecting fluid, in particular fuel, with an improved spray treatment. Fuel injection devices are known in the prior art in various configurations. Frequently be here
Einspritzventile verwendet, bei denen am einspritzseitigen Ende eine Injectors used in which the injection-side end of a
Spritzlochscheibe angeordnet ist. Die in der Spritzlochscheibe vorgesehenen Spritzlöcher definieren dabei u.a. die Spray-Aufbereitung bei der Einspritzung von Kraftstoff. Derartige Spritzlochscheiben haben sich grundsätzlich bewährt, jedoch gibt es ein fortgesetztes Bestreben, durch eine verbesserte Spray- Aufbereitung den Kraftstoffverbrauch weiter zu senken und die Spray hole disc is arranged. The injection holes provided in the spray perforated disk define u.a. the spray treatment during the injection of fuel. Such spray perforated disks have basically proven, but there is a continuing desire to further reduce fuel consumption through an improved spray conditioning and the
Schadstoffemissionen weiter zu reduzieren. Offenbarung der Erfindung To further reduce pollutant emissions. Disclosure of the invention
Die erfindungsgemäße Einspritzvorrichtung zur Einspritzung von Fluid, insbesondere Kraftstoff, mit den Merkmalen des Anspruchs 1 weist The injection device according to the invention for the injection of fluid, in particular fuel, having the features of claim 1
demgegenüber den Vorteil auf, dass eine verbesserte Spray-Aufbereitung möglich ist, wodurch ein Kraftstoffverbrauch und Schadstoffemissionen weiter reduziert werden können. Erfindungsgemäß wird dabei eine Einspritzung derart vorgenommen, dass das eingespritzte Fluid am Austritt aus den Spritzlöchern möglichst breit aufgerissen wird und insbesondere eine Teilhohllamelle bildet, um eine sehr gute Spray-Verteilung zu erreichen. Dies wird erfindungsgemäß dadurch erreicht, dass wenigstens ein erstes und ein zweites Spritzloch in einemIn contrast, the advantage that an improved spray treatment is possible, whereby fuel consumption and pollutant emissions can be further reduced. According to the invention, an injection is carried out in such a way that the injected fluid is torn open at the outlet from the spray holes as wide as possible and in particular forms a partial hollow blade in order to achieve a very good spray distribution. This is inventively achieved in that at least a first and a second injection hole in a
Abstand zueinander angeordnet sind, welcher kleiner oder gleich ist, wie ein zweifacher Öffnungsrandabstand an der Einströmseite der Spritzlöcher. Der Öffnungsrandabstand ist dabei der Abstand, welcher bei Anlegen einer Gerade an der Einströmöffnung den maximalen Abstand zwischen zwei Randpunkten der Einströmöffnung aufweist. Weiter sind erfindungsgemäß Spritzlochachsen der Spritzlöcher in zueinander unterschiedlichen Richtungen angeordnet. Hierdurch wird bei Austritt aus dem ersten und zweiten Spritzloch eine Spray-Aufbereitung in unterschiedlichen Richtungen erreicht, so dass ein relativ breiter Raumbereich mit eingespritztem Fluid überdeckt wird. Durch die erfindungsgemäße relativ nahe Anordnung des ersten und zweiten Spritzlochs zueinander wird ferner insbesondere die Einströmung an den beiden Spritzlöchern positiv beeinflusst, indem sich die Haupteinströmungen in die beiden Spritzlöcher gegenseitig beeinflussen und eine starke Umlenkung an der Einströmseite der Spritzlöcher hervorrufen. Erfindungsgemäß werden somit die Spritzlöcher absichtlich nicht mit gleichen Abständen entlang des Umfangs angeordnet, sondern vorzugsweise paarweise mit kleinem Abstand, so dass eine positive gegenseitige Spaced apart, which is smaller or equal, as a twice the opening edge distance at the inflow side of the spray holes. The opening edge distance is the distance which, when a straight line is formed at the inflow opening, has the maximum distance between two edge points of the inflow opening. Further spray hole axes of the injection holes according to the invention are arranged in mutually different directions. As a result, a spray treatment in different directions is achieved at the outlet from the first and second spray hole, so that a relatively wide space area is covered with injected fluid. Furthermore, due to the relatively close arrangement of the first and second injection holes relative to one another, in particular the inflow at the two injection holes is positively influenced by the main inflows influencing each other in the two injection holes and causing a strong deflection on the inflow side of the injection holes. According to the invention, the injection holes are thus intentionally not arranged at equal intervals along the circumference, but preferably in pairs with a small distance, so that a positive mutual
Beeinflussung der Anströmungen der beiden Spritzlöcher des Spritzlochpaares erreicht wird. Es sei angemerkt, dass die Bedingung auch bei zwei  Influencing the flow of the two injection holes of the injection hole pair is achieved. It should be noted that the condition is two
unterschiedlich großen ersten und zweiten Spritzlöchern erfüllt sein muss, d.h., der Abstand wird durch den größten Öffnungsrandabstand eines der Spritzlöcher definiert. the first and second spray holes of different sizes must be satisfied, that is, the distance is defined by the largest opening edge distance of one of the injection holes.
Die Unteransprüche zeigen bevorzugte Weiterbildungen der Erfindung. The dependent claims show preferred developments of the invention.
Besonders bevorzugt beträgt der Abstand zwischen dem ersten und zweiten Spritzloch das 0,5-fache bis 1 ,5-fache des maximalen Offnungsrandabstands derParticularly preferably, the distance between the first and second injection hole is 0.5 times to 1.5 times the maximum opening edge distance of
Spritzlöcher und besonders bevorzugt entspricht der Abstand zwischen den beiden Spritzlöchern ungefähr dem maximalen Öffnungsrandabstand der Spritzlöcher. Gemäß einer weiteren bevorzugten Ausgestaltung der vorliegenden Erfindung sind die Spritzlochachsen des ersten und zweiten Spritzloches in Spray holes and particularly preferably the distance between the two spray holes corresponds approximately to the maximum opening edge distance of the spray holes. According to a further preferred embodiment of the present invention, the spray hole axes of the first and second spray hole in
unterschiedlichen Neigungswinkeln angeordnet. Erfindungsgemäß wird dabei unter dem Neigungswinkel ein Winkel verstanden, in welchem die arranged at different angles of inclination. According to the invention is understood by the angle of inclination, an angle in which the
Spritzlochachse durch eine die Einströmöffnung umfassenden Ebene verläuft. Die Neigungswinkel der Spritzlochachsen liegen vorzugsweise in einem Bereich von 5° bis 85°, bevorzugt 20° bis 60°, und die Neigungswinkel sind besonders bevorzugt ungefähr bis zu 40°, und vorzugsweise ungefähr 40°. Spray hole axis extends through a plane comprising the inlet opening. The inclination angle of the injection hole axes are preferably in a range from 5 ° to 85 °, preferably 20 ° to 60 °, and the angles of inclination are more preferably approximately up to 40 °, and preferably approximately 40 °.
