EP1693564B1 - Fuel injector with direct needle control for an internal combustion engine - Google Patents
Fuel injector with direct needle control for an internal combustion engine Download PDFInfo
- Publication number
- EP1693564B1 EP1693564B1 EP05112526A EP05112526A EP1693564B1 EP 1693564 B1 EP1693564 B1 EP 1693564B1 EP 05112526 A EP05112526 A EP 05112526A EP 05112526 A EP05112526 A EP 05112526A EP 1693564 B1 EP1693564 B1 EP 1693564B1
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- European Patent Office
- Prior art keywords
- actuator
- control
- nozzle needle
- space
- piston
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- 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.)
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- 239000000446 fuel Substances 0.000 title claims abstract description 31
- 238000002485 combustion reaction Methods 0.000 title claims description 6
- 238000007789 sealing Methods 0.000 claims description 11
- 230000005540 biological transmission Effects 0.000 abstract description 8
- 230000006835 compression Effects 0.000 description 9
- 238000007906 compression Methods 0.000 description 9
- 238000002347 injection Methods 0.000 description 5
- 239000007924 injection Substances 0.000 description 5
- 239000002131 composite material Substances 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- 230000004913 activation Effects 0.000 description 2
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000004146 energy storage Methods 0.000 description 2
- 230000004308 accommodation Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000002996 emotional effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000009715 pressure infiltration Methods 0.000 description 1
- 238000007639 printing Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000003319 supportive effect Effects 0.000 description 1
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M51/00—Fuel-injection apparatus characterised by being operated electrically
- F02M51/06—Injectors peculiar thereto with means directly operating the valve needle
- F02M51/0603—Injectors peculiar thereto with means directly operating the valve needle using piezoelectric or magnetostrictive operating means
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/167—Means for compensating clearance or thermal expansion
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M2200/00—Details of fuel-injection apparatus, not otherwise provided for
- F02M2200/70—Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger
- F02M2200/703—Linkage between actuator and actuated element, e.g. between piezoelectric actuator and needle valve or pump plunger hydraulic
Definitions
- the invention relates to a fuel injector with direct needle control for an internal combustion engine according to the preamble of claim 1.
- Fuel injectors with a so-called direct needle control are known. Such fuel injectors come without an intermediate control valve between an electrically actuated actuator and a nozzle needle. The power transmission between the actuator and the nozzle needle is realized by means of a hydraulic coupler or hydraulic translator.
- piezoelectric actuators are suitable as actuators, which, depending on the energization in the closed state, have a direct or inverse control. In a direct control of the piezoelectric actuator is energized to open the nozzle needle, so that a linear expansion of the piezoelectric actuator realized by a pressing movement opening the injectors, which is amplified by the translator. In the closed state, the piezoelectric actuator has a smaller linear expansion.
- the piezo actuator In the case of inverse activation, the piezo actuator is charged in the closed state of the nozzle needle, so that the piezo actuator keeps the nozzle needle closed in the state of its longitudinal expansion.
- the piezoactuator When the piezoactuator is actuated, the piezoactuator is discharged to initiate the injection process, so that a pressure relief takes place by a pulling movement of the piezoactuator in a control space of the hydraulic booster. As a result, the lifting movement of the piezo actuator is hydraulically translated to open the nozzle needle.
- a fuel injector with direct needle control is already in the DE patent application 10 2004 037 125.3 proposed.
- the fuel injector in this case has an actuator-side booster piston and a nozzle needle-side booster piston, wherein the actuator-side booster piston is assigned to an actuator-side coupler space and the nozzle needle-side booster piston is assigned to a nozzle needle-side coupler space.
- a hydraulic throttle device is formed, which has different flow cross-sections for the inflow or outflow of fuel into and out of the nozzle needle-side control chamber.
- a first slide sleeve for limiting the actuator-side coupler space and the nozzle needle-side booster piston, a further slide sleeve for limiting the nozzle needle-side coupler space is guided axially.
- the pusher sleeves are biased by a compression spring so that they press with one end face against a sealing surface. The use of the pusher sleeves allows axial decoupling of the actuator-side and the nozzle needle-side booster piston, whereby the booster piston can be mounted with an axial offset.
- a fuel injector with direct needle control and an outwardly opening injection valve with a hydraulic coupler to compensate for the linear expansion and pressure-induced expansion of the fuel injector is out DE 101 48 594 A1 known.
- the hydraulic coupler which forms a translator assembly between an actuator and a nozzle needle, includes an actuator-side booster piston and a nozzle needle-side booster piston guided in a guide sleeve.
- a corrugated tube Arranged around the guide sleeve is a corrugated tube which encloses a hydraulic fluid separated from the fuel.
- the stroke-adjustable guide sleeve associated with the actuator-side booster piston acts on a first control surface actuator-side coupler space and with a second control surface on a further coupler space.
- the actuator-side booster piston has with a first pressure surface in the first coupler space and with a further pressure surface in the further coupler space.
- the object of the present invention is to provide a fuel injector with two-stage transmission with different transmission ratios.
- the object of the invention is achieved with the characterizing features of claim 1.
- a fuel injector with direct needle control with compact and small size can be realized, which manages with few moving components to realize the required ratios for a two-stage translation.
- the two-stage gear ratio of the Aktorhubs with different ratios is realized by the control in a first opening phase of the nozzle needle by the applied pressure at its control surfaces in an initial position and at the beginning of a second opening phase of the nozzle needle due to the changing pressure conditions on the control surfaces of the Control lifts the control from the starting position, so that increases the volume in the actuator-side coupler space, whereby the translation between aktor discoveredem and nozzle-side booster piston is changed.
- the control chamber acts as a pressure or energy storage, so that formed to initiate the second opening phase, a pressure threshold in the control room.
