EP1613856B1 - Fuel injector provided with a pressure transmitter controlled by a servo valve - Google Patents
Fuel injector provided with a pressure transmitter controlled by a servo valve Download PDFInfo
- Publication number
- EP1613856B1 EP1613856B1 EP04717030A EP04717030A EP1613856B1 EP 1613856 B1 EP1613856 B1 EP 1613856B1 EP 04717030 A EP04717030 A EP 04717030A EP 04717030 A EP04717030 A EP 04717030A EP 1613856 B1 EP1613856 B1 EP 1613856B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- pressure
- servo valve
- space
- piston
- chamber
- 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 - Fee Related
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- 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
- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- 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
- 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
- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- 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
- F02M63/004—Sliding valves, e.g. spool valves, i.e. whereby the closing member has a sliding movement along a seat for opening and closing
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- 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
-
- 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
- F02M2547/00—Special features for fuel-injection valves actuated by fluid pressure
- F02M2547/001—Control chambers formed by movable sleeves
Definitions
- a fuel injection device for internal combustion engines with a fuel injector with a pressure booster for increasing the injection pressure is known.
- the pressure booster has a pressure booster piston which is exposed to respective pressure surfaces of a working space, a differential pressure chamber and a compression space.
- the pressure intensifier and an injection valve member are driven by a servo valve comprising a switching element and a servo valve piston.
- the servo valve piston acts on a valve member which, with a first sealing seat, separates a first hydraulic space under system pressure from a second hydraulic chamber connected to low pressure and connected to the return system.
- the first hydraulic space is also connected via a control line to the differential space.
- an opening force is exerted on the valve member via the valve piston, which opens the first valve seat and closes the second valve seat, which is assigned to a connection to the system pressure.
- This is the result Control line, which leads into the differential pressure chamber of the pressure booster, connected via the opened first sealing seat with the low pressure side, so that the differential pressure chamber is disconnected from the system pressure.
- the system pressure acting on the working space presses the pressure booster piston into the compression space, whereby fuel is compressed there and passed through a high-pressure line into a nozzle needle pressure chamber, thereby lifting the nozzle needle from the nozzle needle seat and injecting the fuel with the injection pressure boosted by the system pressure.
- DE 101 23 914 has the subject of a fuel injection device for internal combustion engines with a fuel injector which can be supplied by a high-pressure fuel source. Between the fuel injector and the high-pressure fuel source is connected to a movable pressure booster piston having pressure booster.
- the pressure booster piston separates a connectable to the high-pressure fuel source space from a high-pressure chamber connected to the fuel injector. By filling a rear space of the pressure booster device with fuel or by emptying the rear space of fuel, the fuel pressure in the high-pressure chamber can be varied.
- the fuel injector has a movable closing piston for opening and closing injection openings.
- the closing piston protrudes into a closing pressure chamber, so that the closing piston can be acted upon by fuel pressure in order to achieve a force acting on the closing piston in the closing direction.
- the closing pressure chamber and the rear space are formed by a common closing pressure-return chamber, wherein all portions of the closing pressure-return space are permanently interconnected to exchange fuel.
- a high-pressure chamber communicates with the high-pressure fuel source in such a way that, apart from pressure oscillations, at least the fuel pressure of the high-pressure fuel source can constantly be present in the high-pressure chamber, the pressure chamber and the high-pressure chamber passing through a common injection space be formed. All sections of the injection space are permanently connected to each other for the exchange of fuel.
- DE 102 294 15.1 refers to a device for Nadelhubdämpfung pressure-controlled fuel injectors.
- a device for injecting fuel into a combustion chamber of an internal combustion engine which comprises a fuel injector which can be acted upon by a high-pressure source with high-pressure fuel.
- the fuel injector is actuated via a metering valve, wherein an injection valve member is enclosed by a pressure chamber and the injection valve member can be acted upon in the closing direction by a closing force.
- the injection valve member is associated with a independently movable damping element, which limits a damping chamber and at least one overflow channel for connecting the damping chamber having a further hydraulic space.
- the control of the fuel injector with a 3/2-way valve which may represent a cost effective and space-saving injector, but this valve has a relatively large return flow rate of the pressure booster has to control.
- a servo valve designed as a 3/2-way valve which has a hydraulically effective surface which can be acted upon in the opening direction and which is constantly subjected to system pressure.
- the system pressure corresponds to the pressure level prevailing in the high-pressure reservoir.
- the invention proposed designed as a 3/2-way valve servo valve in the idle state does not occur on a guide portion leakage currents.
- a sealing seat formed on the servo valve piston of the servo valve is formed as a flat seat
- the housing of the servo valve can advantageously be designed as a multi-part housing, whereby an axial offset of components relative to one another can be compensated.
- This compensation possibility production-related component tolerances and the good accessibility for the production of the sealing seat ensures a simple and cost manufacturability of the invention proposed servo valve.
- FIG. 1 is a first embodiment of an inventively proposed 3/2-servo valve for controlling a fuel injector containing a pressure booster refer.
- a working space 5 of a pressure booster 3 is acted upon by high-pressure fuel via a pressure source 1 and a high-pressure feed line 2 adjoining it.
- the working space 5 is permanently acted upon by the high pressure fuel of the pressure source 1.
- the pressure booster 3 comprises an integrally formed booster piston 4, which separates the working space 5 from a differential pressure chamber 6 (back space).
- the booster piston 4 is acted upon by a return spring 8, which is supported on the one hand on a recessed in an injector body 19 support disk 7 and on the other hand on a mounted on a pin of the booster piston 4 stop disc.
- the pressure booster 3 further comprises a compression chamber 9 which communicates via an overflow line 10 with a control chamber 12 for an injection valve member 14 in connection. In the overflow line 10 from the differential pressure chamber 6 (back space) to the control chamber 12 for the injection valve member 14, a first throttle body 11 is added.
- a spring element 13 is received, which acts on an end face of the needle-shaped injection valve member 14.
- the injection valve member 14 includes a pressure stage which is enclosed by a pressure chamber 16.
- the pressure chamber 16 is acted upon by a pressure chamber inlet 17, which branches off from the compression chamber 9 of the pressure booster 3, with fuel under pressure translated.
- a discharge line 21 extends into the first housing part 26 of the servo valve housing 25.
- the compression space 9 of the pressure booster 3 acting end face of the booster piston 4 is identified by reference numeral 20. Due to the pressure level at the injection valve member 14, this causes an opening movement when the pressure chamber 16 is pressurized, so that injection openings 22 flow from the pressure chamber 16 along an annular gap and into a combustion chamber 23 of a self-igniting internal combustion engine.
- the injection chamber 14 acting on the control chamber 12 is connected via a second throttle point 15 to the compression chamber 9 of the pressure booster 3 in hydraulic communication.
- a servo valve housing 25 which receives a servo valve 24.
- the servo valve housing 25 is formed in two parts and includes a first housing part 26 and a second housing part 27.
- the two-part design of the servo valve housing 25 according to the in FIG. 1 illustrated embodiment allows good accessibility for processing of the sealing seat and a slide edge, resulting in a simple and cost manufacturability of the servo valve 24 results.
- a supply line 29 branches off into the valve housing 25.
- the supply line 29 opens into a first hydraulic chamber 38 of the first housing part 26 of the servo valve housing 25.
- the first hydraulic chamber 38 encloses a servo valve piston 32, which comprises a passage 33.
- a third throttle body 34 is formed in the passage 33 of the servo valve piston 32.
- fuel flows from the first hydraulic chamber 38 into a control chamber 36 of the servo valve 24.
- a pressure relief of the control chamber 36 takes place upon actuation of a switching valve 30, at its opening control volume from the control chamber 36 via a flow restrictor 37 (fourth throttle) containing return is connected to a further low-pressure side return 31 and fuel is derivable in these.
- the control chamber 36 of the servo valve 24 is limited by an end face 35 at the top of the servo valve piston 32. This is located at the head of the servo valve piston 32 an effective in the opening direction of the servo valve piston 32 annular surface, which is acted upon by the pressure prevailing in the first hydraulic chamber 38, opposite.
- a first sealing seat 40 in a second hydraulic chamber 39 and a control edge 41 are formed on the servo valve piston 32.
