EP1520095B1 - Druckübersetzersteuerung durch bewegung eines einspritzventilgliedes - Google Patents
Druckübersetzersteuerung durch bewegung eines einspritzventilgliedes Download PDFInfo
- Publication number
- EP1520095B1 EP1520095B1 EP03718646A EP03718646A EP1520095B1 EP 1520095 B1 EP1520095 B1 EP 1520095B1 EP 03718646 A EP03718646 A EP 03718646A EP 03718646 A EP03718646 A EP 03718646A EP 1520095 B1 EP1520095 B1 EP 1520095B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- injection
- pressure
- valve
- space
- control
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000002347 injection Methods 0.000 title claims description 150
- 239000007924 injection Substances 0.000 title claims description 150
- 238000006073 displacement reaction Methods 0.000 title 1
- 239000000446 fuel Substances 0.000 claims description 70
- 238000002485 combustion reaction Methods 0.000 claims description 45
- 230000006835 compression Effects 0.000 claims description 24
- 238000007906 compression Methods 0.000 claims description 24
- 238000007789 sealing Methods 0.000 claims description 4
- 230000001960 triggered effect Effects 0.000 claims 2
- 239000000243 solution Substances 0.000 description 10
- 230000004913 activation Effects 0.000 description 7
- 239000002828 fuel tank Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000003213 activating effect Effects 0.000 description 1
- 230000003750 conditioning effect Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M57/00—Fuel-injectors combined or associated with other devices
- F02M57/02—Injectors structurally combined with fuel-injection pumps
- F02M57/022—Injectors structurally combined with fuel-injection pumps characterised by the pump drive
- F02M57/025—Injectors structurally combined with fuel-injection pumps characterised by the pump drive hydraulic, e.g. with pressure amplification
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M47/00—Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure
- F02M47/02—Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure of accumulator-injector type, i.e. having fuel pressure of accumulator tending to open, and fuel pressure in other chamber tending to close, injection valves and having means for periodically releasing that closing pressure
- F02M47/027—Electrically actuated valves draining the chamber to release the closing pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
- F02M59/02—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type
- F02M59/10—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive
- F02M59/105—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive hydraulic drive
-
- 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
- F02M61/04—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
- F02M61/042—The valves being provided with fuel passages
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M63/00—Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
- F02M63/02—Fuel-injection apparatus having several injectors fed by a common pumping element, or having several pumping elements feeding a common injector; Fuel-injection apparatus having provisions for cutting-out pumps, pumping elements, or injectors; Fuel-injection apparatus having provisions for variably interconnecting pumping elements and injectors alternatively
- F02M63/0225—Fuel-injection apparatus having a common rail feeding several injectors ; Means for varying pressure in common rails; Pumps feeding common rails
Definitions
- accumulator injection (Common Rail) allow advantageously the injection pressure to load and to adjust the speed of the self-igniting internal combustion engine. To achieve high specific power and to reduce the emissions of the internal combustion engine In general, the highest possible injection pressure is required.
- DE 199 10 970 A1 relates to a fuel injection device.
- This fuel injection device has one between an accumulator chamber and a nozzle chamber arranged pressure booster unit, whose pressure chamber via a pressure line connected to the nozzle chamber. Furthermore, a connected to the pressure accumulator space Bypass line provided.
- the bypass line is directly connected to the pressure line connected.
- the bypass line is suitable for pressure injection and is parallel arranged to the pressure chamber, so that the bypass line regardless of the movement and position of a displaceable pressure medium of the pressure booster unit throughout is. This measure increases the flexibility of the injection.
- a difference room is connected via a 2/2-way valve with a leakage line and it is a connection from the differential space to the pressure storage room.
- the pressure booster unit is a valve assembly for controlling the same outside the injector at any one Place assigned between the accumulator chamber and the injector.
- DE 100 40 526 A1 also relates to a fuel injection device.
- This one has between a pressure accumulator space and a nozzle chamber arranged pressure booster unit on, comprising a displaceable piston unit to the pressure of the To increase nozzle space to be supplied fuel.
- the piston unit points to the control the pressure intensifier unit a transition from a larger to a smaller one Piston cross-section and a differential space formed thereby.
- the difference space is connected via a filling path with a filling valve to the pressure storage space. There will be a reduction in the amount of control during the activation of the Pressure booster unit and performing a quick reset of the piston unit reached.
