EP0020249B1 - Injection pump for internal-combustion engine - Google Patents

Injection pump for internal-combustion engine Download PDF

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Publication number
EP0020249B1
EP0020249B1 EP80400720A EP80400720A EP0020249B1 EP 0020249 B1 EP0020249 B1 EP 0020249B1 EP 80400720 A EP80400720 A EP 80400720A EP 80400720 A EP80400720 A EP 80400720A EP 0020249 B1 EP0020249 B1 EP 0020249B1
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EP
European Patent Office
Prior art keywords
delivery
chamber
fuel
piston
injection
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
Application number
EP80400720A
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German (de)
French (fr)
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EP0020249A1 (en
Inventor
Dirk Bastenhof
Roger Brisson
Claude Bonniot
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.)
MAN Energy Solutions France SAS
Original Assignee
Societe dEtudes de Machines Thermiques SEMT SA
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Priority claimed from FR7913486A external-priority patent/FR2457987A1/en
Application filed by Societe dEtudes de Machines Thermiques SEMT SA filed Critical Societe dEtudes de Machines Thermiques SEMT SA
Publication of EP0020249A1 publication Critical patent/EP0020249A1/en
Application granted granted Critical
Publication of EP0020249B1 publication Critical patent/EP0020249B1/en
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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
    • F02M45/00Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship
    • F02M45/02Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts
    • F02M45/04Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts with a small initial part, e.g. initial part for partial load and initial and main part for full load
    • F02M45/06Pumps peculiar thereto
    • 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
    • F02M45/00Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship
    • F02M45/02Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts
    • F02M45/04Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts with a small initial part, e.g. initial part for partial load and initial and main part for full load
    • F02M45/06Pumps peculiar thereto
    • F02M45/066Having specially arranged spill port and spill contour on the piston
    • 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
    • F02M59/22Varying quantity or timing by adjusting cylinder-head space

