EP1554488B1 - Pressure-boosted fuel injection device comprising an internal control line - Google Patents
Pressure-boosted fuel injection device comprising an internal control line Download PDFInfo
- Publication number
- EP1554488B1 EP1554488B1 EP03770904A EP03770904A EP1554488B1 EP 1554488 B1 EP1554488 B1 EP 1554488B1 EP 03770904 A EP03770904 A EP 03770904A EP 03770904 A EP03770904 A EP 03770904A EP 1554488 B1 EP1554488 B1 EP 1554488B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- pressure
- chamber
- piston
- pressure booster
- fuel 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 - Lifetime
Links
- 239000000446 fuel Substances 0.000 title claims description 137
- 238000002347 injection Methods 0.000 title claims description 99
- 239000007924 injection Substances 0.000 title claims description 99
- 238000007789 sealing Methods 0.000 claims description 36
- 230000001419 dependent effect Effects 0.000 claims description 3
- 239000012530 fluid Substances 0.000 claims 1
- 238000002485 combustion reaction Methods 0.000 description 28
- 238000004519 manufacturing process Methods 0.000 description 9
- 230000005540 biological transmission Effects 0.000 description 6
- 210000001503 joint Anatomy 0.000 description 4
- 239000000243 solution Substances 0.000 description 3
- 238000004891 communication Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 230000004323 axial length Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 210000003746 feather Anatomy 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 238000007493 shaping process Methods 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
- F02M57/026—Construction details of pressure amplifiers, e.g. fuel passages or check valves arranged in the intensifier piston or head, particular diameter relationships, stop members, arrangement of ports or conduits
-
- 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
- F02M47/025—Hydraulically 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
- 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
- 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
- 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
- F02M61/20—Closing valves mechanically, e.g. arrangements of springs or weights or permanent magnets; Damping of valve lift
- F02M61/205—Means specially adapted for varying the spring tension or assisting the spring force to close the injection-valve, e.g. with damping of valve lift
-
- 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
- F02M63/0003—Fuel-injection apparatus having a cyclically-operated valve for connecting a pressure source, e.g. constant pressure pump or accumulator, to an injection valve held closed mechanically, e.g. by springs, and automatically opened by fuel pressure
- F02M63/0005—Fuel-injection apparatus having a cyclically-operated valve for connecting a pressure source, e.g. constant pressure pump or accumulator, to an injection valve held closed mechanically, e.g. by springs, and automatically opened by fuel pressure using valves actuated by fluid 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
- 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
- F02M63/0003—Fuel-injection apparatus having a cyclically-operated valve for connecting a pressure source, e.g. constant pressure pump or accumulator, to an injection valve held closed mechanically, e.g. by springs, and automatically opened by fuel pressure
- F02M63/0007—Fuel-injection apparatus having a cyclically-operated valve for connecting a pressure source, e.g. constant pressure pump or accumulator, to an injection valve held closed mechanically, e.g. by springs, and automatically opened by fuel pressure using electrically actuated valves
-
- 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
- F02M63/0012—Valves
- F02M63/0014—Valves characterised by the valve actuating means
- F02M63/0015—Valves characterised by the valve actuating means electrical, e.g. using solenoid
-
- 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
- F02M63/0012—Valves
- F02M63/0014—Valves characterised by the valve actuating means
- F02M63/0028—Valves characterised by the valve actuating means hydraulic
- F02M63/0029—Valves characterised by the valve actuating means hydraulic using a pilot valve controlling a hydraulic chamber
-
- 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
- F02M63/0012—Valves
- F02M63/0031—Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
- F02M63/0043—Two-way valves
-
- 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
- F02M63/0012—Valves
- F02M63/0031—Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
- F02M63/0045—Three-way valves
Definitions
- injection systems with high-pressure accumulators have the advantage that the injection pressure can be adapted to the load and speed of the internal combustion engine. To reduce the resulting emissions and to achieve a high specific power of the internal combustion engine, a high injection pressure is required. Since the achievable by high-pressure fuel pumps in the high-pressure accumulator pressure level is limited for strength reasons, can be used to further increase pressure in fuel injectors with a high-pressure accumulator a pressure booster on the fuel injector.
- DE 199 10 907 A1 discloses a fuel injector having a pressurizing unit disposed between a pressure accumulating space and a nozzle space. Its pressure chamber is connected via a pressure line to the nozzle chamber. Furthermore, a bypass line connected to the pressure storage space is provided. The bypass line is connected directly to the pressure line. The bypass line is suitable for a pressure injection and is arranged parallel to the pressure chamber, so that the bypass line is independent of the movement and position of a slidably ordered pressure medium of the pressure booster unit.
- DE 102 18 904.8 refers to a fuel injector.
- a fuel injection device for internal combustion engines is proposed with a fuel injector, which can be supplied by a high-pressure fuel source, and a pressure booster device.
- the closing piston of a fuel injector protrudes into a closing pressure chamber in such a way that the closing piston can be acted upon by fuel pressure to achieve a force acting on the closing piston in the closing direction, whereby the closing pressure space and the rear space of the pressure booster device are formed by a common closing pressure return space. All partial areas of the closing pressure rear space are permanently connected to one another for the purpose of exchanging fuel.
- a fuel injection device with a pressure booster which has a working space, a differential pressure chamber and a high pressure chamber for pressure boosting.
- the pressure booster is controlled by controlling the differential pressure chamber by means of a 2/2-way valve, which the differential pressure chamber to a low pressure / return system
- the filling of the differential pressure chamber takes place via a hydraulically throttled control line, which communicates with the constantly pressurized working space. Less fuel flows through the throttled control line than flows out via the open 2/2 directional valve, so that the differential pressure chamber can be relieved of pressure to control the pressure intensifier.
- the central control line for pressure relief or pressurization of serving for the actuation of the pressure booster differential pressure chamber is substantially coaxial with the axis of symmetry through the pressure booster piston and extends through the pressurized working space of the pressure booster.
- the control line is sealed against the working space via a high-pressure-tight connection.
- the omission of a guided on the outside of the fuel injector with pressure booster control line also reduces the outer dimension of the fuel injector or avoids an eccentric to the fuel injector oriented arrangement of a pressure booster.
- a coaxially extending to the axis of symmetry of the fuel injector control line in the booster piston advantageously avoids Bohrungsverschneidungen, as inevitably occur in external lines due to the connection position of high pressure connections and reduces the material stress, which in turn increases the service life of the fuel injector with pressure booster.
- a seal between the working space and the central control line can be achieved by means of a biased by a spring element sealing sleeve, which advantageously cooperates with a flat seat in the working space. This allows the compensation of production-related tolerances in a running with a plurality of housing parts to be joined fuel injector with pressure booster.
- the central control line extends through an extension formed on the piston of the pressure booster, which has a guide section for the sealing sleeve movably arranged on the piston shoulder.
- a piston extension arranged on the booster piston of the pressure booster can be accommodated in a high-pressure-tight guide, which is embodied in one of the housing parts of the fuel injector with pressure booster.
- the high pressure-tight guide of the piston extension is designed so that it is effective along the entire stroke of the piston of the pressure booster and the central control line separates from the working space of the pressure booster.
- a piston can be received, which has a continuous channel.
- a sealing point can be designed as a flat seat to seal the central control line against the working space of the pressure booster.
- the pressure booster contains a piston element extending continuously through the piston element with a channel extending continuously through it. The channel is connected depending on the stroke of the pressure booster by a first or by a first and a second flow area with the differential pressure chamber of the pressure booster.
- the central control line can be used with all pressure intensifiers that are controlled via a differential pressure chamber.
- FIG. 1 shows an embodiment of a fuel injector with pressure booster whose piston has a piston neck, which is traversed by a portion of the central control line.
- a fuel injection device 1 is acted upon by a high-pressure accumulator 2 (common rail) with fuel under high pressure.
- the high-pressure fuel contained in the high-pressure accumulator 2 flows to an injector body 4 of the fuel injection device 1 via a high-pressure feed line 3.
- an inlet 6 to a switching valve 5 extends from the switching valve 5 branches on the one hand a low-pressure side return 7 in a in FIG. 1 Not shown fuel reservoir discharges, and an overflow line 43, which is in communication with a recess 35 within the first housing part 8.
- the injector body 4 of the fuel injection device 1 comprises a first housing part 8 and a further, second housing part 9 and an injector housing 10 which encloses an injection valve member 24.
- the first housing part 8 and the second housing part 9 abut each other along a butt joint 32.
- a pressure booster 11 is received in the injector body 4 of the fuel injection device 1.
- the pressure booster 11 comprises a working space identified by the reference numeral 12, which can be acted upon by fuel flowing under high pressure via an inlet 13 branching off from the high-pressure line 3.
- the pressure booster 11 comprises a pressure booster piston 14, which includes a first end face 15, which assigns the working space 12, and a second end face 16, which assigns a differential pressure chamber 17.
- the pressure booster piston 14 is supported on the second end face 16 by a return spring 18, which in turn is supported on an annular surface within the second housing part 9 of the injector body 4.
- the pressure booster piston 14 of the pressure booster 11 acts on a high-pressure chamber 19 which is located in the lower region of the second housing part 9.
- the high-pressure space 19 zu josden end face of the pressure booster piston 14, the fuel contained in this compressed again and flows on the one hand into a control chamber 20 and on the other hand via a nozzle chamber inlet 22 into a nozzle chamber 23 in the injector 10th is trained.
- the nozzle chamber 23 encloses the injection valve member 24 of the fuel injection device in a region in which a pressure shoulder is formed on the injection valve member 24.
- an annular gap extends to the combustion chamber end of the fuel injector 1.
- injection openings 25 are acted upon at the combustion chamber end of the fuel injection device 1 with fuel. These are released in a vertical movement of the injection valve member 24, so that can be injected via the injection openings 25 under high pressure fuel in a combustion chamber 26 of a self-igniting internal combustion engine.