- an axially displaceably guided control sleeve is arranged as a control element on the actuator-side booster piston whose first end face is hydraulically coupled as a first control surface to the actuator-side coupler space and whose second end face is assigned to the control chamber as a second control surface.
- the first end face is in relation to a first opening phase of the nozzle needle in an initial position.
- the first end face lifts off from the starting position, so that with respect to the second opening phase of the nozzle needle an effective surface is exposed to the actuator-side coupler space, which is composed of the pressure surface of the booster piston and the first end face.
- the actuator-side booster piston is a stepped piston, with which the first pressure surface and the second pressure surface are formed.
- An expedient embodiment of the fuel injector also consists in that the coupler space associated with the actuator-side pressure booster piston is connected via a hydraulic connection to a nozzle needle-side coupler space assigned to the nozzle needle-side booster piston.
- a slide sleeve is guided on the actuator-side booster piston.
- the in FIG. 1 illustrated fuel injector has an injector 10 with a nozzle body 11 which projects with its lower end into a combustion chamber of an internal combustion engine.
- a nozzle needle guide 12 is formed, in which a nozzle needle 13 is guided with a guide portion 14 axially displaceable.
- a sealing seat 15 is formed, which are arranged downstream of the injection nozzle 16 formed in the nozzle body 11 and projecting into the combustion chamber.
- the injector housing 10 has a receiving space 18 which is connected to a fuel feed, not shown, which is connected to a high-pressure system, for example to a common-rail system of a diesel injection device.
- an intermediate body 19 with an actuator-side surface 23 and a nozzle needle-side surface 24 is arranged, which is designed with connecting bores 21 and with a hydraulic connection acting as a throttle 22.
- the connecting bores 21 serve to forward the fuel introduced into the receiving space 18 via the fuel supply at high pressure into a high-pressure space 25 assigned to the nozzle needle 13.
- a piezoelectric actuator 20 is arranged, which acts on a hydraulic booster 30.
- the hydraulic booster 30 has an actuator-side booster piston 31 which is drive-coupled to the piezo-actuator 20 and which is also housed in the receiving space 18.
- the actuator-side booster piston 31 is designed as a stepped piston with a first piston portion 32 with a diameter d1 and with a second piston portion 33 with a diameter d2, where d2> d1.
- the hydraulic booster 30 further comprises a second piston portion 33 axially guided sliding sleeve 34, an axially between the sleeve 34 and the first piston portion 32 axially guided control sleeve 35, an actuator-side coupler 36 and a control chamber 37.
- a coupler-space-side pressure surface 38 is formed, which faces into the actuator-side coupler space 36. Due to the diameter ratio d1 ⁇ d2 between the first piston section 32 and the second piston section 33, there is an annular surface with a second pressure surface 48 on the second piston section 33 which points into the control chamber 37 as a further control surface.
- the control sleeve 35 has the function of a control element 40 associated with FIG. 3 generally described.
- the control sleeve 35 has a first end face 44 and a second end face 45 and is biased by a compression spring 43 on the actuator-side booster piston 31.
- the compression spring 43 causes the control sleeve 35 is held until the initiation of the second opening phase of the nozzle needle 13 in an initial position.
- the control sleeve 35 is pressed with the first end face 44 against the actuator-side surface 23 of the intermediate body 19, so that the control sleeve 35 limits the actuator-side coupler space 36 in this position.
- the first end face 44 forms a hydraulically coupled first control surface 47 with the actuator-side coupler space 36.
- the second end face 45 which is formed opposite the end face 44 on the control sleeve 35, points into the control space 37 and forms a second control surface 46 with respect to the control space 37 the control sleeve 35.
- the slide sleeve 34 is also biased by a further compression spring 49 on the actuator-side booster piston 31.
- the sliding sleeve 34 according to FIG. 2 pressed with an end face 42 against the actuator-side surface 23 of the intermediate body 19, so that a sealing surface on the surface 23 forms.
- To the hydraulic translator 30 further includes a connected to the nozzle needle 13 nozzle needle-side booster piston 51 having a diameter d3, which has a nozzle needle side pressure surface 52 in a nozzle needle side coupler 53.
- a further slide sleeve 54 is guided axially, which is pressed by means of a closing spring 56 against the nozzle needle-side surface 24 of the intermediate body 19 and so the nozzle needle-side coupler space 53 limited.
- the nozzle needle-side coupler space 53 is connected to the actuator-side coupler space 36 via the hydraulic connection 22.
- the hydraulic connection 22 can act as a throttle.
- the sealing seat 15 of the nozzle needle 13 is closed.
- the system pressure which has reached the receiving space 18 and the pressure space 25 via the fuel supply, equally rests in all pressure chambers.
- 35 leakage gaps are present on the slide sleeves 34, 54 and the control sleeve, such that the system pressure is present in the actuator-side coupler space 36, in the control space 37 and in the nozzle needle-side coupler space 53 via the leakage gaps.
- the hydraulic booster 30 is pressure compensated.
- the piezoelectric actuator 20 is supplied with a voltage, whereby the piezoelectric actuator 20 is elongated in its loaded state in the vertical direction.
- the system pressure applied in the nozzle needle-side coupler chamber 53 acts in the closing direction on the nozzle needle-side booster piston 51.
- the sealing seat 15 of the nozzle needle 13 is closed in this state of the piezoelectric actuator 20.
- the closing spring 56 acts on the nozzle needle, the closing spring 56 which holds the nozzle needle 13 closed in the idle state.
- the length of the piezoelectric actuator 20 in the vertical direction is likewise reduced.
- the piezo actuator 20 is thus operated inversely. Due to the biased by the compression spring 49 in the direction of the piezoelectric actuator 20 actuator-side booster piston 31 this is also moved in the vertical direction due to the reduced vertical length of the piezo-actuator 20.
- the opening pressure is transmitted via the hydraulic connection 22 into the nozzle needle-side coupler space 53, so that the opening pressure also bears against the nozzle needle-side pressure surface 52.
