EP0014142A1 - Einspritzventil mit elektronischer Regelung - Google Patents

Einspritzventil mit elektronischer Regelung Download PDF

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Publication number
EP0014142A1
EP0014142A1 EP80400086A EP80400086A EP0014142A1 EP 0014142 A1 EP0014142 A1 EP 0014142A1 EP 80400086 A EP80400086 A EP 80400086A EP 80400086 A EP80400086 A EP 80400086A EP 0014142 A1 EP0014142 A1 EP 0014142A1
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EP
European Patent Office
Prior art keywords
fuel
plunger
chamber
passages
metering
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.)
Granted
Application number
EP80400086A
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English (en)
French (fr)
Other versions
EP0014142B2 (de
EP0014142B1 (de
Inventor
Albert E. Sisson
Donald J. Lewis
Richard P. Walter
Louis R. Erwin
Charles R. Kelso
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Honeywell International Inc
Original Assignee
Bendix Corp
AlliedSignal Inc
Priority date (The priority date 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 date listed.)
Filing date
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Priority claimed from US06/006,949 external-priority patent/US4235374A/en
Priority claimed from US06/006,948 external-priority patent/US4281792A/en
Application filed by Bendix Corp, AlliedSignal Inc filed Critical Bendix Corp
Priority to AT80400086T priority Critical patent/ATE4737T1/de
Publication of EP0014142A1 publication Critical patent/EP0014142A1/de
Application granted granted Critical
Publication of EP0014142B1 publication Critical patent/EP0014142B1/de
Publication of EP0014142B2 publication Critical patent/EP0014142B2/de
Expired legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • 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
    • F02M59/30—Varying fuel delivery in quantity or timing with variable-length-stroke pistons
    • 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
    • F02M57/023—Injectors structurally combined with fuel-injection pumps characterised by the pump drive mechanical
    • F02M57/024—Injectors structurally combined with fuel-injection pumps characterised by the pump drive mechanical with hydraulic link for varying the piston stroke
    • 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
    • F02M59/32—Varying fuel delivery in quantity or timing fuel delivery being controlled by means of fuel-displaced auxiliary pistons, which effect injection
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00—Engines characterised by air compression and subsequent fuel addition
    • F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition

