EP0174261B1 - Fördermengensteuersystem - Google Patents

Fördermengensteuersystem Download PDF

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Publication number
EP0174261B1
EP0174261B1 EP85630105A EP85630105A EP0174261B1 EP 0174261 B1 EP0174261 B1 EP 0174261B1 EP 85630105 A EP85630105 A EP 85630105A EP 85630105 A EP85630105 A EP 85630105A EP 0174261 B1 EP0174261 B1 EP 0174261B1
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EP
European Patent Office
Prior art keywords
fuel
injector
conduit
valve
pump
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
EP85630105A
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English (en)
French (fr)
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EP0174261A1 (de
Inventor
Thomas Joseph Wich
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AIL Corp
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AIL Corp
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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
    • F02M63/06—Use of pressure wave generated by fuel inertia to open injection 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
    • F02M45/00—Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship
    • F02M45/02—Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts
    • F02M45/04—Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship with each cyclic delivery being separated into two or more parts with a small initial part, e.g. initial part for partial load and initial and main part for full load
    • 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
    • F02M55/00—Fuel-injection apparatus characterised by their fuel conduits or their venting means; Arrangements of conduits between fuel tank and pump F02M37/00
    • F02M55/02—Conduits between injection pumps and injectors, e.g. conduits between pump and common-rail or conduits between common-rail and injectors
    • 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
    • F02M59/20—Varying fuel delivery in quantity or timing
    • F02M59/36—Varying fuel delivery in quantity or timing by variably-timed valves controlling fuel passages to pumping elements or overflow passages
    • F02M59/366—Valves being actuated electrically

