EP0263304B1 - Fuel injection pump for internal combustion engines - Google Patents

Fuel injection pump for internal combustion engines Download PDF

Info

Publication number
EP0263304B1
EP0263304B1 EP87112919A EP87112919A EP0263304B1 EP 0263304 B1 EP0263304 B1 EP 0263304B1 EP 87112919 A EP87112919 A EP 87112919A EP 87112919 A EP87112919 A EP 87112919A EP 0263304 B1 EP0263304 B1 EP 0263304B1
Authority
EP
European Patent Office
Prior art keywords
pump
recess
control slide
control
space
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.)
Expired - Lifetime
Application number
EP87112919A
Other languages
German (de)
French (fr)
Other versions
EP0263304A2 (en
EP0263304A3 (en
Inventor
Josef Güntert
Johann Ing. Grad. Warga
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 EP0263304A2 publication Critical patent/EP0263304A2/en
Publication of EP0263304A3 publication Critical patent/EP0263304A3/en
Application granted granted Critical
Publication of EP0263304B1 publication Critical patent/EP0263304B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • F02M59/00Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/20Varying fuel delivery in quantity or timing
    • F02M59/24Varying fuel delivery in quantity or timing with constant-length-stroke pistons having variable effective portion of stroke
    • 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
    • F02M55/00Fuel-injection apparatus characterised by their fuel conduits or their venting means; Arrangements of conduits between fuel tank and pump F02M37/00
    • F02M55/001Pumps with means for preventing erosion on fuel discharge
    • 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
    • F02M59/00Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/44Details, components parts, or accessories not provided for in, or of interest apart from, the apparatus of groups F02M59/02 - F02M59/42; Pumps having transducers, e.g. to measure displacement of pump rack or piston