Alternativ weisen die Spritzlöcher eines Spritzlochpaares jeweils eine Alternatively, the spray holes of a spray hole pair each have one
Spritzlochachse auf, welche den gleichen Neigungswinkel aufweisen, jedoch in unterschiedliche Richtungen gerichtet sind. Hierdurch können im Wesentlichen gleich geformte Spray-Kegel pro Spritzloch erreicht werden. Spray hole axis, which have the same angle of inclination, but are directed in different directions. As a result, essentially the same shape spray cone per injection hole can be achieved.
Besonders bevorzugt ist eine gerade Anzahl von Spritzlöchern vorgesehen, wobei jeweils zwei der Spritzlöcher paarweise, entsprechend der Anordnung des ersten und zweiten Spritzlochs, angeordnet sind. Dies ermöglicht eine besonders gute Spray-Aufbereitung, wobei insbesondere ein Spraybild mit zwei Particularly preferably, an even number of spray holes is provided, wherein in each case two of the spray holes are arranged in pairs, corresponding to the arrangement of the first and second spray holes. This allows a particularly good spray treatment, in particular a spray pattern with two
Spraystrahlen jeweils in Konusform erzeugbar ist, wobei jeder Spraystrahl durch mehrere Spritzlöcher erzeugt wird. Alternativ ist eine ungerade Anzahl von Spritzlöchern vorgesehen, welche vorzugsweise ein Spraybild mit nur einem einzigen Spraystrahl in Konusform erzeugen. Spray jets can be generated in each case in the form of cones, wherein each spray jet is generated by a plurality of spray holes. Alternatively, an odd number of spray holes are provided, which preferably produce a spray pattern with only a single jet of spray in cone shape.
Vorzugsweise weist wenigstens eines der Spritzlöcher eine sich erweiternde Form, insbesondere eine sich konisch erweiternde Form auf. Die Spritzlochform erweitert sich besonders bevorzugt in Durchströmungsrichtung. Somit ist es möglich, dass eines der Spritzlöcher eines Spritzlochpaares eine sich Preferably, at least one of the injection holes has a widening shape, in particular a conically widening shape. The spray-hole shape expands particularly preferably in the direction of flow. Thus, it is possible that one of the injection holes of a spray hole pair a
erweiternde Form aufweist, wodurch eine zusätzliche Aufweitung des Sprays erreicht wird und insbesondere die einzelnen Spraystrahlen kurz nach Austritt eine Teilhohllamelle bilden und sich die einzelnen Teilhohllamellen zu einem Spraystrahl in Konusform vereinigen. Besonders bevorzugt weisen beidenhas widening shape, whereby an additional widening of the spray is achieved and in particular form the individual spray jets shortly after leaving a partial hollow lamella and unite the individual partial lamellae into a spray jet in the cone shape. Particularly preferred are both
Spritzlöcher eine sich erweiternde Form auf, wobei die sich erweiternden Formen gleich oder auch unterschiedlich sein können. Injection holes have an expanding shape, wherein the expanding shapes may be the same or different.
Besonders bevorzugt ist eine Einströmöffnung eines Spritzlochs kreisrund oder oval. Bei kreisrunden Einströmöffnungen entspricht der maximale Particularly preferably, an inflow opening of a spray hole is circular or oval. For circular inflow openings, the maximum corresponds
Öffnungsrandabstand an der Einströmseite einem Durchmesser der  Opening edge distance at the inflow side a diameter of
Spritzlochöffnung. Bei einer ovalförmigen Einströmöffnung entspricht der maximale Öffnungsrandabstand einer größten Achse einer der ovalförmigen Öffnungen, insbesondere einer Hauptachse einer Ellipse. Vorzugsweise ist das erste und zweite Spritzloch auf einem Kreisumfang angeordnet und die Spritzlochachsen sind in einem Lochabstandswinkel von 20° bis 60°, bevorzugt 20° bis 30°, und vorzugsweise ungefähr 25°, angeordnet. Gemäß einer weiteren bevorzugten Ausgestaltung der vorliegenden Erfindung umfasst die Einspritzvorrichtung ferner einen trichterförmigen Einströmraum, welcher an der Einströmseite der Spritzlöcher angeordnet ist. Durch diesen trichterförmigen Einströmraum wird eine relativ scharfe Umlenkung des Injection port opening. In the case of an oval-shaped inflow opening, the maximum opening edge distance of a largest axis corresponds to one of the oval-shaped openings, in particular a main axis of an ellipse. Preferably, the first and second spray holes are arranged on a circumference and the injection hole axes are arranged at a hole pitch angle of 20 ° to 60 °, preferably 20 ° to 30 °, and preferably about 25 °. According to a further preferred embodiment of the present invention, the injection device further comprises a funnel-shaped inflow space, which is arranged on the inflow side of the injection holes. Through this funnel-shaped inflow a relatively sharp deflection of the
Einströmfluids in die Spritzlöcher erreicht, was eine verstärkte Verwirbelung des Fluids nach sich zieht und zu einer verbesserten Spray-Aufbereitung beiträgt.Inflow fluid reaches the injection holes, which entails an increased turbulence of the fluid and contributes to improved spray conditioning.
Vorzugsweise wird eine Hauptströmung des Fluids zu jedem Spritzloch in einem Einströmwinkel zugeführt, so dass eine Summe aus dem Einströmwinkel und einem Winkel der Spritzlochachse kleiner oder gleich 90° ist. Besonders bevorzugt ist der Einströmwinkel zwischen 40° und 60°. Preferably, a main flow of the fluid is supplied to each spray hole in an inflow angle, so that a sum of the inflow angle and an angle of the spray hole axis is less than or equal to 90 °. Particularly preferred is the inflow angle between 40 ° and 60 °.