- a first gear ratio for opening the nozzle needle 13 is introduced, which is effective due to the area ratios of the pressure surfaces 38 and 52, wherein the gear ratio of the first opening phase by the area ratio d1 2 / d3 2 is determined.
- the volume in the control chamber 37 is increased by the second piston portion 33 and pointing in the control chamber 37 upward movement of the second pressure surface 48, whereby the pressure drops in the control chamber 37.
- the control chamber 37 acts as a pressure accumulator or energy storage in the form of a hydraulic spring.
- the actuator-side coupler space 36 is thus exposed to an effective pressure surface, which is composed of the actuator-side pressure surface 38 of the first piston portion 32 and the first end surface 44 of the control sleeve 35.
- an effective pressure surface which is composed of the actuator-side pressure surface 38 of the first piston portion 32 and the first end surface 44 of the control sleeve 35.
- the inner diameter of the slide sleeve 34 is guided on the diameter d2 of the second piston portion 33 and the control sleeve 35 between the slide sleeve 34 and the first piston portion 32 is arranged, wherein the outer diameter of the control sleeve 35 is guided on the inner diameter of the slide sleeve 34, the composite effective pressure surface determined by the outer diameter of the control sleeve 35, which corresponds to the diameter d2.
- the composite effective pressure surface causes a translation jump, which acts as a second gear ratio on the nozzle needle side pressure surface 52 of the nozzle needle side booster piston 51.
- the stroke of the piezoactuator 20 is transmitted to the nozzle needle 13 with a larger ratio, which results from the area ratios of the composite effective pressure surface to the pressure surface 52, wherein the second transmission ratio is determined by the area ratios d2 2 / d3 2 .
- the nozzle needle 13 is moved at a greater speed and with a larger stroke.
- the control element 40 with the control surface 46 in the control chamber 37 which is shown as a piston, initially remains in one due to the pressure prevailing in the control chamber 37 starting position.
- the compression spring 43 acts only supportive.
- the pressure in the control chamber 37 is further reduced by means of the second piston section 33 until the pressure applied in the space 36 'is fallen below.
- the control element 40 with the area A1 which corresponds to the first control surface 47, emotional.
- the pulling movement of the surface A1 creates an additional volume in the space 36 ', which also becomes effective via the connection 22' in the actuator-side coupler space 36.
- the additional volume is transmitted via the connection 22 to the nozzle needle-side coupler space 53, so that the surface A4 of the nozzle needle-side booster piston 51 now faces the sum of the areas A1 and A3 as the ratio for realizing the second opening phase.
- the gear ratio of the second opening phase (A1 + A3) to A4 is thus greater than the ratio of the first opening phase resulting from the ratio of A3 to A4. Due to the larger transmission ratio of the second opening phase, a larger opening speed is realized with a larger stroke when opening the nozzle needle 13.
- the first piston portion 32 with the pressure surface 38 increases the pressure in the actuator-side coupler space 36, which is transmitted via the hydraulic connection 22 to the nozzle needle-side coupler space 53, wherein the nozzle needle 13 on the sealing seat due to the pressure increase in the nozzle needle-side coupler space 53 by means of the nozzle needle side booster piston 51 15 is pressed and thereby the injection nozzles 16 are separated from the pressure chamber 25.
- a pressure-balanced state is again formed in the pressure chambers of the hydraulic booster 30.
Abstract
Description
Die Erfindung betrifft einen Kraftstoffmjektor mit direkter Nadelsteuerung für eine Brennkraftmaschine nach dem Oberbegriff des Anspruchs 1.The invention relates to a fuel injector with direct needle control for an internal combustion engine according to the preamble of claim 1.
Kraftstoffmjektoren mit einer sogenannten direkten Nadelsteuerung sind bekannt. Derartige Kraftstoffinjektoren kommen ohne ein zwischengeschaltetes Steuerventil zwischen einem elektrisch angesteuerten Aktor und einer Düsennadel aus. Die Kraftübertragung zwischen dem Aktor und der Düsennadel wird dabei mittels eines hydraulischen Kopplers bzw. hydraulischen Übersetzers realisiert. Als Aktoren eignen sich dabei insbesondere piezoelektrische Aktoren, die je nach Bestromung im geschlossenen Zustand eine direkte oder inverse Ansteuerung aufweisen. Bei einer direkten Ansteuerung wird der Piezo-Aktor zum Öffnen der Düsennadel bestromt, so dass eine Längenausdehnung des Piezo-Aktors durch eine drückende Bewegung ein Öffnen der Einspritzdüsen realisiert, die durch den Übersetzer verstärkt wird. Im geschlossenen Zustand weist dabei der Piezo-Aktor eine geringere Längenausdehnung auf. Bei einer inversen Ansteuerung ist der Piezo-Aktor im geschlossenen Zustand der Düsennadel geladen, so dass der Piezo-Aktor im Zustand seiner Längenausdehnung die Düsennadel geschlossen hält. Beim Ansteuern des Piezo-Aktors wird zum Einleiten des Einspritzvorganges der Piezo-Aktor entladen, so dass durch eine ziehende Bewegung des Piezo-Aktors in einem Steuerraum der hydraulische Übersetzer eine Druckentlastung stattfindet. Dadurch wird die Hubbewegung des Piezo-Aktors zum Öffnen der Düsennadel hydraulisch übersetzt.Fuel injectors with a so-called direct needle control are known. Such fuel injectors come without an intermediate control valve between an electrically actuated actuator and a nozzle needle. The power transmission between the actuator and the nozzle needle is realized by means of a hydraulic coupler or hydraulic translator. In particular, piezoelectric actuators are suitable as actuators, which, depending on the energization in the closed state, have a direct or inverse control. In a direct control of the piezoelectric actuator is energized to open the nozzle needle, so that a linear expansion of the piezoelectric actuator realized by a pressing movement opening the injectors, which is amplified by the translator. In the closed state, the piezoelectric actuator has a smaller linear expansion. In the case of inverse activation, the piezo actuator is charged in the closed state of the nozzle needle, so that the piezo actuator keeps the nozzle needle closed in the state of its longitudinal expansion. When the piezoactuator is actuated, the piezoactuator is discharged to initiate the injection process, so that a pressure relief takes place by a pulling movement of the piezoactuator in a control space of the hydraulic booster. As a result, the lifting movement of the piezo actuator is hydraulically translated to open the nozzle needle.