Definitions

  • the invention is based on a fuel injection pump for internal combustion engines according to the generic preamble of the only claim.
  • the injection quantity and / or the start of injection and, in accordance with the set rotational position of the pump piston, the associated injection end is also determined by the axial position of the control slide.
  • the end of high-pressure injection - on the one hand, in terms of time as the injection end, on the other hand, as the end of high-pressure delivery that determines the injection quantity - is determined in that the control opening on the pump piston is exposed by the control slide, so that the fuel, which is under very high pressure, is discharged from the pump work chamber the relief channel and the control opening in the recess of the cylinder liner is controlled.
  • the deflected fuel jet has an extraordinarily high kinetic energy, which leads to a high load on the materials which the jet hits.
  • the pressures in the pump workspace of the pump can reach up to 1,300 bar.
  • the energy losses from the pump work room to the shutdown point are relatively low, since the injection is suddenly interrupted from the shutdown in order to ensure that the nozzle needle closes quickly.
  • This type of beam deflection has the disadvantage that the deflected beam, which is still under very high kinetic energy, either loads the signal box of the control slide or strikes the wall of the suction chamber, which, like the entire pump housing, consists of soft material, for example aluminum, the pump cylinder liner and the spool are made of hardened steel. The result is cavitation and erosion damage to the suction chamber wall of the pump housing and to the control parts in the suction chamber.
  • a further advantage is that the aprons are axially displaced with the control slide secured against twisting, so that there is always a sufficient passage cross-section between the gaps formed by the control slide and recess and the suction space. Furthermore, the opening of the recess is only provided radially on one side with respect to the cylinder liner longitudinal axis, so that the aprons are correspondingly only present at one end of the control slide which faces the suction chamber.
  • the rear wall of the recess, which is formed by the cylinder liner is thus made of hardened steel. so that the deflecting beam striking this cannot do any damage.
  • FIG. 1 shows a partial longitudinal section. by a fuel injection pump according to the invention and Fig. 2 shows a cross section along line II-II in Fig.1.
  • a cylinder liner 2 is inserted, in which a pump piston 3 is driven by means (not shown) for its reciprocating movement.
  • a recess 4 formed in the manner of a bag opening, which receives a control slide 5 which can be axially displaced on the pump piston 3.
  • the recess 4 has an access 6 via which the control slide 5 can be used.
  • an elongated slot 8 into which a lug 9 of the control slide 5 engages, whereby the control slide 5 can perform an axial movement and is secured against rotation.
  • control slide 5 takes place via a rotatable control rod 11, on which a driving member 12 with a head 13 can be tightened by a screw 14 and is therefore adjustable in the rotational position, the head 13 engaging in a transverse groove 15 of the control slide 5.
  • a plurality of such pump elements 2, 3 with control slides 5 are preferably arranged in series in the housing 1, which are then operated together by a control rod 11, the driving elements 12 of which correspond to the number of pump elements.
  • the control rod 11 and the entrainment members 12 are arranged in a pump suction chamber 16 which, as is not shown in more detail, is supplied with fuel under low pressure from a fuel tank via a feed pump.
  • the access 6 of the recess 4 of the pump cylinder 2 faces this suction chamber 16, so that there is an open connection between the recess 4 and the suction chamber 16.
  • the pump piston 3 assumes its bottom dead center position (UT), opening up suction openings 17 of the pump work chamber 18, which are connected to the pump suction chamber 16 via a channel 19 present in the pump cylinder liner 2 or a twist 21 on the cylinder liner 2 .
  • an oblique groove 22 and recess 23 are arranged, which are arranged as control openings in pairs on the pump piston 3 and are connected to one another via a transverse bore 24, which leads via a blind bore 25 to the pump work chamber 18.
  • These control openings namely the oblique grooves 22 and recesses 23, cooperate with two radial bores 26 of the control slide 5 serving as radial openings, the input edges 27 of these radial bores 26 serving as control edges towards the control openings, while the orifices 28 of these radial bores 26 on parallel side walls 29 the recess 4 are directed.
  • the space gaps 31 formed between the side walls 29 and the control slide 5 are covered toward the suction space 16 by aprons 32 arranged on the control slide 5, which have baffle surfaces 33 running perpendicular to the gap expansion.
  • the illustrated embodiment works as follows: In the illustrated UT position of the pump piston 3, the pump working chamber 18 is filled with fuel via the suction openings 17 and the channel 19 or the twist 21 from the pump suction chamber 16. Depending on the axial position of the control slide 5, part of the fuel supply can also take place via the recesses 23 or oblique grooves 22, the transverse bore 24 and the blind bore 25. During the delivery stroke of the pump piston 3, part of the fuel is first displaced from the pump working chamber 18 back into the suction chamber 16 via the supply channels, at least until the suction openings 17 are closed by the pump piston 3 and at the latest until the recesses 23 or Oblique grooves 22 are covered by the control slide 5.
  • the high pressure can develop in the pump work chamber 18 and the injection to the internal combustion engine can begin.
  • This injection is ended when the control openings, namely the oblique grooves 22, overlap with the radial bores 26 of the control slide 5.
  • the fuel which is under very high pressure, is now extracted from the pump working chamber 18 via the blind bore 25, the transverse bore 24, the oblique grooves 22 and the radial bores 26 are conveyed into the space gaps 31, with the control fuel jet being formed meets the opposite side walls 29.
  • the beam is reflected on these side walls 29 and partially strikes the rear wall 7, for the most part the impact surfaces 33 of the aprons 32, in order to then flow into the remaining spaces of the recess 4 above and below the control slide 5. From here, the fuel then reaches the suction chamber 16.
  • the aprons 32 present in the area of the access 6 to the recess 4 at the shoulders widening the control slide 5 and provided with the baffle surfaces 33 can either dive straight into the access 6 of the recess 4 or can remain outside the same, only through the baffle surfaces 33 must be achieved that the fuel jet is reflected for energy destruction.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Description

Die Erfindung geht aus von einer Kraftstoffeinspritzpumpe für Brennkraftmaschinen nach dem gattungsbildenden Oberbegriff des einzigen Patentanspruchs.The invention is based on a fuel injection pump for internal combustion engines according to the generic preamble of the only claim.

Bei derartigen schiebergesteuerten Kraftstoffeinspritzpumpen wird die Einspritzmenge und/oder der Spritzbeginn und entsprechend der eingestellten Drehlage des Pumpenkolbens auch das zugehörige Spritzende durch die axiale Lage des Steuerschiebers bestimmt. In jedem Fall wird aber das Ende der Hochdruckeinspritzung - einerseits zeitlich gesehen als Spritzende andererseits als einspritzmengenbestimmendes Ende der Hochdruckförderung - dadurch bestimmt, daß die auf dem Pumpenkolben vorhandene Steueröffnung vom Steuerschieber freigelegt wird, so daß der unter sehr hohem Druck stehende Kraftstoff aus dem Pumpenarbeitsraum über den Entlastungskanal und die Steueröffnung in die Ausnehmung der Zylinderbüchse abgesteuert wird. Bei dieser mittels Steuerkanten des Steuerschiebers durchgeführten Absteuerung weist der abgesteuerte Kraftstoffstrahl eine außerordentlich hohe kinetische Energie auf, die zu einer hohen Belastung der Werkstoffe führt, auf die der Strahl trifft. Immerhin können die Drücke im Pumpenarbeitsraum der Pumpe bis zu 1.300 bar erreichen. Die Energieverluste vom Pumpenarbeitsraum bis zur Absteuerstelle sind verhältnismäßig gering, da ab Absteuerung die Einspritzung schlagartig unterbrochen wird, um ein schnelles Düsennadelschließen sicherzustellen.In the case of such slide-controlled fuel injection pumps, the injection quantity and / or the start of injection and, in accordance with the set rotational position of the pump piston, the associated injection end is also determined by the axial position of the control slide. In any case, however, the end of high-pressure injection - on the one hand, in terms of time as the injection end, on the other hand, as the end of high-pressure delivery that determines the injection quantity - is determined in that the control opening on the pump piston is exposed by the control slide, so that the fuel, which is under very high pressure, is discharged from the pump work chamber the relief channel and the control opening in the recess of the cylinder liner is controlled. In this deactivation, which is carried out by means of control edges of the control slide, the deflected fuel jet has an extraordinarily high kinetic energy, which leads to a high load on the materials which the jet hits. After all, the pressures in the pump workspace of the pump can reach up to 1,300 bar. The energy losses from the pump work room to the shutdown point are relatively low, since the injection is suddenly interrupted from the shutdown in order to ensure that the nozzle needle closes quickly.