- a nozzle spring 27 is received, which surrounds a pin 28 of the injection valve member and is supported on an annular surface of the injection valve member 24.
- a discharge throttle 30 receiving relief line 29th
- the pressure booster piston 14 of the pressure booster 11 includes a central control line 31.
- the central control line 31 is connected via a formed in the pressure booster piston 14 transverse opening 41 with the differential pressure chamber 17 of the pressure booster 11 in combination.
- the transverse opening 41 in turn is connected to a central control line 31 representing channel 40, which passes through the working space 12 and the differential pressure chamber 17 separating portion of the pressure booster piston 14 and through a on the first end face 15 of the pressure booster piston 14 arranged piston extension 34 extends.
- the piston neck 34 accommodating the channel 40 on the first end face 15 of the pressure-transmitting piston 14 extends into the recess 35 in the first housing part 8 of the injector body 4.
- a first sealing sleeve 36 can be moved within a guide section 42 on the piston shoulder 34 of the pressure booster piston 14.
- the first sealing sleeve 36 comprises an annular projection 39, on which a positioning spring 38 is supported.
- the adjusting spring 38 is supported with its first sealing sleeve 36 opposite end on the first end face 15, the piston neck 34 from surrounding.
- the first sealing sleeve 36 received on the piston shoulder 34 is set with a sealing surface 37 against the lower end face of the first housing part 8 of the injector body 4.
- the in FIG. 1 illustrated embodiment may be formed to compensate for manufacturing tolerances between the first housing part 8 and the second housing part 9 of the fuel injector 4, the high-pressure-tight connection 33 as a flat seat.
- the protruding into the recess 35 of the first housing part 8 portion of the piston extension 34 can be performed with radial clearance in the recess 35 so that a contact-free guidance between the upper portion of the piston extension 34 and the recess 35 in the first housing part 8 can be achieved.
- the differential pressure chamber 17 is pressurized by the high-pressure accumulator 2 via the high pressure line 3, the inlet 6 and the overflow line 43 and the recess 35 in the first housing part 8. From there, the fuel flows through the channel 40 forming the central control line 31 and enters via the transverse opening 41 in the differential pressure chamber 17 and acted upon this again with the pressure prevailing in the high-pressure accumulator 2 pressure level. As a result, the high-pressure chamber 19 is relieved, as well as the nozzle chamber 23 surrounding the injection valve member 24 in the injector housing 10. About the nozzle spring 27, the injection valve member 24 is pressed in its combustion chamber side seat, the injection is completed.
- FIG. 1 illustrated embodiment of the idea underlying the invention is arranged on the first end face 15 of the pressure booster piston 11 of the piston extension 34.
- 1 fuel volume flows either from or into the differential pressure chamber 17.
- a sealing of the recess 35 within the first housing part 8 is achieved in this embodiment by the piston 34 on the first movably guided first sealing sleeve 36.
- the guided on the piston shoulder 34 guided first sealing sleeve 36 is supported by an adjusting spring 38 in an advantageous manner. Due to the dimensioning of the adjusting spring 38, the effectiveness of the high-pressure-tight connection 33 at the lower end side of the first Housing parts 8 are ensured over the entire stroke of the pressure booster piston 14 within the second housing part 9 of the injector body 4.
- the leadership of the central control line 31 substantially coaxially with the line of symmetry of the injector body 4 avoids an additional to be provided on the outside of the injector 4 to the switching valve 5 high-pressure line, which would be required to control the differential pressure chamber 17 of the booster 11.
- a via the differential pressure chamber 17 (also referred to as the back space) controlled pressure intensifier 11 is particularly favorable in terms of its relaxation losses.
- FIG. 2 shows an embodiment of a fuel injector with pressure booster, wherein the central control line extends through a piston neck, which is guided in a high-pressure-tight guide of the injector body 4.
- the fuel injection device 1 is supplied via the pressure accumulator 2 (common rail) with fuel under high pressure. From the pressure accumulator 2, fuel flows via the high-pressure line 3 to the first housing part 8 of the injector body 4. The first housing part 8 of the fuel injection device 1 abuts against a butt joint 32 on the second housing part 9 of the injector body 4.
- the injector body 4 of the fuel injection device 1 further comprises the injector housing 10 in which the injection valve member 24 releasing or closing the injection openings 25, which can be embodied as a nozzle needle, is accommodated.
- the first housing part 8 of the injector body 4 of the fuel injection device 1 flows under high pressure fuel. This is passed via the inlet to the switching valve 5.
- the switching valve 5 comprises a connection to the low-pressure side return 7 and an overflow 43 to the formed in the first housing part 8 recess 35.
- the pressure booster 11 comprises a pressure booster piston 14, which separates the working space 12 of the pressure booster 11 from its differential pressure chamber 17.
- the pressure booster piston 14 comprises the piston extension 34 fastened to the first end face 15.
- a first washer 51 is arranged on the piston extension 34 passing through the working space 12 in the second housing part 9.
- a further, second disc 52 is disposed on the inside of the working space 12 of the pressure booster 11. Between the first and the second disc 51, 52, a return spring 18 is received, via which the pressure booster piston 14 is returned to its initial position within the second housing part 9.
- the lower end face of the pressure booster piston 14 acts on the high pressure chamber 19 formed in the second housing part 9 of the injector body 4.
- the high pressure level achievable in the high-pressure chamber 19 depends on the transmission ratio of the pressure booster 11 and is higher than the pressure level prevailing in the high-pressure reservoir 2.
- From the high-pressure chamber 19 of the pressure intensifier 11 under a further increased pressure level stationary fuel flows through the nozzle chamber inlet 22 to the nozzle chamber 23 in the injector 10 to.
- the injection valve member 24 comprises a pressure shoulder.
- the control chamber 20 for the injection valve member 24 includes a nozzle spring 27, on the one hand on an annular surface of the injection valve member 24, a pin 28 surrounding, is supported. On the other hand, the nozzle spring 27 rests against a wall of the second housing part 9 delimiting the nozzle chamber 20.
- the pressure booster piston 14 of the pressure booster 11 comprises a central control line 31.
- the central control line 31 is formed as a both the piston shoulder 34 and the pressure booster piston 14 passing through channel 40, at its lower, opening into the differential pressure chamber 17 end, a Transverse opening 41 comprises.
- This can be designed as a bore, as a channel or the like in the pressure booster piston 14.
- the channel 40 extends into the recess 35 in the first housing part 8 of the injector body 4.
- the high pressure-tight guide 50 within the first housing part 8 goes into the Recess 35 and is formed in a the stroke of the pressure booster piston 14 corresponding axial length. This ensures that along the entire stroke of the pressure booster piston 14 of the pressure booster 11, a high-pressure seal between the recess 35 is ensured within the first housing part 8 and the working space 12 of the pressure booster 11.
- the pressure booster 11 In the in FIG. 2 shown position is the pressure booster 11 in its rest position.
- the differential pressure chamber 17 and the working chamber 12 are connected via the switching valve 5 and the inlet 13 to the working chamber 12 and via the inlet 43, 35, 40 to the differential pressure chamber 17 with the pressure accumulator 2 in combination. Therefore prevails in the in FIG. 2 illustrated switching position of the switching valve 5 in the working space 12 and the differential pressure chamber 17 identical pressure.
- About the branching off from the differential pressure chamber 17 of the pressure booster relief line 29 and the Budapeststommone flow restrictor 30 is in the differential pressure chamber 17 prevailing pressure level beyond in the control chamber 20 of the injection valve member 24 at.
- the switching valve 5 Upon actuation of the switching valve 5, ie its transfer from the in FIG. 2 shown switching position in which the overflow line 43 is brought into connection with the low-pressure side return 7, the pressure differential of the differential pressure chamber 17 takes place.
- the fuel flows from the differential pressure chamber 17 via the formed in the pressure booster piston 14 transverse opening 41 into the central control line 31 forming channel 40 and from this into the recess 35 within the first housing part 8 a. From the recess 35, the fuel flows via the overflow line 43 into the low-pressure side pressure run 7 and from there into an in FIG. 2 Not shown fuel reservoir from.
- FIG. 2 illustrated variant requires fewer items and is therefore cheaper to manufacture.
- FIG. 3 shows an embodiment of the fuel injector with pressure booster with a partially embedded in the pressure booster piston member.
- FIG. 3 illustrated embodiment of a fuel injector with pressure booster differs from the in FIGS. 1 and 2 illustrated embodiments of a fuel injector with pressure booster in that in the pressure booster piston 14, a piston member 60 is integrated.
- the piston member 60 is slidably received within the pressure booster piston 14.
- There is a space 63 between the lower end face of the piston part 60 and the pressure booster piston and the piston part 60 accommodated in the pressure booster piston 14 comprises on its end face opposite the first housing part 8 a sealing seat 61 which compensates for tolerances between the first housing part 8 and the housing second housing part 9 of the injector body 4 is also designed as a flat seat.
- the central control line 31 which extends as a channel 40 through the piston member 60, sealed against the working space 12 of the pressure booster 11.
- the guide surface for the piston part 60 in the pressure booster piston 14 is designated by reference numeral 64.
- the sealing seat is arranged on a disk-shaped area formed in enlarged diameter. The fuel contained in the working chamber 12 of the pressure booster 11 presses the piston member 60 via this annular surface to the first housing part 8 and thus supports the sealing effect of the sealing seat 61 between the working chamber 12 and the central control line 31 via which the differential pressure chamber 17 of the pressure booster 11 pressure relieved or is pressurizable.
- FIG. 3 illustrated embodiment of a fuel injection device The functioning of the in FIG. 3 illustrated embodiment of a fuel injection device is as follows.
- the volume of fuel contained in the high pressure accumulator flows through the high pressure line 3 to the first housing part 8.