Definitions

  • the invention relates to a system for controlling delivery of fuel from a fuel source to a compression-ignition engine, according to the precharacterizing portion of claim 1.
  • a system for controlling delivery of fuel according to the precharacterizing portion of claim 1 is disclosed in CH-A-433 865 according to which the length of the conduit means between the pump means and the bypass control valve means determines the time delay within which the control valve means must close, which time delay must be shorter than the wave running time.
  • ignition delay For any particular type of diesel engine there exists a characteristic ignition delay which may be predetermined empirically. Further, it is desirable to avoid the sudden injection of the entire quantity of fuel to be combusted as it results in excessive pressure rise causing noise and stress on engine parts and possibly an increase in NO X .
  • pilot injection a relatively small quantity of fuel
  • main fuel injection a relatively small quantity of fuel
  • pilot injection a relatively small quantity of fuel
  • the combustion process is enhanced or optimized inasmuch as the main fuel is injected just as the pilot fuel is beginning to combust.
  • a desirable programming of fuel injection to include pilot injection is one which schedules the main fuel injection to occur a predetermined interval after the pilot injection, which interval is substantially the equivalent of the ignition delay.
  • a fuel injection pump having a first conduit between the pump means and the injector for injecting pilot fuel and a second longer conduit between the pump means for the injector for injecting main fuel after a predetermined hydraulic delay dependent on the length of the second conduit is disclosed in GB-A-539 116.
  • the object of the present invention is to provide an improved system for the delivery of both a pilot injection and a main°injection of fuel to a compression-ignition engine, and which system has a simplified and economical mechanical design.
  • the present invention provides a system for controlling delivery of fuel to a compression ignition engine, which engine has a predetermined characteristic ignition delay.
  • a positive-- displacement pump typically a multiplunger in-line pump, receives fuel from a source and provides intermittent, pressurized pulses of fuel flow.
  • a conduit extends from a pumping chamber to a node to which a normally-closed fuel injector is operatively connected.
  • a normally-open, solenoid-controlled bypass valve has an inlet port connected to the conduit node for allowing fuel to bypass the injector. When a signal is applied to the bypass valve it rapidly closes, causing the pressure at the injector to rapidly increase to a first injector-opening level to inject pilot fuel.
  • the pressure at the injector rapidly increases to a second level greater than the first to provide main fuel injection.
  • the length of the conduit determines the hydraulic delay and is selected to have a predetermined time relation with the engine's ignition delay time.
  • the hydraulic delay substantially corresponds with the ignition delay time in the preferred embodiment.
  • the bypass valve responds rapidly in both the opening and closing directions, and the initiation and duration of the control signal are adjustable during operation.
  • Part of the make-up fuel delivered by the pump is provided by reverse flow of fuel through the open bypass valve.
  • a fuel delivery system for a compression-ignition or diesel engine 10 for a compression-ignition or diesel engine 10.
  • the engine 10 will be presumed to be a four-cylinder, naturally aspirated, medium duty diesel engine having a displacement of approximately one liter per cylinder.
  • a relatively high pressure, four-cylinder, in-line fuel pump 12 is driven by engine 10 for providing intermittent or periodic pulses of fuel flow to respective bypass valve and injector assemblies 14.
  • the pump 12 is capable of delivering fuel pulse pressures as great as about 1000 bar (approximately 15 000 psi) for direct injection.
  • the fuel delivery system of the invention may be used with diesel engines of numerous different configurations and that the pump 12 might alternatively be constituted of individual unit pumps each incorporated with the engine.
  • Fuel is drawn from a source, such as fuel tank 16, by a supply pump 18.
  • Supply pump 18 is of the continuously operating type and may be associated with pump 12 in a known manner or may exist as a stand-alone pump which is driven electrically or by a mechanical takeoff from the engine 10 or the pump 12.
  • the supply pump 18 provides a continuous supply of fuel at a relatively low pressure of about 3 bar (45 psi).
  • the output of supply pump 18 is passed through a filter 20 whereupon it enters a low pressure supply conduit 22.
  • the low pressure supply conduit 22 may also serve in some instances to provide a drain, as will be hereinafter described.
  • the low pressure supply conduit 22 extends, as represented by branches 24, to each of the four pumping cylinders within the in-line pump 12.
  • the low pressure supply conduit 22 also includes separate branches 23 extending to each of the respective injector assemblies 14. Finally, the supply conduit 22 returns to the fuel tank 16 via a low pressure check valve or orifice 26.
  • Each cylinder of the pump 12 includes a respective outlet 28 which forms one end of a respective fuel conduit 30.
  • Each fuel conduit 30 is suited for the delivery of high pressure pulses of fuel to respective injector assemblies 14.