Ein Kraftstoffinjektor mit direkter Nadelsteuerung wird bereits in der
Ein Kraftstoffinjektor mit direkter Nadelsteuerung und einem nach außen öffnenden Einspritzventil mit einem hydraulischen Koppler zur Kompensation der Längenausdehnung und druckbedingter Dehnung des Kraftstoffinjektors ist aus
Aufgabe der vorliegenden Erfindung ist es, einen Kraftstoffinjektor mit zweistufiger Übersetzung mit unterschiedlichen Übersetzungsverhältnissen zu schaffen.The object of the present invention is to provide a fuel injector with two-stage transmission with different transmission ratios.
Die Aufgabe der Erfindung wird mit den kennzeichnenden Merkmalen des Anspruchs 1 gelöst. Mit den Merkmalen des Anspruchs 1 ist ein Kraftstoffinjektor mit direkter Nadelsteuerung mit kompakter und geringer Baugröße realisierbar, der mit wenigen beweglichen Bauteilen zur Realisierung der erforderlichen Übersetzungsverhältnisse für eine zweistufige Übersetzung auskommt.The object of the invention is achieved with the characterizing features of claim 1. With the features of claim 1, a fuel injector with direct needle control with compact and small size can be realized, which manages with few moving components to realize the required ratios for a two-stage translation.
Die zweistufige Übersetzung des Aktorhubs mit unterschiedlichen Übersetzungsverhältnissen wird dadurch realisiert, indem in einer erster Öffnungsphase der Düsennadel das Steuerelement durch die an seinen Steuerflächen anliegenden Drücke in einer Ausgangsposition liegt und indem zu Beginn einer zweiten Öffnungsphase der Düsennadel aufgrund der sich ändernden Druckverhältnisse an den Steuerflächen des Steuerelements das Steuerelement von der Ausgangsposition abhebt, so dass sich das Volumen im aktorseitigen Kopplerraum vergrößert, wodurch die Übersetzung zwischen aktorseitigem und düsenseitigem Übersetzerkolben verändert wird. Der Steuerraum wirkt als Druck- bzw. Energiespeicher, so dass sich zur Einleitung der zweiten Öffnungsphase eine Druckschwelle im Steuerraum ausgebildet.The two-stage gear ratio of the Aktorhubs with different ratios is realized by the control in a first opening phase of the nozzle needle by the applied pressure at its control surfaces in an initial position and at the beginning of a second opening phase of the nozzle needle due to the changing pressure conditions on the control surfaces of the Control lifts the control from the starting position, so that increases the volume in the actuator-side coupler space, whereby the translation between aktorseitigem and nozzle-side booster piston is changed. The control chamber acts as a pressure or energy storage, so that formed to initiate the second opening phase, a pressure threshold in the control room.
Vorteilhafte Weiterbildungen der Erfindung sind durch die Maßnahmen der Unteransprüche möglich.Advantageous developments of the invention are possible by the measures of the subclaims.
Besonders vorteilhaft ist, wenn als Steuerelement am aktorseitigen Übersetzerkolben eine axial verschiebbar geführte Steuerhülse angeordnet ist, deren erste Stirnfläche als erste Steuerfläche mit dem aktorseitigen Kopplerraum hydraulisch gekoppelt und deren zweite Stirnfläche als zweite Steuerfläche dem Steuerraum zugeordnet ist. Die erste Stirnfläche liegt dabei bezüglich einer ersten Öffnungsphase der Düsennadel in einer Ausgangsposition. Bezüglich einer zweiten Öffnungsphase der Düsennadel hebt die erste Stirnfläche von der Ausgangsposition ab, so dass bezüglich der zweiten Öffnungsphase der Düsennadel dem aktorseitigen Kopplerraum eine wirksame Fläche ausgesetzt ist, die sich aus der Druckfläche des Übersetzerkolbens und der ersten Stirnfläche zusammensetzt.It is particularly advantageous if an axially displaceably guided control sleeve is arranged as a control element on the actuator-side booster piston whose first end face is hydraulically coupled as a first control surface to the actuator-side coupler space and whose second end face is assigned to the control chamber as a second control surface. The first end face is in relation to a first opening phase of the nozzle needle in an initial position. With regard to a second opening phase of the nozzle needle, the first end face lifts off from the starting position, so that with respect to the second opening phase of the nozzle needle an effective surface is exposed to the actuator-side coupler space, which is composed of the pressure surface of the booster piston and the first end face.
Zweckmäßigerweise ist der aktorseitige Übersetzerkolben ein Stufenkolben, mit dem die ersten Druckfläche und die zweiten Druckfläche ausgebildet sind. Eine zweckmäßige Ausführungsform des Kraftstoffinjektors besteht außerdem darin, indem der dem aktorseitigen Druckübersetzerkolben zugeordnete Kopplerraum über eine hydraulische Verbindung mit einem dem düsennadelseitigen Übersetzerkolben zugeordneten düsennadelseitigen Kopplerraum verbunden ist. Zur Ausbildung des dem aktorseitigen Übersetzerkolben zugeordneten Steuerraums und Kopplerraums ist am aktorseitigen Übersetzerkolben eine Schieberhülse geführt.Conveniently, the actuator-side booster piston is a stepped piston, with which the first pressure surface and the second pressure surface are formed. An expedient embodiment of the fuel injector also consists in that the coupler space associated with the actuator-side pressure booster piston is connected via a hydraulic connection to a nozzle needle-side coupler space assigned to the nozzle needle-side booster piston. To form the actuator-side booster piston associated control chamber and coupler space a slide sleeve is guided on the actuator-side booster piston.