Bevorzugt umfasst die Einspritzvorrichtung ferner ein drittes und ein viertes Spritzloch, welche in einem Abstand zueinander angeordnet sind, der kleiner oder gleich wie ein zweifacher maximaler Öffnungsrandabstand an der Preferably, the injection device further comprises a third and a fourth injection hole, which are arranged at a distance which is less than or equal to a double maximum opening edge distance at the
Einströmseite der Spritzlöcher ist und deren Spritzlochachsen in zueinander unterschiedlichen Richtungen angeordnet sind. Weiterhin sind das dritte und vierte Spritzloch gegenüber dem ersten und zweiten Spritzloch angeordnet. Inflow side of the injection holes is and whose injection hole axes are arranged in mutually different directions. Furthermore, the third and fourth injection hole are arranged opposite the first and second injection hole.
Weiter bevorzugt umfasst die Einspritzvorrichtung ein fünftes und ein sechstes Spritzloch, welche einander gegenüberliegend angeordnet sind und deren Spritzlochachsen in unterschiedlichen Richtungen angeordnet sind. Dabei sind das fünfte und sechste Spritzloch in einer größeren Entfernung von More preferably, the injection device comprises a fifth and a sixth injection hole, which are arranged opposite to each other and whose spray hole axes are arranged in different directions. The fifth and sixth spray holes are at a greater distance from
benachbarten Spritzlöchern als paarweise angeordnete Spritzlöcher angeordnet. adjacent spray holes arranged as paired spray holes.
Um eine möglichst einfache und kostengünstige Herstellbarkeit zu ermöglichen, sind die Spritzlöcher vorzugsweise in einer Spritzlochscheibe angeordnet. DieIn order to allow the simplest possible and cost-effective manufacturability, the injection holes are preferably arranged in a spray perforated disk. The
Spritzlochscheibe kann dann einfach an der Einspritzvorrichtung befestigt werden. Spray hole disc can then be easily attached to the injector.
Zeichnung Nachfolgend werden unter Bezugnahme auf die begleitende Zeichnung bevorzugte Ausführungsbeispiele der Erfindung im Detail beschrieben. In der Zeichnung ist: drawing Hereinafter, preferred embodiments of the invention will be described in detail with reference to the accompanying drawings. In the drawing is:
Figur 1 eine Draufsicht einer Spritzlochgeometrie eines Figure 1 is a plan view of a spray hole geometry of a
Kraftstoffeinspritzventils gemäß einem ersten Ausführungsbeispiel der Erfindung,  Fuel injection valve according to a first embodiment of the invention,
Figur 2 eine Schnittansicht entlang der Linie II-II von Figur 1 , FIG. 2 shows a sectional view along the line II-II of FIG. 1,
Figur 3 eine schematische Schnittansicht entlang der Linie III-III, und Figure 3 is a schematic sectional view taken along the line III-III, and
Figur 4 bis 10 Draufsichten von Spritzlochgeometrien gemäß weiteren Figures 4 to 10 are plan views of injection hole geometries according to further
Ausführungsbeispielen der Erfindung.  Embodiments of the invention.
Ausführungsformen der Erfindung Embodiments of the invention
Nachfolgend wird unter Bezugnahme auf die Figuren 1 bis 3 ein Hereinafter, with reference to Figures 1 to 3 a
Kraftstoffeinspritzventil mit einer Spritzlochscheibe 2 gemäß einem ersten Ausführungsbeispiel der Erfindung im Detail beschrieben. Fuel injection valve with a spray perforated disk 2 according to a first embodiment of the invention described in detail.
Wie aus der Schnittansicht von Figur 2 und 3 ersichtlich ist, umfasst das Einspritzventil 1 eine Spritzlochscheibe 2, welche an einem Ventilsitz 4 angeordnet ist. Kraftstoff wird für eine Einspritzung durch eine Öffnung 4a im Ventilsitz 4 in einen trichterförmigen, sich weitenden Einströmraum 5 zugeführt und dort zu den Spritzlöchern geführt. In Figur 2 ist die Strömung des Kraftstoffs zu den Spritzlöchern durch die Pfeile A, B, C angedeutet. As can be seen from the sectional view of FIGS. 2 and 3, the injection valve 1 comprises a spray perforated disk 2, which is arranged on a valve seat 4. Fuel is supplied for injection through an opening 4a in the valve seat 4 in a funnel-shaped, expanding inflow space 5 and guided there to the spray holes. In Figure 2, the flow of the fuel to the spray holes indicated by the arrows A, B, C.
Wie aus Figur 1 ersichtlich ist, umfasst die Spritzlochscheibe 2 insgesamt sechs Spritzlöcher, nämlich ein erstes Spritzloch 1 1 , ein zweites Spritzloch 12, ein drittes Spritzloch 13, ein viertes Spritzloch 14, ein fünftes Spritzloch 15 und ein sechstes Spritzloch 16. Dabei sind das erste und das zweite Spritzloch 1 1 , 12 sowie das dritte und das vierte Spritzloch 13, 14 als Spritzlochpaar jeweils relativ nah zueinander angeordnet. Die Spritzlöcher 1 1 , 12, 13, 14, 15, 16 sind zylindrisch und weisen alle jeweils den gleichen Durchmesser auf. In Figur 1 ist aus Übersichtlichkeitsgründen lediglich der erste Durchmesser D1 des ersten Spritzlochs und der Durchmesser D2 des zweiten Spritzlochs eingezeichnet, wobei die zylindrischen Spritzlöcher jeder Draufsicht von Figur 1 ovalförmig erscheinen. Ein Abstand 3 zwischen dem ersten Spritzloch 1 1 und dem zweiten Spritzloch 12 entspricht dabei dem Durchmesser D1 bzw. D2 der beiden As can be seen from Figure 1, the spray perforated disk 2 comprises a total of six injection holes, namely a first injection hole 1 1, a second injection hole 12, a third injection hole 13, a fourth injection hole 14, a fifth injection hole 15 and a sixth injection hole 16. It is first and the second injection hole 1 1, 12 and the third and the fourth injection hole 13, 14 arranged as a spray hole pair each relatively close to each other. The injection holes 1 1, 12, 13, 14, 15, 16 are cylindrical and all each have the same diameter. In FIG. 1, for reasons of clarity, only the first diameter D1 of the first is shown Plotted injection hole and the diameter D2 of the second injection hole, the cylindrical injection holes of each plan view of Figure 1 appear oval-shaped. A distance 3 between the first injection hole 1 1 and the second injection hole 12 corresponds to the diameter D1 or D2 of the two
Spritzlöcher. Somit sind das erste Spritzloch 1 1 und das zweite Spritzloch 12 relativ nah beieinander angeordnet, wodurch sich die Strömung an einer Einströmseite 2a der Spritzlochscheibe 2 gegenseitig beeinflusst. Alternativ können sich die Spritzlöcher in Strömungsrichtung konisch aufweiten oder auch verjüngen oder auch unterschiedliche Durchmesser aufweisen, wobei beliebige Kombinationen möglich sind. Spiracles. Thus, the first injection hole 1 1 and the second injection hole 12 are arranged relatively close to each other, whereby the flow on one inflow side 2 a of the spray orifice plate 2 mutually influenced. Alternatively, the spray holes can conically widen or taper or also have different diameters in the flow direction, wherein any combinations are possible.