  • each fuel conduit 30 is of a predetermined length selected to provide a requisite hydraulic delay between the start of a pilot pulse and the start of the main fuel pulse, which delay is intended to correspond with the engine's characteristic ignition delay, as will be hereinafter described in greater detail.
  • each bypass valve and injector assembly 14 is depicted as including an injector nozzle 32 and a bypass valve 34.
  • the injector 32 and the bypass valve 34 may be housed separately as depictedin Fig. 2 for diagrammatic illustration, they may also be and preferably are, located in a common housing as illustrated in Fig. 3.
  • Each bypass valve 34 includes a pair of ports 36 and 38, with port 36 being connected directly to high pressure conduit 30 and port 38 being connected to the low pressure supply branch conduit 23.
  • the bypass valve 34 includes a valve element 40 joined with an armature 42 for electromagnetic actuation by energization of the coil 44 of a solenoid.
  • the solenoid coil 44 is energized by a signal current applied thereto on a pair of wires represented by a single line 45.
  • the solenoid-actuated bypass valve 40 is in a normally-open condition, as symbolically represented in Fig. 2 by the existence of a spring 46. Energization of coil 44 by the application of an appropriate signal on line 45 serves to rapidly close the bypass valve 34 and conversely, an appropriate signal, such as the cessation of electrical current, allows the valve to rapidly reopen.
  • the fuel injection nozzle 32 includes a needle valve element 50 contained within nozzle body 52 and biased by spring 54 into valve-closing engagement with a valve seat 56.
  • the needle 50 lifts from seat 56 in a known manner to inject fuel directly into the engine via nozzle orifice 60.
  • the fuel which serves both to open the injector valve 50 and to supply fuel to the engine 10 is supplied to injector chamber 58 via an extension 30' ofthe high pressure fluid conduit 30.
  • FIG. 2 diagrammatically illustrates one of the pumping chambers 62 in the in-line pump 12 which serves as the source of pressurized pulses of fuel flow through a respective conduit 30.
  • a piston or plunger 64 reciprocates within the pumping chamber 62 to provide the pressurized pulses of fuel flow. Reciprocation of each plunger 64 is effected by a cam 66 mounted on a shaft 67 and driven directly or indirectly by the engine 10.
  • Pump 12 may for the most part be of a type which is commercially available from any of several pump manufacturers; however, such pump must be modified since the control racks, control mechanisms for control of the pump output and pump delivery valves are not necessary. Additionally, no provision need be made for adjusting the timing of cam 66 during operation.
  • Plunger 64 is depicted at the bottom of its operating stroke, illustrating that the port to the conduit 24 associated with the low pressure supply remains covered. As the plunger 64 is driven upward by the cam 66 it forces fuel contained in pumping chamber 62 out through high pressure conduit 30 for bypass through the bypass valve 34 or for injection through injector 32, as will be hereinafter described. As the plunger 64 nears the top of its stroke, a venting bore 68 formed therein moves into registry with the supply conduit 24, as illustrated in dotted line, to allow fuel to flow in either direction.
  • venting bore 68 When plunger 64 is at the top of its stroke, the registry of venting bore 68 with supply conduit 24 ensures that the small remaining volume of pumping chamber 62 is completely filled with fuel to begin an intake stroke. On the downward stroke of the plunger 64the venting bore 68 will move out of registry with conduit 24 and thus create a suction within the pumping chamber 62.
  • the pumping chamber 62 is not provided with a delivery valve at its outlet and the bypass valve 34 will be open at this stage of operation such that fuel is allowed to flow reversely through a respective low pressure supply branch 23 and reversely through a respective high pressure conduit 30, thereby ensuring a full charge of fuel in the respective pumping chamber 62 when the plunger 64 reaches the bottom of its stroke.
  • the general timing of the initiation and termination of fuel injection to engine 10 is determined by the electronic control unit 70 which provides control signals via respective lines 45 to the respective bypass valves 34.
  • the electronic control unit 70 will respond to sensed engine operating parameters such as speed, load, temperature and the like to provide control signals in accordance with a predetermined control program.
  • the control afforded by electrical signals on lines 45 normally involves the closing of the valve 34 by energization of coil 44 and the reopening of the valve by discontinuing such energization of the coil.
  • fuel flow may occur in either direction past the valve through branch conduit 23 and high pressure conduit 30.
  • branch conduits 23 and high pressure conduits 30 are such that the pressure of fuel flowing therein when bypass valve 34 is open is relatively low even though a pumping plunger 64 is in its upward stroke. Accordingly, the fuel pressure appearing in extension conduit 30' to a respective injector 32 is normally below the threshold level required to overcome the bias of spring 54 for opening the injector.
  • bypass valve 34 if bypass valve 34 is closed and the plunger 64 is in its upward stroke, the pressure of the fuel in conduit 30 and extension 30' will increase and will overcome the bias of injector spring 54 to allow injection offuel into the engine. Absent a consideration of the flow dynamics occasioned by a sudden closing of the bypass valve 34, the fuel pressure in conduit 30 would be determined by the stroke of plunger 64 which is controlled by the profile of cam 66. That pressure increases during the plunger's upward stroke, the rate of increase moderating somewhat when the injector 32 opens.