Ein Ausführungsbeispiel der Erfindung ist in der Zeichnung dargestellt und in der nachfolgenden Beschreibung näher erläutert.An embodiment of the invention is illustrated in the drawing and explained in more detail in the following description.
Es zeigen
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Figur 1 eine Schnittdarstellung durch einen Teil eines erfindungsgemäßen Kraftstoffinjektors, -
einen vergrößerten Ausschnitt X gemäßFigur 2Figur 1 und -
Figur 3 ein hydraulisches Ersatzschaltbild der Wirkungsweise des erfindungsgemäßen Kraftstoffinjektors.
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FIG. 1 a sectional view through a portion of a fuel injector according to the invention, -
FIG. 2 an enlarged section X according toFIG. 1 and -
FIG. 3 a hydraulic equivalent circuit diagram of the operation of the fuel injector according to the invention.
Der in
Im Aufnahmeraum 18 ist ein Piezo-Aktor 20 angeordnet, der auf einen hydraulischen Übersetzer 30 einwirkt. Der hydraulische Übersetzer 30 weist einen aktorseitigen Übersetzerkolben 31 auf, der mit dem Piezo-Aktor 20 antriebsgekoppelt ist und der ebenfalls im Aufnahmeraum 18 untergebracht ist. Der aktorseitige Übersetzerkolben 31 ist als Stufenkolben mit einem ersten Kolbenabschnitt 32 mit einem Durchmesser d1 und mit einem zweiten Kolbenabschnitt 33 mit einem Durchmesser d2 ausgeführt, wobei d2 > d1 ist. Der hydraulische Übersetzer 30 weist ferner eine am zweiten Kolbenabschnitt 33 axial geführte Schieberhülse 34, eine zwischen Schieberhülse 34 und dem ersten Kolbenabschnitt 32 axial geführte Steuerhülse 35, einen aktorseitigen Kopplerraum 36 sowie einen Steuerraum 37 auf. Am ersten Kolbenabschnitt 32 des aktorseitigen Übersetzerkolbens 31 ist gemäß
Die Steuerhülse 35 besitzt die Funktion eines Steuerelements 40, das im Zusammenhang mit
Die Schieberhülse 34 ist mittels einer weiteren Druckfeder 49 ebenfalls am aktorseitigen Übersetzerkolben 31 vorgespannt. Dadurch wird die Schieberhülse 34 gemäß
Zum hydraulischen Übersetzer 30 gehört ferner ein mit der Düsennadel 13 verbundener düsennadelseitiger Übersetzerkolben 51 mit einem Durchmesser d3, der mit einer düsennadelseitigen Druckfläche 52 in einen düsennadelseitigen Kopplerraum 53 weist. Am düsennadelseitigen Übersetzerkolben 51 ist eine weitere Schieberhülse 54 axial geführt, die mittels einer Schließfeder 56 gegen die düsennadelseitige Fläche 24 des Zwischenkörpers 19 gedrückt wird und so den düsennadelseitigen Kopplerraum 53 begrenzt. Der düsennadelseitige Kopplerraum 53 ist über die hydraulische Verbindung 22 mit dem aktorseitigen Kopplerraum 36 verbunden. Die hydraulische Verbindung 22 kann als Drossel wirken. Durch die Verwendung von Schieberhülsen 34 und 54 an den Übersetzerkolben 31 und 51 wird eine axiale Entkopplung des aktorseitigen Übersetzerkolbens 31 und des düsennadelseitigen Übersetzerkolbens 51 realisiert.To the
Im geschlossenen Zustand der Einspritzdüsen 16 ist der Dichtsitz 15 der Düsennadel 13 geschlossen. Der über die Kraftstoffzufiihrung in den Aufnahmeraum 18 und in den Druckraum 25 gelangte Systemdruck liegt in allen Druckräumen gleichermaßen an. Dabei sind an den Schieberhülsen 34, 54 und der Steuerhülse 35 Leckagespalte vorhanden, so dass über die Leckagespalte der Systemdruck sowohl im aktorseitigen Kopplerraum 36, im Steuerraum 37 und im düsennadelseitigen Kopplerraum 53 vorliegt. In diesem Zustand ist der hydraulische Übersetzer 30 druckausgeglichen. Außerdem ist in diesem Zustand der Piezo-Aktor 20 mit einer Spannung versorgt, wodurch der Piezo-Aktor 20 in seinem beladenen Zustand in vertikaler Richtung gelängt ist. Der im düsennadelseitigen Kopplerraum 53 anliegende Systemdruck wirkt in Schließrichtung auf den düsennadelseitigen Übersetzerkolben 51. Dadurch ist in diesem Zustand des Piezo-Aktors 20 der Dichtsitz 15 der Düsennadel 13 geschlossen. Außerdem wirkt auf die Düsennadel die Schließfeder 56, die die Düsennadel 13 im betriebslosen Zustand geschlossen hält.In the closed state of the
Wird die Spannung am Piezo-Aktor 20 reduziert bzw. der Piezo-Aktor 20 über einen Strom entladen, wird ebenso die Länge des Piezo-Aktors 20 in vertikaler Richtung reduziert. Der Piezo-Aktor 20 wird somit invers betrieben. Durch den mittels der Druckfeder 49 in Richtung des Piezo-Aktors 20 vorgespannten aktorseitigen Übersetzerkolbens 31 wird dieser aufgrund der reduzierten vertikalen Länge des Piezo-Aktors 20 ebenfalls in vertikaler Richtung bewegt. Durch diese nach außen gerichtete ziehende Bewegung des aktorseitigen Übersetzerkolbens 31 erfolgt mittels der Druckfläche 38 des ersten Kolbenabschnitts 32 eine Vergrößerung des Volumens im aktorseitigen Kopplerraum 36, wodurch dort eine Druckreduzierung stattfindet, die einen Öffnungsdruck für eine erste Öffnungsphase zum