- the fuel flows via the overflow line 43 to the recessed into the pressure booster piston 14 piston part 60 and passes through the one portion of the central control line 31 forming channel 40.
- the fuel enters the space 63, from which it flows via the transverse opening 41 in the differential pressure chamber 17 of the pressure booster 11.
- the overflow 43 is brought upon actuation of the switching valve 5 with the low-pressure side return 7 in connection, whereby the differential pressure chamber 17 via the transverse opening 41, the space 63 in the piston part 60 formed central control line 31 (channel 40) is relieved of pressure in the low-pressure side return.
- Due to the first end face 15 of the pressure booster piston 14 acting on the fuel in the working chamber 12 moves the pressure booster piston 14 with its the high-pressure chamber 19 assigning end face in this.
- the overflow 43 and thus the upper piston surface of the piston member 60 is at low pressure.
- the surface of the piston member 60 in the working space 12 shows a hydraulic sealing force.
- the piston part 60 is pressed against the housing part 8.
- the injector member 24 which can be formed, for example, as a nozzle needle, comprises a pressure shoulder, which causes a vertical movement in the opening direction of the injection valve member 24 into the control chamber 20 due to the high pressure fuel flowing into the nozzle chamber 23.
- the fuel contained in the nozzle chamber 23 flows via the annular gap surrounding the injection valve member 24 into injection openings 25 and is injected from there into the combustion chamber 26 of the autoignition internal combustion engine.
- the fuel volume displaced in the nozzle chamber 20 when the nozzle of the injection valve member 24 is displaced flows via the relief line 29 and the throttle point 30 contained therein to the pressure-relieved differential pressure chamber 17. From there, the diverted control volume flows via the transverse opening 41, the space 63, the central control line 31 within the piston part 60 and the overflow line 43 to the switching valve 5 and from there into the low-pressure side return 7.
- FIG. 4 is a fuel injector removable with pressure booster, which is controlled by a servohydraulic trained 3/2-way valve.
- the fuel injector shown in Fig. 1 is also controlled by the injector containing a pressure booster 11 via a switching valve 70 arranged on the upper side of the fuel injection device 1, but designed as a servohydraulic 3/2 way valve.
- the servohydraulic switching valve 70 comprises a servo piston (valve body 71) and a control valve arranged at the return 73.
- the switching valve 70 is connected via a line to the working space 12 of the pressure booster in connection.
- ND denotes a low-pressure side return, which also branches off from the valve housing of the switching valve 70.
- a control edge designated VQ1 is opened and a control edge designated VQ2 is closed.
- the control line 31 is thus connected to the working space 12 of the pressure booster.
- the valve 70 is switched, the control edge VQ1 is closed and the control edge VQ2 is opened, so that the central control line 31 communicates with the low-pressure side return ND.
- a low-pressure side return 73 extends to a in FIG. 4 Not shown fuel reservoir, such as the tank of a motor vehicle.
- the servohydraulic 3/2-way valve comprises a valve body 71, which is traversed by a through hole 72 which receives a throttle point.
- the pressure booster piston 14 separates the working space 12 of the pressure booster 11 from the integrated in the injector body 4 differential pressure chamber 17. Within the working space 12 of the pressure booster 11, the return spring 18 is added. This is supported, a sleeve-shaped portion of the pressure booster piston 14 surrounding the first disc 51 and the second disc 52 from.
- the first disc 51 is attached to the upper end face of the pressure booster piston 14, while the second disc 50 may be introduced into the wall of the injector body 4.
- the second disc 52 is located above the first end face 15 of the pressure booster piston, while the second end face 16 of the pressure booster piston 14 is a boundary surface of the differential pressure chamber 17 of the pressure booster 11.
- the control chamber 20 of an injection valve member 80 is integrated into the pressure booster piston 14. Within the control chamber 20, the one end face 79 of the injection valve member 80 acting on nozzle spring 27 is inserted.
- the injection valve member 80 according to the embodiment in FIG. 4 is surrounded by the high-pressure chamber 19 of the pressure booster 11, that is, in this embodiment, the high-pressure chamber 19 and the nozzle chamber 23 are identical.
- the nozzle chamber 23 is formed by the high-pressure chamber 19 of the pressure booster 11.
- the injection valve member 80 is surrounded below the high-pressure chamber 19 of the pressure booster piston 14 by a sealing sleeve 81.
- the sealing sleeve 81 is connected via a spring element 82, which in the high-pressure chamber 19 of the pressure booster 11 is inserted, acted upon and sealed against the high pressure chamber 19 of the pressure booster 11 assigning end face, so that the control chamber 20 and a dipping into this coaxial piston 74 are sealed against the high-pressure chamber 19.
- the injection valve member 80 has a fuel passage 83 which passes through the injection valve 80 in an inclined position and opens at the combustion chamber end of the fuel injection device 1 into an annular gap 84 between injection valve member 80 and injector body 4. Below the annular space 84 in the injector body 4, the combustion chamber-side seat of the injection valve member 80 is closed.
- a coaxial piston 74 is inserted, which is arranged symmetrically to the axis of symmetry of the injector body 4 of the fuel injection device 1 and is received stationary within the injector body 4.
- the coaxial piston 74 is penetrated by the central control line 31 for pressurizing or pressure relief of the differential pressure chamber 17 serving channel 40.
- the coaxial piston 74 comprises a support surface 75.
- a biasing spring 76 is supported, which seals the sealing sleeve 36 against the injector body 4.
- the central control line 31 is sealed against the in the working chamber 12 via the high pressure line 3 pending, prevailing in the high pressure accumulator 2 high pressure.
- the sealing sleeve 36 of the coaxial piston 74 this is enclosed by the recorded in the control chamber 20 nozzle spring 27.
- the coaxial piston 74 traversing transverse opening 41.
- the first outflow cross section 77 has a smaller flow cross section compared to the second outflow cross section and is always effective while the second outflow cross section 78 is opened or closed in accordance with the stroke of the pressure booster piston 14 of the pressure booster 11.
- the fuel flows via the overflow line 43 connected to the injector body 4 into the servohydraulic switching valve 70 and via the control edge VQ2 (valve cross-section) into the low-pressure-side return line ND.
- VQ2 valve cross-section
- the taking place via the outflow cross sections 77 and 78 pressure relief of the differential pressure chamber 17 causes a corresponding to the transmission ratio of the booster 11 failing pressure increase within the high-pressure chamber 19, in the embodiment according to FIG. 4 acts as a nozzle chamber.
- the high-pressure chamber 19 and the control chamber 20 are separated from each other via the second sealing sleeve 81 acted upon by the spring 82, so that no overflow of fuel occurs. Due to the increase in pressure in the high-pressure chamber 19 at this retracting pressure booster piston 14, the pressure increases significantly.
- the increasing fuel pressure acts on one of the injection valve member 80 formed pressure shoulder, which ascends against the force of the nozzle spring 27 in the control chamber 20, ie opens.
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
Zur Einbringung von Kraftstoff in Brennräume selbstzündender Verbrennungskraftmaschinen können sowohl druckgesteuerte als auch hubgesteuerte Einspritzsysteme eingesetzt werden. Einspritzsysteme mit Hochdruckspeichern haben den Vorteil, dass der Einspritzdruck an Last und Drehzahl der Verbrennungskraftmaschine angepasst werden kann. Zur Reduzierung der entstehenden Emissionen und zur Erzielung einer hohen spezifischen Leistung der Verbrennungskraftmaschine ist ein hoher Einspritzdruck erforderlich. Da das durch Hochdruck-Kraftstoffpumpen im Hochdruckspeicher erreichbare Druckniveau aus Festigkeitsgründen begrenzt ist, kann zur weiteren Drucksteigerung bei Kraftstoffeinspritzeinrichtungen mit einem Hochdruckspeicherraum ein Druckverstärker am Kraftstoffinjektor eingesetzt werden.For the introduction of fuel into combustion chambers of self-igniting internal combustion engines, both pressure-controlled and stroke-controlled injection systems can be used. Injection systems with high-pressure accumulators have the advantage that the injection pressure can be adapted to the load and speed of the internal combustion engine. To reduce the resulting emissions and to achieve a high specific power of the internal combustion engine, a high injection pressure is required. Since the achievable by high-pressure fuel pumps in the high-pressure accumulator pressure level is limited for strength reasons, can be used to further increase pressure in fuel injectors with a high-pressure accumulator a pressure booster on the fuel injector.
Von Nachteil bei den aus
Aus
Mit der erfindungsgemäß vorgeschlagenen Lösung lässt sich eine Verbesserung der Hochdruckfestigkeit eines Kraftstoffinjektors mit Druckübersetzer erreichen. Die zentrale Steuerleitung zur Druckentlastung bzw. Druckbeaufschlagung des zur Betätigung des Druckübersetzers dienenden Differenzdruckraumes verläuft dabei im Wesentlichen koaxial zur Symmetrieachse durch den Druckübersetzerkolben und erstreckt sich durch den mit Hochdruck beaufschlagten Arbeitsraum des Druckübersetzers. Die Steuerleitung ist dabei gegen den Arbeitsraum über eine hochdruckdichte Verbindung abgedichtet.With the proposed solution according to the invention, an improvement in the high-pressure resistance of a fuel injector with pressure booster can be achieved. The central control line for pressure relief or pressurization of serving for the actuation of the pressure booster differential pressure chamber is substantially coaxial with the axis of symmetry through the pressure booster piston and extends through the pressurized working space of the pressure booster. The control line is sealed against the working space via a high-pressure-tight connection.
Der Fortfall einer an der Außenseite des Kraftstoffinjektors mit Druckübersetzer vorbei geführten Steuerleitung reduziert außerdem die Außenabmessung des Kraftstoffinjektors oder vermeidet eine exzentrisch zum Kraftstoffinjektor orientierte Anordnung eines Druckübersetzers.The omission of a guided on the outside of the fuel injector with pressure booster control line also reduces the outer dimension of the fuel injector or avoids an eccentric to the fuel injector oriented arrangement of a pressure booster.