Figur 3 zeigt eine Schnittansicht durch das erste und zweite Spritzloch 1 1 und 12. Das Bezugszeichen 1 1 a bezeichnet dabei eine Spritzlochachse des ersten Spritzlochs 1 1 und das Bezugszeichen 12a bezeichnet eine zweite Figure 3 shows a sectional view through the first and second injection hole 1 1 and 12. The reference numeral 1 1 a designates a spray hole axis of the first injection hole 1 1 and the reference numeral 12a denotes a second
Spritzlochachse des zweiten Spritzlochs 12. Das erste Spritzloch 1 1 und das zweite Spritzloch 12 sind in unterschiedlichen Richtungen angeordnet und weisen ferner unterschiedliche Neigungswinkel auf. Der Neigungswinkel der Spritzlöcher ist dabei jeweils derjenige Winkel, welcher an der Einströmseite 2a den kleinsten Winkel mit einer die Spritzlochöffnung umfassenden Ebene bildet. In Figur 3 ist der Neigungswinkel des ersten Spritzlochs mit bezeichnet und derSpray hole axis of the second injection hole 12. The first injection hole 1 1 and the second injection hole 12 are arranged in different directions and also have different angles of inclination. The angle of inclination of the injection holes is in each case the one angle which forms the smallest angle on the inflow side 2a with a plane comprising the injection hole opening. In Figure 3, the inclination angle of the first injection hole is denoted by and
Neigungswinkel des zweiten Spritzlochs 12 mit ß, wobei ca. 45° beträgt und ß ca. 70°. Inclination angle of the second injection hole 12 with ß, which is about 45 ° and ß about 70 °.
Ferner ist in Figur 1 und 3 mit den Pfeilen C die Zuströmung des Kraftstoffs zu den Spritzlöchern 1 1 , 12 dargestellt. Die Pfeile C deuten dabei die Further, in Figures 1 and 3 with the arrows C, the inflow of the fuel to the spray holes 1 1, 12 is shown. The arrows C indicate the
Hauptströmungsrichtung des Kraftstoffs an. Hierbei wird der Kraftstoff zum ersten Spritzloch 1 1 in einem Einströmwinkel γ zugeführt und am zweiten Spritzloch 12 in einem Einströmwinkel δ. Dabei ist eine Summe des Neigungswinkels und des Einströmwinkels γ am ersten Spritzloch 1 1 ca. 85° und somit kleiner als 90°. Die Summe des Einströmwinkels δ und des Neigungswinkels ß am zweiten Main flow direction of the fuel on. Here, the fuel is supplied to the first injection hole 1 1 in an inflow γ and the second injection hole 12 in an inflow δ. In this case, a sum of the inclination angle and the inflow angle γ at the first injection hole 1 1 is about 85 ° and thus smaller than 90 °. The sum of the inflow angle δ and the inclination angle ß on the second
Spritzloch 12 ist ca. 85°. Dadurch, dass die Summe von Neigungswinkel und Einströmwinkel an jedem Spritzloch kleiner als 90° ist, kann eine relativ flache Anströmung der Spritzlöcher erreicht werden. Ferner, wie aus Figur 1 ersichtlich ist, wird durch die enge Anordnung des ersten und zweiten Spritzlochs 1 1 , 12 eine verstärkte einseitige Lochanstromung für jedes Spritzloch erreicht. In Figur 1 sind die Anströmungen der einzelnen Spritzlöcher durch die Pfeile angedeutet, wobei die Länge der Pfeile der Stärke der Anströmung entspricht. Hierbei ist die Hauptanströmung zu den Spritzlöchern jeweils mit dem Buchstaben C gekennzeichnet. Geringere einströmende Kraftstoffmengen sind mit den Pfeilen D und E gekennzeichnet. Spray hole 12 is about 85 °. Because the sum of the angle of inclination and the inflow angle at each injection hole is less than 90 °, a relatively flat flow of the injection holes can be achieved. Further, as is apparent from Figure 1, is achieved by the close arrangement of the first and second spray hole 1 1, 12 a reinforced one-sided Lochanstromung for each injection hole. In Figure 1, the flow of the individual injection holes are indicated by the arrows, wherein the length of the arrows corresponds to the magnitude of the flow. Here, the main flow to the spray holes is marked with the letter C. Lower inflowing fuel quantities are indicated by the arrows D and E.
Wie weiter aus Figur 1 ersichtlich ist, ist ein Lochabstandswinkel ε zwischen dem ersten Spritzloch 1 1 und dem zweiten Spritzloch 12 ca. 25°. Der As can be seen further from FIG. 1, a hole spacing angle ε between the first injection hole 11 and the second injection hole 12 is approximately 25 °. Of the
Lochabstandswinkel ε wird dabei von einem Mittelpunkt M der Spritzlochscheibe 2 aus definiert. Alle Spritzlöcher 1 1 , 12, 13, 14, 15 und 16 liegen dabei auf einem gemeinsamen Kreisumfang K. Alternativ können die Spritzlöcher auch nicht auf einem gemeinsamen Kreisumfang liegen. Hole distance angle ε is defined by a center M of the spray hole 2 from. All spray holes 1 1, 12, 13, 14, 15 and 16 lie on a common circumference K. Alternatively, the injection holes can not lie on a common circumference.