- the control edge 41 which in the in FIG. 1 illustrated variant of the servo valve 24 is formed as a slide sealing edge 43, the pressurized under system pressure first hydraulic chamber 38 is sealed in a vertically moving servo valve piston 32 against the second hydraulic chamber 39.
- the two returns 28, 31 on the low pressure side are combined as possible to a return, which opens into a fuel tank.
- first embodiment of the servo valve 24 allows an extremely compact design of the servo valve 24.
- the first sealing seat 40 of the servo valve 24 is shown in the illustration FIG. 1 formed as a flat seat, but could also be used as a conical seat (see FIG. 2 ) Ball seat or as a slide edge are formed.
- Ball seat or as a slide edge are formed.
- the first sealing seat 40 can be designed either as a sealing edge or as a sealing surface.
- the sealing force can be adjusted via the pressure surface with respect to the flow control chamber 42.
- FIG. 2 shows a further embodiment of the present invention proposed servo valve, wherein the first sealing seat is designed as a conical seat.
- FIG. 2 The representation after FIG. 2 is also a fuel injector 18 can be seen, which contains a pressure booster 3.
- the working space 5 of the pressure booster 3 is supplied via a pressure source 1 (common rail) via high-pressure line 2 with high-pressure fuel.
- the booster piston 4 of the pressure booster 3 according to the illustrations in FIG. 2 formed in several parts.
- a support plate 7 is inserted, which constitutes an upper abutment surface for the upper part of the multi-part booster piston 4.
- the lower part of the booster piston 4 is acted upon by a return spring 8 which is supported on the housing side; the compression space 9 of the pressure booster 3 is limited over the end face 20 of the lower part of the booster piston 4.
- a first throttle point 11 containing overflow line 10 branches off.
- the overflow line 10 connects the differential pressure chamber 6 (back space) of the pressure booster 3 to the control chamber 12 for controlling the lifting movement of the needle-shaped injection valve member 14.
- From the compression chamber 9 of the pressure booster 3 runs the pressure chamber inlet 17, which opens into the pressure chamber 16 surrounding the injection valve member 14.
- the injection valve member 14 includes a pressure stage having a hydraulically effective area. At this attacks the im Pressure chamber 16 pending fuel pressure and opens the injection valve member 14 so that fuel is injected via released when opening the injection valve member 14 injection openings 22, which open into the combustion chamber 23 of the self-igniting internal combustion engine.
- a damping piston 51 is added to the control chamber 12 for the injection valve member 14.
- the damping piston 51 is traversed by a vertically extending channel 53.
- the channel 53 is hydraulically connected via a fifth throttle point 52 in the conversion of the damping piston 51 with the control chamber 12.
- a formed on the damping piston 51 annular surface 55 is acted upon by a housing side supporting spring element 54.
- From the control chamber 12 for the injection valve member 14 extends a filling line 56 which contains a refill valve 50, which may be formed as a check valve to the compression chamber 9 of the pressure booster 3.
- a refill valve 50 which may be formed as a check valve
- the servo valve 24 according to the in FIG. 2 illustrated embodiment is added to the valve body 25.
- the servo valve 24 includes the control chamber 36, which is relieved of pressure via the switching valve 30 in the second low-pressure side return 31. Between the control chamber 36 and the switching valve 30, an outlet throttle 37 (fourth throttle point) is added.
- an outlet throttle 37 (fourth throttle point) is added.
- the control chamber 36 in the valve body 25 of the servo valve 24 Opposite the control chamber 36 in the valve body 25 of the servo valve 24 is the first hydraulic chamber 38, which is separated by the control edge 41 from the second, here conically configured second hydraulic chamber 39.
- the second hydraulic chamber 39 is connected via the diversion line 21 to the differential pressure chamber 6 (back space) of the pressure booster 3.
- the control edge 41 is formed as a slider sealing edge 43. Unlike in FIG.
- the first sealing seat 40 of the servo valve piston 32 is formed as a conical seat.
- the drain control space 42 formed below the servovalve piston 32 in the valve body 25 is sealed so that the first low-pressure-side return 28 is closed.
- a pressurization of the control chamber 36 and the first hydraulic chamber 38 takes place in parallel via the supply line 29, which branches off from the working space 5 of the pressure booster 3. Consequently, the system pressure in the first hydraulic chamber 38, which is acted on via the second supply line section 58, is present via the supply line 29 as well as via a first supply line section 57, the third throttle point Containing 34, in the control chamber 36 of the servo valve 24 at. Due to the identity of the pressures in the first hydraulic chamber 38 and in the control chamber 36, a pilot leakage along the head of the servo valve piston 32 is excluded. The servo valve piston 32 is guided in the valve body 25 high pressure-tight.
- the basic mode of operation of the inventively proposed fuel injector which is controlled via the servo valve 24, is based on the illustration in accordance with FIG. 1 described.
- the working space 5 of the pressure booster 3 is constantly connected to the pressure source 1 and is constantly under the prevailing pressure level there.
- the compression chamber 9 of the push-type translator 3 is constantly connected via the pressure chamber inlet 17 to the pressure chamber 16 which surrounds the injection valve member 14.
- the pressure booster 3 further includes the differential pressure space 6 (back space) for controlling the pressure booster 3 either at system pressure, i. pressurized in the pressure source 1 prevailing pressure level or separated from this pressure in the low-pressure side return 28 is relieved of pressure.
- the supply line 29 is connected to the pressure accumulator 1, so that the pressures in the working chamber 5 and the differential pressure chamber 6 (back space) of the pressure booster correspond to each other and the booster piston 4 is balanced and no pressure boost takes place.
- a pressure relief of the differential pressure chamber 6 (back space).
- the switching valve 30 is activated, ie opened and the control chamber 36 of the servo valve 24 in the low-pressure side return 31 via the outlet throttle 37 relieved of pressure. Due to the falling pressure in the control chamber 36, the servo valve piston 32 moves upward in the vertical direction, moved by the pressing force acting on the opening surface 44 in the first hydraulic space 38. As a result, the first sealing seat 40 is opened while the control edge 41 is closed, since the slide edge 43 covers the opposite housing edge of the valve body 25.
- the throttle body 34 in the passage 33 of the servo valve piston 32 and the outlet throttle 37 is the movement speed of the servo valve piston 32 at its opening movement freely adjustable. Due to the defined opening surface 44 on the underside of the head of the servo valve 24, the servo valve piston 32 is constantly in compression in the opening direction. This allows a precise movement of the servo valve piston 32 and thus a stable persistence of the same at the opening stop in the open state of the servo valve piston 32 bring about.
- servo valve piston 32 When located in its open position servo valve piston 32 is a decoupling of the differential pressure chamber 6 (back space) of the pressure booster 3 from the system pressure, i. of the prevailing pressure in the accumulator 1 pressure levels.
- a control quantity flows out of the differential pressure chamber 6 (back space) via the outlet line 21 into the second hydraulic chamber 39, via the opened first sealing seat 40 into the process control chamber 42. From this flows the fluid which has been diverted from the differential pressure chamber 6 (backspace) Fuel quantity in the low-pressure side return 28 from.
- the first sealing seat 40 can be used both as a flat seat, which allows a high surface pressure, and as a conical seat (comparisons according to FIG FIG. 2 ) are formed as a ball seat or as a slide edge.
- a flat seat which allows a high surface pressure
- a conical seat comparisons according to FIG FIG. 2
- the in FIG. 1 illustrated flat seat as the first sealing seat 40 can compensate for any production-related axial offset.
- the generation of a sufficient closing force so that at the first sealing seat 40 in its closed position, a high surface pressure arises and thus a good sealing effect is ensured.
- FIG. 2 illustrated embodiment using a damping piston 51 which acts on the injection valve member 14, a reduction in the opening speed of the needle-shaped injection valve member 14 can be achieved.
- the damping behavior of the damping piston 51 can be adjusted by the dimensioning of this acting spring element 54 and by the dimensioning of the formed in the wall of the damping piston 51 throttle element 52.
- the refilling of the compression chamber 9 of the pressure booster 3 does not take place via the second throttle point 15 as in the embodiment according to FIG. 1 but via a branching from the control chamber 12 of the injection valve member 14 filling line 56 in which a designed as a check valve refill valve 50 is added.
- the inventively proposed 3/2-servo valve 24 can be used to control all pressure booster 3, which are controlled via a pressure change of their differential pressure chamber 6 (backspace).