Bei einer solchen bekannten Kraftstoffeinspritzpumpe der gattungsgemäßen Bauart (DE-A-34 28 174) sind im Steuerschieber zwei als radiale Absteuerbohrungen ausgebildete Radialöffnungen vorhanden, durch die je eine als Steueröffnung auf dem Pumpenkolben angeordnete schräge Steuernut nach Zurücklegen des effektiven Einspritzhubes aufgesteuert wird. Der Absteuerstrahl schießt beim Aufsteuern durch diese Absteuerbohrungen auf die Seitenwände der Ausnehmung in der Zylinderbüchse. Da diese Wände nur in Spaltbreite von den Mündungen der Absteuerbohrungen entfernt sind, wird jeder Strahl vonder Wand in den Spalt hinein reflektiert und gelangt einesteils auf mindestens eine der Stirnseiten des Steuerschiebers, wodurch unerwünschte Kräfte in das zugehörige Stellwerk gelangen, und andernteils mit sehr hoher Energie in den Saugraum im Pumpengehäuse. Diese Art der Strahlablenkung hat den Nachteil, daß der noch unter sehr hoher kinetischer Energie stehende abgelenkte Strahl entweder das Stellwerk des Steuerschiebers belastet oder die Wand des Saugraums trifft, die, wie das ganze Pumpengehäuse, aus weichem Material, beispielsweise Aluminium besteht, wobei die Pumpenzylinderbüchse und der Steuerschieber aus gehärtetem Stahl bestehen. Die Folge sind Kavitations- und Erosionsschäden an der Saugraumwand des Pumpengehäuses und an den im Saugraum befindlichen Steuerungsteilen.In such a known fuel injection pump of the generic type (DE-A-34 28 174) there are two radial openings in the control slide designed as radial control bores, through which an inclined control groove arranged as a control opening on the pump piston is opened after the effective injection stroke has been completed. The pilot jet shoots through these pilot bores onto the side walls of the recess in the cylinder liner. Since these walls are only a gap away from the mouths of the pilot bores, each beam is reflected from the wall into the gap and reaches part of it on at least one of the end faces of the spool, causing undesirable forces to enter the associated signal box, and part with very high energy into the suction chamber in the pump housing. This type of beam deflection has the disadvantage that the deflected beam, which is still under very high kinetic energy, either loads the signal box of the control slide or strikes the wall of the suction chamber, which, like the entire pump housing, consists of soft material, for example aluminum, the pump cylinder liner and the spool are made of hardened steel. The result is cavitation and erosion damage to the suction chamber wall of the pump housing and to the control parts in the suction chamber.