Eine sich koaxial zur Symmetrieachse des Kraftstoffinjektors erstreckende Steuerleitung im Übersetzerkolben vermeidet in vorteilhafter Weise Bohrungsverschneidungen, wie sich bei außen liegenden Leitungen aufgrund der Anschlusslage der von Hochdruckanschlüssen zwangsläufig auftreten und reduziert die Materialbeanspruchung, was wiederum die Standzeit des Kraftstoffinjektors mit Druckübersetzer erhöht. Eine Abdichtung zwischen dem Arbeitsraum und der zentralen Steuerleitung kann mittels eines durch ein Federelement vorgespannte Dichthülse erreichts werden, die vorteilhafterweise mit einem Flachsitz im Arbeitsraum zusammenwirkt. Dies erlaubt den Ausgleich fertigungsbedingter Toleranzen bei einem mit mehreren miteinander zu fügenden Gehäuseteilen ausgeführten Kraftstoffinjektor mit Druckübersetzer. Die zentrale Steuerleitung erstreckt sich durch einen am Kolben des Druckübersetzers ausgebildeten Fortsatz, der einen Führungsabschnitt für die am Kolbenansatz bewegbar angeordnete Dichthülse aufweist.A coaxially extending to the axis of symmetry of the fuel injector control line in the booster piston advantageously avoids Bohrungsverschneidungen, as inevitably occur in external lines due to the connection position of high pressure connections and reduces the material stress, which in turn increases the service life of the fuel injector with pressure booster. A seal between the working space and the central control line can be achieved by means of a biased by a spring element sealing sleeve, which advantageously cooperates with a flat seat in the working space. This allows the compensation of production-related tolerances in a running with a plurality of housing parts to be joined fuel injector with pressure booster. The central control line extends through an extension formed on the piston of the pressure booster, which has a guide section for the sealing sleeve movably arranged on the piston shoulder.
In einer weiteren Ausführungsvariante des der Erfindung zugrunde liegenden Gedankens kann ein am Übersetzerkolben des Druckverstärkers angeordneter Kolbenfortsatz in einer hochdruckdichten Führung aufgenommen sein, die in einem der Gehäuseteile des Kraftstoffinjektors mit Druckübersetzer ausgeführt wird. Die hochdruckdichte Führung des Kolbenfortsatzes wird so ausgelegt, dass sie entlang des gesamten Hubweges des Kolbens des Druckübersetzers wirksam ist und die zentrale Steuerleitung vom Arbeitsraum des Druckübersetzers trennt.In a further embodiment of the idea underlying the invention, a piston extension arranged on the booster piston of the pressure booster can be accommodated in a high-pressure-tight guide, which is embodied in one of the housing parts of the fuel injector with pressure booster. The high pressure-tight guide of the piston extension is designed so that it is effective along the entire stroke of the piston of the pressure booster and the central control line separates from the working space of the pressure booster.
Anstelle eines die zentrale Steuerleitung aufnehmenden Kolbenansatzes am Kolben des Druckübersetzers, kann in diesem ein Kolben aufgenommen werden, der einen durchgängigen Kanal aufweist. Gemäß dieser Ausführungsvariante kann eine Dichtstelle als Flachsitz ausgeführt werden, um die zentrale Steuerleitung gegen den Arbeitsraum des Druckübersetzers abzudichten. Dies ermöglicht einerseits den Ausgleich fertigungsbedingter Toleranzen zwischen den Gehäuseteilen und andererseits eine fertigungstechnisch einfache Herstellung. In einer weiteren Ausführungsvariante eines Kraftstoffinjektors mit Druckübersetzer enthält der Druckübersetzer ein sich durchgängig durch diesen erstreckendes Kolbenelement mit einem durchgängig durch diesen verlaufenden Kanal. Der Kanal ist je nach Hubweg des Druckübersetzers durch einen ersten oder durch einen ersten und einen zweiten Abflussquerschnitt mit dem Differenzdruckraum des Druckübersetzers verbunden. Damit lässt sich der Druckaufbau des Druckübersetzers entsprechend eines gewünschten Einspritzdruckverlaufes steuern.Instead of a central control line receiving piston shoulder on the piston of the pressure booster, in this a piston can be received, which has a continuous channel. According to this embodiment, a sealing point can be designed as a flat seat to seal the central control line against the working space of the pressure booster. On the one hand, this makes it possible to compensate for production-related tolerances between the housing parts and, on the other hand, a production-technically simple production. In a further embodiment variant of a fuel injector with a pressure booster, the pressure booster contains a piston element extending continuously through the piston element with a channel extending continuously through it. The channel is connected depending on the stroke of the pressure booster by a first or by a first and a second flow area with the differential pressure chamber of the pressure booster. Thus, the pressure build-up of the pressure booster can be controlled according to a desired injection pressure curve.
Die zentrale Steuerleitung lässt sich bei allen Druckübersetzern einsetzen, die über einen Differenzdruckraum gesteuert werden.The central control line can be used with all pressure intensifiers that are controlled via a differential pressure chamber.
Anhand der Zeichnung wird die Erfindung nachstehend näher erläutert.Reference to the drawings, the invention will be explained in more detail below.
Es zeigt:
Figur 1- einen Kraftstoffinjektor mit Druckübersetzer mit hochdruckdichter Ver- bindung am oberen Ende des Arbeitsraumes,
Figur 2- einen Kraftstoffinjektor mit Druckübersetzer, bei dem ein Steuerleitungs- abschnitt in einer hochdruckdichten Führung aufgenommen ist,
Figur 3- eine Ausführungsvariante des Kraftstoffinjektors mit Druckübersetzer mit einem teilweise in den Druckübersetzerkolben eingelassenen, einen Dichtsitz bildenden Kolbenelement und
Figur 4- einen Kraftstoffinjektor mit Druckübersetzer, der über ein servohydrau- lisch unterstützes 3/2-Wege-Ventil angesteuert wird.
- FIG. 1
- a fuel injector with pressure intensifier with high-pressure-tight connection at the upper end of the working space,
- FIG. 2
- a fuel injector with a pressure booster, in which a control line section is accommodated in a high-pressure-tight guide,
- FIG. 3
- a variant of the fuel injector with pressure booster with a partially embedded in the pressure booster piston, a sealing seat forming piston element and
- FIG. 4
- a fuel injector with pressure booster, which is controlled by a servohydraulically assisted 3/2-way valve.
Gemäß des in
Der Injektorkörper 4 der Kraftstoffeinspritzeinrichtung 1 umfasst ein erstes Gehäuseteil 8 sowie ein weiteres, zweites Gehäuseteil 9 und ein Injektorgehäuse 10, welches ein Einspritzventilglied 24 umschließt. Das erste Gehäuseteil 8 und das zweite Gehäuseteil 9 liegen entlang einer Stoßfuge 32 aneinander an.The
Im Injektorkörper 4 der Kraftstoffeinspritzeinrichtung 1 ist ein Druckübersetzer 11 aufgenommen. Der Druckübersetzer 11 umfasst einen mit Bezugszeichen 12 identifizierten Arbeitsraum, der über einen von der Hochdruckleitung 3 abzweigenden Zulauf 13 mit unter hohem Druck stehenden Kraftstoff beaufschlagbar ist. Der Druckübersetzer 11 umfasst einen Druckübersetzer-Kolben 14, der eine erste Stirnseite 15 enthält, die dem Arbeitsraum 12 zuweist, und eine zweite Stirnseite 16 enthält, die einem Differenzdruckraum 17 zuweist. Der Druckübersetzer-Kolben 14 ist an der zweiten Stirnseite 16 durch eine Rückstellfeder 18 abgestützt, die sich ihrerseits auf eine Ringfläche innerhalb des zweiten Gehäuseteiles 9 des Injektorkörpers 4 abstützt. Der Druckübersetzer-Kolben 14 des Druckübersetzers 11 beaufschlagt einen Hochdruckraum 19, der sich im unteren Bereich des zweiten Gehäuseteiles 9 befindet. Entsprechend des Übersetzungsverhältnisses des Druckübersetzers 11 wird bei Einfahren der dem Hochdruckraum 19 zuweisenden Stirnseite des Druckübersetzer-Kolbens 14, der in diesem enthaltene Kraftstoff nochmals komprimiert und strömt einerseits in einen Steuerraum 20 und andererseits über einen Düsenraumzulauf 22 in einen Düsenraum 23, der im Injektorgehäuse 10 ausgebildet ist. Der Düsenraum 23 umschließt das Einspritzventilglied 24 der Kraftstoffeinspritzeinrichtung in einem Bereich, in welchem am Einspritzventilglied 24 eine Druckschulter ausgebildet ist. Vom Düsenraum 23 erstreckt sich ein Ringspalt zum brennraumseitigen Ende der Kraftstoffeinspritzeinrichtung 1. Über den Ringspalt sind Einspritzöffnungen 25 am brennraumseitigen Ende des mit der Kraftstoffeinspritzeinrichtung 1 mit Kraftstoff beaufschlagt. Diese werden bei einer vertikalen Bewegung des Einspritzventilgliedes 24 freigegeben, so dass über die Einspritzöffnungen 25 unter hohem Druck stehender Kraftstoff in einen Brennraum 26 einer selbstzündenden Verbrennungskraftmaschine eingespritzt werden kann.In the