Definitions

  • the present invention relates to an injection pump for an internal combustion engine of the type described in the preamble to the main claim.
  • a pump of this type is known from GB-A-571485.
  • This pump allows a quantity of pre-injection fuel to be discharged before the main injection fuel is discharged, but has the disadvantage of not allowing a variation in the start of the pre-injection discharge.
  • US-A-2 810 375 relates to an injection pump which makes it possible to vary the start of the delivery of fuel from the pump to the injector.
  • This device for varying the start of delivery includes a fuel accumulator chamber, in permanent communication with the intake chamber and of variable volume by a piston mounted movably in said accumulator chamber, against a return spring, under the effect of fuel pressure in the intake chamber.
  • the object of the present invention is to propose an injection pump which makes it possible to vary the start of the pre-injection delivery without influencing the start of the main injection delivery.
  • a rod is fixed to the rear face of the aforementioned piston and the free end of said rod is brought out of the pump structure to determine the length of the piston stroke.
  • the injection pump shown in FIGS. 1 to 5 comprises a cylindrical body 1 and a piston 2 mounted movably in this body 1 in a reciprocating rectilinear reciprocating movement, between a position of bottom dead center and a position of top dead center, under the effect of a control cam (not shown) secured to a shaft driven by the motor.
  • a fuel intake chamber 3 into which open fuel inlet orifices 4. These orifices are located at a level such that they allow the filling of the chamber 3 by the fuel, when the piston occupies its bottom dead center position.
  • the piston 2 has a first circular groove 5 delimited at its lower part by a straight edge 6 and at its upper part by a helical edge 7 forming a helical ramp and ending in a groove 8 which extends parallel to the axis of the piston .
  • This groove establishes permanent communication between the intake chamber 3 and the groove 5.
  • the piston 2 is provided with a second circular groove 9, limited, in the example shown, at the top by a straight edge 10 and at the bottom by a straight edge 11.
  • This second groove 9 communicates with the first groove 5 through axial passages, formed in the example represented by two flats 12 formed on the flange 13 which is delimited between the two grooves 5 and 9. It should be noted that the edges 6, 7, 10 and 11 each have a sharp angle of 90 °.
  • fuel inlet holes 14 are made in the wall of the body 1 of the pump, at a predetermined distance below the inlet ports 4.
  • the holes 14 and the ports 4 are connected to a relatively low pressure fuel source.
  • the distance, in the axial direction of the piston, between the inlet orifices 4 and the inlet holes 14, the distance between the upper surface 15 of the piston 2, on the one hand, and the edges of the two grooves 5 and 9 , on the other hand, as well as the axial height of the flange 13 and the width of the second groove 9 are chosen to ensure the specific operating steps of the pump shown in FIGS. 1 to 4.
  • the intake chamber 3 communicates with the inlet orifices 4, which allows the filling of the chamber 3 with fuel.
  • the piston 2 By moving upwards, that is to say towards its top dead center position , the piston 2 reaches the position illustrated in FIG. 2, in which it begins to close the inlet orifices 4. Since the flange 13 is opposite the inlet holes 14 and closes these, no more communication exists between the chamber 3 and a conduit low pressure fuel supply. This is the start of fuel delivery to the injector in the direction of arrow F1. This start of delivery is designated in FIG. 6 with the letter A.
  • the piston 2 arrives at the position shown in fig. 3, in which the upper edge 10 of the second circular groove 9 comes at the level of the lower edge of the inlet holes 14, which constitutes the start of the connection of these holes 14 and of the groove 9 and, at through the flats 12, of the groove 5 and of the groove 8, with the chamber 3.
  • This state is indicated in fig. 6 by the letter B.
  • This communication and because of it the low pressure inside the chamber 3 persist until the piston reaches the position shown in FIG. 4, in which the lower edge 11 of the groove 9 comes to the level of the upper edge of the inlet holes 14. These are closed by the cylindrical surface of the piston, which follows the groove 9.
  • the position of the bottom dead center of the piston 2 with respect to the movement of the piston of the engine cylinder is chosen such that the start A of the first phase of injection into the engine cylinder is sufficiently advanced relative to the top dead center of the piston of said engine cylinder so that this first injection can constitute a pre-injection ensuring the ignition, in the combustion chamber of an engine cylinder, of the quantity of main injection combustion, practically without ignition delay.
  • the start of pre-injection could take place at an instant corresponding to an angle of rotation of about -30 ° of the crankshaft, before the top dead center of the driving piston and the main injection could be triggered at an angle d 'around -15 °.
  • these values are given only by way of example.
  • the effect of the pre-injection varies as a function of the speed of rotation of the engine.
  • the illustration of the first delivery phase that is to say the pre-injection delivery, in the form of a rectangle according to FIG. 6, corresponds to the phenomena that actually occur.
  • the delivery and the pre-injection take on the appearance of a bell, because the establishment of the relatively high pressure inside the chamber 3 during the delivery of fuel out of the chamber and the drop in pressure in the chamber due to the communication between the latter and the inlet holes 14 require a certain period of time, since the inlet orifices 4 and the inlet holes 14 have cross sections of limited value.
  • the upper and lower edges 10, 11 of the second groove 9 are straight and circular. However, it is possible to configure at least one edge, for example the upper edge, at least partial helical ramp. This would make it possible to vary the instant of the end of the pre-injection delivery (B in FIG. 6), by rotation of the piston 2 around its longitudinal axis. An appropriate configuration of the lower edge of the groove 9 would make it possible to modify the start of the main injection delivery (C).
  • the embodiment represented by FIGS. 2 to 5 comprises a circular groove 9 and twice two inlet holes 14, and this in order to reduce the height of the groove 9 and the diameters of said holes 14, because these two dimensions decide the distance between B and C in fig. 6, that is to say the time of the pre-injection with respect to the main injection, on the one hand, and the lifting of the cam corresponding to this period, on the other hand.
  • These measures make it possible to reduce the length of the inactive part, that is to say without the piston stroke being pushed back, to advance the start of the main injection delivery and / or to delay the start of the pre-injection delivery.
  • Figs 7 and 8 show another embodiment of the injection pump, in which the inlet holes 14 '- two in number in the example shown - are located approximately at the same level as the inlet orifices 4.
  • Two grooves 9 ' the function of which corresponds to that of the circular groove 9 of the first embodiment, are formed in the peripheral surface of the piston, at a predetermined distance from the upper surface 15 of the piston, substantially parallel to the latter.
  • each groove 9 ' opens at one end in a vertical groove 8 and thus communicates, permanently, with the interior of the intake chamber 3.
  • each groove could be in communication with this chamber by its two ends.
  • the operation of this embodiment is the same, in principle, as that illustrated in FIGS. 1 to 4.
  • the pre-injection delivery begins when the orifices 4 are closed by the piston.
  • the inlet holes 14 ' are closed by the part of the peripheral surface 13' of the piston which is located above the grooves 9 '. This discharge is finished at the moment when the grooves 9 'come opposite the holes 14'.
  • the main injection delivery starts after the holes 14 'are closed by the peripheral surface of the piston located below the grooves 9' and ends when the ramp 7 discovers the orifices 4.
  • the injection pump according to the present invention also comprises means which allow the variation of the start of the pre-injection delivery.
  • These means are formed by an accumulator device.
  • the accumulator comprises an accumulator chamber 16 in which is mounted a piston 17 movable against a return spring 18.
  • the chamber 16 communicates permanently with the inlet chamber 3 of the injection pump by a passage 19 which opens into the chamber 3 at a level above the top dead center of the piston.
  • the rear part 20 of the chamber, which houses the spring 18, is in permanent communication with the space 21 from which the inlet orifices leave. This ensures that a relatively low pressure acts on the rear face of the piston 17.
  • the stroke of the piston 17 is limited by a stop 22 formed for example by a shoulder of the wall of the chamber 16.
  • the piston 17 is movable over a length e.
  • the stop 22 is shaped as a sealed seat to produce a sealing barrier between the chamber 16 and the part 20 of the chamber containing the spring 18, when the piston is pushed against the stop under the effect of the high pressure prevailing in chamber 3 of the pump and chamber 16, during the delivery of fuel to the injector.
  • This accumulator operates as follows: When after closing the inlet orifices 4, the piston 2 continues its upward stroke, the pressure inside the receiving chamber 3 increases only slowly since the decrease in the volume of the receiving chamber 3 is compensated by an increase in the volume of the accumulating chamber 16 due to the fact that the piston 17 moves back under the effect of the increase in pressure. Consequently, the pressure which is necessary for the opening of the discharge valve 23 can only be established after the piston has come into contact on its sealed seat stop 22. This means that point A, in FIG . 6, moves to point B and the amount of pre-injection fuel delivered decreases. On the other hand, the interruption of the discharge at point B is independent of the accumulator and determined only by the communication of the additional holes 14 and of the groove 9 for interrupting the discharge. Although the pressure inside the chamber 3 falls, it remains however, due to the piston which continues its upward stroke, at a value sufficient to maintain the piston 17 of the accumulator on its seat.
  • the accumulator has no influence on the start of the main injection delivery, but allows to vary the start of the pre-injection delivery (point A in fig. 6), and thus the quantity of the pre-injection fuel. .
  • Figs 10 and 11 illustrate two embodiments of the accumulator 15 according to the invention.
  • the accumulator is placed next to the device forming a discharge member 23, above the inlet chamber 3 of the injection pump.
  • the accumulator is perfectly incorporated into the structure of the pump.
  • the accumulator shown in fig. 11 is made to allow adjustment of the outside of the start of the pre-injection delivery.
  • a rod 24 is fixed to the rear face of the piston 17. The free end of said rod comes out of the pump.
  • the rod 24 can be controlled from outside the pump, which makes it possible to easily vary the final position of the piston 17. It is also possible to deactivate the pre-injection.

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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)

Description

La présente invention concerne une pompe d'injection pour un moteur à combustion interne du type décrit dans le préambule de la revendication principale.The present invention relates to an injection pump for an internal combustion engine of the type described in the preamble to the main claim.