Öffnen der Düsennadel 13 liefert. Der Öffnungsdruck wird über die hydraulische Verbindung 22 in den düsennadelseitigen Kopplerraum 53 übertragen, so dass der Öffnungsdruck ebenfalls an der düsennadelseitigen Druckfläche 52 anliegt. Dadurch wird ein erstes Übersetzungsverhältnis zum Öffnen der Düsennadel 13 eingeleitet, das aufgrund der Flächenverhältnisse der Druckflächen 38 und 52 wirksam ist, wobei das Übersetzungsverhältnis der ersten Öffnungsphase durch das Flächenverhältnis d12/d32 bestimmt wird. Gleichzeitig mit der ziehenden Bewegung des aktorseitigen Übersetzerkolbens 31 wird durch den zweiten Kolbenabschnitt 33 und der in den Steuerraum 37 weisenden Aufwärtsbewegung der zweiten Druckfläche 48 das Volumen im Steuerraum 37 erhöht, wodurch auch im Steuerraum 37 der Druck abfällt. Der Steuerraum 37 wirkt dabei als Druckspeicher bzw. Energiespeicher in Form einer hydraulischen Feder. Mit zunehmendem Hub der Düsennadel 51 steigt der Druck im düsenseitigen Kopplerraum 53 wegen der Druckunterwanderung am Dichtsitz 15 der Düsennadel 13 wieder an, während der Druck im Steuerraum 37 weiter abfällt. Dies führt zu Bedingungen, die die Steuerhülse 35 von der aktorseitigen Fläche 23 abheben lässt. Dadurch liegt an der Steuerhülse 35 die erste Stirnfläche 44 frei, die nun als erste Steuerfläche 47 auf den aktorseitigen Kopplerraum 36 einwirkt. Der aktorseitige Kopplerraum 36 wird nun radial von der Schieberhülse 34 begrenzt. Dem aktorseitigen Kopplerraum 36 ist somit eine wirksame Druckfläche ausgesetzt, die sich aus der aktorseitigen Druckfläche 38 des ersten Kolbenabschnitts 32 und der ersten Stirnfläche 44 der Steuerhülse 35 zusammensetzt. Dadurch, dass der innere Durchmesser der Schieberhülse 34 am Durchmesser d2 des zweiten Kolbenabschnitts 33 geführt ist und die Steuerhülse 35 zwischen Schieberhülse 34 und ersten Kolbenabschnitt 32 angeordnet ist, wobei der äußere Durchmesser der Steuerhülse 35 am inneren Durchmesser der Schieberhülse 34 geführt ist, wird die zusammengesetzte wirksame Druckfläche durch den Außendurchmesser der Steuerhülse 35 bestimmt, die dem Durchmesser d2 entspricht. Die zusammengesetzte wirksame Druckfläche bewirkt einen Übersetzungssprung, der als zweites Übersetzungsverhältnis auf die düsennadelseitige Druckfläche 52 der düsennadelseitigen Übersetzerkolbens 51 wirkt. Dadurch wird der Hub des Piezo-Aktors 20 mit einer größeren Übersetzung auf die Düsennadel 13 übertragen, der sich aus dem Flächenverhältnisse der zusammengesetzten wirksamen Druckfläche zur Druckfläche 52 ergibt, wobei das zweite Übersetzungsverhältnis durch das Flächenverhältnisse d22/d32 bestimmt wird. Infolgedessen wird die Düsennadel 13 mit einer größeren Geschwindigkeit und mit einem größeren Hubweg bewegt.If the voltage at the
Anhand des in
Durch Bestromen des Piezo-Aktors 20 wird wieder eine Verlängerung des Piezo-Aktors 20 eingeleitet, die vom aktorseitigen Übersetzerkolben 31 auf den Steuerraum 37 und den aktorseitigen Kopplerraum 36 übertragen wird. Zunächst wird unterstützt durch die Druckfeder 43, die Steuerhülse 35 mit der Stirnfläche 44 gegen die Fläche 23 gedrückt, so dass der aktorseitige Kopplerraum 36 unterhalb der aktorseitigen Druckfläche 38 entsteht. Gleichzeitig erhöht der erste Kolbenabschnitt 32 mit der Druckfläche 38 den Druck im aktorseitigen Kopplerraum 36, der über die hydraulische Verbindung 22 auf den düsennadelseitigen Kopplerraum 53 übertragen wird, wobei aufgrund des Druckanstiegs im düsennadelseitigen Kopplerraum 53 mittels des düsennadelseitigen Übersetzerkolbens 51 die Düsennadel 13 auf den Dichtsitz 15 gepresst wird und dadurch die Einspritzdüsen 16 vom Druckraum 25 getrennt werden. Gleichzeitig bildet sich in den Druckräumen des hydraulischen Übersetzers 30 wieder ein druckausgeglichener Zustand aus.By energizing the piezo-
- 1010
- Injektorgehäuseinjector
- 1111
- Düsenkörpernozzle body
- 1212
- DüsennadelführungNozzle needle guide
- 1313
- Düsennadelnozzle needle
- 1414
- Führungsabschnittguide section
- 1515
- Dichtsitzsealing seat
- 1616
- Einspritzdüseninjectors
- 1818
- Aufnahmeraumaccommodation space
- 1919
- Zwischenkörperintermediate body
- 2020
- Piezo-AktorPiezo actuator
- 2121
- Verbindungsbohrungconnecting bore
- 2222
- hydraulische Verbindunghydraulic connection
- 22'22 '
- Verbindungconnection
- 2323
- aktorseitige StirnflächeActuator-side face
- 2424
- düsennadelseitige Stirnflächenozzle needle-side end face
- 2525
- HochdruckraumHigh-pressure chamber
- 3030
- hydraulischer Übersetzerhydraulic translator
- 3131
- aktorseitiger ÜbersetzerkolbenActuator-side booster piston
- 3232
- erster Kolbenabschnittfirst piston section
- 3333
- zweiter Kolbenabschnittsecond piston section
- 3434
- Schieberhülsesliding sleeve
- 3535
- Steuerhülsecontrol sleeve
- 3636