Die Druckbeaufschlagung des Steuerraumes 20 zur Betätigung des beispielsweise als Düsennadel ausbildbaren Einspritzventilgliedes 24 erfolgt über eine den Düsenraum 20 und den Hochdruckraum 19 des Druckübersetzers 11 verbindende Leitung, in der eine Zulaufdrossel 21 aufgenommen ist. Innerhalb des Steurraumes 20 ist eine Düsenfeder 27 aufgenommen, die einen Zapfen 28 des Einspritzventilgliedes umschließt und sich an einer Ringfläche des Einspritzventilgliedes 24 abstützt. Zwischen dem Differenzdruckraum 17 des Druckübersetzers 11 und dem Steuerraum 20 erstreckt sich eine eine Ablaufdrossel 30 aufnehmende Entlastungsleitung 29.The pressurization of the
Der Druckübersetzer-Kolben 14 des Druckübersetzers 11 enthält eine zentrale Steuerleitung 31. Die zentrale Steuerleitung 31 steht über eine im Druckübersetzer-Kolben 14 ausgebildete Queröffnung 41 mit dem Differenzdruckraum 17 des Druckübersetzers 11 in Verbindung. Die Queröffnung 41 ihrerseits ist mit einem die zentrale Steuerleitung 31 darstellenden Kanal 40 verbunden, welcher den den Arbeitsraum 12 und den Differenzdruckraum 17 trennenden Abschnitt des Druckübersetzers-Kolbens 14 durchzieht und durch einen an der ersten Stirnseite 15 des Druckübersetzer-Kolbens 14 angeordneten Kolbenansatz 34 verläuft. Der den Kanal 40 aufnehmende Kolbenansatz 34 an der ersten Stirnseite 15 des Drucküberetzers-Kolbens 14 verläuft bis in die Ausnehmung 35 im ersten Gehäuseteil 8 des Injektorkörpers 4. Am Kolbenansatz 34 des Druckübersetzers-Kolbens 14 ist innerhalb eines Führungsabschnittes 42 eine erste Dichthülse 36 bewegbar. Die erste Dichthülse 36 umfasst einen ringförmigen Ansatz 39, an welchem sich eine Anstellfeder 38 abstützt. Die Anstellfeder 38 stützt sich mit ihrem der ersten Dichthülse 36 gegenüberliegenden Ende auf der ersten Stirnseite 15, den Kolbenansatz 34 umgebend ab. Durch die Anstellfeder 38 wird die am Kolbenansatz 34 aufgenommene erste Dichthülse 36 mit einer Dichtfläche 37 an die untere Stirnseite des ersten Gehäuseteiles 8 des Injektorkörpers 4 angestellt. Dadurch lässt sich eine hochdruckdichte Verbindung 33 erzielen, welche die zentrale Steuerleitung 31 vom Arbeitsraum 12 des Druckübersetzers 11 trennt. Gemäß des in
Die Funktionsweise des in
- Zu Beginn einer Einspritzung wird
das Schaltventil 5 von seiner in dargestellten Lage, welche seiner Schließlage entspricht, in eine Öffnungslage geschaltet. In der Öffnungsposition des Schaltventiles 5 stehen der niederdruckseitige Rücklauf 7 und dieFigur 1Überströmleitung 43 in Verbindung miteinander.Während der Arbeitsraum 12 desDruckübersetzers 11über den Abzweig 13von der Hochdruckleitung 3mit dem Hochdruckspeicher 2 verbunden bleibt, strömt vom Differenzdruckraum 17 über dieQueröffnung 41, und den die zentrale Steuerleitung 31bildenden Kanal 40 Kraftstoff durch den Druckübersetzer-Kolben 1 indie Ausnehmung 35im ersten Gehäuseteil 8 und von dort über die Überströmleitung inden niederungseitigen Rücklauf 7. Aufgrunddes im Arbeitsraum 12 desDruckübersetzers 11 nach wie vor herrschenden Hochdruckniveaus fährt der Druckübersetzer-Kolben 14 mit seiner unteren Stirnseite inden Hochdruckraum 19 ein. Von diesem strömt unter einem - im Vergleich zum Druckniveau des Hochdruckspeicherraumes 2 - entsprechend des Übersetzungsverhältnisses des Druckübersetzers 11 erhöhten Druckniveau - Kraftstoff einerseits inden Düsenzulauf 22im Düsenraum 23 und andererseits über dieZulaufdrossel 21dem Steuerraum 20 zu. Der inden Düsenraum 23 einschießende und unter hohem Druck stehende Kraftstoff greift an der Druckschulter des Einspritzventilgliedes 24 an und bewirkt eine vertikale Hubbewegung des Einspritzventilgliedes 24 in Öffnungsrichtung entgegen der Wirkung der Düsenfeder 27, die ebenfallsim Steuerraum 20 enthalten ist. Durch die Hubbewegung verdrängtes Absteuervolumen strömt über dieDruckentlastungsleitung 29,eine Ablaufdrossel 30 enthaltend, inden Differenzdruckraum 17 desDruckverstärkers 11 ein.
- At the beginning of an injection, the switching
valve 5 of his inFIG. 1 shown, which corresponds to its closed position, switched to an open position. In the opening position of the switchingvalve 5 are the low-pressure side return 7 and theoverflow 43 in communication with each other. While the workingspace 12 of thepressure booster 11 remains connected to the high-pressure accumulator 2 via thebranch 13 from the high-pressure line 3, fuel flows from thedifferential pressure chamber 17 via thetransverse opening 41 and thechannel 40 forming thecentral control line 31 through thepressure booster piston 1 into therecess 35 in thefirst housing part 8 and from there via the overflow in the low-side return 7. Due to the in the workingchamber 12 of thepressure booster 11 still prevailing high pressure levels moves thepressure booster piston 14 with its lower end face in the high-pressure chamber 19 a. From this flows under a - compared to the pressure level of the high-pressure accumulator 2 - corresponding to the transmission ratio of thepressure booster 11 increased pressure level - fuel on the one hand in thenozzle inlet 22 in thenozzle chamber 23 and on the other hand via theinlet throttle 21 to thecontrol chamber 20. The injecting into thenozzle chamber 23 and under high pressure fuel engages the pressure shoulder of theinjection valve member 24 and causes a vertical lifting movement of theinjection valve member 24 in the opening direction against the action of thenozzle spring 27, which is also contained in thecontrol chamber 20. By the lifting movement displaced Absteuervolumen flows through thepressure relief line 29, containing adischarge throttle 30, in thedifferential pressure chamber 17 of the booster 11 a.
Aufgrund der vertikalen Hubbewegung des Einspritzventilgliedes 24 werden die in den Brennraum 26 einer selbstzündenden Verbrennungskraftmaschine hineinragenden Einspritzöffnungen 25 mit unter hohem Druck stehenden Kraftstoff beaufschlagt und spritzen diesen in den Brennraum 26 ein.Due to the vertical lifting movement of the
Beim erneuten Schalten des Schaltventiles 5 erfolgt eine Druckbeaufschlagung des Differenzdruckraumes 17 vom Hochdruckspeicher 2 über die Hockdruckleitung 3, den Zulauf 6 und die Überströmleitung 43 und die Ausnehmung 35 im ersten Gehäuseteil 8. Von dort strömt der Kraftstoff durch den die zentrale Steuerleitung 31 bildenden Kanal 40 und tritt über die Queröffnung 41 in den Differenzdruckraum 17 ein und beaufschlagt diesen wieder mit dem im Hochdruckspeicher 2 herrschenden Druckniveau. Dadurch wird der Hochdruckraum 19 entlastet, ebenso wie der das Einspritzventilglied 24 umgebende Düsenraum 23 im Injektorgehäuse 10. Über die Düsenfeder 27 wird das Einspritzventilglied 24 in seinem brennraumseitigen Sitz gedrückt, die Einspritzung ist beendet. Eine Wiederbefüllung des Steuerraumes 20 erfolgt über die Entlastungsleitung 29, die in diesem Falle in entgegengesetzte Richtung, den Steuerraum 20 befüllend, von Kraftstoff durchströmt wird. Eine Wiederbefüllung des Hochdruckraumes 19 des Druckübersetzers 11 erfolgt durch Überströmen von Kraftstoff aus dem Steuerraum 20 über die die Zulaufdrossel 21 enthaltende Leitung in den Hochdruckraum 19.When the switching
In der in
Gemäß der in
Über die Hochdruckleitung 3 strömt dem ersten Gehäuseteil 8 des Injektorkörpers 4 der Kraftstoffeinpritzeinrichtung 1 unter hohem Druck stehender Kraftstoff zu. Dieser wird über den Zulauf zum Schaltventil 5 geleitet. Das Schaltventil 5 umfasst einen Anschluß zum niederdruckseitigen Rücklauf 7 sowie eine Überströmleitung 43 zu der im ersten Gehäuseteil 8 ausgebildeten Ausnehmung 35. Über den Abzweig 13 der Hochdruckleitung 3 innerhalb des ersten Gehäuseteiles 8 wird der Arbeitsraum 12 des Druckverstärkers 11 mit unter hohem Druck stehenden Kraftstoff beaufschlagt. Der Druckverstärker 11 umfasst einen Druckübersetzer-Kolben 14, der den Arbeitsraum 12 des Druckübersetzers 11 von dessen Differenzdruckraum 17 trennt. Der Druckübersetzer-Kolben 14 umfasst den an der ersten Stirnseite 15 befestigten Kolbenfortsatz 34. Am den Arbeitsraum 12 im zweiten Gehäuseteil 9 durchsetzenden Kolbenfortsatz 34 ist eine erste Scheibe 51 angeordnet. Oberhalb des Druckverstärker-Kolbens 14 ist an der Innenseite des Arbeitsraumes 12 des Druckverstärkers 11 eine weitere, zweite Scheibe 52 angeordnet. Zwischen der ersten und der zweiten Scheibe 51, 52 ist eine Rückstellfeder 18 aufgenommen, über welche der Druckübersetzer-Kolben 14 in seine Ausgangslage innerhalb des zweiten Gehäuseteiles 9 zurückgestellt wird.Via the high-