Une pompe de ce type est connue par le GB-A-571485. Cette pompe permet de refouler une quantité de combustibles de pré-injection avant le refoulement du combustible d'injection principale, mais présente l'inconvénient de ne pas permettre une variation du début du refoulement de pré- injection.A pump of this type is known from GB-A-571485. This pump allows a quantity of pre-injection fuel to be discharged before the main injection fuel is discharged, but has the disadvantage of not allowing a variation in the start of the pre-injection discharge.

Le US-A-2 810 375 a pour objet une pompe d'injection qui permet de faire varier le début du refoulement de combustible hors de la pompe vers l'injecteur. Ce dispositif de variation du début du refoulement comporte une chambre accumulatrice de combustible, en communication permanente avec la chambre d'admission et de volume variable par un piston monté mobile dans ladite chambre accumulatrice, à l'encontre d'un ressort de rappel, sous l'effet de la pression du combustible dans la chambre d'admission.US-A-2 810 375 relates to an injection pump which makes it possible to vary the start of the delivery of fuel from the pump to the injector. This device for varying the start of delivery includes a fuel accumulator chamber, in permanent communication with the intake chamber and of variable volume by a piston mounted movably in said accumulator chamber, against a return spring, under the effect of fuel pressure in the intake chamber.

Si on utilisait ce dispositif de variation du début de refoulement dans la pompe suivant le GB-A-571 485, on obtiendrait une pompe dont non seulement le début du refoulement d'injection principale mais également le début du refoulement d'injection principale serait modifié par l'accumulateur.If we used this device for varying the start of delivery in the pump according to GB-A-571 485, we would obtain a pump in which not only the start of the main injection delivery but also the start of the main injection delivery would be modified by the accumulator.

La présente invention a pour but de proposer une pompe d'injection qui permet de faire varier le début du refoulement de pré-injection sans influencer le début du refoulement d'injection principale.The object of the present invention is to propose an injection pump which makes it possible to vary the start of the pre-injection delivery without influencing the start of the main injection delivery.

Ce but est atteint grâce aux caractéristiques énoncées dans la partie caractérisante de la revendication principale, et notamment du fait que le piston de l'accumulateur vient en appui étanche sur un siège formant butée de limitation de la course du piston pendant la pré-injection et est maintenu sur ce siège sous l'effet d'une pression égale à celle produite, pendant l'interruption du refoulement, par le piston de pompe continuant sa course monté pendant cette interruption.This object is achieved thanks to the characteristics set out in the characterizing part of the main claim, and in particular the fact that the accumulator piston comes into leaktight support on a seat forming a stop limiting the stroke of the piston during the pre-injection and is maintained on this seat under the effect of a pressure equal to that produced, during the interruption of the delivery, by the pump piston continuing its stroke mounted during this interruption.

Concernant le US-A-2 810 375, ce document ne contient aucun enseignement que pendant une période d'interruption de refoulement, le piston de l'accumulateur reste appliqué sur sa butée et ne révèle pas non plus que le piston de l'accumulateur vient en appui étanche sur un siège formant butée de limitation de la course du piston. C'est cependant ce siège étanche prévu par l'invention, qui empêche des fuites entre le piston et la paroi de la chambre de l'accumulateur de manière que le piston peut rester appliqué contre ce siège pendant la période d'interruption.Concerning US-A-2 810 375, this document contains no teaching that during a period of interruption of delivery, the piston of the accumulator remains applied on its stop and does not reveal either that the piston of the accumulator comes into watertight support on a seat forming a stop for limiting the stroke of the piston. It is however this sealed seat provided by the invention, which prevents leaks between the piston and the wall of the accumulator chamber so that the piston can remain pressed against this seat during the period of interruption.

Selon une caractéristique avantageuse de l'invention, une tige est fixée à la face arrière du piston précité et l'extrémité libre de ladite tige est amenée hors de la structure de la pompe pour déterminer la longueur de la course du piston.According to an advantageous characteristic of the invention, a rod is fixed to the rear face of the aforementioned piston and the free end of said rod is brought out of the pump structure to determine the length of the piston stroke.

L'invention sera mieux comprise, et d'autres buts, caractéristiques, détails et avantages de celle-ci apparaîtront plus clairement au cours de la description explicative qui va suivre faite en référence aux dessins schématiques annexés donnés uniquement à titre d'exemple illustrant deux modes de réalisation de l'invention et dans lesquels:

  • Les figs 1 à 4 sont des vues en coupe longitudinales d'un premier mode de réalisation d'une pompe d'injection et illustrent des étapes spécifiques du fonctionnement de la pompe; la fig. 5 est une vue en coupe suivant la ligne V-V de la fig. 2; la fig. 6 illustre les phases de refoulement de combustible hors de la chambre de la pompe d'injection, en fonction de la position du piston du cylindre du moteur, exprimé en position angulaire de l'arbre manivelle; la fig. 7 est une vue en coupe longitudinale d'un deuxième mode de réalisation d'une pompe d'injection; la fig. 8 est une vue en coupe suivant la ligne VIII-VIII de la fig. 7; la fig. 9 montre en une vue en coupe et de façon schématique le dispositif accumulateur selon l'invention, et les figs 10 et 11 illustrent deux modes de réalisation concrètes d'un accumulateur selon l'invention.
The invention will be better understood, and other objects, characteristics, details and advantages thereof will appear more clearly during the explanatory description which follows, made with reference to the appended schematic drawings given solely by way of example illustrating two embodiments of the invention and in which:
  • Figs 1 to 4 are longitudinal section views of a first embodiment of an injection pump and illustrate specific steps in the operation of the pump; fig. 5 is a sectional view along the line VV of FIG. 2; fig. 6 illustrates the fuel delivery phases out of the injection pump chamber, as a function of the position of the piston of the engine cylinder, expressed in angular position of the crankshaft; fig. 7 is a view in longitudinal section of a second embodiment of an injection pump; fig. 8 is a sectional view along line VIII-VIII of FIG. 7; fig. 9 shows in a sectional view and schematically the accumulator device according to the invention, and FIGS. 10 and 11 illustrate two concrete embodiments of an accumulator according to the invention.