- aktorseitiger Kopplerraumactuator-side coupler space
- 36'36 '
- Raumroom
- 3737
- Steuerraumcontrol room
- 3838
- kopplerraumseitige DruckflächeCoupling chamber-side pressure surface
- 4040
- Steuerelementcontrol
- 4242
- Stirnflächeface
- 4343
- Druckfedercompression spring
- 4444
- erste Stirnflächefirst end face
- 4545
- zweite Stirnflächesecond end face
- 4646
- zweite Steuerflächesecond control surface
- 4747
- erste Steuerflächefirst control surface
- 4848
- zweite Druckflächesecond printing surface
- 4949
- weitere Druckfederfurther compression spring
- 5151
- düsennadelseitiger ÜbersetzerkolbenNozzle needle-side booster piston
- 5252
- düsennadelseitige Druckflächenozzle needle side pressure surface
- 5353
- düsennadelseitiger Kopplerraumnozzle needle-side coupler space
- 5454
- düsennadelseitige Schieberhülsenozzle needle side slide sleeve
- 5656
- Schließfederclosing spring
Claims (9)
- Fuel injector for an internal combustion engine having a nozzle needle (13) which is guided in a nozzle body and which acts on a nozzle needle sealing seat (15), having an actuator (20) and having a hydraulic booster (30) with an actuator-side booster piston (31) which is connected to the actuator and with a nozzle-needle-side booster piston (51) which is connected to the nozzle needle (13), with the actuator-side booster piston (31) and the nozzle-needle-side booster piston (51) acting on at least one booster space, with an actuator-side coupler space (36) being formed as a booster space, which coupler space (36) is assigned a pressure surface (38) of the actuator-side booster piston (31), with the nozzle needle (13) being lifted up from the nozzle needle sealing seat (15) as a function of the pressure in the actuator-side coupler space (36) and with highly pressurized fuel thereby being injected, with a stroke-adjustable control element (40) being provided in addition to the actuator-side booster piston (31), which control element (40) is hydraulically coupled with a first control surface (A1, 47) to the actuator-side coupler space (36) and is assigned with a second control surface (46) to a control space (37), and with the actuator-side booster piston (31) having a second pressure surface (48) which is assigned, as a further control surface, to the control space (37), characterized in that, in a first opening phase of the nozzle needle (13), the control element (40) is in a starting position and in that, in a second opening phase of the nozzle needle (13), the control element (40) lifts up from the starting position.
- Fuel injector according to Claim 1, characterized in that the control element (40) is guided in a stroke-adjustable fashion on the actuator-side booster piston (31).
- Fuel injector according to Claim 1 or 2, characterized in that the control element (40) is a control sleeve (35) which is guided axially on the actuator-side booster piston (31) and whose first end surface (44) is hydraulically coupled, as a first control surface (47), to the actuator-side coupler space (36) and whose second end surface (45) is assigned, as a second control surface (46), to the control space (37).
- Fuel injector according to Claim 3, characterized in that, with regard to a first opening phase of the nozzle needle (13), the first end surface (44) is in a starting position, and in that, with regard to a second opening phase of the nozzle needle (13), the first end surface (44) lifts up from the starting position, such that with regard to the second opening phase of the nozzle needle (13), an effective surface, which is composed of the pressure surface (38) of the booster piston (31) and the first end surface (44), is exposed to the actuator-side coupler space (36).
- Fuel injector according to Claim 4, characterized in that a pressure spring (43) is provided which places the control sleeve (35) into a starting position before the start of the first opening phase of the nozzle needle (13) .
- Fuel injector according to one of the preceding claims, characterized in that the actuator-side booster piston (31) is a stepped piston with a first piston section (32) and with a second piston section (33) and in that the actuator-side coupler space (36) is assigned to the first piston section (32) with the pressure surface (38) and the control space (37) is assigned to the second piston section (33) with a second pressure surface (48).
- Fuel injector according to Claim 6, characterized in that the control sleeve (35) is guided axially on the first piston section (32).
- Fuel injector according to Claim 6 or 7, characterized in that a sliding sleeve (34) is guided axially on the second piston section (33) and in that the control sleeve (35) is guided axially between the first piston section (32) and the sliding sleeve (34).