Definitions

  • the invention relates to a fuel injector and to a method of electronically operating a fuel injector.
  • Fuel injection systems which employ hydraulic adjustment means to alter the timing of the injection phase of the cycle of operation of a set of injectors mechanically driven from the crankshaft of an internal combustion engine, and the hydraulic means may be responsive to the speed of the engine and/or the load imposed thereon. While the prior art systems functioned satisfactorily in most instances, several operational deficiencies were noted. For example, the hydraulic adjustment means functioned effectively over a relatively narrow range of speeds, and responded rather slowly to changes in the operating parameters of the engine. Also, problems were encountered in sealing the hydraulic adjustment means, for a rotor-distributor pump was utilized to deliver hydraulic fluid to each of the fuel injectors in the set employed within the fuel injection system.
  • timing phase, and the subsequent injection phase, of the cycle of operation can be easily altered in dependence upon any of one or more parameters of engine operation, utilizing existing control units, which respond rapidly to several engine parameters in addition to engine speed and load, and generate appropriate signals for an electronically controlled valve associated with the fuel injector.
  • the invention proposes .a fuel injector adapted to be disposed in timed operative relationship to the combustion chamber of an internal combustion engine in response to an electronic control unit, characterized in that it comprises a body having an axially extending central bore, a primary pumping plunger and a secondary plunger positioned within said bore for axial movement therein, a nozzle situated at the end of said central bore remote from said primary pumping plunger, a timing chamber defined in said body between said primary pumping plunger and said secondary plunger bore, a metering chamber defined in said bore between-said secondary plunger and said nozzle, passages in said body of said injector for receiving pressurized fuel and transmitting said fuel into said timing chamber and said metering chamber, and electronically operated control valve means situated intermediate said passages and said timing chamber and adapted to be selectively energized by the electronic control unit to regulate the timing of the discharge of fuel from the metering chamber through the nozzle, and to regulate the quantity of fuel discharged through the nozzle, and to control the quantity of fuel stored
  • the invention proposes a method of electronically operating a fuel injector, adapted to be disposed in operative relationship to a combustion chamber of an internal combustion engine in response to an electronic control unit, said injector including a body having an axially extending bore, a primary pumping plunger and a secondary plunger positioned therewithin for axial movement, a nozzle situated at one end of the bore remote from the primary pumping plunger, a timing chamber defined in said bore between said plungers, a metering chamber defined in said bore between said secondary plunger and said nozzle, passages in said body for introducing fuel into said chambers, and electronically operated control valve means situated intermediate said passages and said timing chamber, characterized in that said method comprises the steps of :
  • the present invention obviates the prior art problems of sealing hydraulic flow lines, utilizing a pump-distributor for sequentially feeding each injector within an injection system, and flexing of the fluid lines. Also, the present arrangement provides a simple and less costly approach.
  • Figure 1 schematically depicts the major components of a fuel injection system employing an electronically operated control valve for regulating the timing and metering functions of each injector within the system.
  • the system includes a fuel injector 10 that is supported by a support block 12 and is controlled to deliver fuel through a nozzle 14 directly into the combustion chamber (not shown) of an internal combustion engine 16.
  • a fuel injector 10 is operated in synchronism with the operation of the engine through the reciprocal actuation of a follower 20, the follower 20 being biased upwardly by a heavy duty spring 18.
  • a cam 22 is secured to the camshaft 24 of the internal combustion engine 16.
  • Cam 22 rotates at a speed which is a function of engine speed, for the camshaft is driven via meshing gears 23, 25 from the crankshaft 26.
  • the gear ratio of gears 23, 25 may vary from engine to engine depending on various factors, including, inter alia, whether the engine is a two-cycle or four-cycle engine.
  • the crankshaft drives the pistons (not shown) within the combustion chambers of the engine 16 in the usual manner.
  • a roller 27 rides along the profile of the cam, and a push rod 28 and rocker arm 30 translate the movement of the follower into the application of axially directed forces upon the follower 20 and the primary piston ; the forces act in opposition to main spring 18 and vary in magnitude with the speed of the engine and the profile of the cam.
  • the cam profile is of particular importance to the operation of the injector and will be discussed more fully in the discussion of Figures 8 and 9.
  • a reservoir 32 serves as a source of supply for the fuel to be dispensed by each injector 10, and fuel is withdrawn from the reservoir by transfer pump 34.
  • Filters 36, 38 remove impurities in the fuel, and distribution conduit 40 introduces the fuel, at supply pressure, to each of the injectors 10.
  • a branch conduit 42 extends between distribution conduit 40 and block 12 and makes fuel, at supply pressure, available for circulation through injector 10. The fuel that is not dispensed into a combustion chamber in the engine is returned to the reservoir 32 via branch return conduit 44 and return conduit 46.
  • a fixed orifice 48 is disposed in return conduit 46 to control rate of return flow into the reservoir.
  • Directional arrows and legends adjacent to the conduits indicate the direction of fuel flow.
  • the fuel injection system of Figure 1 responds to several parameters of engine performance.