Die untere Stirnseite des Druckübersetzer-Kolbens 14 beaufschlagt den im zweiten Gehäuseteil 9 des Injektorkörpers 4 ausgebildeten Hochdruckraum 19. Das in dem Hochdruckraum 19 erzielbare hohe Druckniveau ist abhängig von dem Übersetzungsverhältnis des Druckverstärkers 11 und liegt höher als das im Hochdruckspeicher 2 herrschende Druckniveau. Vom Hochdruckraum 19 des Druckverstärkers 11 strömt unter einem weiter erhöhten Druckniveau stehender Kraftstoff über den Düsenraumzulauf 22 den Düsenraum 23 im Injektorgehäuse 10 zu. Im Bereich des Düsenraumes 23, der das als Düsennadel beispielsweise ausbildbare Einspritzventilglied 24 umgibt, umfasst das Einspritzventilglied 24 eine Druckschulter. Vom Düsenraum 23 innerhalb des Injektorgehäuses 10 erstreckt sich ein Ringspalt, über welchen der unter hohem Druck stehende Kraftstoff auf vom Düsenraum 23 den Einspritzöffnung 25 zuströmt. Bei geöffneten Einspritzventilglied 24 wird über die Einspritzöffnungen 25 unter sehr hohem Druck stehender Kraftstoff in den Brennraum 26 der selbstzündenden Verbrennungskraftmaschine eingespritzt.The lower end face of the
Vom Hochdruckraum 19 erstreckt sich ferner ein Leitungsabschnitt zum Düsenraum 20. In diesem Leitungsabschnitt ist eine Zulaufdrossel 21 aufgenommen. Der Steuerrraum 20 für das Einspritzventilglied 24 enthält eine Düsenfeder 27, die sich einerseits an einer Ringfläche des Einspritzventilgliedes 24, einen Zapfen 28 umgebend, abstützt. Andererseits liegt die Düsenfeder 27 an einer den Düsenraum 20 begrenzenden Wandung des zweiten Gehäuseteiles 9 an. Ein Überströmen von Steuervolumen aus Düsenraum 20 in den Differenzdruckraum 17 des Druckübersetzers 11 erfolgt über die den Düsenraum 20 in den Differenzdruckraum 17 verbindende Entlastungsleitung 29, in der eine Ablaufdrossel 30 aufgenommen ist.From the high-
Der Druckübersetzer-Kolben 14 des Druckübersetzers 11 umfasst eine zentrale Steuerleitung 31. Die zentrale Steuerleitung 31 ist als ein sowohl den Kolbenansatz 34 als auch den Druckübersetzer-Kolben 14 durchziehender Kanal 40 ausgebildet, der an seinem unteren, in den Differenzdruckraum 17 mündenden Ende, eine Queröffnung 41 umfasst. Diese kann als Bohrung, als Kanal oder dergleichen im Druckübersetzer-Kolben 14 ausgeführt sein. Von der Queröffnung 41 im Druckübersetzer-Kolben 14 erstreckt sich der Kanal 40 bis in die Ausnehmung 35 im ersten Gehäuseteil 8 des Injektorkörpers 4. Im ersten Gehäuseteil 8 ist der Kopfbereich des Kolbenansatzes 34 in einer hochdruckdichten Führung 50 aufgenommen. Die hochdruckdichte Führung 50 innerhalb des ersten Gehäuseteiles 8 geht in die Ausnehmung 35 über und ist in einer dem Hubweg des Druckübersetzer-Kolben 14 entsprechenden axialen Länge ausgebildet. Dadurch ist gewährleistet, dass entlang des gesamten Hubweges des Druckübersetzer-Kolbens 14 des Druckübersetzers 11 eine Hochdruckabdichtung zwischen der Ausnehmung 35 innerhalb des ersten Gehäuseteiles 8 und dem Arbeitsraum 12 des Druckübersetzers 11 gewährleistet ist.The
In der in
Bei der Betätigung des Schaltventiles 5, d. h. dessen Überführung von der in
Wird hingegen das Schaltventil 5 in seine in
Die in
Die in
Im übrigen entspricht das in
Die Funktionsweise des in
Eine Druckentlastung des Differenzdruckraumes 17 des Druckübersetzers 11 erfolgt über eine Betätigung des Schaltventiles 5. Die Überströmleitung 43 wird bei Betätigung des Schaltventiles 5 mit dem niederdruckseitigen Rücklauf 7 in Verbindung gebracht, wodurch der Differenzdruckraum 17 über die Queröffnung 41, den Raum 63, die im Kolbenteil 60 ausgebildete zentrale Steuerleitung 31 (Kanal 40) in den niederdruckseitigen Rücklauf druckentlastet wird. Aufgrund des die erste Stirnseite 15 des Druckübersetzer-Kolbens 14 beaufschlagenden Kraftstoff im Arbeitsraum 12 fährt der Druckübersetzer-Kolben 14 mit seiner dem Hochdruckraum 19 zuweisenden Stirnseite in diesen ein.A pressure relief of the
Bei Betätigung des Schaltventiles 5 liegt die Überströmleitung 43 und damit die obere Kolbenfläche des Kolbenteiles 60 auf Niederdruck. Die Fläche des Kolbenteiles 60 im Arbeitsraum 12 zeigt eine hydraulische Dichtkraft. Das Kolbenteil 60 wird gegen das Gehäuseteil 8 gepresst. Daneben ist es auch möglich, das Kolbenteil mittels einer Feder vorzuspannen, um diesen an die untere Stirnfläche des Gehäuseteiles 8, welches den Arbeitsraum 12 begrenzt, anzustellen.Upon actuation of the switching
Beim Einfahren der unteren Stirnseite des Druckübersetzer-Kolbens 14 in den Hochdruckraum 19 erfolgt eine Druckerhöhung des in diesem enthaltenden Kraftstoffes gemäß des Druckübersetzungsverhältnisses des Druckübersetzers 11. Der Kraftstoff strömt vom Hochdruckraum 19 über den Düsenraumzulauf 22 dem Düsenraum 23 zu. Im Bereich des Düsenraumes 23 umfasst das beispielsweise als Düsennadel ausbildbare Einspritzventilglied 24 eine Druckschulter, die aufgrund des unter hohem Druck stehenden, in den Düsenraum 23 einströmenden Kraftstoffes eine Vertikalbewegung in Öffnungsrichtung des Einspritzventilgliedes 24 in den Steuerraum 20 bewirkt. Der im Düsenraum 23 enthaltene Kraftstoff strömt über den das Einspritzventilglied 24 umgebenden Ringspalt in Einspritzöffnungen 25 zu und wird von dort in den Brennraum 26 der selbstzünden Verbrennungskraftmaschine eingespritzt. Das beim Auffahren der Düse des Einspritzventilgliedes 24 im Düsenraum 20 verdrängte Kraftstoffvolumen strömt über die Entlastungsleitung 29 und die darin enthaltene Drosselstelle 30 dem druckentlasteten Differenzdruckraum 17 zu. Von dort strömt das abgesteuerte Steuervolumen über die Queröffnung 41, den Raum 63, die zentrale Steuerleitung 31 innerhalb des Kolbenteiles 60 und die Überströmleitung 43 zum Schaltventil 5 und von dort in den niederdruckseitigen Rücklauf 7 ab.When retracting the lower end face of the
Sowohl während der Befüllung als auch während der Druckentlastung des Differenzdruckraumes 17 des Druckübersetzers 11 ist der Arbeitsraum 12, der stets durch das im Hochdruckspeicher 2 enthaltene Kraftstoffdruckniveau beaufschlagt ist, wirksam gegen die zentrale Steuerleitung 31, die als Kanal 40 das Kolbenteil 60 durchzieht, abgedichtet. Ein Ausgleich von fertigungsbedingten Bauteiltoleranzen zwischen dem ersten Gehäuseteil 8 und dem zweiten Gehäuseteil 9 an der Stoßfuge 32 kann in vorteilhafter Weise dadurch erreicht werden, dass im Kopfbereich, d. h. an dem ersten Gehäuseteil 8 zuweisenden, verdickt ausgeführten Ende des Kolbenteiles 60 ein Flachsitz 61 ausgebildet ist.Both during filling and during the pressure relief of the
Bei den in
Vom Hochdruckspeicher 2 strömt über die Hochdruckleitung 3 unter hohem Druck stehender Kraftstoff in den Arbeitsraum 12 des Druckübersetzers 11 ein. In diesen Ausführungsbeispiel befindet sich der Arbeitsraum 12 im oberen Bereich des Injektorkörpers 4 der Kraftstoffeinspritzeinrichtung 1. Das servohydraulische Schaltventil 70 umfasst einen Servokolben (Ventilkörper 71) sowie ein am Rücklauf 73 angeordnetes Steuerventil. Das Schaltventil 70 steht über eine Leitung mit dem Arbeitsraum 12 des Druckübersetzers in Verbindung. Mit ND ist ein niederdruckseitiger Rücklauf bezeichnet, der ebenfalls vom Ventilgehäuse des Schaltventiles 70 abzweigt. Im Ruhezustand des Schaltventiles 70 ist eine mit VQ1 bezeichnete Steuerkante geöffnet und eine mit VQ2 bezeichnete Steuerkante geschlossen. Die Steuerleitung 31 ist somit mit dem Arbeitsraum 12 des Druckübersetzers verbunden. Beim Schalten des Ventiles 70 wird die Steuerkante VQ1 geschlossen und die Steuerkante VQ2 geöffnet, so dass die zentrale Steuerleitung 31 mit dem niederdruckseitigen Rücklauf ND in Verbindung tritt.From the
Vom servohydraulischen 3/2-Wege-Ventil erstreckt sich ein niederdruckseitiger Rücklauf 73 zu einem in
Der Druckübersetzer-Kolben 14 trennt den Arbeitsraum 12 des Druckübersetzers 11 von dem im Injektorkörper 4 integrierten Differenzdruckraum 17. Innerhalb des Arbeitsraumes 12 des Druckübersetzers 11 ist die Rückstellfeder 18 aufgenommen. Diese stützt sich, einen hülsenförmigen Bereich des Druckübersetzer-Kolbens 14 umgebend an der ersten Scheibe 51 sowie an der zweiten Scheibe 52 ab. Die erste Scheibe 51 ist an der oberen Stirnseite des Druckübersetzer-Kolbens 14 angebracht, während die zweite Scheibe 50 in die Wandung des Injektorkörpers 4 eingebracht sein kann. Die zweite Scheibe 52 befindet sich oberhalb der ersten Stirnseite 15 des Druckübersetzer-Kolbens, während die zweite Stirnseite 16 des Druckübersetzer-Kolben 14 eine Begrenzungsfläche des Differenzdruckraumes 17 des Druckübersetzers 11 darstellt.The