- Fuel injector according to one of the preceding claims, characterized in that a nozzle-needle-side coupler space (53) is provided, to which a nozzle-needle-side pressure surface (52) of the nozzle-needle-side booster piston (51) is exposed, and in that the actuator-side coupler space (36) and the nozzle-needle-side coupler space (53) are connected by means of a hydraulic connection (22).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102005007543A DE102005007543A1 (en) | 2005-02-18 | 2005-02-18 | Fuel injector with direct needle control for an internal combustion engine |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1693564A2 EP1693564A2 (en) | 2006-08-23 |
EP1693564A3 EP1693564A3 (en) | 2007-01-10 |
EP1693564B1 true EP1693564B1 (en) | 2008-07-23 |
Family
ID=36337484
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05112526A Not-in-force EP1693564B1 (en) | 2005-02-18 | 2005-12-20 | Fuel injector with direct needle control for an internal combustion engine |
Country Status (4)
Country | Link |
---|---|
US (1) | US7258283B2 (en) |
EP (1) | EP1693564B1 (en) |
AT (1) | ATE402337T1 (en) |
DE (2) | DE102005007543A1 (en) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10352736A1 (en) * | 2003-11-12 | 2005-07-07 | Robert Bosch Gmbh | Fuel injector with direct needle injection |
DE102005015735A1 (en) * | 2005-04-06 | 2006-10-12 | Robert Bosch Gmbh | Fuel injector |
JP4459183B2 (en) * | 2006-03-16 | 2010-04-28 | 株式会社デンソー | Injector |
EP1837515A1 (en) * | 2006-03-20 | 2007-09-26 | Delphi Technologies, Inc. | Damping arrangement for a fuel injector |
EP1837518B1 (en) * | 2006-03-20 | 2011-05-25 | Delphi Technologies Holding S.à.r.l. | Damping arrangement for a fuel injector |
DE102006048979B8 (en) * | 2006-10-17 | 2017-02-23 | Continental Automotive Gmbh | Method and injection system for injecting a fluid |
DE102007002282A1 (en) | 2007-01-16 | 2008-07-17 | Robert Bosch Gmbh | Fuel injector with coupler |
DE102007002278A1 (en) * | 2007-01-16 | 2008-07-17 | Robert Bosch Gmbh | Fuel injector for combustion chamber of internal combustion engine, has valve piston formed in two areas with two different diameters, where valve piston is enclosed in one of areas by ring unit, which is movable relative to valve piston |
DE102008003851A1 (en) * | 2008-01-10 | 2009-07-16 | Robert Bosch Gmbh | Fuel injector |
US8201543B2 (en) * | 2009-05-14 | 2012-06-19 | Cummins Intellectual Properties, Inc. | Piezoelectric direct acting fuel injector with hydraulic link |
US8479711B2 (en) * | 2009-06-10 | 2013-07-09 | Cummins Intellectual Propeties, Inc. | Piezoelectric direct acting fuel injector with hydraulic link |
US8500036B2 (en) | 2010-05-07 | 2013-08-06 | Caterpillar Inc. | Hydraulically amplified mechanical coupling |
US9284930B2 (en) * | 2011-06-03 | 2016-03-15 | Michael R. Harwood | High pressure piezoelectric fuel injector |
DE102012212614A1 (en) | 2012-07-18 | 2014-01-23 | Continental Automotive Gmbh | Piezo injector with hydraulically coupled nozzle needle movement |
DE102012222509A1 (en) | 2012-12-07 | 2014-06-12 | Continental Automotive Gmbh | piezoinjector |
DE102012223934B4 (en) * | 2012-12-20 | 2015-10-15 | Continental Automotive Gmbh | piezoinjector |
DE102013210843A1 (en) * | 2013-06-11 | 2014-12-11 | Continental Automotive Gmbh | injector |
DE102014210101A1 (en) * | 2014-05-27 | 2015-12-03 | Robert Bosch Gmbh | fuel injector |
US10006429B2 (en) * | 2016-03-31 | 2018-06-26 | GM Global Technology Operations LLC | Variable-area poppet nozzle actuator |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5505384A (en) * | 1994-06-28 | 1996-04-09 | Caterpillar Inc. | Rate shaping control valve for fuel injection nozzle |
US6520423B1 (en) * | 2000-03-21 | 2003-02-18 | Delphi Technologies, Inc. | Hydraulic intensifier assembly for a piezoelectric actuated fuel injector |
DE60126380T2 (en) * | 2000-07-18 | 2007-11-15 | Delphi Technologies, Inc., Troy | Fuel injection valve |
DE10148594A1 (en) * | 2001-10-02 | 2003-04-10 | Bosch Gmbh Robert | Fuel injection valve has corrugated tube around guide sleeve with sealed connections to pistons that seals storage chamber for hydraulic fluid with respect to enclosing fuel chamber |
DE10160263A1 (en) * | 2001-12-07 | 2003-06-18 | Bosch Gmbh Robert | Fuel injection device for an internal combustion engine |
DE10251679A1 (en) * | 2002-11-07 | 2004-05-19 | Robert Bosch Gmbh | Pressure booster with stroke-dependent damping for supplying self-ignition internal combustion engine combustion chambers has damping choke passing fuel from working chamber to hydraulic chamber |
DE10326259A1 (en) * | 2003-06-11 | 2005-01-05 | Robert Bosch Gmbh | Injector for fuel injection systems of internal combustion engines, in particular direct injection diesel engines |
DE10333696A1 (en) * | 2003-07-24 | 2005-02-24 | Robert Bosch Gmbh | Fuel injector |
DE102004037125A1 (en) | 2004-07-30 | 2006-03-23 | Robert Bosch Gmbh | Common rail injector |
DE102004062006A1 (en) * | 2004-12-23 | 2006-07-13 | Robert Bosch Gmbh | Fuel injector with directly controlled injection valve member |
-
2005
- 2005-02-18 DE DE102005007543A patent/DE102005007543A1/en not_active Ceased
- 2005-12-20 AT AT05112526T patent/ATE402337T1/en not_active IP Right Cessation
- 2005-12-20 EP EP05112526A patent/EP1693564B1/en not_active Not-in-force
- 2005-12-20 DE DE502005004797T patent/DE502005004797D1/en active Active
-
2006
- 2006-02-21 US US11/357,036 patent/US7258283B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US20060186221A1 (en) | 2006-08-24 |
US7258283B2 (en) | 2007-08-21 |
DE502005004797D1 (en) | 2008-09-04 |
EP1693564A2 (en) | 2006-08-23 |
DE102005007543A1 (en) | 2006-08-24 |
ATE402337T1 (en) | 2008-08-15 |
EP1693564A3 (en) | 2007-01-10 |
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