- FIG. 3 is a variant of a 3/2-Servovalve with a servo valve piston refer to which a control sleeve is added.
- FIG. 3 illustrated embodiment of a fuel injector 18 with pressure booster 3 is acted upon by a high pressure source 1 via the high pressure supply line 2 with high pressure fuel.
- the working space 5 of the pressure booster 3 is filled with system pressure, in which a return spring 8 is added, which is supported on the one hand on a support plate 7 and on the other hand via a stop surface biases the booster piston 4, which separates the working chamber 5 from the differential pressure chamber 6.
- the end face 20 of the booster piston 4 limits the compression chamber 9, which is acted upon by the activation of the pressure booster 3 via the pressure chamber inlet 17 of the pressure chamber 16 with high pressure fuel.
- the fuel injector 18 includes the control chamber 12, which is bounded by a control chamber sleeve 62.
- the control chamber sleeve 62 is biased by the spring 13, wherein the spring 13 is supported on a collar of the injection valve member 14.
- feed surfaces 64 formed as polished portions are formed below the collar. Via these inflow surfaces 64, the fuel flows from the pressure chamber to injection openings 22, which open into the combustion chamber 23 of the self-igniting internal combustion engine.
- the control chamber 12 of the fuel injector 18 is acted upon on the one hand via a first throttle point 11, which branches off from the pressure chamber inlet 17 with fuel; the pressure relief of the control chamber 12 via the second throttle body 15 upon actuation of a switching valve 60. If the switching valve 60 is actuated, a Abberichtmenge via the second throttle point 15 is derived in an injector 61 return.
- the pressure booster 3 is actuated via the servo valve 24.
- the servo valve 24 includes the valve piston 32 having a servo valve piston portion 65.
- the servo valve piston 32, 65 is controlled via the pressurization or pressure relief of the control chamber 36.
- the control chamber 36 of the servo valve 24 is acted upon by the high-pressure fuel via the first supply line section 57, in which the throttle restriction 34 is accommodated.
- a pressure relief of the control chamber 36 of the servo valve 24 via an actuation of the switching valve 30.
- the servo valve 24 comprises a housing 25, which comprises a plurality of housing parts 26, 27.
- the servo valve piston 32, 65 is enclosed by the first hydraulic chamber 38 and the second hydraulic chamber 39.
- the first hydraulic chamber 38 is acted upon by the supply line 29, which branches off from the high-pressure line 2, with high-pressure fuel.
- In the second hydraulic chamber 39 opens the Abtechnisch 21, via which a pressure relief of the differential pressure chamber 6 (back space) of the pressure booster 3 takes place.
- the servo valve piston 32 also includes the hydraulic surface 44, on which a force acting on the servo valve piston 32 in the open position pressure force upon pressure relief of the control chamber 36 of the servo valve 24 attacks.
- first recesses 63 are formed, which have slide sealing edges 43.
- the slider sealing edges 43 of the first recesses 63 cooperate with a control edge 41 formed on the second housing part 27.
- a control sleeve 67 is received, which is biased by a control sleeve spring 68, which in turn is supported on the first housing part 26 of the servo valve housing 25.
- the control sleeve 67 has a sleeve recess 71.
- the first sealing seat 40 according to the in FIG. 3 illustrated embodiment is designed as a flat seat and seals the Abêtraum 42 (low pressure space) against the low-pressure side return 28 from.
- the functioning of in FIG. 3 illustrated embodiment of the controlled via the servo valve 24 Kraftsoffinjektors 18 with pressure booster 3 is as follows:
- the first sealing seat 40 can be designed in many ways. In addition to the in FIG. 3 illustrated embodiment of the first sealing seat 40 as a flat seat, this can according to the embodiments, in FIG. 2 is shown, also formed as a conical seat or ball seat. Particularly advantageous is the in FIG. 3 represented by a multipart valve body, such as housing parts 26, 27 and 66, a simple manufacture of the valve seat of the first sealing seat 40 can be achieved. By the in FIG. 3 flat seat shown is compensated for any axial misalignment of the valve body to each other. In the FIG. 3 illustrated embodiment also has a large closing pressure force exerted by the pending in the control chamber 36 fuel pressure on the first sealing seat 40, which adjusts to this a high surface pressure and thus an excellent sealing effect.
- the first sealing seat 40 When opening, first the first sealing seat 40 is opened and the slider sealing edge 43 is brought into register with the control edge 41.
- the control sleeve 67 is now employed by the hydraulic pressure force in the second hydraulic chamber 39 to the third housing part 66, whereby a high-pressure-tight connection is achieved. Only then is an opening of the slide seal 69, when the servo valve piston section 65, the sleeve recess 71 releases. As a result, no short-circuit leakage current flows from the first hydraulic chamber 38 into the return line.
- the differential pressure chamber 6 (back space) of the pressure booster 3 is now connected via the second hydraulic chamber 39, the slide seal 69, the first sealing seat 40 and the Abêtraum 42 (low pressure space) with the low-pressure side return 28 and the pressure booster 3 thus activated.
- the servo valve piston 32, 65 moves through the force acting in the closing direction hydraulic pressure force in the control chamber 36 in its starting position.
- the hydraulic closing force ensures a precisely defined closing movement over the entire area of the servo valve piston 32, 65.
- a spring force can be provided to assist the closing movement.
- the representation according to FIG. 4 is a variant with stretched trained Servoventilkolben a servo valve to remove.
- the servo valve piston 32 has a stretched servo valve piston section 65.
- 65 second recesses 70 are formed on the the Ab Kunststoffraum 42 (low pressure space) facing the end of the Servoventilkolbenabterrorismes 65.
- the slide seal 69 is integrated directly into the first housing part 26 of the servo valve housing 25.
- the servo valve piston section 65 in FIG. 3 illustrated control sleeve 67 omitted.
- FIG. 4 illustrated embodiment is identical to that in connection with FIG. 3 illustrated operation of this embodiment of the fuel injector 18th
- FIG. 4 is formed at the Abêtraum 42 (low pressure space) facing end face of the Servoventilkolbenabiteses 65 a flat seat.
- the servo valve 24 may also be formed as a pure slide-valve slide. In this case, care must be taken for a sufficient overlap length at the slide seal 69 in order to keep the leakage flow in the idle state of the fuel injector 18 small.
- the servo valve 24 may also be formed as a 4/2-way valve, in which the function of the check valve is integrated into the slide valve.
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Abstract
Description
Zum Einbringen von Kraftstoff in direkteinspritzende Verbrennungskraftmaschinen werden hubgesteuerte Einspritzsysteme mit Hochdruckspeicherraum (Common Rail) eingesetzt. Der Vorteil dieser Einspritzsysteme liegt darin, dass der Einspritzdruck an Last und Drehzahl in weiten Bereichen angepasst werden kann. Zur Reduzierung der Emissionen und zum Erzielen einer hohen spezifischen Leistung ist ein hoher Einspritzdruck erforderlich. Das erreichbare Druckniveau von Hochdruckkraftstoffpumpen ist aus Festigkeitsgründen begrenzt, so dass zur weiteren Drucksteigerung bei Kraftstoffeinspritzsystemen Druckverstärker in den Kraftstoffinjektoren zum Einsatz kommen.For introducing fuel into direct-injection internal combustion engines, stroke-controlled injection systems with high-pressure storage space (common rail) are used. The advantage of these injection systems is that the injection pressure can be adapted to load and speed in a wide range. To reduce emissions and achieve high specific power, high injection pressure is required. The achievable pressure level of high-pressure fuel pumps is limited for reasons of strength, so that pressure amplifiers in the fuel injectors are used to further increase the pressure in fuel injection systems.