  • engine speed which is reflected in the rate of rotation of the cam 22 secured upon camshaft 24
  • sensors 50 are operatively associated with engine 16 to determine, inter alia, engine speed, temperature, manifold absolute pressure, load on the engine, altitude, and air-fuel ratio.
  • the sensors 50 generate electrical signals representative of the measured parameters, and deliver the electrical signals to an electronic control unit, or ECU, 52.
  • the electronic control unit compares the measured parameters with reference values which may be stored within a memory in the unit, takes into account the rotational speed and angular position of cam 22, and generates a signal to be delivered to each injector.
  • the signal in turn, governs the timing and metering functions of each injector.
  • Leads 54, 56 and a connector 58 interconnect the electronic control unit 52 and the control valve 146 for the representative injector shown in Figure 1.
  • Figure 2 depicts the components of a representative injector 10. The segment at the left hand side of Figure 2 fits atop the segment at the right hand side of Figure 2.
  • a primary pumping plunger 62 is joined to the lower end of follower 20, the follower 20 and primary pumping plunger 62 moving as a unitary member.
  • a cylindrical guide 64 insures the axial movement of follower 20, while a seal guide 66 provides a seal and insures the axial movement of primary pumping plunger 62. It is to be understood that block 12 and guides 64, 66 may be formed as an integral unit.
  • a slot 68 in the follower 20 cooperates with stop 60 to prevent the follower 20 and spring 18 from becoming disassembled from the remainder of the injector prior to association with the cam 30 and to limit the downward travel of follower 20.
  • An internally threaded jacket 70 is screwed into engagement with the mounting block 12, and the interior of the jacket surrounds the distinct segments that comprise the body of the fuel injector 10.
  • Each segment of the body is generally cylindrical in shape, is generally executed in metal, has a central bore and has passages drilled, or otherwise formed therethrough, in alignment with the central bore and the passages of the adjacent segment.
  • fuel injector 10 includes an elongated sleeve 72, a disc-like segment 74, and a spring cage 76 that communicates with nozzle 14.
  • a seal 78 seals the juncture between the block 12 and the threaded jacket 70.
  • Supply passages 80, 82 of which there are two pairs of each, only one each of which are shown, extend through the various segments, and an annnular cavity 84 is defined beneath the seal guide 66 and the upper end of the axial passages.
  • the lowermost ends of passages 80, 82 extend radially inwardly to terminate in annulus 83.
  • the passages 80, 82 (a total of four passages arranged around piston 62) also extend radially inwardly to terminate in annulus 85, spaced above annulus 83 in the sleeve of the injector.
  • a cylindrical recess 86 is located in the lower end of the primary pumping plunger 62, and a stud 88 is located whithin the recess to form a spring retaining member.
  • a secondary plunger 90 is axially movable within the central bore of the sleeve 72, and a valve seat insert 92, with a recess 94 in its upper surface, is situated at the upper end of the secondary plunger.
  • a spring 96 extends between stud 88 and the insert 92 and constantly maintains a downwardly directed biasing force upon the secondary plunger.
  • a variable volume timing chamber 98 is defined between the lower end of plunger 62 and the upper end of secondary plunger 90. Secondary plunger 90 slides freely within the bore of sleeve 72 and primary plunger 62 travels within the bore 97 of support block 12.
  • a passage 99 extends axially through the valve seat insert 92 to communicate with cross-hole passage 100 which opens into annulus 102 formed on the surface of secondary plunger 90.
  • a first check valve 104 preferably in the form of a poppet valve, is normally biased by spring 106 against a valve seat 108 formed in passage 100 to control fluid communication between chamber 98 and passage 100. The spring 106 is seated in a guide cavity 110 in the secondary plunger 90.
  • An annulus 112 is formed in the outer surface of secondary plunger 90 at approximately the mid-section thereof, annulus 112 communicating with a cross-hole passage 114 and an axial passage 116.
  • a second check valve 118 in the secondary-plunger is biased against its valve seat 120 by a spring 121 disposed in a cavity 122 formed in the plunger 90.
  • Valve 118 thus controls communication between passage 116 and inverted L-shaped passages 124, 126, of which there are two each, which extend axially through the lower end of the secondary plunger.
  • the passages open into an annulus 125 formed in the exterior surface of plunger 90.
  • a variable volume metering chamber 128 is defined between the lower end of secondary plunger 90 and the disc-like segment 74.
  • a disc 130 fits within a recess 132 at the upper end of segment 74, and the disc is of sufficient area to seal off one end of metering chamber 128 to prevent gases in the cylinders in the engine from blowing back into the injector in the event the nozzle 14 fails to seal.
  • the recess 132 opens downwardly into a plurality of passages 134, 136, sets of which are arranged circumferentially around the central axis of injector 10, passage 136 commrnunicating with nozzle 14.
  • a needle valve 144 is secured to a spring retaining member 142, and a spring 138 is disposed between element 74 and member 142 to bias valve 144 downwardly against a valve seat 145 to prevent fuel from being dispensed from the nozzle 14. Only when the pressure in passage 136 significantly exceeds the combined forces of the spring biasing pressure and the supply pressure is the needle valve unseated t Q permit a fine atomized spray of fuel to be issued from nozzle 14.
  • Branch conduit 42 introduces fuel, at supply pressures of 3,5 to 14 kg/cm 2 , into support block 12 through conduit 43 and thence into injector 10.
  • An electronically operated control valve 146 is disposed between conduit 42 and conduit 43 to control both the timing and the metering functions for injector 10 as will be more fully explained hereafter.