Vorteile der ErfindungAdvantages of the invention

Bei der erfindungsgemäßen Kraftstoffeinspritzpumpe mit den kennzeichnenden Merkmalen des einzigen Patentanspruchs wird demgegenüber in vorteilhafter Weise erreicht, daß der Absteuerstrahl mehrfach reflektiert wird, nämlich von den Seitenwänden der Ausnehmung und des Steuerschiebers auf die Prallflächen der Schürzen und von diesen wieder zurück, so daß durch den relativ langen Weg in den Raumspalten die Strahlenergie nahezu vernichtet wird, bevor dann der Kraftstoff im wesentlichen oberhalb bzw. unterhalb der Schürzen zum Saugraum strömt. Durch eine solche mehrmalige Umlenkung im Bereich gehärteter Bauteile wird so viel Energie des austretenden Kraftstoffstrahls abgebaut, daß keine merklichen Karitationsschäden mehr an den benachbarten Wandungen des üblicherweise aus Aluminium bestehenden Pumpengehäuses auftreten. Ein weiterer Vorteil dabei ist, daß die Schürzen mit dem gegen Verdrehen gesicherten Steuerschieber axial verschoben werden und so stets ein ausreichender Durchtrittsquerschnitt zwischen den durch Steuerschieber und Ausnehmung gebildeten Spalten und dem Saugraum besteht. Des weiteren ist der Zugang der Ausnehmung in bezug auf die Zylinderbüchsenlängsachse radial nur einseitig vorgesehen so daß auch die Schürzen entsprechend nur an dem einen Ende des Steuerschiebers vorhanden sind, das dem Saugraum zugewandt ist. Die Rückwand der Ausnehmung, die durch die Zylinderbüchse gebildet wird, besteht somit aus gehärtetem Stahl. so daß der auf diese treffende Ablenkstrahl keinen Schaden anrichten kann.In the fuel injection pump according to the invention with the characterizing features of the single patent claim, on the other hand, it is advantageously achieved that the exhaust beam is reflected several times, namely from the side walls of the recess and the control slide on the baffles of the aprons and back again, so that by the relative long way in the gaps in the beam energy is almost destroyed before the fuel then essentially above or below the aprons to the suction chamber flows. Such repeated deflection in the area of hardened components dissipates so much energy from the emerging fuel jet that no noticeable damage to the adjacent walls of the pump housing, which is usually made of aluminum, occurs. A further advantage is that the aprons are axially displaced with the control slide secured against twisting, so that there is always a sufficient passage cross-section between the gaps formed by the control slide and recess and the suction space. Furthermore, the opening of the recess is only provided radially on one side with respect to the cylinder liner longitudinal axis, so that the aprons are correspondingly only present at one end of the control slide which faces the suction chamber. The rear wall of the recess, which is formed by the cylinder liner, is thus made of hardened steel. so that the deflecting beam striking this cannot do any damage.

Weitere Vorteile und vorteilhafte Ausgestaltungen der Erfindung sind der nachfolgenden Beschreibung und der Zeichnung entnehmbar.Further advantages and advantageous embodiments of the invention can be found in the following description and the drawing.

Zeichnungdrawing

Ein Ausführungsbeispiel des Gegenstandes der Erfindung ist in der Zeichnung dargestellt und im folgenden näher beschrieben. Es zeigen Fig. 1 einen Teillängsschnitt. durch eine erfindungsgemäße Kraftstoffeinspritzpumpe und Fig. 2 einen Querschnitt nach Linie II-II in Fig.1.An embodiment of the object of the invention is shown in the drawing and described in more detail below. 1 shows a partial longitudinal section. by a fuel injection pump according to the invention and Fig. 2 shows a cross section along line II-II in Fig.1.

Beschreibung des AusführungsbeispielsDescription of the embodiment

In einem nur teilweise gezeigten Pumpengehäuse 1 einer Kraftstoffeinspritzpumpe ist eine Zylinderbüchse 2 eingesetzt, in der ein Pumpenkolben 3 durch nicht dargestellte Mittel für seine hin- und hergehende Bewegung angetrieben wird. In der Zylinderbüchse 2 ist eine in Art einer Sacköffnung gebildete Ausnehmung 4 vorhanden, die einen auf dem Pumpenkolben 3 axial verschiebbaren Steuerschieber 5 aufnimmt. Die Ausnehmung 4 weist einen Zugang 6 auf, über den der Steuerschieber 5 einsetzbar ist. In der Rückwand 7 der Ausnehmung 4 ist ein Langsschlitz 8 vorhanden, in den eine Nase 9 des Steuerschiebers 5 greift, wodurch der Steuerschieber 5 eine Axialbewegung durchführen kann und gegen Verdrehen gesichert ist.In a pump housing 1 of a fuel injection pump, which is only partially shown, a cylinder liner 2 is inserted, in which a pump piston 3 is driven by means (not shown) for its reciprocating movement. In the cylinder liner 2 there is a recess 4 formed in the manner of a bag opening, which receives a control slide 5 which can be axially displaced on the pump piston 3. The recess 4 has an access 6 via which the control slide 5 can be used. In the rear wall 7 of the recess 4 there is an elongated slot 8 into which a lug 9 of the control slide 5 engages, whereby the control slide 5 can perform an axial movement and is secured against rotation.

Die axiale Betätigung des Steuerschiebers 5 erfolgt über eine verdrehbare Regelstange 11, auf der ein Mitnahmeglied 12 mit einem Kopf 13 durch eine Schraube 14 festspannbar und damit in der Drehlage verstellbar angeordnet ist, wobei der Kopf 13 in eine Quernut 15 des Steuerschiebers 5 greift.The axial actuation of the control slide 5 takes place via a rotatable control rod 11, on which a driving member 12 with a head 13 can be tightened by a screw 14 and is therefore adjustable in the rotational position, the head 13 engaging in a transverse groove 15 of the control slide 5.