Aus
An Stelle der aus
Um eine definierte Bewegung eines Servoventilskolbens eines Servoventiles zur Betätigung eines Kraftstoffinjektors zu erreichen, wird ein als 3/2-Wegeventil ausgebildetes Servoventil vorgeschlagen, welches eine in Öffnungsrichtung beaufschlagbare hydraulisch wirksame Fläche aufweist, die ständig mit Systemdruck beaufschlagt ist. Der Systemdruck entspricht dem im Hochdruckspeicherraum herrschenden Druckniveau. Durch diese Maßnahme lässt sich die Bewegung des Servoventilkolbens problemlos durch die Abstimmung von Zu- bzw. Ablaufdrossel am Servoventil einstellen. Durch eine langsam ablaufende Öffnungsbewegung des Servoventilkolbens kann eine gute Darstellbarkeit von kleinen Voreinspritzmengen und ein schwingungsfreier Druckaufbau gewährleistet werden. Aufgrund der definierten Öffnungskraft wird das erfindungsgemäß vorgeschlagene Servoventil toleranzunemfindlich gegenüber Reibungseinflüssen, so dass eine fertigungsbedingte Toleranzstreuung und damit einhergehende starke Streuungen von Einspritzmengen vermieden werden können.In order to achieve a defined movement of a servo valve piston of a servo valve for actuating a fuel injector, a servo valve designed as a 3/2-way valve is proposed which has a hydraulically effective surface which can be acted upon in the opening direction and which is constantly subjected to system pressure. The system pressure corresponds to the pressure level prevailing in the high-pressure reservoir. By this measure, the movement of the servo valve piston can be easily by the vote of inlet and outlet throttle on servo valve. By a slowly proceeding opening movement of the servo valve piston, a good representability of small pilot injection quantities and a vibration-free pressure build-up can be ensured. Due to the defined opening force, the servo valve proposed according to the invention becomes insensitive to tolerance to frictional influences, so that manufacturing-related tolerance scattering and the associated large scatter of injection quantities can be avoided.
Ferner weist das erfindungsgemäß vorgeschlagene, als 3/2-Wegeventil ausgebildete Servoventil im Ruhezustand keine an einem Führungsabschnitt auftretenden Leckageströme auf. Dies bedeutet eine erhebliche Verbesserung des Injektorwirkungsgrades; aufgrund der dadurch am Servoventilkolben möglichen kleinen Führungslängen lässt sich eine geringe Baulänge des Servoventiles ermöglichen, was die Gesamtbauhöhe eines Kraftstoffinjektors mit Druckübersetzer in einem Injektorkörper, das Servoventil umfassend, günstig beeinflusst, d.h. der Platzbedarf eines solcherart ausgebildeten Kraftstoffinjektors wird erheblich reduziert.Furthermore, the invention proposed, designed as a 3/2-way valve servo valve in the idle state does not occur on a guide portion leakage currents. This means a significant improvement in injector efficiency; due to the small guide lengths possible thereby on the servo valve piston, a small structural length of the servo valve can be made possible, which favorably influences the overall height of a fuel injector with pressure booster in an injector body comprising the servo valve, i. The space requirement of such a trained fuel injector is considerably reduced.
Wird ein am Servoventilkolben des Servoventiles ausgebildeter Dichtsitz als Flachsitz ausgebildet, kann in vorteilhafter Weise das Gehäuse des Servoventiles als ein mehrteiliges Gehäuse ausgebildet werden, womit ein Achsversatz von Bauteilen zueinander ausgeglichen werden kann. Diese Ausgleichsmöglichkeit fertigungsbedingter Bauteiltoleranzen und die gute Zugänglichkeit zur Fertigung des Dichtsitzes stellt eine einfache und kostengünstige Herstellbarkeit des erfindungsgemäß vorgeschlagenen Servoventiles sicher.If a sealing seat formed on the servo valve piston of the servo valve is formed as a flat seat, the housing of the servo valve can advantageously be designed as a multi-part housing, whereby an axial offset of components relative to one another can be compensated. This compensation possibility production-related component tolerances and the good accessibility for the production of the sealing seat ensures a simple and cost manufacturability of the invention proposed servo valve.
Anhand der Zeichnung wird die Erfindung nachstehend eingehender beschrieben:
- Es zeigt:
Figur 1- eine erste Ausführungsvariante eines als 3/2-Wege-Ventil ausgebildeten Servoventiles mit führungsleckagefreiem Servoventilkolben,
Figur 2- eine weitere Ausführungsvariante eines Servoventilkolbens eines 3/2-Servoventiles mit einem als Kegel-Dichtsitz ausgebildeten ersten Sitz und einem als Schieberdichtung ausgebildeten weiteren Sitz,
Figur 3- eine Ausführungsvariante eines 3/2-Servoventiles mit einem Servoventilkolben, an dem eine Steuerhülse aufgenommen ist und
Figur 4- eine Ausführungsvariante eines 3/2-Servoventiles mit gestrecktem Servoventilkolben.
- It shows:
- FIG. 1
- a first embodiment of a trained as a 3/2-way valve servo valve with guide leak-free servo valve piston,
- FIG. 2
- 2 shows a further embodiment variant of a servo valve piston of a 3/2 servo valve with a first seat designed as a conical sealing seat and a further seat constructed as a slide seal,
- FIG. 3
- a variant of a 3/2-servo valve with a servo valve piston to which a control sleeve is received and
- FIG. 4
- a variant of a 3/2-Servoventiles with stretched servo valve piston.
Über eine Druckquelle 1 und eine sich an diesen anschließenden Hochdruckzuleitung 2 wird ein Arbeitsraum 5 eines Druckübersetzers 3 mit unter hohem Druck stehenden Kraftstoff beaufschlagt. Der Arbeitsraum 5 ist permanent mit dem unter hohem Druck stehenden Kraftstoff der Druckquelle 1 beaufschlagt. Der Druckübersetzer 3 umfasst einen einteilig ausgebildeten Übersetzerkolben 4, welcher den Arbeitsraum 5 von einem Differenzdruckraum 6 (Rückraum) trennt. Der Übersetzerkolben 4 ist durch eine Rückstellfeder 8 beaufschlagt, die sich einerseits an einer in einem Injektorkörper 19 eingelassenen Stützscheibe 7 und andererseits an einer an einem Zapfen des Übersetzerkolbens 4 angebrachten Anschlagscheibe abstützt. Der Druckübersetzer 3 umfasst darüber hinaus einen Kompressionsraum 9 der über eine Überströmleitung 10 mit einem Steuerraum 12 für ein Einspritzventilglied 14 in Verbindung steht. In der Überströmleitung 10 vom Differenzdruckraum 6 (Rückraum) zum Steuerraum 12 für das Einspritzventilglied 14 ist eine erste Drosselstelle 11 aufgenommen.A working
Im Steuerraum 12 für das Einspritzventilglied 14 ist ein Federelement 13 aufgenommen, welches eine Stirnseite des nadelförmig ausgebildeten Einspritzventilgliedes 14 beaufschlagt. Das Einspritzventilglied 14 umfasst eine Druckstufe, die von einem Druckraum 16 umschlossen ist. Der Druckraum 16 wird über einen Druckraumzulauf 17, welcher vom Kompressionsraum 9 des Druckübersetzers 3 abzweigt, mit unter übersetztem Druck stehenden Kraftstoff beaufschlagt. Vom Differenzdruckraum 6 des Druckübersetzers 3 verläuft eine Absteuerleitung 21 in das erste Gehäuseteil 26 des Servoventilgehäuses 25. Die den Kompressionsraum 9 des Druckübersetzers 3 beaufschlagende Stirnfläche des Übersetzerkolben 4 ist durch Bezugszeichen 20 identifiziert. Aufgrund der Druckstufe am Einspritzventilglied 14 führt dieses bei Druckbeaufschlagung des Druckraums 16 eine Öffnungsbewegung aus, so dass vom Druckraum 16 Kraftstoff entlang eines Ringspaltes Einspritzöffnungen 22 zuströmt und in einen Brennraum 23 einer selbstzündenden Verbrennungskraftmaschine gelangt.In the