  • Branch conduit 43 as suggested by the diagonally extending dotted lines, communicates fuel at supply pressure with timing chamber 98 when the control valve 146 is open.
  • control valve 146 is shown in its normally opened condition to allow fuel at supply pressure in the branch conduit 42 access to supply passage 43 and the timing chamber 98.
  • an equilibrium pressure condition exists (supply pressure) as the primary plunger 62 has ceased its upward motion and is - prepared to start its downward motion due to the action of camshaft 24 and cam 22 on plunger 62 as will be seen from a description of Figures 8 and 9.
  • the timing chamber 98 and metering chamber 128 previously have been filled with fuel as will be seen from a description of Figures 6 and 7.
  • check valve 104 is biased against its seat by spring 106 and check valve 118 is biased against its seat by spring 121.
  • timing chamber 98 is in its equilibrium condition, so that when rocker arm 30 forces follower 20 and primary pumping plunger 62 downwardly, at the rate suggested by the arrow beneath plunger 62, fuel is forced out of timing chamber 98 through passages 43, 42.
  • the secondary plunger is unaffected by such movement and remains stationary under the bias of spring 96 and trapped fluid in metering chamber 128.
  • the duration of the period during which valve 146 is maintained in its opened condition relative to a fixed reference is a variable quantity determined by the electronic control unit 52 in response to actual engine conditions and independent of the travel of plunger 62.
  • the instant at which the valve 146 is closed, and the timing chamber 98 isolated from the supply passage 42 can be adjusted relative to the fixed reference, e.g., the top dead center (TDC) position of the crankshaft 26, over fairly broad limits.
  • TDC top dead center
  • Figure 4 shows the various components of the fuel injector 10 at the instant that injection starts through nozzle 14 due to the high pressure (several hundred kg/em 2 ) created by the trapped fluid in timing chamber 98 and metering chamber 128.
  • the valve 146 is closed as described above. With the valve closed, timing chamber 98 is sealed, and the continued downward movement of plunger 62 causes the downward movement of secondary plunger 90 to rapidly increase the pressure of the fuel trapped in chamber 128.
  • the downward movement of the secondary plunger 90 pressurizes the fuel in chamber 128 to a level sufficient to unseat needle valve 144 and permits a fine spray of pressurized fuel to be discharged through the pin holes in nozzle 14.
  • the second check valve 118 remains seated during the injection phase of the cycle of operation due to the fact that the high pressure below check valve 118 created by the pressure in metering chamber 128, as communicated thereto by passages 124, 126, is greater than the supply pressure in passages 80, 82 and cross-hole 114.
  • FIG 5 shows the various components of the fuel injector immediately after the termination of the injection shown in Figure 4, Figure 5 illustrating the "dumping" or pressure relieving phase of operation.
  • the control valve 146 is still closed and the primary pumping plunger 62 is approaching its limit of downward travel, as suggested by the small arrow beneath the plunger.
  • the annulus 125 is in fluid communication with annulus 83 thereby communicating the high pressure in passages 124, 126, 136 wit ⁇ the supply pressure in passages 80, 82.
  • the pressure on the needle valve is insufficient to hold valve 144 oppen and the needle valve 144 is again seated against seat 145.
  • the pressure build-up in passage 136 and metering chamber 128 is rapidly relieved, so that the undesirable dribble of fuel through the nozzle is prevented.
  • the pressure of the fuel in timing chamber 98 which has been intensified by the downward movement of plunger 62, is relieved to permit the primary plunger 62 to complete its downward travel after the termination of injection and precludes excess pressure on the parts of the injector subject to the pressure in timing chamber 98.
  • the annulus 102 is in fluid communication with annulus 85 thereby communicating passage 100 below valve 104 with the supply pressure in passages 80, 82.
  • the pressurized fuel in chamber 98 as compared to supply pressure in passage 100, creates a pressure differential across first check valve 104 to unseat check valve 104. Fuel flows from timing chamber 98, through check valve 104, annulus 102, and annulus 85 back into axial passages 80, 82.
  • Check valve 104 has been provided to check the flow of fuel from passage 80 to timing chamber 98, through annuli 85, 102, just prior to the metering phase of operation. If valve 104 did not seat, fuel flow from passage 80 to timing chamber 98 would preclude the metering to be described below.
  • Figure 6 shows the various components of the fuel injector after the primary pumping plunger 62 has completed its downward travel and has started its upward travel under the urging of spring 18 to create the "metering"phase of operation.
  • the control valve 146 is retained in its closed condition, and annulus 102 is out of communication with annulus 85, thereby sealing timing chamber 98.
  • the fuel in timing chamber 98 is approximately at supply pressure due to the dumping shown in Figure 5.
  • First check valve 104 which was unseated during the "dumping" phase of the cycle of operation, as shown in Figure 5 is again held against its seat 108 by spring 106 to prevent communication between chamber 98 and passage 100.
  • the quantity of fuel that flows into metering chamber 128 is proportional to the volumetric displacement of plunger 90 created by the pressure differential across plunger 90.
  • the plunger 90 can only move in concert with plunger 62 while control valve 146 is closed.
  • the quantity of fuel introduced into the metering chamber 128 is proportionally related to the duration or interval, in crankshaft degrees, during which the control valve 146 is held closed after the start of the upward travel of secondary plunger 90. Obviously, when the valve 146 is held closed by a signal from the electronic control unit 52 for the entire interval in crankshaft degrees allocated for metering, the chamber 128 will be filled with the maximum amount of fuel.