Die paarweise Anordnung von Spritzlöchern mit relativ geringem Abstand ermöglicht somit eine verstärkte einseitige Spritzlochanströmung. Besonders bevorzugt ist diese Anströmung dabei entgegen einer Neigungsrichtung desThe paired arrangement of spray holes with a relatively small distance thus allows an increased one-sided spray hole flow. Particularly preferably, this flow is contrary to a direction of inclination of the
Spritzloches, so dass ein möglichst kleiner Winkel zwischen der Spray holes, allowing the smallest possible angle between the
Hauptanströmung des Spritzlochs und der Spritzlochachse realisiert ist. Dies ermöglicht eine sehr gute Kraftstoffaufbereitung. Ferner sei angemerkt, dass die Spritzlochachsen der Spritzlöcher derart angeordnet sind, dass sich die erzeugten Spray-Strahlen im Einspritzraum nicht treffen. Dies stellt eine möglichst weite Verbreitung der Kraftstofftröpfchen im Einspritzraum ohne Überschneidungen sicher. Eine Dicke der Spritzlochscheibe 2 entspricht dabei ungefähr einem Durchmesser der Spritzlöcher. Main flow of the injection hole and the injection hole axis is realized. This allows a very good fuel conditioning. It should also be noted that the injection hole axes of the injection holes are arranged such that the spray jets generated do not meet in the injection space. This ensures the widest possible spread of the fuel droplets in the injection space without overlaps. A thickness of the spray perforated disk 2 corresponds approximately to a diameter of the injection holes.
Wie weiter aus Figur 1 ersichtlich ist, ist die Hauptanströmung des fünften und sechsten Spritzlochs 15, 16 aufgrund der Neigung der Spritzlochachsen 15a und 16a nach innen sowie der Form des Einströmraums 5 hauptsächlich von außen. Im Gegensatz dazu ist die Hauptanströmung bei den paarweise angeordneten Spritzlöchern 1 1 , 12 sowie 13, 14 im Wesentlichen in einem mittleren Bereich von der Außenseite des Spritzlochpaares. An den inneren Bereichen der Spritzlöcher ist eine relativ geringe Anströmung vorhanden. Weiterhin ist der Winkel der Spritzlochachse unterschiedlich zum Hauptanströmwinkel, was zu einem zusätzlichen Prall im Spritzloch führt. Hierdurch wird der durch das Spritzloch erzeugte Strahl stärker zu einem Hohlkegel deformiert, was die1, the main flow of the fifth and sixth spray holes 15, 16 is mainly due to the inclination of the injection hole axes 15a and 16a inwardly and the shape of the inflow space 5 mainly from the outside. In contrast, the main flow is in the paired spray holes 1 1, 12 and 13, 14 substantially in a central region from the outside of the injection hole pair. At the inner areas of the injection holes a relatively small flow is present. Furthermore, the angle of the injection hole axis is different to Hauptanströmwinkel, resulting in an additional impact in the spray hole. As a result, the jet generated by the injection hole is deformed more to a hollow cone, which the
Kraftstoffaufbereitung weiter verbessert. Beispielsweise beträgt der Spritzlochwinkel am ersten Spritzloch ca. 45° und der Hauptanströmwinkel γ beträgt ca. 35°. Der Unterschied zuwischen dem Hauptanströmwinkel γ und dem Neigungswinkel ist vorzugsweise gleich oder größer 10°. Fuel treatment further improved. For example, the Spray hole angle at the first injection hole about 45 ° and the main flow angle γ is about 35 °. The difference between the main flow angle γ and the tilt angle is preferably equal to or greater than 10 °.
Nachfolgend werden weitere Ausführungsbeispiele unter Bezugnahme auf die Figuren 4 bis 10 im Detail beschrieben, wobei gleiche bzw. funktional gleiche Teile mit den gleichen Bezugszeichen wie im ersten Ausführungsbeispiel bezeichnet sind. Die in den Figuren 4 bis 10 eingezeichneten Pfeile an den Spritzlöchern geben dabei jeweils die Neigungsrichtungen der Spritzlöcher an, wobei die Figuren 4 bis 10 jeweils eine Draufsicht auf die Einströmseiten 2a der Spritzlochscheiben 2 darstellen. In the following, further exemplary embodiments are described in detail with reference to FIGS. 4 to 10, wherein identical or functionally identical parts are designated by the same reference numerals as in the first exemplary embodiment. The arrows on the spray holes shown in FIGS. 4 to 10 indicate the directions of inclination of the spray holes, wherein FIGS. 4 to 10 each show a plan view of the inflow sides 2 a of the spray perforated disks 2.
Bei dem in Figur 4 gezeigten zweiten Ausführungsbeispiel sind insgesamt acht Spritzlöcher 1 1 bis 18 vorgesehen, wobei zwei Paare von Spritzlöchern 1 1 , 12 und 13, 14 mit einem Abstand 3 angeordnet sind, welcher einen maximalen Öffnungsrandabstand der Spritzlöcher an der Einströmseite entspricht. Wie aus Figur 4 ersichtlich ist, sind die Einspritzlöcher in diesem Ausführungsbeispiel zylindrisch ausgebildet und aufgrund der Neigung bilden die zylindrischen Spritzlöcher an der Oberfläche der Spritzlochscheibe Ovale, so dass der Abstand 3 einer Längsachse des Ovals entspricht. In the second embodiment shown in Figure 4 a total of eight spray holes 1 1 to 18 are provided, wherein two pairs of spray holes 1 1, 12 and 13, 14 are arranged at a distance 3, which corresponds to a maximum opening edge distance of the injection holes on the inflow side. As can be seen from FIG. 4, the injection holes in this exemplary embodiment are cylindrical, and because of the inclination, the cylindrical injection holes on the surface of the spray perforated disc form ovals, so that the distance 3 corresponds to a longitudinal axis of the oval.