La pompe d'injection représentée sur les figs 1 à 5 comprend un corps cylindrique 1 et un piston 2 monté mobile dans ce corps 1 suivant un mouvement alternatif rectiligne de va-et-vient, entre une position de point mort bas et une position de point mort haut, sous l'effet d'une came de commande (non représentée) solidaire d'un arbre mû par le moteur.The injection pump shown in FIGS. 1 to 5 comprises a cylindrical body 1 and a piston 2 mounted movably in this body 1 in a reciprocating rectilinear reciprocating movement, between a position of bottom dead center and a position of top dead center, under the effect of a control cam (not shown) secured to a shaft driven by the motor.

Dans le corps 1, au-dessus du piston 2, est délimitée une chambre d'admission de combustible 3, dans laquelle débouchent des orifices d'arrivée de combustible 4. Ces orifices sont situés à un niveau tel qu'ils permettent le remplissage de la chambre 3 par le combustible, lorsque le piston occupe sa position de point mort bas.In the body 1, above the piston 2, is defined a fuel intake chamber 3, into which open fuel inlet orifices 4. These orifices are located at a level such that they allow the filling of the chamber 3 by the fuel, when the piston occupies its bottom dead center position.

En haut de la chambre, non représenté, il faut imaginer un orifice de refoulement de combustible en direction de la flèche F1, vers un injecteur associé à un cylindre d'un moteur à combustion interne. Cet orifice de refoulement est obturable par un organe de décharge, de façon connue en soi.At the top of the chamber, not shown, it is necessary to imagine a fuel delivery orifice in the direction of arrow F1, towards an injector associated with a cylinder of an internal combustion engine. This discharge orifice can be closed off by a discharge member, in a manner known per se.

Le piston 2 comporte une première gorge circulaire 5 délimitée à sa partie inférieure par une arête droite 6 et à sa partie supérieure par une arête hélicoïdale 7 formant une rampe hélicoïdale et aboutissant à une rainure 8 qui s'étend parallèlement à l'axe du piston. Cette rainure établit une communication permanente entre la chambre d'admission 3 et la gorge 5.The piston 2 has a first circular groove 5 delimited at its lower part by a straight edge 6 and at its upper part by a helical edge 7 forming a helical ramp and ending in a groove 8 which extends parallel to the axis of the piston . This groove establishes permanent communication between the intake chamber 3 and the groove 5.

Le piston 2 est pourvu d'une deuxième gorge circulaire 9, limitée, dans l'exemple représenté, en haut par une arête droite 10 et en bas par une arête droite 11. Cette deuxième gorge 9 communique avec la première gorge 5 à travers des passages axiaux, formés dans l'exemple représenté par deux méplats 12 pratiqués sur la collerette 13 qui est délimitée entre les deux gorges 5 et 9. Il est à noter que les arêtes 6, 7, 10 et 11 présentent chacune un angle vif de 90°.The piston 2 is provided with a second circular groove 9, limited, in the example shown, at the top by a straight edge 10 and at the bottom by a straight edge 11. This second groove 9 communicates with the first groove 5 through axial passages, formed in the example represented by two flats 12 formed on the flange 13 which is delimited between the two grooves 5 and 9. It should be noted that the edges 6, 7, 10 and 11 each have a sharp angle of 90 °.

Comme il ressort des figures, des trous d'arrivée 14 du combustible sont pratiqués dans la paroi du corps 1 de la pompe, à une distance prédéterminée en dessous des orifices d'arrivée 4. Les trous 14 et les orifices 4 sont reliés à une source de combustible de relativement faible pression.As shown in the figures, fuel inlet holes 14 are made in the wall of the body 1 of the pump, at a predetermined distance below the inlet ports 4. The holes 14 and the ports 4 are connected to a relatively low pressure fuel source.

La distance, dans le sens axial du pistion, entre les orifices d'arrivée 4 et les trous d'arrivée 14, la distance entre la surface supérieure 15 du piston 2, d'une part, et les arêtes des deux gorges 5 et 9, d'autre part, ainsi que la hauteur axiale de la collerette 13 et la largeur de la deuxième gorge 9 sont choisies pour assurer les étapes de fonctionnement spécifiques de la pompe représentées sur les figs 1 à 4.The distance, in the axial direction of the piston, between the inlet orifices 4 and the inlet holes 14, the distance between the upper surface 15 of the piston 2, on the one hand, and the edges of the two grooves 5 and 9 , on the other hand, as well as the axial height of the flange 13 and the width of the second groove 9 are chosen to ensure the specific operating steps of the pump shown in FIGS. 1 to 4.

Dans la position du piston, représentée sur la fig. 1, la chambre d'admission 3 communique avec les orifices d'arrivée 4, ce qui permet le remplissage en combustible de la chambre 3. En se déplaçant vers le haut, c'est-à-dire vers sa position de point mort haut, le piston 2 atteint la position illustrée sur la fig. 2, dans laquelle il commence à obturer les orifices d'arrivée 4. Etant donné que la collerette 13 se trouve en face des trous d'arrivée 14 et obture ceux-ci, plus aucune communication n'existe entre la chambre 3 et un conduit d'arrivée de combustible de faible pression. C'est le début de refoulement de combustible vers l'injecteur dans la direction de la flèche F1. Ce début de refoulement est désigné sur la fig. 6 par la lettre A.In the piston position, shown in fig. 1, the intake chamber 3 communicates with the inlet orifices 4, which allows the filling of the chamber 3 with fuel. By moving upwards, that is to say towards its top dead center position , the piston 2 reaches the position illustrated in FIG. 2, in which it begins to close the inlet orifices 4. Since the flange 13 is opposite the inlet holes 14 and closes these, no more communication exists between the chamber 3 and a conduit low pressure fuel supply. This is the start of fuel delivery to the injector in the direction of arrow F1. This start of delivery is designated in FIG. 6 with the letter A.