  • bypass valve 34 during the pumping stroke of a respective plunger 64 operates to immediately stop the flow of fuel at the inlet port 36 to the bypass valve, which results in a rapid and significant rise in the pressure of the fuel in that region.
  • This phenomenon in water pipes is known as “water hammer” and for the purposes of the present invention, is referred to as “fuel hammer”.
  • This rapid increase in the fuel pressure in conduit 30 occurs most immediately in the region of bypass valve inlet port 36, and thus also soon thereafter in the region of injector 32 inasmuch as the conduit extension 30' is relatively short compared to the overall length of conduit 30 and is in general proximity with the inlet port 36 of the bypass valve. This rapid pressure increase is such that the opening bias in injector 32 is overcome and injection of fuel into engine 10 begins.
  • bypass valve 34 The rapid rise in the pressure of the fuel in conduit 30 at bypass valve 34 travels the short distance of any conduit extension 30" to the node or junction 30a at which conduit extension 30' joins conduit 30, and then travels back along conduit 30 to the outlet 28 and pumping chamber 62 of pump 12, whereupon it is reflected back along conduit 30 toward the injector 32. Because the closure of bypass valve 34 occurs during the compression stroke of plunger 64, the pressure traces depicted in Fig. 5 result.
  • a pumping chamber 62 of pump 12 the pressure at the outlet 28 of a pumping chamber 62 of pump 12 is illustrated in dotted line as a function of time. It will be appreciated that the scale of the X-axis might alternatively have been crank angle or pump cam angle at some engine operating condition, however a time base more appropriately illustrates the principles of the invention.
  • the solid line trace in Fig. 5 depicts the pressure of fuel in conduit 30' at the injector 32.
  • the pressure at pump 12 increases very gradually between to and t, as the plunger 64 begins its compression stroke and the bypass valve 34 remains open.
  • a control signal is applied to line 45 and the bypass valve 34 rapidly closes.
  • the fuel pressure in conduit 30' at the fuel injector 32, and specifically in chamber 58 of the injector rapidly increases from less than 70 bar (1,000 psi) to a level at t 2 which exceeds the opening threshold pressure, Th o .
  • the delay between t 1 and t 2 is determined mainly by the response time of the bypass valve 34 plus a hydraulic delay proportional to the length of conduit 30'.
  • conduit 30' will be relatively short.
  • the pressure at which injector 32 opens is approximately 280 bar (4,000 psi) and this initial fuel pressure pulse may have a pressure of about 350 bar (5,000 psi). Then, both because the needle 50 of the fuel injector 32 has opened and because the pressure pulse is moving upstream along conduit 30 while the pumping plunger 64 is continuing its upward stroke, there is relatively little change in the fuel pressure in conduit 30' at injector 32 for a hydraulic delay interval (HD) which is controlled to substantially correspond with the characteristic ignition delay (ID) of the engine 10.
  • HD hydraulic delay interval
  • This interval HD is depicted in Fig. 5 as extending from time t 2 until t 3 and it is determined by the length L of conduit 30 between pump 12 and conduit node 30a.
  • This delay interval HD is determined principally by the time it takes the pressure pulse generated by the abrupt closing of bypass valve 34 to travel the length L of conduit 30 from node 30a to the pump 12 and back again. It will be appreciated that the length of conduit extension 30' will not affect the length of the interval HD. The length of conduit extension 30' does not affect the interval HD because the initial pressure pulse is also moving toward pump 12 while it is moving along extension 30'.
  • the hydraulic delay interval HD from t 2 to t 3 on Fig. 5 is also approximately 1 millisecond.
  • the speed of such a pressure pulse within the liquid fuel medium and at the pressures present will tend to be in the range of 1200 m/sec (4,000 ft/sec) ⁇ several hundred m/ sec.
  • the length L of that conduit 30 may be preselected to provide the hydraulic delay which corresponds with the requisite ignition delay.
  • Each conduit 30 should have the same length L.
  • the pulse velocity of 1200 m/sec (4,000 ft/sec) may be considered a constant.
  • characteristic ignition delays for differing types of engines may range from approximately 0.5 milliseconds to slightly over 1 millisecond.
  • the length L will need to be approximately 0.3 m (one foot). It will be appreciated that the shorter the length L is required to be, the closer the pump 12 will need to be to the several injectors 32 such that the length L of the conduits 30 to each respective injector need not exceed approximately 0.3 m (one foot).
  • the conduit length L is required to be relatively long, it may be accommodated by a curved or serpentine patterning of the conduit.
  • the pilot fuel pulse will have mixed with the air in the engine and increased to an ignition or near-ignition temperature and the immediate follow-on of the main fuel pulse serves to optimize the fuel combustion process. Most of the fuel is injected during the main fuel pulse, with only about 25-35% being injected during the pilot phase.
