GB2320292A - A method of operating an electronically-controlled unit fuel pump injector for an i.c. engine - Google Patents

A method of operating an electronically-controlled unit fuel pump injector for an i.c. engine Download PDF

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Publication number
GB2320292A
GB2320292A GB9801389A GB9801389A GB2320292A GB 2320292 A GB2320292 A GB 2320292A GB 9801389 A GB9801389 A GB 9801389A GB 9801389 A GB9801389 A GB 9801389A GB 2320292 A GB2320292 A GB 2320292A
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United Kingdom
Prior art keywords
fuel
injection
injector
storage chamber
valve
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
GB9801389A
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GB2320292B (en
GB9801389D0 (en
GB2320292A8 (en
Inventor
Dennis H Gibson
Gregory W Hefler
Ronald D Shinogle
Mark F Sommars
Howard N Cannon
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Caterpillar Inc
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Caterpillar Inc
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Publication date
Application filed by Caterpillar Inc filed Critical Caterpillar Inc
Priority claimed from GB9506193A external-priority patent/GB2289313B/en
Publication of GB9801389D0 publication Critical patent/GB9801389D0/en
Publication of GB2320292A publication Critical patent/GB2320292A/en
Publication of GB2320292A8 publication Critical patent/GB2320292A8/en
Application granted granted Critical
Publication of GB2320292B publication Critical patent/GB2320292B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M63/00Other 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
    • F02M63/0012Valves
    • F02M63/0014Valves characterised by the valve actuating means
    • F02M63/0015Valves characterised by the valve actuating means electrical, e.g. using solenoid
    • F02M63/0017Valves characterised by the valve actuating means electrical, e.g. using solenoid using electromagnetic operating means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M45/00Fuel-injection apparatus characterised by having a cyclic delivery of specific time/pressure or time/quantity relationship
    • F02M45/02Fuel-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
    • F02M45/04Fuel-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M47/00Fuel-injection apparatus operated cyclically with fuel-injection valves actuated by fluid pressure
    • F02M47/02Fuel-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
    • F02M47/027Electrically actuated valves draining the chamber to release the closing pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M57/00Fuel-injectors combined or associated with other devices
    • F02M57/02Injectors structurally combined with fuel-injection pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M57/00Fuel-injectors combined or associated with other devices
    • F02M57/02Injectors structurally combined with fuel-injection pumps
    • F02M57/022Injectors structurally combined with fuel-injection pumps characterised by the pump drive
    • F02M57/023Injectors structurally combined with fuel-injection pumps characterised by the pump drive mechanical
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M59/00Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/02Pumps 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
    • F02M59/10Pumps 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
    • F02M59/102Mechanical drive, e.g. tappets or cams
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M59/00Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/20Varying fuel delivery in quantity or timing
    • F02M59/36Varying fuel delivery in quantity or timing by variably-timed valves controlling fuel passages to pumping elements or overflow passages
    • F02M59/366Valves being actuated electrically
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M59/00Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/44Details, components parts, or accessories not provided for in, or of interest apart from, the apparatus of groups F02M59/02 - F02M59/42; Pumps having transducers, e.g. to measure displacement of pump rack or piston
    • F02M59/46Valves
    • F02M59/466Electrically operated valves, e.g. using electromagnetic or piezoelectric operating means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M63/00Other 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
    • F02M63/0012Valves
    • F02M63/0031Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
    • F02M63/0049Combined valve units, e.g. for controlling pumping chamber and injection valve
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M63/00Other 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
    • F02M63/0012Valves
    • F02M63/0059Arrangements of valve actuators
    • F02M63/0061Single actuator acting on two or more valve bodies
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/14Direct injection into combustion chamber
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Abstract

The method comprises the steps of: (1) opening fluid communication between a fixed-volume fuel storage chamber and a control passage; (2) closing fluid communication between the storage chamber and the fuel injection orifice(s); (3) displacing a variably-selected volume of fuel from the storage chamber to the control passage; (4) closing fluid communication between the storage chamber and the control passage; (5) displacing another variably-selected volume of fuel in the storage chamber and thereby pressurizing the fuel to a selected pressure; (6) opening fluid communication between the storage chamber and the fuel injection orifice(s) to begin fuel injection; and (7) closing fluid communication between the storage chamber and the fuel injection orifice(s) to end fuel injection.