Die Mittelpunkte der Spritzlöcher 1 1 bis 18 liegen alle auf einem gemeinsamen Kreisumfang K. Ferner sind die Spritzrichtungen der Spritzlöcher derart gewählt, dass lediglich zwei Richtungen vorhanden sind. Dabei sind bei den paarweise angeordneten Spritzlöchern 1 1 und 12 sowie 13 und 14 die Spritzrichtungen derart gewählt, dass sie einander entgegengesetzt sind (vgl. Figur 4). The centers of the injection holes 1 1 to 18 are all on a common circumference K. Further, the injection directions of the injection holes are chosen such that only two directions are present. Here, in the paired spray holes 1 1 and 12 and 13 and 14, the injection directions are chosen such that they are opposite to each other (see Figure 4).
Beim dritten Ausführungsbeispiel von Figur 5 sind insgesamt sechs Spritzlöcher 1 1 bis 16 vorgesehen, wobei die Spritzlöcher ebenfalls zylindrisch ausgebildet sind. Die Mittelpunkte der Spritzlöcher liegen auf einem gemeinsamen In the third embodiment of Figure 5 a total of six injection holes 1 1 to 16 are provided, wherein the injection holes are also formed cylindrically. The centers of the injection holes lie on a common
Kreisumfang K. Die Spritzlöcher sind dabei in zueinander unterschiedlichen Richtungen geneigt, so dass an der Abströmseite, wie durch die Pfeile angedeutet, Kraftstoff in verschiedenste Richtungen austritt. Circumference K. The injection holes are inclined in mutually different directions, so that at the downstream side, as indicated by the arrows, fuel exits in various directions.
Bei dem in Figur 6 gezeigten Ausführungsbeispiel sind lediglich vier Spritzlöcher 1 1 bis 14 angeordnet. Die Spritzlöcher liegen wieder auf einem Kreisumfang K und die Öffnungsrichtungen der Spritzlöcher sind so gewählt, dass die In the embodiment shown in Figure 6, only four injection holes 1 1 to 14 are arranged. The injection holes are again on a circumference K and the opening directions of the injection holes are selected so that the
Spritzlochachsen der paarweisen Spritzlöcher um einen Winkel γ um ca. 140° einander entgegengesetzt gerichtet sind. Somit sind bei diesem Spray hole axes of the pairwise injection holes are directed by an angle γ by about 140 ° opposite to each other. Thus, in this
Ausführungsbeispiel alle vorhandenen Spritzlöcher paarweise angeordnet, was zu einer besonders guten Kraftstoffaufbereitung führt. Embodiment all existing spray holes arranged in pairs, resulting in a particularly good fuel processing.
Das in Figur 7 gezeigte fünfte Ausführungsbeispiel entspricht im Wesentlichen dem dritten Ausführungsbeispiel von Figur 5, wobei im Unterschied dazu die Spritzrichtungen der Spritzlöcher jeweils nur in zwei Richtungen gerichtet sind. Diese Richtungen sind einander um 180° entgegengesetzt, wobei von den sechs angeordneten Spritzlöchern vier in zwei Spritzlochpaaren angeordnet sind und die Spritzlöcher 1 1 , 12 und 13, 14 in jeweils entgegengesetzte Richtungen gerichtet sind. Das in Figur 8 gezeigte sechste Ausführungsbeispiel weist ebenfalls insgesamt sechs Spritzlöcher 1 1 bis 16 auf, wobei die Spritzlöcher 1 1 und 12 sowie 13 und 14 jeweils mit einem Abstand 3 zueinander angeordnet sind. In diesem The fifth embodiment shown in Figure 7 substantially corresponds to the third embodiment of Figure 5, in contrast to the injection directions of the injection holes are directed in each case only in two directions. These directions are opposite to each other by 180 °, of the six arranged spray holes four are arranged in two spray-hole pairs and the spray holes 1 1, 12 and 13, 14 are directed in opposite directions. The sixth embodiment shown in Figure 8 also has a total of six injection holes 1 1 to 16, wherein the injection holes 1 1 and 12 and 13 and 14 are each arranged at a distance 3 to each other. In this
Ausführungsbeispiel ist der Abstand 3 gleich dem zweifachen maximalen Öffnungsrandabstand der Spritzlöcher 1 1 , 12, 13, 14. Da die zylindrischen Spritzlöcher in diesem Ausführungsbeispiel wieder zur axialen Richtung geneigt sind, ist der maximale Öffnungsrandabstand die Hauptachse der Ovale der Spritzlöcher. Die Einspritzrichtung aller Spritzlöcher 1 1 bis 16 ist dabei nach innen gerichtet, so dass eine hohe Kraftstoffkonzentration in einem mittleren Bereich eines Einspritzraums erhalten wird. Embodiment, the distance 3 is equal to twice the maximum opening edge distance of the injection holes 1 1, 12, 13, 14. Since the cylindrical injection holes are inclined in this embodiment again to the axial direction, the maximum opening edge distance is the major axis of the ovals of the injection holes. The injection direction of all injection holes 1 1 to 16 is directed inwards, so that a high fuel concentration is obtained in a central region of an injection space.
Das in Figur 9 gezeigte siebte Ausführungsbeispiel entspricht im Wesentlichen dem in Figur 8 gezeigten Ausführungsbeispiel, wobei die Einspritzrichtungen der Spritzlöcher 1 1 bis 16 unterschiedlich sind. Die Einspritzrichtung der Spritzlöcher 1 1 und 12 ist nach außen gerichtet. The seventh embodiment shown in FIG. 9 substantially corresponds to the exemplary embodiment shown in FIG. 8, wherein the injection directions of the injection holes 11 to 16 are different. The injection direction of the injection holes 1 1 and 12 is directed to the outside.
Figur 10 zeigt ein achtes Ausführungsbeispiel der Erfindung, welches im FIG. 10 shows an eighth embodiment of the invention, which is shown in FIG
Wesentlichen dem in Figur 6 gezeigten entspricht. Im Unterschied dazu ist ein Abstand 3 zwischen dem ersten und zweiten Spritzloch 1 1 , 12 und dem dritten und vierten Spritzloch 13, 14 gleich einem zweifachen Öffnungsrandabstand der Spritzlöcher 1 1 , 12 bzw. 13, 14. Ferner sind die beiden Spritzlochpaare einander entgegengesetzt angeordnet und auch die Einspritzrichtungen der jeweiligen Einspritzlöcher gehen im Wesentlichen nach Innen. Substantially corresponds to that shown in Figure 6. In contrast, a distance 3 between the first and second injection hole 1 1, 12 and the third and fourth injection hole 13, 14 equal to a double opening edge distance of the injection holes 1 1, 12 and 13, 14. Further, the two injection hole pairs each other arranged opposite and also the injection directions of the respective injection holes go substantially inward.