  • the main fuel pulse is terminated by reopening the bypass valve 34 at time t 4 whereupon, following the brief interval required to transit conduit extensions 30" and 30', the fuel pressure at the injector 32 rapidly drops below the closing threshold, The, of about 210 bar (3,000 psi) at time t 5 and injection is terminated. It will be noted that the pressure at pumping chamber 62 drops off rapidly also, but is delayed slightly as a result of the length of the conduit 30.
  • valve 34 will need to be timed such that t 2 occurs at the predetermined hydraulic interval HD prior to that desired instant for t 3 .
  • This hydraulic delay HD is determined by length L of conduit 30, and the desired time for t, is determinable and is substantially constant relative to t 3 .
  • the crank or cam angles of these times will vary with speed.
  • bypass valve 34 be capable of closing its valve element 40 as rapidly as possible so as to effect the rapid pressure rise between t, and t 2 seen in Fig. 5. It is also desirable that valve 34 be capable of rapidly opening its valve element 40 to abruptly terminate fuel injection. Moreover, it is preferable that the bypass valve 34 and the injector 32 be positioned as close to one another as possible to simplify the fluid dynamics of the system.
  • the particular solenoid-actuated, pressure-assisted bypass valve 34 illustrated in Figs. 3 and 4 in integral combination with the injector 32 is particularly suited to this end.
  • the high pressure conduit 30 is operatively connected to the injector nozzle body 52 in which is located node 30a and from which extends conduit branch 30' to the injector chamber 58 and conduit branch 30" extending toward the bypass valve 34.
  • Conduit extension 30" extends upwardly in valve body 52 to an opening positioned centrally in the upper surface 74 of the nozzle body.
  • the solenoid-actuated bypass valve assembly 34 is positioned immediately above nozzle body 52 and is integrally joined therewith, as by a pair of holddown bolts extending through a flange in valve cover 76 and into threaded engagement with a corresponding flange on the valve body 52.
  • the active elements of the bypass valve are located in a housing cavity formed between the spaced, axially-opposing faces of valve cover 76 and nozzle body 52 and radially within a cylindrical collar 77 whose opposite ends extend around the valve cover 76 and the upper end of nozzle body 52 respectively.
  • a rod-like or spindle-like valve seat member 37 extends axially between the upper surface 74 of the nozzle body 52 and the cover 76.
  • Valve seat 37 includes an upwardly-extending blind bore which defines at least part of inlet port 36.
  • the valve seat 37 is positioned such that the bore or port 36 is aligned with the upper end of conduit 30".
  • the lower end of valve seat 37 is urged into substantially fluid sealing engagement with the upper surface 74 of nozzle body 52 by means of one or more Belleville washers 78 acting downwardly upon a surface of shoulder of valve seat 37 and upwardly upon the undersurface of cover 76.
  • valve seat 37 The concentric positioning of the valve seat 37 and the retention of the Belleville washer 78 on that valve seat may be assured by a pilot pin 79 extending from the upper end of the valve seats and into a centered bore in the undersurface of cover 76.
  • Belleville washers 78 typically apply a 900-1400 N (200-300 pound) downward force on valve seat 37 to maintain it in substantially fixed sealing engagement with the upper surface 74 of the injector body 52.
  • the valve seat spindle 37 has a constant diameter over most of its lower extent and includes a region of larger diameter thereabove. In the region of larger diameter there is formed an annular control edge 80 whose diameter is greater than that of the lower spindle portion of the valve seat 37.
  • An annular recess 81 is machined in the valve seat 37 immediately below the control edge 80 both to form that control edge and to provide a small high pressure plenum 81' adjacent to the valve seat.
  • One or more radial bores 36' extend inwardly from the recess 81 to the axial port bore 36 to provide liquid communication between the port 36 and the plenum formed by the recess.
  • the moving valve element is a valve sleeve 140 comprised of a cylindrical sleeve disposed about the lower portion of valve seat 37 and sized for close axial sliding relation therewith.
  • the inner diameter of the valve sleeve 140 is, for most of its length, only slightly larger than the outside diameter of the lower portion of the valve seat 37 and somewhat less than the diameter of the control edge 80 of the valve seat 37.
  • the outside diameter of the valve sleeve 140 is greater than the diameter of the control edge 80, and the transition from the inside diameter to the outside diameter near the upper end includes an upwardly inclined or inverted frustoconical surface 82 for contacting the control edge 80 when the valve is closed.
  • An annular armature 42 is joined to the valve sleeve 140 near its lower end, as through threaded engagement or preferably by means of a snap ring 83 received in a recess in the sleeve 140 and retaining the armature in fixed engagement with a shoulder of that sleeve.
  • a plurality of bleed holes 84 extend axially through the armature 42 to minimize fluid resistance during actuation.
  • An annular stator structure 85 which includes the solenoid coil 44 as an integral part thereof, surrounds and is outwardly spaced from the valve sleeve 140. Stator 85 is positioned against the undersurface of cover 76 and is maintained in predetermined spaced relation with the upper surface 74 of the injector body 52 by means of an annular spacer 87. The leads from the coil 44 extend to a pair of terminals, here represented by a single terminal 45.