In dem in
In den Druckübersetzer-Kolben 14 gemäß des Ausführungsbeispieles in
In der der in
Durch die 2. Dichthülse 81 ist der Steuerraum 20 und damit der Differenzdruckraum 17 des Druckübersetzers 11 vom als Düsenraum fungierenden Hochdruckraum 19 des Druckübersetzer 11 getrennt. Die Abdichtwirkung der 2. Dichthülse 81 wird durch die diese beaufschlagende, im Hochdruckraum 19 aufgenommene Vorspannfeder 82 unterstützt.By the
Mit dem in
Die über die Abströmquerschnitte 77 bzw. 78 erfolgende Druckentlastung des Differenzdruckraumes 17 bewirkt eine entsprechend des Übersetzungsverhältnisses des Druckverstärkers 11 ausfallende Druckerhöhung innerhalb des Hochdruckraumes 19, der in dem Ausführungsbeispiel gemäß
- 11
- KraftstoffeinspritzeinrichtungFuel injection system
- 22
- HochdruckspeicherHigh-pressure accumulator
- 33
- HochdruckleitungHigh-pressure line
- 44
- Injektorkörperinjector
- 55
- Schaltventilswitching valve
- 66
- Zulauf SchaltventilInlet switching valve
- 77
- niederdruckseitiger Rücklauflow-pressure side return
- 88th
- erstes Gehäuseteilfirst housing part
- 99
- zweites Gehäuseteilsecond housing part
- 1010
- Injektorgehäuseinjector
- 1111
- DruckübersetzerPressure intensifier
- 1212
- Arbeitsraumworking space
- 1313
- Abzweigjunction
- 1414
- Druckübersetzer-KolbenPressure booster piston
- 1515
- erste Stirnseitefirst end face
- 1616
- zweite Stirnseitesecond end face
- 1717
- DifferenzdruckraumDifferential pressure chamber
- 1818
- RückstellfederReturn spring
- 1919
- HochdruckraumHigh-pressure chamber
- 2020
- Steuerraumcontrol room
- 2121
- Zulaufdrosselinlet throttle
- 2222
- DüsenraumzulaufNozzle chamber inlet
- 2323
- Düsenraumnozzle chamber
- 2424
- EinspritzventilgliedInjection valve member
- 2525
- EinspritzöffnungInjection port
- 2626
- Brennraumcombustion chamber
- 2727
- Düsenfedernozzle spring
- 2828
- Zapfenspigot
- 2929
- Entlastungsleitungrelief line
- 3030
- Ablaufdrosseloutlet throttle
- 3131
- zentrale Steuerleitungcentral control line
- 3232
- Stoßfugebutt joint
- 3333
- Hochdruckdichte VerbindungHigh pressure density connection
- 3434
- Kolbenansatzpiston extension
- 3535
- Ausnehmung erstes GehäuseteilRecess first housing part
- 3636
- Dichthülsesealing sleeve
- 3737
- Dichtungpoetry
- 3838
- Anstellfederadjusting spring
- 3939
- Stützfläche erste DichthülseSupport surface first sealing sleeve
- 4040
- Kanalchannel
- 4141
- Queröffnungtransverse opening
- 4242
- Führungsabschnitt (Zentrierung 1. Dichthülse)Guide section (centering 1st sealing sleeve)
- 4343
- Überströmleitungoverflow
- 5050
- hochdruckdichte Führunghigh pressure-tight guide
- 5151
- erste Scheibefirst disc
- 5252
- zweite Scheibesecond disc
- 6060
- Kolbenteilpiston part
- 6161
- Dichtsitzsealing seat
- 6363
- FührupgsraumFührupgsraum
- 6464
- Führungsflächeguide surface
- 7070
-
servohydraulisches 3/2-Wege-Ventil
Servohydraulic 3/2-way valve - 7171
- Ventilkörpervalve body
- 7272
- DurchgangsbohrungThrough Hole
- 7373
- niederdruckseitiger Rücklauflow-pressure side return
- 7474
- Koaxial-KolbenCoaxial piston
- 7575
- Stützflächesupport surface
- 7676
- Vorspannfederbiasing spring
- 7777
- erster Abströmquerschnittfirst outflow cross section
- 7878
- zweiter Abströmquerschnittsecond outflow cross section
- 7979
- Stirnseite EinspritzventilgliedFront side injection valve member
- 8080
- EinspritzventilgliedInjection valve member
- 8181
- 2. Dichthülse2nd sealing sleeve
- 8282
- Federfeather
- 8383
- KraftstoffkanalFuel channel
- 8484
- Ringspaltannular gap
- VQ1V.sub.Q1
- erste Steuerkante (erster Ventilquerschnitt)first control edge (first valve cross-section)
- VQ2V Q2
- zweite Steuerkante (zweiter Ventilquerschnitt)second control edge (second valve cross-section)
- NDND
- niederdruckseitiger Rücklauflow-pressure side return
Claims (16)
- Fuel injection device (1) which is connected to a high-pressure source (2), having a multi-part injector body (4, 8, 9, 10) in which a pressure booster (11) which can be actuated by means of a differential pressure chamber (17) is held, the pressure booster piston (14) of which pressure booster (11) separates a working chamber (12) from the differential pressure chamber (17), and the fuel injection valve device (1) can be actuated by means of a switching valve (5, 70), with a pressure change in the differential pressure chamber (17) of the pressure booster (11) taking place via a central control line (31) which extends through the pressure booster piston (14), characterized in that the central control line (31) runs substantially coaxially with respect to the axis of symmetry of the pressure booster piston (14) and in that the central control line (31) extends through the working chamber (12) of the pressure booster (11) and is sealed off with respect to said working chamber (12) by means of a high-pressure-tight connection (33, 50, 61).
- Fuel injection device according to Claim 1, characterized in that the central control line (31) runs substantially coaxially with respect to the axis of symmetry of the injector body (4; 8, 9, 10).
- Fuel injection device according to Claim 1, characterized in that the pressure booster piston (14) comprises a line section (34, 60, 74) of the central flow line (31), through which line section (34, 60, 74) the duct (40) which constitutes the central control line (31) runs in the working chamber (12) of the pressure booster (11).
- Fuel injection device according to Claim 1, characterized in that the duct (40) opens out into a recess (35) within a first housing part (8) of the injector body (4; 8, 9, 10), which recess (35) is connected via an overflow line (43) to the switching valve (5, 70).
- Fuel injection device according to Claim 3, characterized in that the line section of the central control line (31) is formed as a tubular piston extension (34).
- Fuel injection device according to Claim 3, characterized in that the line section of the central control line (31) is designed as a coaxial piston (74), relative to which the pressure booster piston (14) is movable.
- Fuel injection device according to Claims 1 and 3, characterized in that a spring-loaded sealing sleeve (36) is held on the line section (34) of the central control line (31), which sealing sleeve (36) is movable relative to said line section (34) and provides a high-pressure sealing (33) of the working chamber (12).
- Fuel injection device according to Claims 1 and 3, characterized in that the line section (34) comprises a high-pressure-tight guide section (50) which is guided in a first housing part (8) of the injector body (4; 8, 9, 10).
- Fuel injection device according to Claims 1 and 3, characterized in that a piston part (60) which forms a line section of the central control line (31) is held in a movable fashion in the pressure booster piston (14), which piston part (60) is surrounded by said pressure booster piston (14) and in the head region of which piston part (60) is formed a sealing surface (61) which constitutes a high-pressure-tight connection.
- Fuel injection device according to Claim 7, characterized in that the sealing sleeve (36) is loaded against the injector body (4; 8, 9, 10) by means of a spring element (38, 76) which is supported either on the line section (74) or on an end side (15) of the pressure booster piston (14).
- Fuel injection device according to Claim 3, characterized in that the piston part (60), which forms a line section of the central control line (31), has a hydraulically acting surface and is loaded against a delimiting surface of the working chamber (12) of the pressure booster (11), so as to generate a high-pressure-tight connection (61), by the fluid which is held in the working chamber (12).
- Fuel injection device according to Claim 3, characterized in that outflow cross sections (77, 78) from the differential pressure chamber (17) to the central control line (31) can be controlled in a stroke-dependent fashion.
- Fuel injection device according to Claim 12, characterized in that the pressure change in the differential pressure chamber (17) takes place via a control chamber (20) into which the first outflow cross section (77) opens out.
- Fuel injection device according to Claim 12, characterized in that the second outflow cross section (78) exceeds the cross section of the first outflow cross section (77).
- Fuel injection device according to Claim 1, characterized in that the switching valve (5) is designed as a 3/2 directional valve.