Der das Einspritzventilglied 14 beaufschlagende Steuerraum 12 steht über eine zweite Drosselstelle 15 mit dem Kompressionsraum 9 des Druckübersetzers 3 in hydraulischer Verbindung.The
Oberhalb des Injektorkörpers 19 eines Kraftstoffinjektors 18 ist ein Servoventilgehäuse 25 angeordnet, welches ein Servoventil 24 aufnimmt. In der
Von der Hochdruckzuleitung 2, über welche der Arbeitsraum 5 des Druckübersetzers 3 mit unter hohem Druck stehenden Kraftstoff beaufschlagt wird, zweigt eine Versorgungsleitung 29 in das Ventilgehäuse 25 ab. Die Versorgungsleitung 29 mündet in einem ersten hydraulischen Raum 38 des ersten Gehäuseteiles 26 des Servoventilgehäuses 25. Der erste hydraulische Raum 38 umschließt einen Servoventilkolben 32, welcher einen Durchgangskanal 33 umfasst. Im Durchgangskanal 33 des Servoventilkolbens 32 ist eine dritte Drosselstelle 34 ausgebildet. Über den Durchgangskanal 33 strömt Kraftstoff vom ersten hydraulischen Raum 38 in einen Steuerraum 36 des Servoventiles 24. Eine Druckentlastung des Steuerraumes 36 erfolgt bei Betätigung eines Schaltventiles 30, bei dessen Öffnen Steuervolumen aus dem Steuerraum 36 über eine eine Ablaufdrosselstelle 37 (vierte Drosselstelle) enthaltenden Rücklauf mit einem weiteren niederdruckseitigen Rücklauf 31 verbunden wird und Kraftstoff in diesen ableitbar ist. Der Steuerraum 36 des Servoventiles 24 ist durch eine Stirnfläche 35 an der Oberseite des Servoventilkolbens 32 begrenzt. Dieser liegt am Kopf des Servoventilkolbens 32 einer in Öffnungsrichtung des Servoventilkolben 32 wirksamen Ringfläche, die vom im ersten hydraulischen Raum 38 herrschenden Druck beaufschlagt ist, gegenüber. Am Servoventilkolben 32 sind darüber hinaus ein erster Dichtsitz 40 in einem zweiten hydraulischen Raum 39 sowie eine Steuerkante 41 ausgebildet. Über den ersten Dichtsitz 40 wird die Verbindung zu einem Ablaufsteuerraum 42, von dem ein niederdruckseitiger Rücklauf 28 abzweigt, freigegeben bzw. verschlossen. Mittels der Steuerkante 41, der in der in
Zur Unterstützung der Bewegung des Servoventilkolben 32 im ersten Gehäuseteil 26 können - obwohl in
Der Darstellung nach
Im Unterschied zu in
Das Servoventil 24 gemäß der in
In Abwandlung des Servoventilkolbens 32 gemäß der Darstellung in
Die prinzipielle Arbeitsweise des erfindungsgemäß vorgeschlagenen Kraftstoffinjektors, der über das Servoventil 24 angesteuert wird, wird anhand der Darstellung gemäß
Der Arbeitsraum 5 des Druckübersetzers 3 ist ständig mit der Druckquelle 1 verbunden und steht ständig unter dem dort herrschenden Druckniveau. Der Kompressionsraum 9 des Drückübersetzers 3 ist über den Druckraumzulauf 17 ständig mit dem Druckraum 16, der das Einspritzventilglied 14 umgibt, verbunden. Der Druckübersetzer 3 umfasst darüber hinaus den Differenzdruckraum 6 (Rückraum) der zur Steuerung des Druckübersetzers 3 entweder mit Systemdruck, d.h. dem in der Druckquelle 1 herrschenden Druckniveau beaufschlagt oder von diesem abgetrennt in den niederdruckseitigen Rücklauf 28 druckentlastet wird. Im deaktivierten Zustand ist der Differenzdruckraum 6 (Rückraum) des Druckübersetzers 3 über die Absteuerleitung 21, die geöffneten Steuerkante 41, die Versorgungsleitung 29 mit dem Druckspeicher 1 verbunden, so dass die Drücke im Arbeitsraum 5 und im Differenzdruckraum 6 (Rückraum) des Druckübersetzers einander entsprechen und der Übersetzerkolben 4 ausgeglichen ist und keine Druckverstärkung stattfindet.The working
Zur Aktivierung des Druckübersetzers 3 erfolgt eine Druckentlastung des Differenzdruckraumes 6 (Rückraum). Um diese Druckentlastung herbeizuführen, wird das Schaltventil 30 aktiviert, d.h. geöffnet und der Steuerraum 36 des Servoventiles 24 in den niederdruckseitigen Rücklauf 31 über die Ablaufdrosselstelle 37 druckentlastet. Aufgrund des fallenden Druckes im Steuerraum 36 bewegt sich der Servoventilkolben 32 in vertikaler Richtung nach oben, bewegt durch die an der öffnenden Fläche 44 im ersten hydraulischen Raum 38 angreifende Druckkraft. Dadurch wird der erste Dichtsitz 40 geöffnet, während die Steuerkante 41 geschlossen wird, da die Schieberkante 43 die dieser gegenüberliegenden Gehäusekante des Ventilkörpers 25 überdeckt. Durch die Auslegung der Drosselstelle 34 im Durchgangskanal 33 des Servoventilkolbens 32 und die Ablaufdrossel 37 ist die Bewegungsgeschwindigkeit des Servoventilkolbens 32 bei seiner Öffnungsbewegung beliebig einstellbar. Aufgrund der definierten öffnenden Fläche 44 an der Unterseite des Kopfes des Servoventiles 24, steht am Servoventilkolben 32 ständig eine diesen in Öffnungsrichtung beaufschlagende Druckkraft an. Dadurch lässt sich eine exakte Bewegung des Servoventilkolbens 32 und damit ein stabiles Verharren desselben am Öffnungsanschlag im geöffneten Zustand des Servoventilkolbens 32 herbeiführen.To activate the
Bei in seiner Öffnungsstellung befindlichen Servoventilkolbens 32 erfolgt eine Abkopplung des Differenzdruckraumes 6 (Rückraum) des Druckübersetzers 3 vom Systemdruck, d.h. des im Druckspeicher 1 herrschenden Druckniveaus. Bei geschlossener Steuerkante 41 erfolgt ein Abströmen einer Steuermenge aus dem Differenzdruckraum 6 (Rückraum) über die Absteuerleitung 21 in den zweiten hydraulischen Raum 39, über den geöffneten ersten Dichtsitz 40 in den Ablaufsteuerraum 42. Von diesem strömt die aus dem Differenzdruckraum 6 (Rückraum) abgesteuerte Kraftstoffmenge in den niederdruckseitigen Rücklauf 28 ab.When located in its open position
Aufgrund der Einfahrbewegung der Stirnfläche 20 des Übersetzerkolbens 4 in den Kompressionsraum 9, erfolgt in diesem eine Druckerhöhung, so dass über den Druckraumzulauf 17 entsprechend des Übersetzungsverhältnisses des Druckübersetzers 3 unter erhöhtem Druck stehender Kraftstoff dem Druckraum 16, der das Einspritzventilglied 14 umgibt, zuströmt. Aufgrund der am Einspritzventilglied 14 im Bereich des Druckraumes 16 ausgebildeten Druckstufe öffnet dieses entgegen der Wirkung der Feder 13, so dass die Einspritzdüsen 22 am brennraumseitigen Ende des Kraftstoffinjektors 18 geöffnet werden und Kraftstoff in den Brennraum 23 der Verbrennungskraftmaschine eingespritzt werden kann. Bei vollständig geöffnetem Einspritzventilglied 14 wird die zweite Drosselstelle 15 zwischen dem Steuerraum 12 und dem Kompressionraum 9 des Druckübersetzers 3 verschlossen, so dass sich während des Einspritzvorganges kein Verluststrom einstellt.Due to the retraction movement of the
Zum Beenden des Einspritzvorganges erfolgt eine erneute Betätigung des Schaltventiles 30, dieses wird in seine Schließstellung gefahren, so dass sich im Steuerraum 36 über den Durchgangskanal 33, den ersten hydraulischen Raum 38 und die in diesen mündende Versorgungsleitung 29 der im Druckspeicher 1 herrschende Systemdruck aufbaut. Durch die sich im Steuerraum 36 aufbauende Druckkraft bewegt sich der Servoventilkolben 32 nach unten in seine Ausgangsstellung, wobei der erste Dichtsitz 40 zum niederdrucksseitigen Rücklauf 28 verschlossen und die Steuerkante 41 geöffnet wird. Da die Stirnfläche 35, auf welche der im Steuerraum 36 herrschende Druck einwirkt, größer bemessen ist als die öffnende Druckfläche 44 im ersten hydraulischen Raum 38, wird eine definierte und schnell ablaufende Schließbewegung des Servoventilkolbens 32 in seine Schließstellung erreicht.To terminate the injection process, a renewed actuation of the switching
Zu Unterstützung der Hubbewegung des Servoventilkolbens 32 könnten auch zusätzliche Federn im 1. Gehäuseteil 26 angeordnet werden.To support the lifting movement of the