  • valve 146 When the valve 146 is held closed by a signl from the electronic control unit for only half of the interval, defined in degrees of crankshaft rotation, then the metering chamber will be half filled. Other proportional relationships are available in accordance with the fraction of the crankshaft rotational interval selected to hold valve 146 closed. This proportionallity will become more apparent during the discussion of Figures 8 and 9.
  • Figure 7 shows the various components of the fuel injector at the termination of the metering phase of the cycle of operation.
  • the metering phase is terminated by terminating the electricl signal from electronic control unit 52 to the control valve 146, which then returns to its normally opened condition.
  • valve 146 opened the fuel at supply pressure in passages 42, 43 and the fuel in timing chamber 98 quickly establish an equilibrium condition at approximately supply pressure level.
  • the pressure differential across plunger 90 is removed and secondary plunger 90 is, in effect, disconnected and cannot follow primary pumping plunger 62 as plunger 62 continues its upward movement.
  • valve 146 opened the combined forces of the fuel in timing chamber 98 and spring 96 are greater than the force of the fuel, at supply pressure, retained in metering chamber 128.
  • plunger 90 is "locked” or retained in fixed position.
  • the instant at which the signal to valve 146 is terminated is determined by engine operating parameters sensed by the electronic control unit relative to the number of degrees of angular rotation of the camshaft 24 as measured by the crankshaft 26 rotation from the above-described fixed reference, as determined by conventional sensors.
  • Primary pumping plunger 62 continues upwardly, following the cam surface, under the urging of spring 18 independently of secondary plunger 90, as suggested by the arrow atop follower 20 in Figure 7.
  • primary pumping plunger 62 reaches its uppermost position, as shown in Figure 3, then the cycle of operation for the fuel injection can be repeated in the manner shown progressively in Figures 3 to 7.
  • Figure 8 illustrates, in graphic form, the profile, or lift, of the cam surface of cam 22 (Fig. 1) relative to the number of degress of crankshaft rotation
  • Figure 9 illustrates, in graphic form, the vertical motion of primary pumping plunger 62 relative to the same number of degrees of crankshaft rotation and the relationship thereto of the single electronic control unit pulse which initiates injection and terminates metering.
  • Both figures, Figure 9 particularly, correlate the various phases of injector operation described in conjunction with the description of Figures 3 to 7 with degrees of crankshaft rotation.
  • a very graphic illustration of the proportionallity of the metering phase may be seen.
  • the termination of the electronic control unit pulse to control valve 146 will be seen to be linearly related to the'number of degrees of crankshaft rotation after a preselected reference point (for example, tcpdead center).
  • FIG. 8 there is illustrated the lift of the cam, or cam profile surface plotted against the number of degrees of crankshaft rotation, and includes various points (A, B, C, D) along_the curve.
  • the curve approaches point A, which is the lowest point of the curve, and will be seen to correspond to the arbitrarily selected starting position described in conjunction with the description of Figure 3.
  • the curve progresses through the injection phase, between points B and C ; the dumping phase, between points C and D; and the metering phase, between points D and E.
  • Point E corresponds to the end of the metering phase and a point F corresponds for the next sequence to point A for the previous sequence.
  • Figure 9 is a ,composite graphic representation of the operation of one injector 10 in the set of injectors employed in the instant fuel injection system.
  • the upper graph plots the movement, or stroke, of primary pumping plunger 62 along the vertical axis against the degrees of rotational movement of the crankshaft 26 ; the rotational movement being measured by_sensors that provide a signal representative of crankshaft rotation in degrees.
  • the trace of the plunger 62 shows that the plunger instantaneously peaks, then moves downwardly until it reaches a nadir position, and then linearly returns upwardly to the peak position.
  • a complete cycle occurs within 360° of rotational movement of the crankshaft ; for a four cycle engine, a complete cycle occurs within 720° of rotational movement of the crankshaft.
  • The'lower graph in Figure 9 plots the opening and closing of control valve 146 by the electronic control unit, and other events, against the degrees of rotational movement of the crankshaft 26.
  • the leading edge of the signal to control valve 146 causes the valve to change state from its normally opened state to its closed state, and the trailing edge of the signal causes the valve to change state again and return to its normally opened position.
  • a single pulse from the electronic control unit initiates the injection phase and terminates the metering phase, while the internal configuration of the injector (annuli, check valves, etc.) terminates the injection phase and initiates the metering phase.
  • the upper and lower graphs of Figure 9 may be correlated by following the progression of steps indicated by reference characters A, B, C, D, E and F. It is to be understood that the duration of the period A to D, in degrees, is determined by the sum of injection timing variation and injection duration. It is believed that the determination of the duration of the period A to D is well within the scope of one skilled in the art.
  • the plunger 62 assumes its peak upward position under the bias of main spring 18 at the start of the cycle of operation ( Figure 3). This is point A on the curve and, with the control valve 146 still in its normally opened state, as seen at the bottom of Figure 9, the plunger 62 starts downwardly under the force of rocker arm 30 pressing against follower 20.