En continuant sa course de montée, le piston 2 arrive à la position montrée sur la fig. 3, dans laquelle l'arête supérieure 10 de la deuxième gorge 9 circulaire vient au niveau du bord inférieur des trous d'arrivée 14, ce qui constitue le début de la mise en communication de ces trous 14 et de la gorge 9 et, à travers les méplats 12, de la gorge 5 et de la rainure 8, avec la chambre 3. Il en résulte une brusque chute de pression à l'intérieur de la chambre 3. Le refoulement de combustible s'arrête, bien que le piston continue sa course de montée. Cet état est indiqué sur la fig. 6 par la lettre B. Cette communication et en raison d'elle la faible pression à l'intérieur de la chambre 3 persistent jusqu'à ce que le piston atteigne la position représentée sur la fig. 4, dans laquelle l'arête inférieure 11 de la gorge 9 vient au niveau du bord supérieur des trous d'arrivée 14. Ceux-ci se trouvent obturés par la surface cylindrique du piston, qui fait suite à la gorge 9. Dans cette position les orifices d'arrivée 4 sont encore fermés. La chambre 3 ainsi coupée des conduits de faible pression 4, 14, la pression du combustible à l'intérieur de la chambre augmente et le refoulement de combustible vers l'injecteur reprend, comme ceci est indiqué par la lettre C sur la fig. 6. Le refoulement prend fin en D, lorsque la rampe hélicoïdale 7 vient en regard d'un orifice d'arrivée 4. L'injection est plus rapide entre C et D qu'entre A et B, car la vitesse de la came de commande du piston est encore faible entre A et B, étant donné qu'elle se situe relativement au début de la montée du piston.Continuing its climb stroke, the piston 2 arrives at the position shown in fig. 3, in which the upper edge 10 of the second circular groove 9 comes at the level of the lower edge of the inlet holes 14, which constitutes the start of the connection of these holes 14 and of the groove 9 and, at through the flats 12, of the groove 5 and of the groove 8, with the chamber 3. This results in a sudden drop in pressure inside the chamber 3. The fuel delivery stops, although the piston continues its climb stroke. This state is indicated in fig. 6 by the letter B. This communication and because of it the low pressure inside the chamber 3 persist until the piston reaches the position shown in FIG. 4, in which the lower edge 11 of the groove 9 comes to the level of the upper edge of the inlet holes 14. These are closed by the cylindrical surface of the piston, which follows the groove 9. In this position the inlet orifices 4 are still closed. The chamber 3 thus cut off from the low pressure conduits 4, 14, the fuel pressure inside the chamber increases and the fuel delivery to the injector resumes, as indicated by the letter C in FIG. 6. The discharge ends in D, when the helical ramp 7 comes opposite an inlet orifice 4. The injection is faster between C and D than between A and B, because the speed of the cam piston control is still weak between A and B, since it is located relatively to the start of the piston rise.

La position du point mort bas du piston 2 par rapport au mouvement du piston du cylindre du moteur est choisie telle que le début A de la première phase d'injection dans le cylindre du moteur est suffisamment avancé par rapprt au point mort haut du piston dudit cylindre du moteur pour que cette première injection puisse constituer une préinjection assurant l'allumage, dans la chambre de combustion d'un cylindre du moteur, de la quantité de combustion d'injection principale, pratiquement sans délai d'allumage. Par exemple le début de préinjection pourrait avoir lieu à un instant correspondant à un angle de rotation d'environ -30° de l'arbre manivelle, avant le point mort haut du piston moteur et l'injection principale pourrait être déclenchée à un angle d'environ -15°. Bien entendu, ces valeurs sont données uniquement à titre d'exemple.The position of the bottom dead center of the piston 2 with respect to the movement of the piston of the engine cylinder is chosen such that the start A of the first phase of injection into the engine cylinder is sufficiently advanced relative to the top dead center of the piston of said engine cylinder so that this first injection can constitute a pre-injection ensuring the ignition, in the combustion chamber of an engine cylinder, of the quantity of main injection combustion, practically without ignition delay. For example, the start of pre-injection could take place at an instant corresponding to an angle of rotation of about -30 ° of the crankshaft, before the top dead center of the driving piston and the main injection could be triggered at an angle d 'around -15 °. Of course, these values are given only by way of example.

Il s'est avéré que l'effet de la préinjection varie en fonction de la vitesse de rotation du moteur. A des vitesses relativement basses, l'illustration de la première phase de refoulement, c'est-à-dire du refoulement de préinjection, sous forme d'un rectangle suivant la fig. 6, correspond aux phénomènes qui se produisent réellement.It has been found that the effect of the pre-injection varies as a function of the speed of rotation of the engine. At relatively low speeds, the illustration of the first delivery phase, that is to say the pre-injection delivery, in the form of a rectangle according to FIG. 6, corresponds to the phenomena that actually occur.

Mais, à des vitesses plus élevées, le refoulement et la préinjection, en fonction du temps, prennent plutôt l'allure d'une cloche, du fait que l'établissement de la pression relativement élevée à l'intérieur de la chambre 3 pendant le refoulement de combustible hors de la chambre et la chute de la pression dans la chambre en raison de la mise en communication de celle-ci avec les trous d'arrivée 14 nécessitent un certain délai de temps, puisque les orifices d'arrivée 4 et les trous d'arrivée 14 présentent des sections transversales de valeur limitée.However, at higher speeds, the delivery and the pre-injection, as a function of time, take on the appearance of a bell, because the establishment of the relatively high pressure inside the chamber 3 during the delivery of fuel out of the chamber and the drop in pressure in the chamber due to the communication between the latter and the inlet holes 14 require a certain period of time, since the inlet orifices 4 and the inlet holes 14 have cross sections of limited value.