- a pressure intensifier under Dispensing with a separate actuator directly via the movement of an injection valve member which is designed in an advantageous manner as a nozzle needle to achieve.
- the pressure booster can be switched on during the opening movement of the injection valve member become.
- the pressure booster comprises a working space and control room separating it Piston unit on which a partial stroke is adjustable, after passing through the pressure booster can be switched on. This can be with regard to the design of a fuel injector achieve considerable advantages with a pressure intensifier.
- pilot injections into the combustion chamber of a self-igniting internal combustion engine possible without activating the pressure intensifier. It can therefore a pilot injection is generated, which takes place at a pressure level which is in the essentially in the interior of a high-pressure accumulator space (common rail) prevailing Pressure levels corresponds.
- a pilot injection is generated, which takes place at a pressure level which is in the essentially in the interior of a high-pressure accumulator space (common rail) prevailing Pressure levels corresponds.
- the intensifier can build up pressure during the main injection phase to the maximum allowable pressure with the injection valve member in the open position be achieved.
- the pressure booster before closing the injection valve member, which preferably as a nozzle needle is formed reach, causing pressure peaks above the maximum Avoid injection pressure when closing the needle. This has a favorable effect the life of the fuel injection system on a self-igniting internal combustion engine out.
- a main injection phase can be achieved reach downstream post-injection phase under very high injection pressure, as well as a remote post-injection, which in a slightly longer sized Time interval follows the main injection.
- FIG. 1 is a first embodiment of an actuatable via an injection valve member Removable pressure intensifier, which is shown in a first state, in which the Control chamber of the pressure booster from the return, i. from the low pressure area of the fuel injection system is disconnected.
- a high-pressure inlet 2 extends to a Pressure Translator 3.
- the high pressure inlet 2 comprises a high pressure line 7, in a Check valve 8 may be included.
- Parallel to the high pressure line 7 is through the high pressure inlet 2 from the high pressure source 1 from a parallel branch 11 is applied, in which a filling valve 10 may be included.
- another parallel branch 12 which includes a throttle 13.
- the former, the filling valve 10 receiving Parallel branch opens as well as the other parallel branch 12, the throttle point 13 receives, in a control chamber 15 of the pressure booster 3.
- the pressure booster 3 comprises In addition, a working space 14, which also via the high-pressure inlet 2 is in communication with the high pressure source 1.
- the fuel injector 4 shown in Figure 1 comprises an injection valve member 34, which is advantageously designed as a nozzle needle.
- the injection valve member 34 is acted upon in the embodiment of Figure 1 by a one-piece valve element 27, which may be designed as a valve piston.
- the end face 29 of the integrally formed valve element 27 limits the control chamber 21, which can be filled via the inlet throttle point 23 and pressure relief via the outlet throttle point 24.
- Below the control chamber 21 formed as a valve piston one-piece valve element 27 is surrounded by an annular space 33, in which the control line 19 opens, which connects the annular space 33 with the control chamber 15 of the pressure booster 3.
- a control edge 31 is formed, which cooperates with a control edge 30, which is embodied on the one-piece valve element 27.
- the injection takes place from the exceeding of the stroke h 1 (see reference numeral 32) with a translated, ie higher pressure.
- This can be a boat-shaped injection achieve.
- the first injection phase for example the pre-injection phase, takes place at the pressure level which is available, for example, as a high-pressure reservoir (common rail) high-pressure source 1, followed by another injection phase at a much higher injection pressure level, which is due to the pressure surface conditions the piston unit 17 of the pressure booster 3 results and is present on the compression space line 20 in the nozzle chamber 36 in the nozzle body 6 of the fuel injector 4.
- Figure 2 shows the embodiment of a fuel injector according to Figure 1 with a Pressure intensifier in a second state.
- control valve 25 which preferably as a 2/2-way valve is formed, closed, so that in the control chamber 21 of the injection valve member 34 sets a pressure build-up. Due to the application of the end face 29 of the one-piece Valve element 27 moves with this cooperating injection valve member 34 in the closing direction. Upon reaching the control edge 31 on the nozzle body 6 takes place an overlap of the control edges 30 and 31 with each other, so that the formed by them Slider seal is closed. As a result, the connection of the control room 15 via the control line 19 and the annular space 33 in the low-pressure side return 26th closed and the pressure booster 3 thus deactivated.