  • the amplitude of the stroke of valve sleeve 140 is determined by the contact of its surface 82 with the control edge 80 in the valve-closed position illustrated, and by contact of the lower end of the sleeve with the upper surface 74 of the injector body 52 in the full-open position illustrated in broken line in Fig. 4. That stroke or displacement of valve sleeve 140 may be closely controlled by the axial dimensioning of sleeve 140 and the selection of the angle of face 82 thereon. In the illustrated embodiment, that stroke is about 0.1524 mm (0.006 inch). Similarly, the axial positioning of the armature 42 on the valve sleeve 140 is preselected such that when the coil 44 is energized and the valve is closed as shown in Fig.
  • valve sleeve 140 determines the air gap spacing when the valve is fully open and, in the present instance, that air gap spacing is about 0.254 mm-(0.01 inch). Accordingly, adjustment of the open and closed air gap spacings may be controlled by adjustment of the valve sleeve stroke length and/ or the positioning of the armature 42 on the valve sleeve 140 and/or the height of spacer 87.
  • a radially inner, upper surface of the stator 85 is conically beveled and includes a truncated conical spill deflector 90 of relatively hard metal to protect the stator.
  • the region above the spill deflector 90 and below the undersurface of the valve cover 76 defines a low pressure plenum which communicates, via one or more angled bores 38' in the cover, with a large central bore 38 which defines the- low pressure drain port associated with the valve.
  • valve sleeve 140 Assuming the valve sleeve 140 to be in its normally open position in which its lower end contacts surface 74 of injector body 52, a resulting gap or control orifice will exist between the control edge 80 and the surface 82 of the sleeve 140 through which fuel is free to pass in either direction depending upon pressure differences. For instance, if the fuel pressure in conduit 30" is relatively high, as during a pumping stroke from pump 12, the open valve will serve to bypass fuel in the forward direction and exhaust it through drain port 38 to branch conduit 23 and thence to low pressure conduit 22. On the other hand, if the pump plunger is on its down stroke and is filling the pumping chamber, fuel may flow in the reverse direction by entering port 38 and exiting port 36.
  • valve sleeve 140 Two forces act to rapidly open valve sleeve 140. Principally, assuming the pressure in conduit 30" to be significantly greater than that in the region of port 38, the resulting hydraulic forces operate to open the valve. Secondarily, the valve seat spindle 37 and the valve sleeve 140 are preferably oriented vertically such that the force of gravity aids in opening the valve. Typically, at the instant it is desired to open the valve 34 the fuel pressure in conduit 30" will be on the order of several hundred bar (several thousand psi), whereas the fuel pressure at port 38 will be less than 7 bar (100 psi).
  • valve sleeve 140 The resulting differential in pressure will act axially downwardly on that narrow annular portion of the valve sleeve 140 which extends radially outward from the inner diameter of that valve sleeve to its point of contact with the control edge 80 of the valve seat 37.
  • the remainder of the valve sleeve 140 and armature 42 radially outward of the control orifice between edge 80 and surface 82 is in a "low" pressure region of equalized force in both the opening and closing directions.
  • the side diameter of the valve sleeve 140 is 5.99 mm (0.236 inch) and the diameter of the control edge 80 is 6.4 mm (0.252 inch).
  • valve sleeve 140 remains in its full-open position until the next closing signal is applied to the solenoid coil 44 in order to ensure a predictable and uniform interval from the instant of the signal until the valve is closed.
  • a component of engine vibration axially of valve sleeve 140 could be capable of causing oscillation or "chatter" of sleeve 140, particularly during the low pressure phase of the pumping cycle, unless some bias force is maintained in the "valve opening" direction.
  • the effect of gravity is not particularly significant and accordingly, a hydraulic bias of one pound or more of force is employed.
  • valve sleeve 140 and armature 42 are pressure-balanced in the axial direction, care is taken to provide some portion of the valve sleeve 140 and/or armature 42 which receives a net "opening" hydraulic bias while the valve is open. This is accomplished in the present embodiment by the axially-facing area at the bottom end of valve sleeve 140 being smooth and in full, liquid-excluding contact with smooth surface 74 of injector body 52. The resulting hydraulic force serving to bias valve sleeve 140 to the open position will then be the product of the low supply pressure, i.e.
  • 1,7-3,5 bar 25-50 psi
  • the unbalanced area i.e., about 0.425 cm 2 (0.066 square inch).
  • the resulting force is in excess of 4.5N (one pound) and substantially eliminates unwanted valve oscillations.
  • a solenoid valve assembly possessing the aforementioned characteristics is capable of being actuated from its normally open to its closed position in 1 millisecond or less and - conversely, the valve is capable of being actuated from its fully closed to its fully opened position in 1 millisecond or less. In each instance there is no requirement for mechanical biasing means to aid or control the movement of the valve sleeve 140.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • High-Pressure Fuel Injection Pump Control (AREA)