Ainsi, à des vitesses de rotation élevées, la pression augmentera dans la chambre avant l'obturation des orifices d'arrivée 4 et le découvre- ment des trous d'arrivée 14 par la collerette 13 n'entraînera pas tout de suite la chute de la pression dans la chambre. Par conséquent, un refoulement de combustible et un effet d'injection se produiront même à vitesse élevée du moteur, lorsque l'ouverture des trous 14 intervient avant l'obturation des orifices. Ce refoulement de combustible hors de la chambre par effet de «laminage» peut se produire par exemple pour un piston pourvu d'un cran dans sa surface supérieure 15 et fonctionnant à une position angulaire dans laquelle le cran vient en regard des orifices d'arrivée 4, ce qui retarde la fermeture de ces orifices. Si le cran est suffisamment profond, la gorge 9 peut venir en face des trous 14 avant l'obturation des orifices d'arrivée. A faible vitesse, la phase de refoulement A-B (fig. 6) ne se produirait pas. Mais, à pleine vitesse, grâce à l'effet de laminage, il y aura quand même un refoulement et une préinjection.Thus, at high rotational speeds, the pressure will increase in the chamber before closing the inlet orifices 4 and the discovery of the inlet holes 14 by the flange 13 will not immediately cause the fall of the pressure in the room. Consequently, a fuel backflow and an injection effect will occur even at high engine speed, when the opening of the holes 14 occurs before the orifices are closed. This delivery of fuel out of the chamber by the “rolling” effect can occur, for example, for a piston provided with a notch in its upper surface 15 and operating at an angular position in which the notch comes opposite the inlet orifices. 4, which delays the closing of these orifices. If the notch is deep enough, the groove 9 can come in front of the holes 14 before closing the inlet orifices. At low speed, the delivery phase A-B (fig. 6) would not occur. However, at full speed, thanks to the rolling effect, there will still be a backflow and a pre-injection.

Dans l'exemple décrit et représenté, les arêtes supérieure et inférieure 10, 11 de la deuxième gorge 9 sont droites et circulaires. Mais, il est possible de configurer au moins une arête, par exemple l'arête supérieure, au moins partiellement en rampe hélicoïdale. Ceci permettrait de varier l'instant de la fin du refoulement de préinjection (B sur la fig. 6), par rotation du piston 2 autour de son axe longitudinal. Une configuration appropriée de l'arête inférieure de la gorge 9 permettrait de modifier le début du refoulement d'injection principale (C).In the example described and shown, the upper and lower edges 10, 11 of the second groove 9 are straight and circular. However, it is possible to configure at least one edge, for example the upper edge, at least partial helical ramp. This would make it possible to vary the instant of the end of the pre-injection delivery (B in FIG. 6), by rotation of the piston 2 around its longitudinal axis. An appropriate configuration of the lower edge of the groove 9 would make it possible to modify the start of the main injection delivery (C).

Le mode de réalisation représenté par les figs 2 à 5 comprend une gorge 9 circulaire et deux fois deux trous d'arrivée 14, et ceci dans le but de réduire la hauteur de la gorge 9 et les diamètres desdits trous 14, car ces deux dimensions décident de la distance entre B et C sur la fig. 6, c'est-à-dire le moment de la préinjection par rapport à l'injection principale, d'une part, et la levée de la came correspondant à cette période, d'autre part. Ces mesures permettent de diminuer la longueur de la partie inactive, c'est-à-dire sans refoulement de la course du piston, d'avancer le début du refoulement d'injection principale et/ou retarder le début du refoulement de préinjection.The embodiment represented by FIGS. 2 to 5 comprises a circular groove 9 and twice two inlet holes 14, and this in order to reduce the height of the groove 9 and the diameters of said holes 14, because these two dimensions decide the distance between B and C in fig. 6, that is to say the time of the pre-injection with respect to the main injection, on the one hand, and the lifting of the cam corresponding to this period, on the other hand. These measures make it possible to reduce the length of the inactive part, that is to say without the piston stroke being pushed back, to advance the start of the main injection delivery and / or to delay the start of the pre-injection delivery.

Les figs 7 et 8 montrent un autre mode de réalisation de la pompe d'injection, dans lequel les trous d'arrivée 14' - au nombre de deux dans l'exemple représenté - sont situés approximativement au même niveau que les orifices d'arrivée 4. Deux gorges 9' dont la fonction correspond à celle de la gorge circulaire 9 du premier mode de réalisation sont pratiquées dans la surface périphérique du piston, à une distance prédéterminée de la surface supérieure 15 du piston, sensiblement parallèlement à celle-ci.Figs 7 and 8 show another embodiment of the injection pump, in which the inlet holes 14 '- two in number in the example shown - are located approximately at the same level as the inlet orifices 4. Two grooves 9 ', the function of which corresponds to that of the circular groove 9 of the first embodiment, are formed in the peripheral surface of the piston, at a predetermined distance from the upper surface 15 of the piston, substantially parallel to the latter.

Comme il ressort clairement des figs 7 et 8, chaque gorge 9' débouche à une extrémité dans une rainure verticale 8 et communique ainsi, de façon permanente, avec l'intérieur de la chambre d'admission 3. Selon une variante de réalisation, chaque rainure pourrait être en communication avec cette chambre par ses deux extrémités.As is clear from FIGS. 7 and 8, each groove 9 'opens at one end in a vertical groove 8 and thus communicates, permanently, with the interior of the intake chamber 3. According to an alternative embodiment, each groove could be in communication with this chamber by its two ends.

Le fonctionnement de ce mode de réalisation est le même, au niveau du principe, que celui illustré par les figs 1 à 4. Le refoulement de préinjection débute lorsque les orifices 4 sont obturés par le piston. Les trous d'arrivée 14' sont fermés par la partie de la surface périphérique 13' du piston qui se trouve au-dessus des gorges 9'. Ce refoulement est terminé à l'instant où les gorges 9' viennent en regard des trous 14'. Le refoulement d'injection principale commence après l'obturation des trous 14' par la surface périphérique du piston situé en dessous des gorges 9' et prend fin lorsque la rampe 7 découvre les orifices 4.The operation of this embodiment is the same, in principle, as that illustrated in FIGS. 1 to 4. The pre-injection delivery begins when the orifices 4 are closed by the piston. The inlet holes 14 'are closed by the part of the peripheral surface 13' of the piston which is located above the grooves 9 '. This discharge is finished at the moment when the grooves 9 'come opposite the holes 14'. The main injection delivery starts after the holes 14 'are closed by the peripheral surface of the piston located below the grooves 9' and ends when the ramp 7 discovers the orifices 4.