- the stroke h 1 (reference numeral 32) and the closing speed of the injection valve member 34 and the valve member 27 can be the shutdown time of the pressure booster 3, that is, the timing of the overlap of the control edges 30 and 31, tune optimally to the end of the respective injection phase.
- the injection valve member 34 which is preferably designed as a nozzle needle, not completely along the entire stroke h 1 (reference numeral 32) are opened, so that the pressure booster 3 remains deactivated.
- any number of pilot injections can be realized without activated pressure booster 3.
- the pressure level within the scope of the pilot injection for conditioning the combustion mixture contained in the combustion chamber 41 is within the scope of these pilot injections at the pressure level which the high-pressure source 1, for example a high-pressure reservoir (common rail), provides and can not be increased to that achievable by the pressure booster 3 pressure level.
- the number and duration of the respective pilot injection phases and the duration of the main injection at an elevated pressure level can be adjusted by the activation time of the control valve 25.
- FIG. 3 a further embodiment variant of FIG Injector valve operated pressure intensifier with two valve elements in one another out.
- the Ksaftstoffinjektor 4 shown in Figure 3 for fuel supply of a self-igniting Internal combustion engine comprises an integrated in the injector body 5 Compressor 3. From a high pressure source 1 via a high-pressure inlet 2 a high-pressure line 7, a first parallel branch 11 and a further parallel branch 12 and the working space 14 of the pressure booster 3 acted upon.
- a filling valve 10 12 further included a throttle point 13 in parallel branch.
- a check valve 8 is received in the high-pressure line 7, a check valve 8 is received.
- the pressure intensifier 3 according to the further embodiment in Figure 3 comprises analog for the pressure booster 3 shown in FIG. 1, a piston unit 17 which houses the working space 14 separates from the control room 15. With the underside of the piston unit 17, the compression space 18 in the injector body 5 of the pressure booster 3 is acted upon by the compression space line 20 branches off to the nozzle chamber inlet 9 and with the high pressure line 7 united by the high pressure source 1.
- the injection valve member 34 is acted on by a multipart valve element 28, as shown in FIG.
- the multi-part valve element 28 comprises a first valve element 28.1 and a further, second valve element 28.2 surrounding this.
- the first valve element 28.1 and the further valve element 28.2 can be formed in the shape of a piston.
- An annular surface 60 on the second valve element 28.2 partially delimits the control chamber 21.
- an opening 61 is formed, via which an end face 62 of the first valve element 28.1 can be acted upon by the pressure prevailing in the control chamber 21.
- a stroke h 1 (reference numeral 32) is set between the inner, first valve element 28. 1, ie its end face 62, and a collar at the opening 61 in the second valve element 28. 2 of the multi-part valve element 28.
- On the second valve element 28.2 is the control edge 30, which cooperates with a seat of a valve chamber 63.
- the control line 19 from the control chamber 15 of the pressure booster 3.
- From the valve chamber 63 branches off a first return line 64 to the low pressure side of the fuel supply system.
- a piston extension 66 is formed, which has a smaller diameter than the piston part of the first valve element 28.1.
- the piston extension 66 passes through a further, arranged below the valve chamber 63 in the nozzle body 6 cavity in which a closing spring 67 is received.
- the end face of the piston extension 66 bears against the end face of the injection valve member 34, which is preferably in the form of a nozzle needle.
- FIG. 4 shows a variant of an embodiment of an injection valve member actuated Pressure booster with two valve elements, one of which is spring-loaded is.
- the high-pressure inlet 2 extends over both High-pressure line branch 7, which contains a check valve 8 as well as a first Parallel branch 11 and another parallel branch 12 to the control chamber 15 of the pressure booster 3.
- the high-pressure source 1 acts on a high-pressure storage space (Common rail), the working space 14 of the pressure booster 3 directly.
- the working chamber 14 and the control chamber 15 of the pressure booster 3 are via a piston unit 17 separated from each other, wherein the working space 14 zu josde end face the piston unit 17 has a larger diameter than that end face of the Piston unit 17, which limits the compression space 18 of the pressure booster 3.
- From the compression space 18 within the injector body 5 of the fuel injector 4 extends a compression space line 20, which is connected to the check valve. 8 receiving high pressure line 7 combined and merges into the nozzle chamber inlet 9.