Vorzugsweise sind bei einer Kraftstoffeinspritzpumpe mehrere solcher Pumpenelemente 2, 3 mit Steuerschiebern 5 in Reihe im Gehäuse 1 angeordnet, die dann gemeinsam durch eine Regelstange 11 bedient werden, deren Mitnahmeglieder 12 der Zahl der Pumpenelemente entsprechen. Die Regelstange 11 und die Mitnahmeglieder 12 sind in einem Pumpensaugraum 16 angeordnet, der, wie nicht näher dargestellt, über eine Förderpumpe von einem Kraftstoffbehälter aus mit Kraftstoff unter niederem Druck versorgt wird. Der Zugang 6 der Ausnehmung 4 des Pumpenzylinders 2 ist zu diesem Saugraum 16 hin gewandt, so daß zwischen Ausnehmung 4 und Saugraum 16 eine offene Verbindung besteht.In the case of a fuel injection pump, a plurality of such pump elements 2, 3 with control slides 5 are preferably arranged in series in the housing 1, which are then operated together by a control rod 11, the driving elements 12 of which correspond to the number of pump elements. The control rod 11 and the entrainment members 12 are arranged in a pump suction chamber 16 which, as is not shown in more detail, is supplied with fuel under low pressure from a fuel tank via a feed pump. The access 6 of the recess 4 of the pump cylinder 2 faces this suction chamber 16, so that there is an open connection between the recess 4 and the suction chamber 16.

Der Pumpenkolben 3 nimmt in der dargestellten Stellung seine untere Totpunktlage (UT) ein, wobei er Saugöffnungen 17 des Pumpenarbeitsraums 18 aufsteuert, die über einen in der Pumpenzylinderbüchse 2 vorhandenen Kanal 19 bzw. eine Abdrehung 21 an der Zylinderbüchse 2 mit dem Pumpensaugraum 16 verbunden sind.In the position shown, the pump piston 3 assumes its bottom dead center position (UT), opening up suction openings 17 of the pump work chamber 18, which are connected to the pump suction chamber 16 via a channel 19 present in the pump cylinder liner 2 or a twist 21 on the cylinder liner 2 .

In der Mantelfläche des Pumpenkolbens 3 ist eine Schrägnut 22 und Ausnehmung 23 angeordnet, die als Steueröffnungen paarweise auf dem Pumpenkolben 3 angeordnet über eine Querbohrung 24 miteinander verbunden sind, welche über eine Sackbohrung 25 zum Pumpenarbeitsraum 18 führt. Diese Steueröffnungen, nämlich die Schrägnuten 22 und Ausnehmungen 23, wirken mit zwei als Radialöffnungen dienenden Radialbohrungen 26 des Steuerschiebers 5 zusammen, wobei die Eingangskanten 27 dieser Radialbohrungen 26 als Steuerkante zu den Steueröffnungen hin dienen, während die Mündungen 28 dieser Radialbohrungen 26 auf parallele Seitenwände 29 der Ausnehmung 4 gerichtet sind.In the lateral surface of the pump piston 3, an oblique groove 22 and recess 23 are arranged, which are arranged as control openings in pairs on the pump piston 3 and are connected to one another via a transverse bore 24, which leads via a blind bore 25 to the pump work chamber 18. These control openings, namely the oblique grooves 22 and recesses 23, cooperate with two radial bores 26 of the control slide 5 serving as radial openings, the input edges 27 of these radial bores 26 serving as control edges towards the control openings, while the orifices 28 of these radial bores 26 on parallel side walls 29 the recess 4 are directed.

Die zwischen den Seitenwänden 29 und dem Steuerschieber 5 gebildeten Raumspalte 31 sind zum Saugraum 16 hin durch am Steuerschieber 5 angeordnete Schürzen 32 verdeckt, die senkrecht zur Spaltausdehnung verlaufende Prallflächen 33 aufweisen.The space gaps 31 formed between the side walls 29 and the control slide 5 are covered toward the suction space 16 by aprons 32 arranged on the control slide 5, which have baffle surfaces 33 running perpendicular to the gap expansion.