La pompe d'injection selon la présente invention comprend également des moyens qui permettent la variation du début du refoulement de préinjection. Ces moyens sont formés par un dispositif accumulateur. Selon la représentation schématique donnée par la fig. 9, l'accumulateur comprend une chambre accumulatrice 16 dans laquelle est monté un piston 17 mobile à l'encontre d'un ressort de rappel 18. La chambre 16 communique de façon permanente avec la chambre d'admission 3 de la pompe d'injection par un passage 19 qui débouche dans la chambre 3 à un niveau au-dessus du point mort haut du piston. La partie arrière 20 de la chambre, qui loge le ressort 18, est en communication permanente avec l'espace 21 d'où partent les orifices d'arrivée. Ceci assure qu'une pression relativement basse agit sur la face arrière du piston 17. La course du piston 17 est limitée par une butée 22 formée par exemple par un épaulement de la paroi de la chambre 16. Le piston 17 est déplaçable sur une longueur e. La butée 22 est conformée en siège étanche pour produire une barrière d'étanchéité entre la chambre 16 et la partie 20 de la chambre contenant le ressort 18, lorsque le piston est poussé contre la butée sous l'effet de la forte pression qui règne dans la chambre 3 de la pompe et la chambre 16, lors du refoulement du combustible vers l'injecteur.The injection pump according to the present invention also comprises means which allow the variation of the start of the pre-injection delivery. These means are formed by an accumulator device. According to the schematic representation given in FIG. 9, the accumulator comprises an accumulator chamber 16 in which is mounted a piston 17 movable against a return spring 18. The chamber 16 communicates permanently with the inlet chamber 3 of the injection pump by a passage 19 which opens into the chamber 3 at a level above the top dead center of the piston. The rear part 20 of the chamber, which houses the spring 18, is in permanent communication with the space 21 from which the inlet orifices leave. This ensures that a relatively low pressure acts on the rear face of the piston 17. The stroke of the piston 17 is limited by a stop 22 formed for example by a shoulder of the wall of the chamber 16. The piston 17 is movable over a length e. The stop 22 is shaped as a sealed seat to produce a sealing barrier between the chamber 16 and the part 20 of the chamber containing the spring 18, when the piston is pushed against the stop under the effect of the high pressure prevailing in chamber 3 of the pump and chamber 16, during the delivery of fuel to the injector.

Cet accumulateur fonctionne de la façon suivante: Lorsqu'après obturation des orifices d'arrivée 4, le piston 2 continue sa course de montée, la pression à l'intérieur de la chambre 3 réceptrice n'augmente que doucement puisque la diminution du volume de la chambre réceptrice 3 est compensée par une augmentation du volume de la chambre accumulatrice 16 du fait que le piston 17 recule sous l'effet de l'augmentation de la pression. Par conséquent, la pression qui est nécessaire pour l'ouverture du clapet de refoulement 23 ne peut s'établir qu'après que le piston soit venu en contact sur sa butée de siège étanche 22. Ceci signifie que le point A, sur la fig. 6, se déplace vers le point B et que la quantité de combustible de préinjection refoulé diminue. Par contre, l'interruption du refoulement au point B est indépendant de l'accumulateur et déterminé uniquement par la mise en communication des trous supplémentaires 14 et de la gorge 9 d'interruption du refoulement. Bien que la pression à l'intérieur de la chambre 3 tombe, elle reste cependant, en raison du piston qui continue sa course de montée, à une valeur suffisante pour le maintien sur son siège du piston 17 de l'accumulateur.This accumulator operates as follows: When after closing the inlet orifices 4, the piston 2 continues its upward stroke, the pressure inside the receiving chamber 3 increases only slowly since the decrease in the volume of the receiving chamber 3 is compensated by an increase in the volume of the accumulating chamber 16 due to the fact that the piston 17 moves back under the effect of the increase in pressure. Consequently, the pressure which is necessary for the opening of the discharge valve 23 can only be established after the piston has come into contact on its sealed seat stop 22. This means that point A, in FIG . 6, moves to point B and the amount of pre-injection fuel delivered decreases. On the other hand, the interruption of the discharge at point B is independent of the accumulator and determined only by the communication of the additional holes 14 and of the groove 9 for interrupting the discharge. Although the pressure inside the chamber 3 falls, it remains however, due to the piston which continues its upward stroke, at a value sufficient to maintain the piston 17 of the accumulator on its seat.

Ceci signifie que l'accumulateur n'a aucune influence sur le début du refoulement d'injection principale, mais permet de faire varier le début du refoulement de préinjection (point A sur la fig. 6), et ainsi la quantité du combustible de préinjection.This means that the accumulator has no influence on the start of the main injection delivery, but allows to vary the start of the pre-injection delivery (point A in fig. 6), and thus the quantity of the pre-injection fuel. .

Les figs 10 et 11 illustrent deux modes de réalisation de l'accumulateur 15 conforme à l'invention. Dans les deux cas, l'accumulateur est disposé à côté du dispositif formant organe de décharge 23, au-dessus de la chambre d'admission 3 de la pompe d'injection. Ainsi, l'accumulateur est parfaitement incorporé à la structure de la pompe.Figs 10 and 11 illustrate two embodiments of the accumulator 15 according to the invention. In both cases, the accumulator is placed next to the device forming a discharge member 23, above the inlet chamber 3 of the injection pump. Thus, the accumulator is perfectly incorporated into the structure of the pump.