- the control chamber 21 within the fuel injector 4 is via a high-pressure branch 22 pressurized with inlet throttle point 23 and is via an outlet throttle point 24th upon actuation of a control valve 25 in the low-pressure side return 26 pressure relieved.
- a multipart valve element 28 is used.
- the multi-part trained Valve element 28, which the injection valve member 34 in the nozzle body 6 of the fuel injector 4 acted upon, comprises a first valve element 28.1, whose end face 62 the control chamber 21 limited.
- the first valve element 28.1 comprises a piston extension 66, which with its lower end face abuts the end face of the injection valve member 34.
- the first Valve element 28.1 is surrounded by a second, further valve element 28.2, wherein between the first valve element 28.1 and the second valve element 28.2 a Passage gap 72 sets.
- control valve 25 which is preferably designed as a 2/2-way valve
- the control valve 25 which is preferably designed as a 2/2-way valve
- the control chamber 21 above the end face 62 of the first valve element 28.1 as long pressure relieved that the end face of the injection valve member 34 abuts the lower annular surface of the second valve element 28.2, ie the stroke is exceeded h 1 (reference numeral 32)
- the pressure booster 3 through the injection valve member 34 activated because due to the force acting on the pressure shoulder 35 hydraulic force in the nozzle chamber 36 of the sealing seat between the control edges 30 on the second valve element 28.2 and the control edge 31 of the valve chamber 63 is opened and a pressure reduction in the control chamber 15 of the pressure booster 3 via the line 19 in the first low-pressure side return 64 can take place.
- the fuel compressed in the compression space 18 of the pressure booster 3 is in the nozzle space 36 via the compression space line 20 to the nozzle chamber inlet 9 at the discharge point 37 of the nozzle chamber inlet 9 in the nozzle chamber 36.
- the solution shown in Figure 4 can be given a certain pressure relief of the control chamber 21 of the injection valve member 34 within certain limits, ie so that the Auffahrweg of the injection valve member 34 below the stroke h 1 (reference numeral 32), pilot injection phases on the pressure prevailing in the high pressure source 1 pressure level represent, from a further sustained pressure relief of the control chamber 21 via the injection valve member 34, an activation of the pressure booster 3 takes place, and a main injection phase can be realized with rate-shaping at an elevated pressure level.
- one or more pilot injection phases can be made, only depending on the drive times and the control program of the control valve 25, which can be preferably designed as a 2/2-way valve.
- a first pressure level for example, the pressure level of a high-pressure source. 1 equivalent.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Fuel-Injection Apparatus (AREA)
Description
- Figur 1
- eine Ausführungsvariante eines über ein Einspritzventilglied betätigten Druckübersetzers in einem ersten Zustand,
- Figur 2
- die Ausführungsvariante der erfindungsgemäß vorgeschlagenen Lösung gemäß Figur 1 mit einem Druckübersetzer in einem zweiten Zustand,
- Figur 3
- eine weitere Ausführungsvariante eines über ein Einspritzventilglied betätigbaren Druckübersetzers mit zwei ineinandergeführten Ventilelementen und
- Figur 4
- eine Ausführungsvariante eines über ein Einspritzventilglied betätigten Druckübersetzers mit zwei Ventilelementen, von denen eines federbeaufschlagt gestaltet ist.