Das dargestellte Ausführungsbeispiel arbeitet wie folgt:
In der dargestellten UT-Lage des Pumpenkolbens 3 wird der Pumpenarbeitsraum 18 über die Saugöffnungen 17 und - den Kanal 19 bzw. die Abdrehung 21 vom Pumpensaugraum 16 her mit Kraftstoff aufgefüllt. Je nach Axiallage des Steuerschiebers 5 kann auch ein Teil der Kraftstoffversorgung über die Ausnehmungen 23 bzw. Schrägnuten 22, die Querbohrung 24 und die Sackbohrung 25 erfolgen. Beim Förderhub des Pumpenkolbens 3 wird zuerst über die Versorgungskanäle ein Teil des Kraftstoffes aus dem Pumpenarbeitsraum 18 wieder zurück in den Saugraum 16 verdrängt, mindestens so lange bis die Saugöffnungen 17 durch den Pumpenkolben 3 geschlossen sind und spätestens so lange bis auch die Ausnehmungen 23 bzw. Schrägnuten 22 durch den Steuerschieber 5 verdeckt sind. Ab dieser Förderhubstellung kann sich im Pumpenarbeitsraum 18 der Hochdruck entwickeln und die Einspritzung zur Brennkraftmaschine beginnen. Diese Einspritzung wird dann beendet, wenn die Steueröffnungen, nämlich die Schrägnuten 22, in Überdeckung gelangen mit den Radialbohrungen 26 des Steuerschiebers 5. Der unter sehr hohem Druck stehende Kraftstoff wird nun aus dem Pumpenarbeitsraum 18 über die Sackbohrung 25, die Querbohrung 24, die Schrägnuten 22 und die Radialbohrungen 26 in die Raumspalte 31 gefördert, wobei der sich dabei bildende Absteuerkraftstoffstrahl auf die gegenüberliegenden Seitenwände 29 trifft. An diesen Seitenwänden 29 wird der Strahl reflektiert und trifft teilweise auf die Rückwand 7, zum größten Teil auf die Prallflächen 33 der Schürzen 32, um danach in die verbleibenden Räume der Ausnehmung 4 oberhalb und unterhalb des Steuerschiebers 5 zu strömen. Von hier aus gelangt dann der Kraftstoff in den Saugraum 16.
The illustrated embodiment works as follows:
In the illustrated UT position of the pump piston 3, the pump working chamber 18 is filled with fuel via the suction openings 17 and the channel 19 or the twist 21 from the pump suction chamber 16. Depending on the axial position of the control slide 5, part of the fuel supply can also take place via the recesses 23 or oblique grooves 22, the transverse bore 24 and the blind bore 25. During the delivery stroke of the pump piston 3, part of the fuel is first displaced from the pump working chamber 18 back into the suction chamber 16 via the supply channels, at least until the suction openings 17 are closed by the pump piston 3 and at the latest until the recesses 23 or Oblique grooves 22 are covered by the control slide 5. From this delivery stroke position, the high pressure can develop in the pump work chamber 18 and the injection to the internal combustion engine can begin. This injection is ended when the control openings, namely the oblique grooves 22, overlap with the radial bores 26 of the control slide 5. The fuel, which is under very high pressure, is now extracted from the pump working chamber 18 via the blind bore 25, the transverse bore 24, the oblique grooves 22 and the radial bores 26 are conveyed into the space gaps 31, with the control fuel jet being formed meets the opposite side walls 29. The beam is reflected on these side walls 29 and partially strikes the rear wall 7, for the most part the impact surfaces 33 of the aprons 32, in order to then flow into the remaining spaces of the recess 4 above and below the control slide 5. From here, the fuel then reaches the suction chamber 16.

Die im Bereich des Zugangs 6 zur Ausnehmung 4 an den den Steuerschieber 5 verbreiternden Absätzen vorhandenen, mit den Prallflächen 33 versehenen Schürzen 32 können entweder noch gerade in den Zugang 6 der Ausnehmung 4 tauchen oder aber auch außerhalb desselben bleiben, wobei nur durch die Prallflächen 33 erreicht sein muß, daß der Kraftstoffstrahl zur Energievernichtung reflektiert wird.The aprons 32 present in the area of the access 6 to the recess 4 at the shoulders widening the control slide 5 and provided with the baffle surfaces 33 can either dive straight into the access 6 of the recess 4 or can remain outside the same, only through the baffle surfaces 33 must be achieved that the fuel jet is reflected for energy destruction.