  • the electronic control unit 52 delivers a signal to valve 146, and closes the valve as described in conjunction with the description of Figure 4.
  • Point B on the curve designates the instant at which injection occurs during the timing function due to the closing of the valve 146, while point C indicates when the injection ceases due to the communication of annuli 102, 85 as described in conjunction with the description of Figure 5.
  • the electronic control unit can be adjusted, either manually or automatically, in accordance with actual engine operating parameters, to shift the timing of the leading edge of the signal relative to the downward movement of the plunger 62. Point B will then shift along the curve to reflect such adjustments.
  • the ability to adjust the instant at which valve 146 is closed to start the injection function assists in more completely burning the fuel discharged into each combustion chamber in the engine 16.
  • the closure of valve 146 starts the injection phase of the cycle of operation as shown in Figure 4.
  • the compression-injection phase of the cycle of operation lasts for the brief interval B-C, the length of which is determined by the quantity of fuel which has been metered into metering chamber 98.
  • the secondary plunger follows the primary plunger downwardly and forces the fuel out of metering chamber 128 and through nozzle 14.
  • the plungers are coupled through the sealed timing chamber 98 which forms a hydraulic link between the two plungers.
  • Point C on the curve designates the cessation of the injection phase of the cycle of operation and the period between points C-D represents the overtravel and dumping portion of the cycle.
  • the passages 124 and 126 in the secondary plunger 90 are in fluid communication with the annuli 125, 83 to communicate metering chamber 128 and passage 136 with the supply pressure in passages 80, 82 and vent, or dump, the pressurized fuel trapped in the metering chamber 128 and the nozzle 14 back into the low pressure of axial passages 80, 82.
  • the venting of the nozzle enables the needle valve to be re-seated and prevent dribble of fuel through the nozzle into the combustion chamber.
  • the downward travel of the primary pumping plunger 62 continues for the interval C-D, or until the plunger 62 reaches its maximum travel.
  • the overtravel of the plunger 62 beyond the termination of injection (point C) and end of dumping (point D) provides sufficient time to equalize the pressures in the injector at supply pressure and to provide the necessary range of timing and injection.
  • point D the nadir of travel, and then starts to travel upwardly under the urging of main spring 18, its return trip to its peak upward position occurs over a major portion of the cycle of operation which corresponds to the metering phase ( Figures 6 and 7).
  • the curve from point D through points E and F is a linear curve having a constant slope.
  • the linear slope is achieved by a unique profile on the cam 22, which slope is important to the proportional operation of the metering phase of operation.
  • Point E represents the instant that the metering function ceases and corresponds to the termination of the signal from the electronic control unit.
  • the termination of the signal to control valve 146 causes the control valve to return to its normally opened condition, which allows the timing chamber 98 to reach an equilibrium condition with the fuel at supply pressure in passage 42.
  • Spring 96 locks secondary plunger 90 in fixed position in metering chamber 128, and plunger 62 can move independently in response to the application of forces by rocker arm 30_and spring 18. This termination is described in conjunction with the description of Figure 7.
  • the metering function can be terminated at any point along the slope D-F ; if the metering function is terminated shortly after the primary plunger starts its return trip, then the interval D-E will be shorter than the interval from E-F. The greater the interval D-E, the greater the volume of fuel admitted into metering chamber 128. It is to be noted that the linearity of the portion of the curve between points D and F permits a direct, proportional relationship between the amount of fuel metered and the number of degrees of camshaft rotation.
  • the interval, in degrees of rotation, between points D and F represents the maximum volume of fuel which can be metered, any lesser amount is a direct function (proportional) to the number of degrees of rotation the control valve remains closed after point D. Thus, if point E occurs one-half the number of degrees between D and F, one-half the quantity of fuel is metered.
  • the metering function can occur, potentially, over more than half the cycle of operation. This "stretching out" of the metering function increases the opportunity to accurately fill the metering chamber 128 to the desired level.
  • the slope of the curve D.:..F through the metering function is linearly proportional to the degrees of angular rotation of the crankshaft 26.
  • the primary pumping plunger 62 and follower 20 could be formed as a unitary plunger, and the check valves 104, 112, which are preferably shown as poppet valves, could be disc valves, ball valves, etc.
  • the control valve 146 which is shown as a gate valve responsive to electromagnetic forces, could assume diverse other forms.
  • the profile of cam 22 can also be altered to adjust the duration of the metering function and the rate of return of the primary plunger 62.
  • the spring 96 could be joined to the central bore of the injector, and need not have one end seated in a cavity in the primary pumping plunger ; the key consideration is the ability of the spring 96 to always exert a downward force on the secondary plunger and, when necessary, at the end of the metering operation, lock plunger 90 in fixed position.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
EP80400086A 1979-01-25 1980-01-21 Einspritzventil mit elektronischer Regelung Expired EP0014142B2 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT80400086T ATE4737T1 (de) 1979-01-25 1980-01-21 Einspritzventil und verfahren zur elektronischen betaetigung eines einspritzventils.