Zu allen beschriebenen Ausführungsformen sei angemerkt, dass wenigstens zwei Spritzlöcher ein Spritzlochpaar bilden, welches in einem maximalen Abstand 3 eines doppelten Öffnungsrandabstands voneinander entfernt angeordnet ist. Hierdurch wird eine positive gegenseitige Beeinflussung des Strömungsverhaltens an der Einströmseite 2a erreicht, wodurch sich eine verbesserte Spray-Aufbereitung ergibt. Die Form (Kreisform, Ellipse, etc.), die Richtung des Spritzlochachse, der Neigungswinkel der Spritzlochachse, die Innenform (zylindrisch, konisch, sich verjüngend, etc.) der Spritzlöcher können dabei verschieden gewählt werden, wobei für die Spritzlöcher des For all described embodiments, it should be noted that at least two spray holes form a spray hole pair, which is arranged at a maximum distance 3 of a double opening edge distance from each other. As a result, a positive mutual influence of the flow behavior is achieved on the inflow side 2a, resulting in an improved spray conditioning. The shape (circular shape, ellipse, etc.), the direction of the injection hole axis, the inclination angle of the injection hole axis, the inner shape (cylindrical, conical, tapered, etc.) of the injection holes can be chosen differently, wherein for the injection holes of
Spritzlochpaares die Bedingung gilt, dass der Abstand 3 zwischen den beiden Spritzlöchern kleiner als der zweifache, maximale Offnungsrandabstand an der Einströmseite ist und die Spritzlochachsen der beiden Spritzlöcher in zueinander unterschiedlichen Richtungen angeordnet sind, um zu vermeiden, dass sich die erzeugten Kraftstoff-Sprays überschneiden. Spray hole pair the condition is that the distance 3 between the two spray holes is smaller than twice the maximum opening edge distance on the inflow side and the injection hole axes of the two injection holes are arranged in mutually different directions, to avoid that the generated fuel sprays overlap.

Claims

Ansprüche claims
1 . Einspritzvorrichtung zur Einspritzung von Fluid, insbesondere Kraftstoff, umfassend: 1 . Injection device for injecting fluid, in particular fuel, comprising:
wenigstens ein erstes Spritzloch (1 1 ) und ein zweites Spritzloch (12), welche ein Spritzlochpaar bilden,  at least a first injection hole (1 1) and a second injection hole (12), which form a spray hole pair,
wobei das erste und zweite Spritzloch (1 1 , 12) derart angeordnet ist, dass ein Abstand (3) zwischen den beiden Spritzlöchern (1 1 , 12) kleiner oder gleich ist, wie ein zweifacher maximaler  wherein the first and second spray holes (1 1, 12) is arranged such that a distance (3) between the two spray holes (1 1, 12) is less than or equal to, such as a double maximum
Öffnungsrandabstand (D1 , D2) an einer Einströmseite (2a) der beiden Spritzlöcher (1 1 , 12), und  Opening edge distance (D1, D2) on an inflow side (2a) of the two injection holes (1 1, 12), and
wobei Spritzlochachsen (1 1 a, 12a) des ersten und zweiten Spritzlochs (1 1 , 12) in zueinander unterschiedlichen Richtungen angeordnet sind.  wherein injection hole axes (1 1 a, 12 a) of the first and second injection holes (1 1, 12) are arranged in mutually different directions.
2. Einspritzvorrichtung nach Anspruch 1 , dadurch gekennzeichnet, dass der Abstand (3) zwischen dem ersten Spritzloch (1 1 ) und dem zweiten 2. Injection device according to claim 1, characterized in that the distance (3) between the first injection hole (1 1) and the second
Spritzloch (12) in einem Bereich von 0,5 bis 1 ,5 des maximalen  Spray hole (12) in a range of 0.5 to 1, 5 of the maximum
Öffnungsrandabstands des ersten und/oder zweiten Spritzlochs ist und vorzugsweise, dass der Abstand (3) gleich dem maximalen  Opening edge distance of the first and / or second injection hole is and preferably that the distance (3) equal to the maximum
Öffnungsrandabstand des ersten und/oder zweiten Spritzlochs ist.  Opening edge distance of the first and / or second spray hole is.
3. Einspritzvorrichtung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Spritzlochachsen (1 1 a, 12a) des ersten und zweiten Spritzlochs (1 1 , 12) in unterschiedlichen Neigungswinkeln ( , ß) angeordnet sind. 3. Injection device according to one of the preceding claims, characterized in that the injection hole axes (1 1 a, 12 a) of the first and second injection hole (1 1, 12) at different angles of inclination (, ß) are arranged.
4. Einspritzvorrichtung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass jedes der Spritzlöcher (1 1 , 12) eine Spritzlochachse aufweist, welche gleiche Neigungswinkel ( , ß) aufweisen, jedoch in unterschiedliche Richtungen gerichtet sind. Einspritzvorrichtung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass wenigstens vier Spritzlöcher (1 1 , 12, 13, 14) vorgesehen sind, wobei jeweils zwei Spritzlöcher ein Spritzlochpaar bilden. 4. Injection device according to one of the preceding claims, characterized in that each of the injection holes (1 1, 12) has a spray hole axis, which have the same inclination angle (, ß), but are directed in different directions. Injection device according to one of the preceding claims, characterized in that at least four injection holes (1 1, 12, 13, 14) are provided, wherein each two injection holes form a spray hole pair.
Einspritzvorrichtung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass wenigstens eines der Spritzlöcher eine sich erweiternde Form, insbesondere eine sich konisch erweiternde Form aufweist. Injection device according to one of the preceding claims, characterized in that at least one of the injection holes has an expanding shape, in particular a conically widening shape.