BezugszahlenlisteList of reference numbers

11
PumpengehäusePump housing
22nd
ZylinderbüchseCylinder liner
33rd
PumpenkolbenPump piston
44th
AusnehmungRecess
55
SteuerschieberSpool
66
ZugangAccess
77
Rückwand von 4Rear wall of 4
88th
LängsschlitzLongitudinal slot
99
Nasenose
1010th
--
1111
RegelstangeControl rod
1212
MitnahmegliedDriving link
1313
Kopfhead
1414
Schraubescrew
1515
QuernutCross groove
1616
PumpensaugraumPump suction room
1717th
SaugöffnungeSuction openings
1818th
PumpenarbeitsraumPump work room
1919th
Kanalchannel
2020th
--
2121
AbdrehungCalibration
2222
SchrägnutOblique groove
2323
AusnehmungRecess
2424th
QuerbohrungCross hole
2525th
SackbohrungBlind hole
2626
Radialbohrungen (in Anspruch Radialöffnungen)Radial bores (use radial openings)
2727th
Eingangskanten an 26Entrance edges at 26
2828
Mündungen von 26Mouths of 26
2929
Seitenwände von 4Sidewalls of 4
3030th
--
3131
RaumspaltSpace gap
3232
SchürzenAprons
3333
senkr. Flächenvertical Surfaces

Claims (1)

  1. Fuel injection pump for internal combustion engines, with at least one pump element, on the pump plunger (3) and in the barrel (2) of which, the said barrel being inserted in the pump casing (1), there is arranged, in a recess (4) present there and having a radial access opening (6), a control slide (5) guided in axially displaceable fashion, secured against rotation and serving to control the fuel, two radial and mutually parallel space-forming gaps (31) which serve to guide the fuel being formed between the control slide (5) and two mutually opposite, parallel side walls (29) of the recess (4); with two control openings (oblique grooves 22, recesses 23) on the lateral surface of the pump plunger (3), which are connected to the pump working space (18) by a relief passage (24, 25) extending in the pump plunger (3) and, to end the injection, can be opened by the control slide (5) and, for this purpose, interact in each case with a control edge (27) of two radial openings (26) of the control slide (5), the said radial openings pointing towards the side walls (29), in such a way that the discharged jet in each case strikes one of the side walls (29) of the recess (4), and with a pump suction space (16) which is arranged in the pump casing (1) and into which the two radial space-forming gaps (31) open via the access opening (6) of the recess (4), characterised in that on the control slide (5), in the region of the access opening (6) of the recess (4) extending in the form of a blind hole from the pump suction space (16) into the barrel (2), there is in each case a skirt (32) for at least partially covering over the radial space-forming gaps (31) towards the pump suction space (16), each skirt having a rebound face (33) which extends at right angles to the space-forming gaps (31) and side walls (29) of the recess (4), and is present on the shoulders widening the control slide (5).
EP87112919A 1986-10-04 1987-09-04 Fuel injection pump for internal combustion engines Expired - Lifetime EP0263304B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3633899 1986-10-04
DE19863633899 DE3633899A1 (en) 1986-10-04 1986-10-04 FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES

Publications (3)

Publication Number Publication Date
EP0263304A2 EP0263304A2 (en) 1988-04-13
EP0263304A3 EP0263304A3 (en) 1989-04-19
EP0263304B1 true EP0263304B1 (en) 1992-04-29

Family

ID=6311091

Family Applications (1)

Application Number Title Priority Date Filing Date
EP87112919A Expired - Lifetime EP0263304B1 (en) 1986-10-04 1987-09-04 Fuel injection pump for internal combustion engines

Country Status (4)

Country Link
US (1) US4811716A (en)
EP (1) EP0263304B1 (en)
JP (1) JPS6390664A (en)
DE (2) DE3633899A1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3844430A1 (en) * 1988-12-31 1990-07-05 Bosch Gmbh Robert FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES
DE3902670A1 (en) * 1989-01-30 1990-08-02 Voest Alpine Automotive INJECTION PUMP FOR DIESEL ENGINES
US5364243A (en) * 1989-08-02 1994-11-15 Diesel Kiki Co., Ltd. Fuel injection pump
DE4016435C2 (en) * 1990-05-22 1997-05-28 Daimler Benz Ag A diaphragm-controlled fuel injection pump for internal combustion engines having a control slide, in particular as a direct injector for commercial vehicles
DE4041503C2 (en) * 1990-12-22 2001-02-15 Bosch Gmbh Robert Fuel injection pump for internal combustion engines
DE4041656A1 (en) * 1990-12-22 1992-07-02 Bosch Gmbh Robert FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES
DE4132505A1 (en) * 1991-09-30 1993-04-01 Bosch Gmbh Robert FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES
DE4132502C2 (en) * 1991-09-30 2001-09-27 Bosch Gmbh Robert Fuel injection pump
DE4211886A1 (en) * 1992-04-09 1993-10-14 Bosch Gmbh Robert Fuel injection pump for internal combustion engines
DE19919430C1 (en) * 1999-04-29 2000-10-19 Bosch Gmbh Robert Injection pump
EP1801411B1 (en) * 2001-01-05 2009-08-05 Hitachi, Ltd. Fluid pump and high-pressure fuel feed pump