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US06/006,949 US4235374A (en) 1979-01-25 1979-01-25 Electronically controlled diesel unit injector
US6949 1979-01-25
US06/006,948 US4281792A (en) 1979-01-25 1979-01-25 Single solenoid unit injector
US6948 1979-01-25

Publications (3)

Publication Number Publication Date
EP0014142A1 true EP0014142A1 (de) 1980-08-06
EP0014142B1 EP0014142B1 (de) 1983-09-21
EP0014142B2 EP0014142B2 (de) 1989-06-21

Family

ID=26676279

Family Applications (1)

Application Number Title Priority Date Filing Date
EP80400086A Expired EP0014142B2 (de) 1979-01-25 1980-01-21 Einspritzventil mit elektronischer Regelung

Country Status (7)

Country Link
EP (1) EP0014142B2 (de)
AU (1) AU535759B2 (de)
BR (1) BR8000300A (de)
DE (1) DE3064859D1 (de)
ES (1) ES487024A1 (de)
SU (1) SU1135433A3 (de)
UA (1) UA5760A1 (de)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0055654A1 (de) * 1980-12-17 1982-07-07 The Bendix Corporation Verteilerpumpe mit durch Einzelelektroventil gesteurtem Freikolben
FR2500566A1 (fr) * 1981-02-23 1982-08-27 Cummins Engine Co Inc Soupape de commande notamment pour injecteur de carburant
EP0067369A2 (de) * 1981-06-12 1982-12-22 Robert Bosch Gmbh Kraftstoffeinspritzeinrichtung für Brennkraftmaschinen
EP0068924A2 (de) * 1981-06-23 1983-01-05 Allied Corporation Kraftstoffeinspritzpumpe
EP0070222A1 (de) * 1981-07-13 1983-01-19 The Bendix Corporation Druck-Zeit gesteuertes Einspitzventil
EP0091862A1 (de) * 1982-04-02 1983-10-19 The Bendix Corporation Durch Einzelsolenoid gesteuerte Pumpen/Düsen-Einheit mit Doppelablass
EP0095026A1 (de) * 1982-03-25 1983-11-30 Deere & Company Pumpen-Düsen-Einheit mit durch Hülsenventil gesteuertem Freikolben für Brennkraftmaschinen
EP0260720A2 (de) * 1986-09-19 1988-03-23 Cummins Engine Company, Inc. Hochdruckpump-Düseneinheit
GB2252135A (en) * 1991-01-14 1992-07-29 Bosch Gmbh Robert Fuel injection pump for supplying fuel and a further liquid to diesel engines
EP0629776A1 (de) * 1993-06-03 1994-12-21 Cummins Engine Company, Inc. Kraftstoffeinspritzventil für Verbrennungsmotor
CN103850846A (zh) * 2012-11-29 2014-06-11 谈世新 靶式喷油点火器

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006021736A1 (de) * 2006-05-10 2007-11-15 Robert Bosch Gmbh Kraftstoffinjektor mit druckausgeglichenem Steuerventil