Claims (10)

1. System zum Steuern der Förderung von Kraftstoff aus einer Kraftstoffquelle (16) zu einem Dieselmotor (10), der eine charakteristische Zündzeitverzögerung hat, wobei das System eine Kraftstoffeinspritzvorrichtung (32) aufweist, die in eine normalerweise geschlossene Position vorgespannt ist, eine Pumpeinrichtung (12) zum Empfangen von Kraftstoff aus der Quelle, eine erste Leitung (30), die sich von der Pumpeinrichtung (12) zu einem Knotenpunkt (30a) erstreckt, wobei die Kraftstoffeinspritzvorrichtung (32) in dem Knotenpunkt (30a) mit der ersten Leitung (30) in Wirkverbindung ist, und eine Bypass-Steuerventileinrichtung (34), die auf ein elektrisches Steuersignal hin schnell zwischen einer offenen und einer geschlossenen Position bewegbar ist, wobei die Ventileinrichtung (34) eine erste Öffnung (36) hat, die in dem Knotenpunkt (30a) mit der ersten Leitung (30) in Wirkverbindung ist, und eine zweite Öffnung (38) zu einem Gebiet relativ niedrigen Druckes, wobei der Kraftstoffstrom in der ersten Leitung (30) die Einspritzvorrichtung (32) effektiv umgeht, wenn die Steuerventileinrichtung (34) offen ist, und so ist, daß, wenn die Steuerventileinrichtung (34) schnell schließt, sein Druck an der Einspritzvorrichtung (32) schnell auf einen Wert ansteigt, der die Vorspannung der Einspritzvorrichtung (32) übersteigt, um das Einspritzen von Kraftstoff zu bewirken, dadurch gekennzeichnet, daß die Pumpeinrichtung (12) eine Verdrängerpumpeinrichtung ist, die intermittierende Stöße unter Druck stehenden Kraftstoffes liefert, daß beim Schließen der Steuerventileinrichtung (34) der Druck an der Einspritzvorrichtung (32) schnell auf einen ersten Wert ansteigt, um eine Kraftstoffvoreinspritzung zu bewirken, und anschließend, nach einem vorbestimmten hydraulischen Verzögerungsintervall, das eine vorbestimmte Zeitbeziehung zu der Zündverzögerungszeit hat, schnell auf einen zweiten Wert ansteigt, der größer als der erste Wert ist, um eine Kraftstoffhaupteinspritzung zu bewirken, und daß die erste Leitung (30) eine besondere vorgewählte Länge hat, so daß das vorbestimmte hydraulische Verzögerungsintervall zwischen dem Start der Voreinspritzung und dem Start der Haupteinspritzung im wesentlichen gleich der Zündverzögerungszeit ist.
2. Kraftstofförderungssteuersystem nach Anspruch 1, dadurch gekennzeichnet, daß die Einspritzvorrichtung (32) und die Bypass-Steuerventileinrichtung (34) jeweils mit der ersten Leitung (30) in dem Knotenpunkt (30a) durch eine Verlängerungsleitung (30' bzw. 30") verbunden sind, wobei jede Verlängerungsleitung (30, 30") im Vergleich zu der Länge der ersten Leitung (30) relativ kurz ist.
3. Kraftstofförderungssteuersystem nach Anspruch 1, dadurch gekennzeichnet, daß eine zweite Leitung (22, 23) in Wirkverbindung mit der zweiten Öffnung (38) der Bypass-Steuerventileinrichtung (34) ist und daß die Bypass-Steuerventileinrichtung (34) normalerweise offen ist und die Pumpeinrichtung (12) wenigstens einen Teil des Kraftstoffes aus der Quelle (16) durch Gegenstrom in der zweiten und in der ersten Leitung (22, 23, 30) empfängt.
4. Kraftstofförderungssteuersystem nach Anspruch 1, dadurch gekennzeichnet, daß die Zeitsteuerung wenigstens des Öffnens oder des Schließens der Bypass-Steuerventileinrichtung (34) während des Betriebes einstellbar ist.
5. Kraftstofförderungssteuersystem nach Anspruch 1, für einen Motor, der mehrere Zylinder hat, dadurch gekennzeichnet, daß jeder Zylinder eine Kraftstoffeinspritzvorrichtung (32) hat, wobei jede Kraftstoffeinspritzvorrichtung (32) mit Kraftstoff über eine separate erste Leitung (30) versorgt wird und wobei jeder ersten Leitung (30) eine separate Bypass-Steuerventileinrichtung (34) zugeordnet ist, und daß die Pumpeinrichtung (12) eine Einrichtung enthält zum Fördern der Stöße des Kraftstoffstroms zu den ersten Leitungen (30) in einer vorbestimmten Sequenz.
6. Kraftstofförderungssteuersystem nach Anspruch 5, dadurch gekennzeichnet, daß die Pumpeinrichtung (12) eine In-line-Pumpe ist, die mehrere Pumpzylinder (62) hat, wobei jeder Pumpzylinder (62) einer der Kraftstoffeinspritzvorrichtungen (32) entspricht.
7. Kraftstofförderungssteuersystem nach Anspruch 1, dadurch gekennzeichnet, daß der Kraftstoff durch die Einspritzvorrichung (32) direkt in einen Zylinder des Motors eingespritzt wird und daß die Pumpeinrichtung (12) eine Hochdruckpumpeinrichtung ist, die in der Lage ist, Kraftstoffdrücke von wenigstens etwa 700 bar (10000 psi) zu liefern.
8. Kraftstofförderungssteuersystem nach Anspruch 1, dadurch gekennzeichnet, daß die Bypass-Steuerventileinrichtung (34) und die Einspritzvorrichtung (32) in einem gemeinsamen Gehäuse untergebracht sind.
9. Kraftstofförderungssteuersystem nach Anspruch 8, dadurch gekennzeichnet, daß die Bypass-Steuerventileinrichtung (34) ein normalerweise offenes Verschlußstück (40) und einen elektromagnetischen Stellantrieb enthält, der auf das elektrische Steuersignal anspricht, um das Verschlußstück (40) in weniger als einer Millisekunde aus seiner offenen Position in seine geschlossene Position zu bewegen.
10. Kraftstofförderungssteuersystem nach Anspruch 9, dadurch gekennzeichnet, daß das Verschlußstück (40) der Bypass-Steuerventileinrichtung (34) aus seiner geschlossenen Position in seine offene Position bei Beendigung des elektrischen Steuersignals durch eine Öffnungskraft in weniger als einer Millisekunde bewegt wird, wobei die Öffnungskraft durch den Druck des Kraftstoffes und unabhängig von mechanischen Vorspannkräften geliefert wird.
EP85630105A 1984-08-14 1985-07-05 Fördermengensteuersystem Expired EP0174261B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US64064084A 1984-08-14 1984-08-14
US640640 1991-01-14