- Fuel injection device according to Claim 1, characterized in that the switching valve (70) is designed as a servo-hydraulic 3/2 directional valve.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10247903A DE10247903A1 (en) | 2002-10-14 | 2002-10-14 | Pressure-reinforced fuel injection device for internal combustion engine has central control line acting on pressure transmission piston |
DE10247903 | 2002-10-14 | ||
PCT/DE2003/003314 WO2004036027A1 (en) | 2002-10-14 | 2003-10-07 | Pressure-boosted fuel injection device comprising an internal control line |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1554488A1 EP1554488A1 (en) | 2005-07-20 |
EP1554488B1 true EP1554488B1 (en) | 2010-07-21 |
Family
ID=32038675
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP03770904A Expired - Lifetime EP1554488B1 (en) | 2002-10-14 | 2003-10-07 | Pressure-boosted fuel injection device comprising an internal control line |
Country Status (5)
Country | Link |
---|---|
US (1) | US7513440B2 (en) |
EP (1) | EP1554488B1 (en) |
JP (1) | JP2006503209A (en) |
DE (2) | DE10247903A1 (en) |
WO (1) | WO2004036027A1 (en) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1613856B1 (en) * | 2003-04-02 | 2008-07-09 | Robert Bosch Gmbh | Fuel injector provided with a pressure transmitter controlled by a servo valve |
DE10315016A1 (en) * | 2003-04-02 | 2004-10-28 | Robert Bosch Gmbh | Fuel injector with a leak-free servo valve |
DE10315015B4 (en) * | 2003-04-02 | 2005-12-15 | Robert Bosch Gmbh | Fuel injector with pressure booster and servo valve with optimized control quantity |
DE10352736A1 (en) * | 2003-11-12 | 2005-07-07 | Robert Bosch Gmbh | Fuel injector with direct needle injection |
JP2006257874A (en) * | 2004-04-30 | 2006-09-28 | Denso Corp | Injector |
DE102004022267A1 (en) | 2004-05-06 | 2005-12-01 | Robert Bosch Gmbh | Method and device for shaping the injection pressure at a fuel injector |
DE102004022268A1 (en) * | 2004-05-06 | 2005-12-01 | Robert Bosch Gmbh | A driving method for influencing the opening speed of a control valve on a fuel injector |
JP3994990B2 (en) * | 2004-07-21 | 2007-10-24 | 株式会社豊田中央研究所 | Fuel injection device |
DE102004051757A1 (en) * | 2004-10-23 | 2006-04-27 | Robert Bosch Gmbh | Fuel injector with hydraulically operated pressure intensifier for injecting fuel in combustion chamber of internal combustion engine with minimum injector opening |
DE102004053422A1 (en) | 2004-11-05 | 2006-05-11 | Robert Bosch Gmbh | Fuel injection system |
SE529810C2 (en) * | 2006-04-10 | 2007-11-27 | Scania Cv Ab | Injection means for an internal combustion engine |
JP4548465B2 (en) * | 2007-01-23 | 2010-09-22 | 株式会社デンソー | Injector |
DE102007021326A1 (en) * | 2007-05-07 | 2008-11-13 | Robert Bosch Gmbh | Pressure boosting system for at least one fuel injector |
DE102007023384A1 (en) * | 2007-05-18 | 2008-11-20 | Robert Bosch Gmbh | Injector for a fuel injection system |
US20080296412A1 (en) * | 2007-06-01 | 2008-12-04 | Caterpillar Inc. | Fuel injector having a flow passage insert |
JP4894804B2 (en) * | 2008-03-28 | 2012-03-14 | 株式会社デンソー | Fuel injection valve |
FI122557B (en) * | 2009-04-02 | 2012-03-30 | Waertsilae Finland Oy | Fuel injection arrangement for a piston engine |
DE102010008467A1 (en) * | 2010-02-18 | 2011-08-18 | Continental Automotive GmbH, 30165 | High pressure fuel injector for an internal combustion engine |
KR101330693B1 (en) | 2011-12-26 | 2013-11-19 | 자동차부품연구원 | Injector for direct injection type diesel engine |
EP2674608B1 (en) * | 2012-06-13 | 2015-08-12 | Delphi International Operations Luxembourg S.à r.l. | Fuel injector |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3048347A1 (en) | 1980-12-20 | 1982-07-22 | Volkswagenwerk Ag, 3180 Wolfsburg | FUEL INJECTION DEVICE |
DE3102697A1 (en) | 1980-12-20 | 1982-10-21 | Volkswagenwerk Ag, 3180 Wolfsburg | Fuel injection device |
US4538576A (en) * | 1983-07-21 | 1985-09-03 | Allied Corporation | Diesel fuel injector with double dump configuration |
JPS60192872A (en) * | 1984-03-15 | 1985-10-01 | Nippon Denso Co Ltd | Accumulator type fuel injection valve |
DE19910970A1 (en) * | 1999-03-12 | 2000-09-28 | Bosch Gmbh Robert | Fuel injector |
DE19954288A1 (en) * | 1999-11-11 | 2001-05-17 | Bosch Gmbh Robert | Fuel injection valve for fitting to internal combustion engines has an injection valve element to control injection openings, a control valve to affect movement in injection valve elements and a valve element for regulating pressure |
DE10031579A1 (en) * | 2000-06-29 | 2002-01-17 | Bosch Gmbh Robert | Pressure controlled injector with vario register injector |
DE10124207A1 (en) | 2001-05-11 | 2002-11-21 | Bosch Gmbh Robert | Fuel injection device pressure amplifier has control channel in low pressure chamber connected to difference chamber, opening closed/opened depending on piston unit part movement |
DE10123914B4 (en) | 2001-05-17 | 2005-10-20 | Bosch Gmbh Robert | Fuel injection device with pressure booster device and pressure booster device |
DE10218904A1 (en) * | 2001-05-17 | 2002-12-05 | Bosch Gmbh Robert | Fuel injection system |
EP1399666B1 (en) | 2001-05-17 | 2006-08-30 | Robert Bosch Gmbh | Fuel injection device |
DE10123911A1 (en) | 2001-05-17 | 2002-11-28 | Bosch Gmbh Robert | Fuel injection device for internal combustion engine has transfer piston separating chamber connected to source from high pressure and return chambers |
-
2002
- 2002-10-14 DE DE10247903A patent/DE10247903A1/en not_active Ceased
-
2003
- 2003-10-07 WO PCT/DE2003/003314 patent/WO2004036027A1/en active Application Filing
- 2003-10-07 DE DE50312913T patent/DE50312913D1/en not_active Expired - Lifetime
- 2003-10-07 JP JP2004543953A patent/JP2006503209A/en active Pending
- 2003-10-07 US US10/531,166 patent/US7513440B2/en not_active Expired - Fee Related
- 2003-10-07 EP EP03770904A patent/EP1554488B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE10247903A1 (en) | 2004-04-22 |
US7513440B2 (en) | 2009-04-07 |
EP1554488A1 (en) | 2005-07-20 |
JP2006503209A (en) | 2006-01-26 |
US20060043209A1 (en) | 2006-03-02 |
WO2004036027A1 (en) | 2004-04-29 |
DE50312913D1 (en) | 2010-09-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1554488B1 (en) | Pressure-boosted fuel injection device comprising an internal control line | |
EP1485609B1 (en) | Device for injecting fuel to stationary internal combustion engines | |
EP1613856B1 (en) | Fuel injector provided with a pressure transmitter controlled by a servo valve | |
EP1520096B1 (en) | Common rail injection system comprising a variable injector and booster device | |
EP1584813A2 (en) | Injector for combustion engine with a direct controlled nozzle needle | |
EP1520099B1 (en) | Boosted fuel injector with rapid pressure reduction at end of injection | |
EP1269008B1 (en) | Injection valve with bypass throttle | |
DE10315015B4 (en) | Fuel injector with pressure booster and servo valve with optimized control quantity | |
WO2002084106A1 (en) | Valve for controlling liquids | |
EP1520100B1 (en) | Device for attenuating the stroke of the needle in pressure-controlled fuel injectors | |
EP1651862B1 (en) | Control valve for a fuel injector comprising a pressure exchanger | |
EP1872008B1 (en) | Fuel-injector with two-stage opening | |
EP1682769B1 (en) | Fuel injector with a multipart, directly controlled injection valve element | |
WO2005015000A1 (en) | Control valve with pressure compensation for a fuel injector comprising a pressure intensifier | |
DE10033428A1 (en) | Pressure controlled injector for injecting fuel | |
EP1709319B1 (en) | Fuel injector with direct needle control | |
EP1483499B1 (en) | Installation for the pressure-modulated formation of the injection behavior | |
DE10033426B4 (en) | Injector / nozzle needle combination with control room coupling | |
EP1908953B1 (en) | Fuel injection device | |
EP1961949B1 (en) | Injector with additional servo-valve | |
DE10325620A1 (en) | Servo-controlled fuel injector with pressure intensifier | |
DE10315489B3 (en) | Fuel injector for use in internal combustion engine has integrated damping piston and has pressure increasing system connected to fuel pressure reservoir | |
DE102018200565A1 (en) | Injector for metering gaseous fuel, Gaseinblassystem with such an injector and method for operating this injector | |
DE10066102B4 (en) | Control valve for an injection injector | |
WO2007009641A1 (en) | Fuel injector |
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: 20050517 |
|
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 |
|
RBV | Designated contracting states (corrected) |
Designated state(s): DE FR GB |
|
17Q | First examination report despatched |
Effective date: 20070201 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAC | Information related to communication of intention to grant a patent modified |
Free format text: ORIGINAL CODE: EPIDOSCIGR1 |
|
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 |
|
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: 50312913 Country of ref document: DE Date of ref document: 20100902 Kind code of ref document: P |
|
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: 20110426 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20101021 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 50312913 Country of ref document: DE Effective date: 20110426 |
|
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: 20101021 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20141021 Year of fee payment: 12 Ref country code: DE Payment date: 20141208 Year of fee payment: 12 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 50312913 Country of ref document: DE |
|
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: 20160503 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20160630 |
|
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: 20151102 |