Einspritzvorrichtung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Spritzlöcher an der Einströmseite (2a) eine Kreisform aufweisen, wobei der maximale Offnungsrandabstand an der Einströmseite (2a) ein Durchmesser des Spritzlochs ist, oder dass die Spritzlöcher an der Einströmseite eine ovale Form, insbesondere eine Ellipsenform aufweisen, wobei der maximale Offnungsrandabstand an der Einströmseite (2a) als größte Achse der ovalen Form definiert ist. Injection device according to one of the preceding claims, characterized in that the injection holes on the inflow side (2a) have a circular shape, wherein the maximum opening edge distance on the inflow side (2a) is a diameter of the injection hole, or that the injection holes on the inflow side of an oval shape, in particular have an elliptical shape, wherein the maximum opening edge distance at the inflow side (2a) is defined as the largest axis of the oval shape.
Einspritzvorrichtung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass das erste und zweite Spritzloch (1 1 , 12) auf einem Kreisumfang (K) angeordnet sind und die Spritzlochachsen (1 1 a, 12a) in einem Lochabstandswinkel (ε ) von 20° bis 60°, vorzugsweise ungefähr 25°, angeordnet sind. Injection device according to one of the preceding claims, characterized in that the first and second injection hole (1 1, 12) on a circumference (K) are arranged and the injection hole axes (1 1 a, 12 a) in a hole spacing angle (ε) of 20 ° to 60 °, preferably about 25 °, are arranged.
Einspritzvorrichtung nach einem der vorhergehenden Ansprüche, ferner umfassend einen trichterförmigen Einströmraum (5), welcher an einer Einströmseite (2a) der Spritzlöcher angeordnet ist. Injection device according to one of the preceding claims, further comprising a funnel-shaped inflow space (5), which is arranged on an inflow side (2a) of the injection holes.
Einspritzvorrichtung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass eine Hauptströmung (C) des Fluids zu jedem Injection device according to one of the preceding claims, characterized in that a main flow (C) of the fluid to each
Spritzloch in einem Einströmwinkel (γ, δ) derart zugeführt wird, dass eine Summe aus dem Einströmwinkel (γ, δ) und einem Neigungswinkel ( , ß) der Spritzlochachsen (1 1 a, 12a) kleiner oder gleich 90° ist. Spray hole in an inflow angle (γ, δ) is supplied such that a sum of the inflow angle (γ, δ) and an inclination angle (, ß) of the injection hole axes (1 1 a, 12a) is less than or equal to 90 °.
Einspritzvorrichtung nach einem der Ansprüche 5 bis 10, umfassend ein drittes Spritzloch (13) und ein viertes Spritzloch (14), wobei das dritte und vierte Spritzloch (13, 14) derart angeordnet ist, dass ein Abstand (3) zwischen dem dritten und vierten Spritzloch kleiner oder gleich ist wie ein zweifacher maximaler Offnungsrandabstand (D1 , D2) an der Einströmseite (2a) des dritten und vierten Spritzlochs und wobei Spritzlochachsen des dritten und vierten Spritzlochs (13, 14) in zueinander unterschiedlichen Richtungen angeordnet sind, wobei das dritte und vierte Spritzloch gegenüber dem ersten und zweiten Spritzloch (1 1 , 12) angeordnet ist. Injection device according to one of claims 5 to 10, comprising a third injection hole (13) and a fourth injection hole (14), wherein the third and fourth injection hole (13, 14) is arranged such that a distance (3) between the third and fourth injection hole is less than or equal to a double maximum opening edge distance (D1, D2) on the inflow side (2a) of the third and fourth injection hole and Spray hole axes of the third and fourth injection hole (13, 14) are arranged in mutually different directions, wherein the third and fourth injection hole with respect to the first and second injection hole (1 1, 12) is arranged.
12. Einspritzvorrichtung nach Anspruch 1 1 , ferner umfassend ein fünftes 12. Injection device according to claim 1 1, further comprising a fifth
Spritzloch (15) und ein sechstes Spritzloch (16), welche einander gegenüberliegend angeordnet sind und deren Spritzlochachsen (15a, 16a) in unterschiedlichen Richtungen angeordnet sind.  Spray hole (15) and a sixth injection hole (16), which are arranged opposite to each other and whose injection hole axes (15a, 16a) are arranged in different directions.
Einspritzvorrichtung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Spritzlöcher (1 1 , 12, 13, 14, 15, 16) in einer Spritzlochscheibe (2) angeordnet sind. Injection device according to one of the preceding claims, characterized in that the injection holes (1 1, 12, 13, 14, 15, 16) are arranged in a spray perforated disc (2).
EP11724597.7A 2010-07-22 2011-05-27 Injection device having improved spray preparation Active EP2596230B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102010031653A DE102010031653A1 (en) 2010-07-22 2010-07-22 Injection device with improved spray treatment
PCT/EP2011/058770 WO2012010356A1 (en) 2010-07-22 2011-05-27 Injection device having improved spray preparation

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EP2596230A1 true EP2596230A1 (en) 2013-05-29
EP2596230B1 EP2596230B1 (en) 2016-12-07

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EP (1) EP2596230B1 (en)
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DE102011118299A1 (en) * 2011-11-10 2013-05-16 Daimler Ag injection
JP2016530135A (en) * 2013-09-06 2016-09-29 スリーエム イノベイティブ プロパティズ カンパニー Injection molded nozzle preform with undercut microforms
EP3376019B1 (en) * 2015-11-10 2023-01-04 Nissan Motor Co., Ltd. Method for controlling internal combustion engine
JP6654875B2 (en) * 2015-11-26 2020-02-26 日立オートモティブシステムズ株式会社 Fuel injection valve
US9964088B2 (en) * 2016-01-18 2018-05-08 Ford Global Technologies, Llc Multi-hole fuel injector with sequential fuel injection
DE102016222606A1 (en) * 2016-11-17 2018-05-17 Robert Bosch Gmbh Injection valve for internal combustion engines

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JP3837283B2 (en) * 2000-10-24 2006-10-25 株式会社ケーヒン Fuel injection valve
JP3865603B2 (en) * 2001-07-13 2007-01-10 株式会社日立製作所 Fuel injection valve
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WO2012010356A1 (en) 2012-01-26
EP2596230B1 (en) 2016-12-07
US20130181068A1 (en) 2013-07-18

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