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1446048A (en) * 1964-05-25 1966-07-15 Bryce Berger Ltd Advanced pump for liquid fuel injection
GB1271799A (en) * 1968-09-24 1972-04-26 Cav Ltd Fuel injection pumps
DE3017730A1 (en) * 1980-05-09 1981-11-12 Robert Bosch Gmbh, 7000 Stuttgart FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES
DE3136751A1 (en) * 1981-09-16 1983-03-31 Robert Bosch Gmbh, 7000 Stuttgart FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES
WO1985005152A1 (en) * 1984-05-08 1985-11-21 Mitsubishi Jidosha Kogyo Kabushiki Kaisha Fuel injection pump and method of adjusting the same pump
DE3428176C2 (en) * 1984-07-31 1994-08-25 Bosch Gmbh Robert Fuel injection pump for internal combustion engines
DE3428174A1 (en) * 1984-07-31 1986-02-13 Robert Bosch Gmbh, 7000 Stuttgart FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES
DE3435987A1 (en) * 1984-10-01 1986-04-10 Robert Bosch Gmbh, 7000 Stuttgart FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES
JPS61123756A (en) * 1984-11-16 1986-06-11 Diesel Kiki Co Ltd Fuel injection pump
DE3447375A1 (en) * 1984-12-24 1986-07-03 Robert Bosch Gmbh, 7000 Stuttgart FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES
JPH0541262Y2 (en) * 1985-04-17 1993-10-19
US4737086A (en) * 1986-05-27 1988-04-12 Diesel Kiki Co., Ltd. Fuel injection pump having variable prestroke mechanism

Also Published As

Publication number Publication date
EP0263304A2 (en) 1988-04-13
DE3633899A1 (en) 1988-04-07
EP0263304A3 (en) 1989-04-19
DE3778629D1 (en) 1992-06-04
JPS6390664A (en) 1988-04-21
US4811716A (en) 1989-03-14

Similar Documents

Publication Publication Date Title
EP0178427A2 (en) Electrically controlled fuel injection pump for internal combustion engines
EP0263304B1 (en) Fuel injection pump for internal combustion engines
DE3926166A1 (en) FUEL INJECTION PUMP FOR DIESEL INTERNAL COMBUSTION ENGINES
DE3809700C2 (en)
DE2911447A1 (en) CONTROLLING THE FUEL FLOW CONTROL UNIT FOR INJECTION DEVICES IN PARTICULAR AIR COMPRESSING ENGINES
DE3943419A1 (en) FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES, IN PARTICULAR PUMPEDUESE
EP0971123B1 (en) Fuel injection pump
EP0263807B1 (en) Pump element of a fuel pump for an injection combustion engine
DE3624700A1 (en) INJECTION PUMP WITH SPRAY ADJUSTMENT
DE4127032C2 (en) Fuel injection pump for internal combustion engines
EP0713002B1 (en) High pressure fuel pump for internal combustion engines
EP0269610A1 (en) Pump element of a fuel injection pump for an injection combustion engine
EP0906506B1 (en) Fuel injection pump for an internal combustion engine
DE3644150C2 (en) Fuel injection pump for internal combustion engines
DE4041503C2 (en) Fuel injection pump for internal combustion engines
DE4139907A1 (en) High pressure fuel injection device - has labyrinth seal between pump piston and cylinder liner, or between nozzle pin and housing
AT227480B (en) Pump working with a reciprocating movement and self-regulating the delivery rate, especially for fuel injection in engines
DE3535808A1 (en) FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES
EP0444256B1 (en) Fuel injection device for injection-type internal combustion engines
DE4041656A1 (en) FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES
AT394891B (en) Piston-type pump, in particular a fuel injection pump for internal combustion engines
DE3644595A1 (en) PRESSURE RELIEF VALVE FOR FUEL INJECTION PUMPS
DE4110011A1 (en) FUEL INJECTION PUMP FOR INTERNAL COMBUSTION ENGINES
DE4110010A1 (en) Fuel injection pump for IC engine - has spring-loaded sleeve engaging on stepped turning of control slide
DE4040865A1 (en) Fuel injection pump for IC engine - has at least one cylinder and piston rotatable for fuel control, cylinder having recess

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): DE FR GB IT

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): DE FR GB IT

17P Request for examination filed

Effective date: 19891130

17Q First examination report despatched

Effective date: 19900320

RAP3 Party data changed (applicant data changed or rights of an application transferred)

Owner name: ROBERT BOSCH GMBH

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB IT

REF Corresponds to:

Ref document number: 3778629

Country of ref document: DE

Date of ref document: 19920604

ET Fr: translation filed
GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)
ITF It: translation for a ep patent filed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Effective date: 19920904

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 19920904

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Effective date: 19930528

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Effective date: 19930602

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20050904