- 1
- Hochdruckquelle (Common-Rail)
- 2
- Hochdruckzulauf
- 3
- Druckübersetzer
- 4
- Kraftstoffinjektor
- 5
- Injektorkörper
- 6
- Düsenkörper
- 7
- Hochdruckleitung
- 8
- Rückschlagventil
- 9
- Abzweigen Düsenraumzulauf
- 10
- Füllventil
- 11
- erster Parallelzweig
- 12
- weiterer Parallelzweig
- 13
- Drosselstelle
- 14
- Arbeitsraum
- 15
- Steuerraum
- 16
- Federelement
- 17
- Kolbeneinheit
- 18
- Kompressionsraum
- 19
- Steuerleitung für Steuerraum
- 20
- Kompressionsraumleitung
- 21
- Steuerraum
- 22
- Hochdruckabzweig zum Steuerraum
- 23
- Zulaufdrosselstelle
- 24
- Ablaufdrosselstelle
- 25
- Steuerventil (2/2-Wege-Ventil)
- 26.1
- erster niederdruckseitiger Rücklauf
- 26.2
- zweiter niederdruckseitiger Rücklauf
- 27
- einteiliges Ventilelement
- 28
- mehrteiliges Ventilelement
- 28.1
- erstes Ventilelement
- 28.2
- zweites Ventilelement
- 29
- Stirnfläche einteiliges Ventilelement
- 30
- Steuerkante Ventilelement
- 31
- Steuerkante Gehäuse
- 32
- Hubweg h1
- 33
- Ringraum Ventilelement
- 34
- Einspritzventilglied
- 35
- Druckschulter
- 36
- Düsenraum
- 37
- Mündungsstelle Düsenraumzulauf
- 38
- Ringspalt
- 39
- Einspritzöffnung
- 40
- brennraumseitiger Sitz
- 41
- Brennraum
- 42
- verschlossene Einspritzöffnung
- 50
- niederdruckseitige Verbindung
- 51
- Einspritzventilglied 34 (aufgefahrene Position)
- 52
- freigegebene Einspritzöffnungen
- 60
- Ringfläche zweites Ventilelement
- 61
- Durchgangsöffnung
- 62
- Stirnseite erstes Ventilelement
- 63
- Ventilraum
- 64
- erste Rücklaufleitung
- 65
- zweite Rücklaufleitung
- 66
- Kolbenfortsatz
- 67
- Schließfeder
- 68
- Anschlag erstes Ventilelement am zweiten Ventilelement
- 70
- Federelement für zweites Ventilelement
- 71
- Anschlag Federelement
- 72
- Überströmspalt
Claims (17)
- Vorrichtung zum Einspritzen von Kraftstoff in einen Brennraum (41) einer Verbrennungskraftmaschine mit einem Injektorkörper (5, 6), in welchem ein Einspritzventilglied (34) aufgenommen ist, das über Druckbeaufschlagung/Druckentlastung eines Steuerraumes (21) betätigbar ist, was über ein Steuerventil (25) bewirkt wird und mit einem Druckübersetzer (3), der eine einen Arbeitsraum (14) und einen Steuerraum (15) trennende Kolbeneinheit (17) umfaßt, die einen Kompressionsraum (18) beaufschlagt, der mit einem das Einspritzventilglied (34) umgebenden Düsenraum (36) in Verbindung (9, 20) steht, dadurch gekennzeichnet, daß die Druckbeaufschlagung (2, 11, 12)/Druckentlastung (19, 26, 64) des Steuerraumes (15) des Druckübersetzers (3) abhängig von der Hubbewegung des Einspritzventilgliedes (34) erfolgt.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß Anspruch 1, dadurch gekennzeichnet, daß dem Einspritzventilglied (34) ein Ventilelement (27, 28) zugeordnet ist, welches innerhalb eines hydraulischen Raumes (33, 63) bewegbar ist, in den eine Steuerleitung (19) vom Steuerraum (15) des Druckübersetzers (3) mündet.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß Anspruch 2, dadurch gekennzeichnet, daß das innerhalb des hydraulischen Raumes (33, 63) angeordnete Ventilelement (27, 28) die den brennraumseitigen Einspritzöffnungen (39) abgewandte Stirnseite des Einspritzventilgliedes (34) beaufschlagt.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß Anspruch 2, dadurch gekennzeichnet, daß das Ventilelement (27, 28) mit einer hydraulisch beaufschlagbaren Fläche (29, 60, 62) in einen das Einspritzventilglied (34) druckbeaufschlagenden Steuerraum (21) hineinragt.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß Anspruch 2, dadurch gekennzeichnet, daß das Ventilelement (27) einteilig ausgebildet ist und eine Steuerkante (30) aufweist, die mit einer Steuerkante (31) am hydraulischen Raum (33) eine Schieberdichtung bildet.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß Anspruch 2, dadurch gekennzeichnet, daß vom hydraulischen Raum (33, 63) eine Rücklaufleitung (26.2, 64) in den Niederdruckbereich abzweigt.