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EP0174261A1 EP0174261A1 (de) 1986-03-12
EP0174261B1 true EP0174261B1 (de) 1989-01-11

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Families Citing this family (7)

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Publication number Priority date Publication date Assignee Title
DE3910793C2 (de) * 1989-04-04 1996-05-23 Kloeckner Humboldt Deutz Ag Brennstoffeinspritzvorrichtung
DE4106015A1 (de) * 1991-02-26 1992-08-27 Ficht Gmbh Druckstoss-kraftstoffeinspritzung fuer verbrennungsmotoren
EP0507191B1 (de) * 1991-04-04 1994-09-21 Toyota Jidosha Kabushiki Kaisha Kraftstoffeinspritzvorrichtung einer Brennkraftmaschine
EP0630442B1 (de) * 1992-03-04 1996-12-27 Ficht GmbH & Co. KG Kraftstoff-einspritzvorrichtung nach dem festkörper-energiespeicher-prinzip für brennkraftmaschinen
DE19963390A1 (de) * 1999-12-28 2001-07-05 Bosch Gmbh Robert Kraftstoffeinspritzeinrichtung für Brennkraftmaschinen
DE102006014767A1 (de) * 2006-03-30 2007-10-04 Robert Bosch Gmbh Kraftstoffeinspritzeinrichtung für eine mehrzylindrige Brennkraftmaschine
CN110748446B (zh) * 2019-11-27 2024-10-01 英嘉动力科技无锡有限公司 一种共轨高压进出油阀组件及共轨高压供油泵

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US3851635A (en) * 1969-05-14 1974-12-03 F Murtin Electronically controlled fuel-supply system for compression-ignition engine
US4258674A (en) * 1979-03-28 1981-03-31 Wolff George D Engine fuel injection system

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GB539116A (en) * 1939-03-27 1941-08-28 Sulzer Ag Improvements in or relating fuel injecting apparatus for internal combustion engines
DE1003506B (de) * 1955-04-28 1957-02-28 Hanns Dieter Paschke Dipl Ing Kraftstoffeinspritzanlage
CH433865A (de) * 1965-07-14 1967-04-15 Max Prof Berchtold Kraftstoffeinspritzanlage für Verbrennungsmotoren
DE2012485A1 (de) * 1969-05-07 1971-01-14 Technische Hochschule Otto von Guencke Magdeburg, χ 3010 Magdeburg Hydraulische Druckstoß Einspntzvor richtung mit Vor und Haupteinspritzung, insbesondere fur Dieselmotoren
GB2110300A (en) * 1981-11-27 1983-06-15 Lucas Ind Plc Fuel injection system for a compression ignition engine

Patent Citations (2)

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Publication number Priority date Publication date Assignee Title
US3851635A (en) * 1969-05-14 1974-12-03 F Murtin Electronically controlled fuel-supply system for compression-ignition engine
US4258674A (en) * 1979-03-28 1981-03-31 Wolff George D Engine fuel injection system

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JPS61106970A (ja) 1986-05-24
EP0174261A1 (de) 1986-03-12
DE3567506D1 (en) 1989-02-16

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