L'accumulateur représenté sur la fig. 11 est réalisé pour permettre un réglage de l'extérieur du début du refoulement de préinjection. A cet effet, une tige 24 est fixée à la face arrière du piston 17. L'extrémité libre de ladite tige ressort de la pompe. La tige 24 peut être commandée depuis l'extérieur de la pompe, ce qui permet de varier facilement la position finale du piston 17. Il est aussi possible de mettre hors service la préinjection.The accumulator shown in fig. 11 is made to allow adjustment of the outside of the start of the pre-injection delivery. To this end, a rod 24 is fixed to the rear face of the piston 17. The free end of said rod comes out of the pump. The rod 24 can be controlled from outside the pump, which makes it possible to easily vary the final position of the piston 17. It is also possible to deactivate the pre-injection.

Claims (2)

1. Injection pump for an internal combustion engine adapted to deliver an amount of pre-injection fuel before the delivery of the main injection fuel, of the type comprising a fuel receiving chamber (3) defined by a body (1) which is cylindrical and variable in volume by the displacement within this body (1) of a piston (2) in a rectilinear reciprocating motion, the said chamber (3) being provided with fuel admission orifices (4) connected to a source of fuel of relatively low pressure, and obturable by the said piston (2) during its displacement towards its upper dead center to allow the delivery of fuel from the said chamber (3), the said piston (2) having a head provided with at least one helical edge (7) generally intended to define the end of the delivery by the pump and a groove (9) for interrupting the delivery communicating with the said chamber (3), the interruption of the delivery taking place when the groove (9) is opposite at least one passage (14) through the said body (1) and communicating with the said source of fuel, the said passage (14) having a predetermined flow cross-section, characterized in that, in a manner known per se, the pump comprises a device for varying the beginning of the delivery which includes a fuel accumulating chamber 16 in permanent communication with the admission chamber (3) and the volume of which is varied by a plunger (17) mounted movably in the said accumulating chamber (16), counter to a return spring (18), under the action of the fuel pressure in the admission chamber (3) and in that the plunger (17) is sealingly forced onto a seat (22) constituting a stop for limiting the travel of the plunger (17) during the pre-injection and is retained on the seat (22) under the action of a pressure equal to the one produced, during the interruption of the delivery, by the pump piston (2) continuing its upward travel during the said interruption without influencing the beginning of the main injection delivery.
2. An injection pump according to claim 1, characterized in that a stem (24) is secured to the rear face of the said plunger (17) and in that the free end of the said stem (24) projects outwardly of the pump structure to determine the length of the plunger travel.
EP80400720A 1979-05-28 1980-05-22 Injection pump for internal-combustion engine Expired EP0020249B1 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
FR7913486A FR2457987A1 (en) 1979-05-28 1979-05-28 Fuel pump for internal combustion engine - pre-injects small quantity of fuel through small secondary inlet port at beginning of each stroke
FR7913486 1979-05-28
FR8011046 1980-05-16
FR8011046A FR2482669A2 (en) 1979-05-28 1980-05-16 IMPROVEMENT TO INJECTION PUMP FOR INTERNAL COMBUSTION ENGINE

Publications (2)

Publication Number Publication Date
EP0020249A1 EP0020249A1 (en) 1980-12-10
EP0020249B1 true EP0020249B1 (en) 1984-08-22

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US (1) US4426198A (en)
EP (1) EP0020249B1 (en)
JP (1) JPS55161958A (en)
KR (1) KR840001289B1 (en)
AU (1) AU544751B2 (en)
CS (1) CS243455B2 (en)
DD (1) DD151205A5 (en)
DE (1) DE3069004D1 (en)
ES (1) ES8103592A1 (en)
FR (1) FR2482669A2 (en)
PL (1) PL136603B1 (en)
YU (1) YU42508B (en)

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DE923400C (en) * 1941-04-03 1955-02-10 Versuchsanstalt Fuer Luftfahrt Regulation of the fuel quantity of internal combustion engines according to the Otto method with split injection
GB571485A (en) * 1942-09-16 1945-08-27 Bendix Aviat Corp Improvements in or relating to fuel injection apparatus
GB641575A (en) * 1948-01-03 1950-08-16 Cav Ltd Improvements relating to liquid fuel injection pumps
FR1037219A (en) * 1950-05-24 1953-09-15 Cav Ltd Fuel injection pump for internal combustion engines
US2713310A (en) * 1951-11-20 1955-07-19 Cav Ltd Liquid fuel injection pumps
US2810375A (en) * 1953-04-13 1957-10-22 Nordberg Manufacturing Co Injection pump for internal combustion engines
US3792692A (en) * 1972-03-22 1974-02-19 Teledyne Ind Fuel injection device
JPS5221639Y2 (en) * 1973-07-18 1977-05-18
JPS50157721A (en) * 1974-06-10 1975-12-19
JPS525391Y2 (en) * 1974-10-03 1977-02-03
DE2501764A1 (en) * 1975-01-17 1976-07-22 Guenther Kuske Diesel engine fuel injection pump - has plunger with intermediate groove to produce pre-injection before main injection

Also Published As

Publication number Publication date
JPS55161958A (en) 1980-12-16
EP0020249A1 (en) 1980-12-10
AU5882880A (en) 1980-12-04
PL224562A1 (en) 1981-02-27
AU544751B2 (en) 1985-06-13
DD151205A5 (en) 1981-10-08
YU142580A (en) 1983-01-21
CS243455B2 (en) 1986-06-12
YU42508B (en) 1988-10-31
CS375080A2 (en) 1985-08-15
US4426198A (en) 1984-01-17
DE3069004D1 (en) 1984-09-27
JPH0214542B2 (en) 1990-04-09
ES491946A0 (en) 1981-03-16
KR840001289B1 (en) 1984-09-07
PL136603B1 (en) 1986-03-31
FR2482669B2 (en) 1984-07-06
ES8103592A1 (en) 1981-03-16
KR830003002A (en) 1983-05-31
FR2482669A2 (en) 1981-11-20

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