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß der Ansprüche 5 und 6, dadurch gekennzeichnet, daß bei einer durch Druckentlastung des Steuerraumes (21) ausgelösten Hubbewegung des Einspritzventilgliedes (34), die kleiner als ein Hubweg h1 (32) - der Überdeckung der Steuerkanten (30, 31) - ist, die Schieberdichtung (30, 31) geschlossen bleibt und eine Einspritzung von Kraftstoff in einen Brennraum (41) auf einem ersten Druckniveau erfolgt.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß der Ansprüche 5 und 6, dadurch gekennzeichnet, daß bei einer durch weitere Druckentlastung des Steuerraums (21) ausgelösten Hubbewegung des Einspritzventilgliedes (34), welche den Hubweg h1 (32) übersteigt, der Steuerraum (15) des Druckübersetzers (3) über die Steuerleitung (19) und die offenstehenden Steuerkanten (30, 31) mit dem zweiten niederdruckseitigen Rücklauf (26.2) verbindbar ist und eine Einspritzung von Kraftstoff in einen Brennraum (41) auf einem zweiten, höheren Druckniveau erfolgt.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß Anspruch 2, dadurch gekennzeichnet, daß das Ventilelement (28) mehrteilig ausgebildet ist und ein erstes Ventilteil (28.1) sowie ein zweites Ventilteil (28.2) umfaßt, von denen mindestens eines durch den im Steuerraum (21) des Einspritzventilgliedes (34) herrschenden Druck beaufschlagt ist.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß Anspruch 9, dadurch gekennzeichnet, daß das erste Ventilteil (28.1) im zweiten Ventilteil (28.2) geführt ist und zwischen einer Stirnseite (29) des ersten Ventilteils (28.1) und einem Hubanschlag (68) des zweiten Ventilteils (28.2) ein Hubweg h1 (32) eingestellt ist.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß Anspruch 10, dadurch gekennzeichnet, daß das zweite Ventilteil (28.2) eine Steuerkante (30) aufweist, die mit einem Dichtsitz im hydraulischen Raum (63) zusammenwirkt.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß der Ansprüche 10 und 11, dadurch gekennzeichnet, daß bei Druckentlastung des Steuerraums (21) das erste Ventilteil (28.1) um den Hubweg h1 (32) gegen den Anschlag (68) fährt und das Einspritzventilglied (34) eine Einspritzung von Kraftstoff in den Brennraum (41) auf einem ersten Druckniveau ausführt.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß der Ansprüche 10 und 11, dadurch gekennzeichnet, daß bei weiterer Druckentlastung des Steuerraums (21) das erste Ventilteil (28.1) nach Durchmessen des Hubweges h1 (32) das zweite Ventilteil (281.2) am Dichtsitz im hydraulischen Raum (63) aufsteuert, der Steuerraum (15) über die Steuerleitung (19), und den hydraulischen Raum (63) niederdruckseitig entlastet und eine Einspritzung von Kraftstoff auf einem zweiten, höheren Druckniveau erfolgt.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß Anspruch 9, dadurch gekennzeichnet, daß eines der Ventilteile (28.1, 28.2) des mehrteiligen Ventilelementes (28) von einem Federelement (70) beaufschlagt in einen Dichtsitz im hydraulischen Raum (63) gestellt ist.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß der Ansprüche 9 und 14, dadurch gekennzeichnet, daß ein Kolbenfortsatz (66) des ersten Ventilteils (28.1) das zweite Ventilteil (28.2) einen Ringspalt (72) bildend durchsetzt und der Kolbenfortsatz (66) des ersten Ventilteils (28.1) das Einspritzventilglied (34) stirnseitig beaufschlagt.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß der Ansprüche 9 und 14, dadurch gekennzeichnet, daß zwischen dem zweiten Ventilteil (28.2) und dem Einspritzventilglied (34) ein Hubweg h1 (32) vorgebbar ist, um welchen das Einspritzventilglied (34) bei Druckentlastung eines Steuerraums (21) zum Einspritzen von Kraftstoff auf einem ersten Druckniveau bewegbar ist.