Im Differenzdruckraum 6 (Rückraum) des Druckverstärkers und im Steuerraum 12, über welchen das Einspritzventilglied 14 gesteuert wird, erfolgt jetzt ein Druckaufbau auf das im Druckspeicher 1 herrschende Druckniveau über die Versorgungsleitung 29, die von der Hochdruckzuleitung 2 des Hochdruckspeicher 1 abzweigt, die geöffneten Steuerkante 41, den zweiten hydraulischen Raum 39 und die Absteuerleitung 21, die in den Differenzdruckraum 6 (Rückraum) mündet. Von dort erfolgt ein Druckaufbau über die Überströmleitung 10, die die erste Drosselstelle 11 enthält in den Steuerraum 12.In the differential pressure chamber 6 (back space) of the booster and in the
Gleichzeitig erfolgt bei Druckaufbau im Differenzdruckraum 6 (Rückraum) des Druckübersetzers eine Wiederbefüllung des Kompressionsraumes 9 über die vom Steuerraum 12 zur Betätigung des Einspritzventilgliedes 14 abzweigende Leitung, in welcher die zweite Drosselstelle 15 ausgebildet ist.At the same time takes place at pressure build-up in the differential pressure chamber 6 (back space) of the pressure booster refilling the
Der erste Dichtsitz 40 kann sowohl als Flachsitz, welcher eine hohe Flächenpressung ermöglicht, als auch als Kegelsitz (Vergleiche darstellen gemäß
Mit der in
Das erfindungsgemäß vorgeschlagene 3/2-Servoventil 24 kann zur Steuerung sämtlicher Druckübersetzer 3 eingesetzt werden, die über eine Druckänderung ihres Differenzdruckraumes 6 (Rückraums) angesteuert werden.The inventively proposed 3/2-
Die in
Die in
Der Druckübersetzer 3 gemäß der in
Das Servoventil 24 umfasst ein Gehäuse 25, welches mehrere Gehäuseteile 26, 27 umfasst.The
Der Servoventilkolben 32, 65 ist von dem ersten hydraulischen Raum 38 sowie dem zweiten hydraulischen Raum 39 umschlossen. Der erste hydraulische Raum 38 wird über die Versorgungsleitung 29, die von der Hochdruckleitung 2 abzweigt, mit unter hohem Druck stehenden Kraftstoff beaufschlagt. In den zweiten hydraulischen Raum 39 mündet die Absteuerleitung 21, über welche eine Druckentlastung des Differenzdruckraumes 6 (Rückraum) des Druckübersetzers 3 erfolgt.The
Der Servoventilkolben 32 umfasst darüber hinaus die hydraulische Fläche 44, an welcher eine den Servoventilkolben 32 in Öffnungsstellung bewegende Druckkraft bei Druckentlastung des Steuerraumes 36 des Servoventiles 24 angreift. Im Servoventilkolbenabschnitt 65 sind erste Aussparungen 63 ausgebildet, welche Schieberdichtkanten 43 aufweisen. Die Schieberdichtkanten 43 der ersten Aussparungen 63 wirken mit einer am zweiten Gehäuseteil 27 ausgebildeten Steuerkante 41 zusammen. Am Servoventilkolbenabschnitt 65 ist eine Steuerhülse 67 aufgenommen, die durch eine Steuerhülsenfeder 68 vorgespannt ist, die sich ihrerseits am ersten Gehäuseteil 26 des Servoventilgehäuses 25 abstützt. Die Steuerhülse 67 weist einen Hülsenaussparung 71 auf. Der erste Dichtsitz 40 gemäß der in
Im Ausgangszustand herrscht im Steuerraum 36 des Servoventiles 24 Systemdruck, der bei geschlossenem Schaltventil 30 im Steuerraum 36 über die dritte Drosselstelle 34 ansteht. Durch die Druckkraft innerhalb des Steuerraumes 36 des Servoventilkolbens, die auf die Stirnfläche 35 des Servoventilkolbens 32 wirkt und welche größer ist als die öffnende Druckkraft, die über die hydraulische in Öffnungsrichtung wirksame Fläche 44 am Servoventilkolben 32 ansteht, wird der Servoventilkolben 32 in seine untere Position gefahren. In dieser Position stehen die Steuerkante 41 und die Schieberdichtkante 43 am Servoventilkolbenabschnitt 65 offen, wohingegen die Schieberdichtung 69 am Servoventilkolbenabschnitt 65 geschlossen ist. Ferner ist befindet sich der erste Dichtsitz 40 gegen den Absteuerraum 42 (Niederdruckraum) in seiner geschlossenen Position. Da der zweite hydraulische Raum 39 durch den ersten Dichtsitz 40 gegenüber dem Absteuerraum 42 (Niederdruckraum) abgedichtet ist, entsteht bei geschlossenem Servoventilkolben 32, 65 kein Leckagestrom in den niederdruckseitigen Rücklauf 28, wodurch geringere Anforderungen an die Führungsleckage (Führungslänge und Spiel) der am Servoventilkolbenabschnitt 65 aufgenommenen Steuerhülse 67 gestellt werden können.In the initial state prevails in the
Der erste Dichtsitz 40 kann in vielfältiger Weise gestaltet werden. Neben der in
Im Ruhezustand des Servoventiles 24 ist der Differenzdruckraum (Rückraum) 6 des Druckübersetzers 3 über die ersten Aussparungen 63 am Servoventilkolben 65, sowie den ersten hydraulischen Raum 38 mit Systemdruck beaufschlagt und der Druckübersetzer 3 bleibt aufgrund der hydraulischen Verbindung zwischen dem zweiten hydraulischen Raum 39 die Absteuerleitung 21 mit dem Differenzdruckraum verbunden. Aufgrund des gleichen Druckniveaus im Differenzdruckraum 6 und dem Arbeitsraum 5 ist der Druckübersetzer 3 deaktiviert. Bei Ansteuerung des Schaltventiles 30 erfolgt eine Druckentlastung des Steuerraumes 36 des Servoventils 24, wodurch der Servoventilkolben 32, 65 öffnet. Aufgrund der über den ersten hydraulischen Raum 38 an der hydraulischen Fläche 44 angreifenden Öffnungskraft erfolgt ein exaktes Öffnen des Servoventilkolbens 32. Beim Öffnen wird zuerst der erste Dichtsitz 40 geöffnet und die Schieberdichkante 43 in Überdeckung mit der Steuerkante 41 gebracht. Die Steuerhülse 67 wird nun durch die hydraulische Druckkraft im zweiten hydraulischen Raum 39 an das dritte Gehäuseteil 66 angestellt, wodurch eine hochdruckdichte Verbindung erreicht wird. Erst danach erfolgt ein Öffnen der Schieberdichtung 69, wenn der Servoventilkolbenabschnitt 65 die Hülsenaussparung 71 freigibt. Dadurch entsteht kein Kurzschlussleckagestrom aus dem ersten hydraulischen Raum 38 in den Rücklauf. Der Differenzdruckraum 6 (Rückraum) des Druckverstärkers 3 ist nunmehr über den zweiten hydraulischen Raum 39, die Schieberdichtung 69, den ersten Dichtsitz 40 und den Absteuerraum 42 (Niederdruckraum) mit dem niederdruckseitigen Rücklauf 28 verbunden und der Druckübersetzer 3 somit aktiviert.In the idle state of the
Wird hingegen das Schaltventil 30 wieder geschlossen, so bewegt sich der Servoventilkolben 32, 65 durch die in Schließrichtung wirkende hydraulische Druckkraft im Steuerraum 36 in seine Ausgangsstellung. Durch die hydraulische Schließkraft wird eine exakt definierte Schließbewegung über den gesamten Bereich des Servoventilkolbens 32, 65 gewährleistet. Zusätzlich kann zur Unterstützung der Schließbewegung eine Federkraft vorgesehen werden. Beim Schließen des Servoventilkolbens 32, 65 erfolgt zunächst ein Schließen der Schieberdichtung 69. Dadurch wird der Differenzdruckraum 6 (Rückraum) des Druckübersetzers 3 vom niederdruckseitigen Rücklauf 28 abgekoppelt. Erst nach einem weiteren Schließhub und damit nach einer Verzugszeit ti, erfolgt ein Öffnen der Steuerkanten 41, 43, so dass der Druckübersetzer 3 vollständig deaktiviert ist. Anschließend wird der erste Dichtsitz 40 geschlossen.If, however, the switching
Durch die Verzugszeit t1 zwischen dem Schließen der Schieberdichtung 69 und dem Öffnen der Steuerkanten 41 bzw. der Schieberdichtkante 43 bleibt nach der Haupteinspritzung noch für kurze Zeit ein Druckpolster am Einspritzventilglied 14 erhalten, welches für eine Nacheinspritzung unter hohem Druck benutzt werden kann. Gemäß dieser Schaltfolge wird ein Überschneiden der Öffnungsquerschnitte an der Schieberdichtung 69 sowie den Steuerkanten 41, 43 vermieden.Due to the delay time t 1 between the closing of the
Der Darstellung gemäß
Die Funktionsweise der in
Gemäß der Darstellung nach
Neben den in
- 11
- Druckquellepressure source
- 22
- HochdruckzuleitungHigh pressure supply line
- 33
- DruckübersetzerPressure intensifier
- 44
- ÜbersetzerkolbenBooster piston
- 55