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE231352C (de) *
DE459676C (de) * 1925-09-19 1928-05-10 Fried Krupp Germaniawerft Akt Brennstoffeinspritzpumpe fuer Dieselmaschinen mit Iuftloser Einspritzung
AT195685B (de) * 1954-12-28 1958-02-25 Wilhelm Schneider Einspritzpumpe für Brennkraftmaschinen
US2843043A (en) * 1954-06-15 1958-07-15 Schneider Wilhelm Injection pumps
DE2131841B2 (de) * 1971-06-26 1973-06-14 Maschinenfabrik Augsburg Nürnberg AG, 8900 Augsburg Vorrichtung zur steuerung der brennstoffeinspritzung bei brennkraftmaschinen
US4129253A (en) * 1977-09-12 1978-12-12 General Motors Corporation Electromagnetic unit fuel injector
US4134549A (en) * 1974-05-30 1979-01-16 Cummins Engine Company, Inc. Injectors of a fuel supply system for an internal combustion engine
DE2854921A1 (de) * 1977-12-21 1979-07-05 William H Leckie Brennstoff-einspritzvorrichtung

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE231352C (de) *
DE459676C (de) * 1925-09-19 1928-05-10 Fried Krupp Germaniawerft Akt Brennstoffeinspritzpumpe fuer Dieselmaschinen mit Iuftloser Einspritzung
US2843043A (en) * 1954-06-15 1958-07-15 Schneider Wilhelm Injection pumps
AT195685B (de) * 1954-12-28 1958-02-25 Wilhelm Schneider Einspritzpumpe für Brennkraftmaschinen
DE2131841B2 (de) * 1971-06-26 1973-06-14 Maschinenfabrik Augsburg Nürnberg AG, 8900 Augsburg Vorrichtung zur steuerung der brennstoffeinspritzung bei brennkraftmaschinen
US4134549A (en) * 1974-05-30 1979-01-16 Cummins Engine Company, Inc. Injectors of a fuel supply system for an internal combustion engine
US4129253A (en) * 1977-09-12 1978-12-12 General Motors Corporation Electromagnetic unit fuel injector
DE2854921A1 (de) * 1977-12-21 1979-07-05 William H Leckie Brennstoff-einspritzvorrichtung

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0055654A1 (de) * 1980-12-17 1982-07-07 The Bendix Corporation Verteilerpumpe mit durch Einzelelektroventil gesteurtem Freikolben
FR2500566A1 (fr) * 1981-02-23 1982-08-27 Cummins Engine Co Inc Soupape de commande notamment pour injecteur de carburant
EP0067369A3 (en) * 1981-06-12 1984-01-11 Robert Bosch Gmbh Fuel injection apparatus for internal-combustion engines
EP0067369A2 (de) * 1981-06-12 1982-12-22 Robert Bosch Gmbh Kraftstoffeinspritzeinrichtung für Brennkraftmaschinen
EP0068924A2 (de) * 1981-06-23 1983-01-05 Allied Corporation Kraftstoffeinspritzpumpe
EP0068924A3 (en) * 1981-06-23 1984-01-11 The Bendix Corporation Fuel injection pump
EP0070222A1 (de) * 1981-07-13 1983-01-19 The Bendix Corporation Druck-Zeit gesteuertes Einspitzventil
EP0095026A1 (de) * 1982-03-25 1983-11-30 Deere & Company Pumpen-Düsen-Einheit mit durch Hülsenventil gesteuertem Freikolben für Brennkraftmaschinen
EP0091862A1 (de) * 1982-04-02 1983-10-19 The Bendix Corporation Durch Einzelsolenoid gesteuerte Pumpen/Düsen-Einheit mit Doppelablass
EP0260720A2 (de) * 1986-09-19 1988-03-23 Cummins Engine Company, Inc. Hochdruckpump-Düseneinheit
EP0260720A3 (en) * 1986-09-19 1989-10-11 Cummins Engine Company, Inc. High pressure unit fuel injector
GB2252135A (en) * 1991-01-14 1992-07-29 Bosch Gmbh Robert Fuel injection pump for supplying fuel and a further liquid to diesel engines
GB2252135B (en) * 1991-01-14 1994-11-02 Bosch Gmbh Robert Fuel injection pump for diesel engines
EP0629776A1 (de) * 1993-06-03 1994-12-21 Cummins Engine Company, Inc. Kraftstoffeinspritzventil für Verbrennungsmotor
CN103850846A (zh) * 2012-11-29 2014-06-11 谈世新 靶式喷油点火器

Also Published As

Publication number Publication date
AU535759B2 (en) 1984-04-05
BR8000300A (pt) 1980-09-30
SU1135433A3 (ru) 1985-01-15
DE3064859D1 (en) 1983-10-27
EP0014142B2 (de) 1989-06-21
UA5760A1 (uk) 1994-12-29
AU5401479A (en) 1980-07-31
ES487024A1 (es) 1980-06-16
EP0014142B1 (de) 1983-09-21

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