- Vorrichtung zum Einspritzen von Kraftstoff gemäß der Ansprüche 9 und 16, dadurch gekennzeichnet, daß bei einer weiteren Druckentlastung des Steuerraums (21) und einer dem Hubweg h1 (32) übersteigenden Öffnungsbewegung des Einspritzventilgliedes (34), dieses das zweite Ventilteil (28.2) aus seinem Sitz im hydraulischen Raum (63) bewegt, und dem Steuerraum (15) des Druckübersetzers (3) über eine Steuerleitung (19) niederdruckseitig entlastet, so daß eine Einspritzung von Kraftstoff in den Brennraum (41) auf einem zweiten, höheren Druckniveau erfolgt.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10229413A DE10229413A1 (de) | 2002-06-29 | 2002-06-29 | Druckübersetzersteuerung durch Bewegung eines Einspritzventilgliedes |
DE10229413 | 2002-06-29 | ||
PCT/DE2003/001100 WO2004003373A1 (de) | 2002-06-29 | 2003-04-03 | Druckübersetzersteuerung durch bewegung eines einspritzventilgliedes |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1520095A1 EP1520095A1 (de) | 2005-04-06 |
EP1520095B1 true EP1520095B1 (de) | 2005-11-02 |
Family
ID=29796046
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP03718646A Expired - Lifetime EP1520095B1 (de) | 2002-06-29 | 2003-04-03 | Druckübersetzersteuerung durch bewegung eines einspritzventilgliedes |
Country Status (5)
Country | Link |
---|---|
US (1) | US20050116058A1 (de) |
EP (1) | EP1520095B1 (de) |
JP (1) | JP2005531714A (de) |
DE (2) | DE10229413A1 (de) |
WO (1) | WO2004003373A1 (de) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004017305A1 (de) * | 2004-04-08 | 2005-10-27 | Robert Bosch Gmbh | Kraftstoffeinspritzeinrichtung für Brennkraftmaschinen mit direkt ansteuerbaren Düsennadeln |
DE102004019836A1 (de) * | 2004-04-23 | 2005-11-17 | Robert Bosch Gmbh | Kraftstoffeinspritzventil für Brennkraftmaschinen |
DE102004022268A1 (de) * | 2004-05-06 | 2005-12-01 | Robert Bosch Gmbh | Ansteuerverfahren zur Beeinflussung der Öffnungsgeschwindigkeit eines Steuerventiles an einem Kraftstoffinjektor |
DE102004028521A1 (de) * | 2004-06-11 | 2005-12-29 | Robert Bosch Gmbh | Kraftstoffinjektor mit mehrteiligem Einspritzventilglied und mit Druckverstärker |
DE102004035293A1 (de) * | 2004-07-21 | 2006-02-16 | Robert Bosch Gmbh | Kraftstoffinjektor mit Nadelhubdämpfung |
JP4075894B2 (ja) * | 2004-09-24 | 2008-04-16 | トヨタ自動車株式会社 | 燃料噴射装置 |
US7334741B2 (en) * | 2005-01-28 | 2008-02-26 | Cummins Inc. | Fuel injector with injection rate control |
DE102005033123B3 (de) * | 2005-07-15 | 2006-12-21 | L'orange Gmbh | Kraftstoffinjektor |
DE102006062216A1 (de) * | 2006-12-22 | 2008-06-26 | Robert Bosch Gmbh | Kraftstoffinjektor |
US7832374B2 (en) * | 2008-10-21 | 2010-11-16 | Gm Global Technology Operations, Inc. | Fuel pressure amplifier |
US8775054B2 (en) | 2012-05-04 | 2014-07-08 | GM Global Technology Operations LLC | Cold start engine control systems and methods |
US10550808B2 (en) * | 2014-12-19 | 2020-02-04 | Volvo Truck Corporation | Injection system of an internal combustion engine and automotive vehicle including such an injection system |
CN104847553A (zh) * | 2015-04-09 | 2015-08-19 | 中国第一汽车股份有限公司无锡油泵油嘴研究所 | 可优化喷油速率且可增压式共轨喷油器 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19706469A1 (de) * | 1997-02-19 | 1998-08-27 | Daimler Benz Ag | Speichereinspritzsystem für eine mehrzylindrige Brennkraftmaschine mit magnetventilgesteuerten Kraftstoffeinspritzventilen |
DE19910970A1 (de) * | 1999-03-12 | 2000-09-28 | Bosch Gmbh Robert | Kraftstoffeinspritzeinrichtung |
DE19956598A1 (de) * | 1999-11-25 | 2001-06-13 | Bosch Gmbh Robert | Ventil zum Steuern von Flüssigkeiten |
-
2002
- 2002-06-29 DE DE10229413A patent/DE10229413A1/de not_active Withdrawn
-
2003
- 2003-04-03 US US10/504,965 patent/US20050116058A1/en not_active Abandoned
- 2003-04-03 DE DE50301573T patent/DE50301573D1/de not_active Expired - Fee Related
- 2003-04-03 WO PCT/DE2003/001100 patent/WO2004003373A1/de active IP Right Grant
- 2003-04-03 EP EP03718646A patent/EP1520095B1/de not_active Expired - Lifetime