- Arbeitsraumworking space
- 66
- Differenzdruckraum (Rückraum)Differential pressure chamber (backspace)
- 77
- Stützscheibesupport disc
- 88th
- RückstellfederReturn spring
- 99
- Kompressionsraumcompression chamber
- 1010
- Überströmleitungoverflow
- 1111
- 1. Drosselstelle1. restriction
- 1212
- Steuerraum für EinspritzventilgliedControl chamber for injection valve member
- 1313
- Federfeather
- 1414
- EinspritzventilgliedInjection valve member
- 1515
- 2. Drosselstelle2. Throttling point
- 1616
- Druckraumpressure chamber
- 1717
- DruckraumzulaufPressure chamber inlet
- 1818
- Kraftstoffinjektorfuel injector
- 1919
- Injektorkörperinjector
- 2020
-
Stirnfläche Druckübersetzerkolben 4Face
pressure intensifier piston 4 - 2121
- Absteuerleitungdiversion line
- 2222
- EinspritzöffnungInjection port
- 2323
- Brennraumcombustion chamber
- 2424
- Servoventilservo valve
- 2525
- ServoventilgehäuseServo valve housing
- 2626
- 1. Gehäuseteil1st housing part
- 2727
- 2. Gehäuseteil2nd housing part
- 2828
- niederdruckseitiger Rücklauflow-pressure side return
- 2929
- Versorgungsleitung ServoventilSupply line servo valve
- 3030
- Schaltventilswitching valve
- 3131
- weiterer niederdruckseitiger Rücklauffurther low-pressure side return
- 3232
- ServoventilkolbenServo valve piston
- 3333
- DurchgangskanalThrough channel
- 3434
- 3. Drosselstelle3. Throttling point
- 3535
- Steuerfläche ServoventilkolbenControl surface Servo valve piston
- 3636
- Steuerraum ServoventilControl room Servovalve
- 3737
- Ablaufdrossel (4. Drosselstelle)Outlet throttle (4th throttle point)
- 3838
- 1. hydraulischer Raum1. hydraulic space
- 3939
- 2. hydraulischer Raum2. hydraulic space
- 4040
- erster Dichtsitzfirst sealing seat
- 4141
- Steuerkantecontrol edge
- 4242
- Absteuerraum (Niederdruckraum)Absteuerraum (low-pressure room)
- 43.43rd
- SchieberdichtkanteSlide sealing edge
- 4444
- Öffnende FlächeOpening surface
- 5050
- WiederbefüllventilWiederbefüllventil
- 5151
- Dämpfungskolbendamping piston
- 5252
- 5. Drosselstelle5. Throttling point
- 5353
- Kanalchannel
- 5454
- Federelementspring element
- 5555
- Ringflächering surface
- 5656
- Befüllleitungfilling line
- 5757
- 1. Versorgungsleitungsabschnitt1. supply line section
- 5858
- 2. Versorgungsleitungsabschnitt2. Supply line section
- 6060
- InjektorschaltventilInjektorschaltventil
- 6161
- Injektorrücklaufinjector return
- 6262
- SteuerraumhülseControl chamber sleeve
- 6363
- 1. Aussparungen1. recesses
- 6464
- Zulaufflächen (Anschliff)Inlet areas (polished section)
- 6565
- ServoventilkolbenabschnittServo valve piston section
- 6666
- 3. Gehäuseteil3rd housing part
- 6767
- Steuerhülsecontrol sleeve
- 6868
- SteuerhülsenfederControl sleeve spring
- 6969
- Schieberdichtungslide seal
- 7070
- 2. Aussparungen2. recesses
- 7171
- SteuerhülsenaussparungControl sleeve recess
Claims (16)
- Fuel injector for injecting fuel into a combustion chamber (23) of an internal combustion engine, having a pressure booster (3), whose booster piston (4) separates a working space (5), which is acted on permanently with fuel by means of a pressure source (1, 2), from a differential pressure space (6) which can be relieved of pressure, with a pressure change in the differential pressure space (6) taking place by means of an actuation of a servo valve (24) which opens or closes off a hydraulic connection (21, 39, 42) of the differential pressure space (6) to a low-pressure-side return line (28), with the servo valve (24) having a servo valve piston (32, 65) which is guided between a control space (36) and a first hydraulic space (38), and with the servo valve piston (32) having a first sealing seat (40), which opens or closes off the low-pressure-side return line (28), and a control edge (41) which separates the first hydraulic space (38) from a second hydraulic space (39), characterized in that the control space (36) is delimited by an end face (35) of the servo valve piston (32, 65), which end face (35), on the head of the servo valve piston (32, 65), is situated opposite an effective annular face which forms an effective hydraulic face (44) which is acted on at all times in the opening direction of the servo valve piston (32, 65) by a system pressure.
- Fuel injector according to Claim 1, characterized in that the control space (36) and the first hydraulic space (38) are acted on with system pressure by means of a supply line (29) which proceeds from the pressure accumulator (1).
- Fuel injector according to Claim 2, characterized in that the control space (36) of the servo valve (24) is acted on with system pressure by means of a passage duct (33), which extends through the servo valve piston (32), from the first hydraulic space (38) into which the supply line (29) opens out.
- Fuel injector according to Claim 3, characterized in that the passage duct (33) of the servo valve piston (32) contains an integrated throttle point (34).
- Fuel injector according to Claim 2, characterized in that the control space (36) and the first hydraulic space (38) are acted on in parallel with system pressure, the control space (36) being acted on with system pressure by means of a second supply line section (58) which branches off from the supply line (29) and the first hydraulic space (38) being acted on with system pressure by means of a supply line section (58) which branches off from the supply line (29).
- Fuel injector according to Claim 5, characterized in that the first supply line section (57) contains a first throttle point (34).
- Fuel injector according to Claim 1, characterized in that the first sealing seat (40) is embodied as a flat seat or as a conical seat and closes off an outflow control space (42) which is arranged at the low-pressure side.
- Fuel injector according to Claim 1, characterized in that the control edge (41) is embodied as a slide sealing edge (43).
- Fuel injector according to Claim 1, characterized in that the differential pressure space (6) which can be relieved of pressure via the servo valve (24) into the low-pressure-side return line (28) is hydraulically coupled to a control space (12), which holds a damping piston (51), for an injection valve element (14), with the damping piston (51) comprising a throttle point (52) which defines the opening speed of the injection valve element (14), and with the control space (12) being connected, for the actuation of the injection valve element (14), via a filling line (56) either to the control space (12) or to one of the hydraulic spaces (5, 6, 9) of the pressure booster (3).
- Fuel injector according to Claim 1, characterized in that the actuation of the servo valve (24) takes place by means of a switching valve (30) which connects the control space (36) to a return line (31).
- Fuel injector according to Claim 1, characterized in that the servo valve piston (32) comprises a reduced-diameter servo piston section (65) on which is held a preloaded control sleeve (67).
- Fuel injector according to Claim 1, characterized in that the control sleeve (67) forms a slide control edge (69) with the servo valve piston section (65).
- Fuel injector according to Claim 12, characterized in that the slide control edge (69) controls the connection to the low-pressure-side return line (28).
- Fuel injector according to Claim 11, characterized in that the servo valve piston section (65) of the servo valve piston (32) has first cutouts (63) which comprise a slide sealing edge (43) which interact with a control edge (41) which is formed on the servo valve housing.