- 2003-04-03 JP JP2004516440A patent/JP2005531714A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
DE10229413A1 (de) | 2004-01-29 |
EP1520095A1 (de) | 2005-04-06 |
WO2004003373A1 (de) | 2004-01-08 |
US20050116058A1 (en) | 2005-06-02 |
JP2005531714A (ja) | 2005-10-20 |
DE50301573D1 (de) | 2005-12-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1520096B1 (de) | Speichereinspritzsystem mit variodüse und druckübersetzungseinrichtung | |
EP1654455B1 (de) | Steuerventil für einen einen drucküberbesetzer enthaltenden kraftstoffinjektor | |
EP1078160B1 (de) | Kraftstoffeinspritzeinrichtung | |
EP1520099B1 (de) | Druckübersetzer kraftstoffinjektor mit schnellem druckabbau bei einspritzende | |
EP1613856A1 (de) | Servoventilangesteuerter kraftstoffinjektor mit druckübersetzer | |
EP1520095B1 (de) | Druckübersetzersteuerung durch bewegung eines einspritzventilgliedes | |
EP1584813A2 (de) | Kraftstoffeinspritzeinrichtung für Brennkraftmaschinen mit direkt ansteuerbaren Düsennadeln | |
EP1125054B1 (de) | Verfahren und vorrichtung zur durchführung einer kraftstoffeinspritzung | |
EP1520100B1 (de) | Einrichtung zur nadelhubdämpfung an druckgesteuerten kraftstoffinjektoren | |
EP1552137B1 (de) | Einrichtung zur unterdrückung von druckwellen an speichereinspritzsystemen | |
WO2004003378A1 (de) | Kraftstoffinjektor mit druckübersetzer für mehrfacheinspritzung | |
WO2003054374A1 (de) | Kraftstoffeinspritzeinrichtung fuer eine brennkraftmaschine | |
DE10221384A1 (de) | Kraftstoffeinspritzeinrichtung für eine Brennkraftmaschine | |
DE10132732A1 (de) | Kraftstoffeinspritzeinrichtung | |
EP1651861B1 (de) | Schaltventil mit druckausgleich für einen kraftstoffinjektor mit druckverstärker | |
WO2004040117A1 (de) | Kraftstoff-einspritzeinrichtung für brennkraftmaschinen | |
EP1682769B1 (de) | Kraftstoffinjektor mit mehrteiligem, direktgesteuertem einspritzventilglied | |
DE102005032464A1 (de) | Kraftstoffinjektor mit Vorsteuerraum | |
WO2004070201A1 (de) | Kraftstoffeinspritzeinrichtung für eine brennkraftmaschine | |
EP1392965B1 (de) | Druckverstärker einer kraftstoffeinspritzeinrichtung | |
EP1354133A2 (de) | Die erfindung betrifft eine kraftstoffeinspritzeinrichtung gemäss dem oberbegriff des patentanspruchs 1 | |
WO2007009641A1 (de) | Kraftstoffinjektor | |
DE102004038189A1 (de) | Kraftstoffeinspritzeinrichtung für Brennkraftmaschinen mit direkt ansteuerbaren Düsennadeln | |
DE10251679A1 (de) | Druckverstärker mit hubabhängiger Bedämpfung | |
DE102005029805A1 (de) | Kraftstoffinjektor mit Verzögerungseinrichtung zur Verlängerung der Druckverstärkungsphase |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20050131 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
RBV | Designated contracting states (corrected) |
Designated state(s): DE FR GB IT |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB IT |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REF | Corresponds to: |
Ref document number: 50301573 Country of ref document: DE Date of ref document: 20051208 Kind code of ref document: P |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20060221 |
|
ET | Fr: translation filed | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed |
Effective date: 20060803 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20080626 Year of fee payment: 6 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20090420 Year of fee payment: 7 Ref country code: IT Payment date: 20090429 Year of fee payment: 7 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20090424 Year of fee payment: 7 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20091103 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20100403 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20101230 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20100403 Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20100403 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20100430 |