- Fuel injector according to Claim 11, characterized in that the control sleeve (67) is acted on by means of a spring element (68) which is supported against a housing part (26) of the servo valve housing (25).
- Fuel injector according to Claim 11, characterized in that the servo valve piston section (65) of the servo valve piston (32) has first cutouts (63) between the first hydraulic space (38) and the second hydraulic space (39), and second cutouts (70) which form a slide seal (69).
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10315014 | 2003-04-02 | ||
DE10325620A DE10325620A1 (en) | 2003-04-02 | 2003-06-05 | Servo-controlled fuel injector with pressure intensifier |
PCT/DE2004/000413 WO2004088122A1 (en) | 2003-04-02 | 2004-03-04 | Fuel injector provided with provided with a pressure transmitter controlled by a servo valve |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1613856A1 EP1613856A1 (en) | 2006-01-11 |
EP1613856B1 true EP1613856B1 (en) | 2008-07-09 |
Family
ID=33132671
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP04717030A Expired - Fee Related EP1613856B1 (en) | 2003-04-02 | 2004-03-04 | Fuel injector provided with a pressure transmitter controlled by a servo valve |
Country Status (4)
Country | Link |
---|---|
US (1) | US7320310B2 (en) |
EP (1) | EP1613856B1 (en) |
JP (1) | JP2006522254A (en) |
WO (1) | WO2004088122A1 (en) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004017305A1 (en) * | 2004-04-08 | 2005-10-27 | Robert Bosch Gmbh | Fuel injection device for internal combustion engines with directly controllable nozzle needles |
DE102004017304A1 (en) * | 2004-04-08 | 2005-10-27 | Robert Bosch Gmbh | Servo valve controlled fuel injector |
DE102004022267A1 (en) * | 2004-05-06 | 2005-12-01 | Robert Bosch Gmbh | Method and device for shaping the injection pressure at 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 |
DE102004053274A1 (en) * | 2004-11-04 | 2006-05-11 | Robert Bosch Gmbh | Fuel injection system |
DE102004053271A1 (en) * | 2004-11-04 | 2006-05-11 | Robert Bosch Gmbh | Electrohydraulic servo valve |
EP1836385B1 (en) * | 2004-12-03 | 2010-12-29 | Ganser-Hydromag AG | Fuel injection valve with pressure gain |
JP4608554B2 (en) * | 2005-02-22 | 2011-01-12 | シーメンス ヴィディーオー オートモーティヴ コーポレイション | Fuel system with pressure amplification function |
ATE458910T1 (en) * | 2005-06-28 | 2010-03-15 | Renault Trucks | COMBUSTION ENGINE COMPRISING MULTIPLE FUEL INJECTION ARRANGEMENTS |
US8100110B2 (en) * | 2005-12-22 | 2012-01-24 | Caterpillar Inc. | Fuel injector with selectable intensification |
JP4793315B2 (en) * | 2006-07-20 | 2011-10-12 | 株式会社デンソー | Fuel injection device |
DE102006038840A1 (en) * | 2006-08-18 | 2008-02-21 | Robert Bosch Gmbh | Fuel injector with piston return of a pressure booster piston |
DE102007002445A1 (en) * | 2007-01-17 | 2008-07-24 | Robert Bosch Gmbh | Check valve and injector with hydraulic interrupter and check valve |
DE102008001330A1 (en) * | 2008-04-23 | 2009-10-29 | Robert Bosch Gmbh | Fuel injection valve for internal combustion engines |
US9163597B2 (en) * | 2008-10-01 | 2015-10-20 | Caterpillar Inc. | High-pressure containment sleeve for nozzle assembly and fuel injector using same |
US8291889B2 (en) | 2009-05-07 | 2012-10-23 | Caterpillar Inc. | Pressure control in low static leak fuel system |
ATE546636T1 (en) * | 2009-08-26 | 2012-03-15 | Delphi Tech Holding Sarl | FUEL INJECTOR |
EP2290219B1 (en) | 2009-08-26 | 2013-01-23 | Delphi Technologies Holding S.à.r.l. | Three-way control valve |
DE102010040581A1 (en) * | 2010-02-24 | 2011-08-25 | Robert Bosch GmbH, 70469 | Fuel injector and method for producing and / or mounting a nozzle needle assembly |
EP2410168A1 (en) * | 2010-07-23 | 2012-01-25 | Wärtsilä Schweiz AG | Fluid dispenser and method for providing an operating fluid using a fluid dispenser |
FI124350B (en) * | 2012-03-09 | 2014-07-15 | Wärtsilä Finland Oy | Hydraulic actuator |
US9228550B2 (en) | 2013-03-11 | 2016-01-05 | Stanadyne Llc | Common rail injector with regulated pressure chamber |
RU2554151C1 (en) * | 2014-05-20 | 2015-06-27 | Федеральное государственное унитарное предприятие "Центральный ордена Трудового Красного Знамени научно-исследовательский автомобильный и автомоторный институт "НАМИ" | Diesel engine fuel system |
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 |
CN104819083A (en) * | 2015-04-27 | 2015-08-05 | 江苏海事职业技术学院 | High-pressure common rail fuel injection control system of large-sized low-speed two-stroke diesel engine |
GB2560513A (en) * | 2017-03-13 | 2018-09-19 | Ap Moeller Maersk As | Fuel injection system |
CN114458498B (en) * | 2022-02-24 | 2022-10-28 | 哈尔滨工程大学 | High-pressure common rail oil injector for realizing high-stability injection based on throttling resistance-capacitance effect |
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JPS57124073A (en) * | 1981-01-24 | 1982-08-02 | Diesel Kiki Co Ltd | Fuel injection device |
JP2885076B2 (en) * | 1994-07-08 | 1999-04-19 | 三菱自動車工業株式会社 | Accumulator type fuel injection device |
DE19949848A1 (en) | 1999-10-15 | 2001-04-19 | Bosch Gmbh Robert | Pressure converter for fuel injection system includes compensation for hydraulic forces acting between injections on the low pressure side |
DE19952512A1 (en) * | 1999-10-30 | 2001-05-10 | Bosch Gmbh Robert | Pressure booster and fuel injection system with a pressure booster |
DE10063545C1 (en) * | 2000-12-20 | 2002-08-01 | Bosch Gmbh Robert | Fuel injection system |
DE10218904A1 (en) | 2001-05-17 | 2002-12-05 | Bosch Gmbh Robert | Fuel injection system |
DE10123914B4 (en) | 2001-05-17 | 2005-10-20 | Bosch Gmbh Robert | Fuel injection device with pressure booster device and pressure booster device |
DE10158951A1 (en) * | 2001-12-03 | 2003-06-12 | Daimler Chrysler Ag | Fuel Injection system for IC engine, operates with pressure conversion, has connection from control chamber and admission chamber to return line passing via common valve connection |
DE10229419A1 (en) * | 2002-06-29 | 2004-01-29 | Robert Bosch Gmbh | Pressure-translated fuel injector with rapid pressure reduction at the end of injection |
DE10247903A1 (en) | 2002-10-14 | 2004-04-22 | Robert Bosch Gmbh | Pressure-reinforced fuel injection device for internal combustion engine has central control line acting on pressure transmission piston |
DE10337574A1 (en) * | 2003-08-14 | 2005-03-10 | Bosch Gmbh Robert | Fuel injection device for internal combustion engines |
DE102004022270A1 (en) * | 2004-05-06 | 2005-12-01 | Robert Bosch Gmbh | Fuel injector for internal combustion engines with multi-stage control valve |
-
2004
- 2004-03-04 WO PCT/DE2004/000413 patent/WO2004088122A1/en active IP Right Grant
- 2004-03-04 US US10/551,461 patent/US7320310B2/en not_active Expired - Fee Related
- 2004-03-04 EP EP04717030A patent/EP1613856B1/en not_active Expired - Fee Related
- 2004-03-04 JP JP2006504247A patent/JP2006522254A/en not_active Ceased
Also Published As
Publication number | Publication date |
---|---|
EP1613856A1 (en) | 2006-01-11 |
US20060243252A1 (en) | 2006-11-02 |
US7320310B2 (en) | 2008-01-22 |
WO2004088122A1 (en) | 2004-10-14 |
JP2006522254A (en) | 2006-09-28 |
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