Description

1 2320292 ELECTRONICALLY-CONTROLLED FLUID INJECTOR SYSTEM HAVING
PRE-INJECTION PRESSURIZABLE FLUID STORAGE CHAMBER AND DIRECT-OPERATED CHECK The present invention relates generally to fluid injection and, for example, more particularly to electronically-controlled fuel injectors.
Examples of conventional electronically-controlled fuel injection systems are shown in U.S. Patent No. 4,392,612 issued to Deckard et al. on 12 July 1983, U.S. Patent No. 5,094,215 issued to Gustafson on 10 March 1992, and U.S. Patent No. 5,156,132 issued to Iwanga on 20 October 1992.
In Deckard et al., the mechanical ly-actuated injector is constructed and operates in such a way so peak fuel injection pressure is drastically reduced as engine speed is reduced if fuel delivery (i.e., quantity during an injection cycle) is kept constant. The direct relationship between peak injection pressure and engine speed associated with this type of injector limits desirably higher fuel injection pressures to be attained at lower engine speeds and/or lighter loads. This consequently limits the engine's ability to achieve lower emissions, especially with respect to smoke or particulates.
In Gustafson, the injector has a conventional springloaded check which has a fixed valve closing pressure (VCP). A problem with a f ixed VCP is the time delay associated with closing the check as the fuel injection pressure bleeds down to the VCP. The time delay and pressure drop can cause poor atomization of fuel injected into the engine combustion chamber late in the combustion cycle. A sharper end of injection would be desirable for reducing emissions, especially particulates or smoke. Moreover in Gustafson, the injector also has a variablevolume fuel pressurization chamber 36 whose volume is 2 determined by a complex two-part plunger assembly 24 having a spring 38 as well as an external apparatus for varying the pressure of fuel supplied to the injector. Manufacturing variations in the spring rate as well as the variable pressure apparatus may cause imprecise control of the variable volume 36 resulting in imprecise control of the fuel injection quantity, peak fuel injection pressure and pressure decay or drop during an injection cycle.
In Iwanga, fuel injection pressure is used to assist closure of the movable check for ending fuel injection. One problem that may occur is unacceptably high impact loading of the check against the nozzle tip seat at high injection pressures thereby causing failure or breakage of the nozzle tip. Thus, peak fuel injection pressure is capability of the injector is undesirably limited.
In one aspect of the present invention, an electronically-controlled fluid injector system is disclosed comprising a fluid control passage, a fluid storage chamber, a first valve portion, a fluid pressurization member, at least one fluid injection orifice, a direct- operated check, and a second valve portion which may be separate or integral with the first valve portion. The first valve portion selectively opens and closes fluid communication between the storage chamber and the control passage. When the first valve portion is opened, the pressurization member selectively displaces a variably selected volume of fluid from the storage chamber to the control passage. When the first valve portion is closed, the pressurization member selectively displaces another variably selected volume of fluid trapped in the storage chamber thereby pressurizing such fluid to a variably selected pressure. The check selectively closes and opens fluid communication between the storage chamber and the fluid injection orifice. Injection of pressurized fluid occurs through the fluid injection orifice when the second valve portion causes hydraulic unbalancing of the check to open the check. Injection of pressurized fluid 3 ends when the second valve portion causes hydraulic balancing of the check allowing closure of the check.
In another aspect of the present invention, an electronically-controlled unit fluid pump injector is disclosed in which the above elements are unitized in a single housing assembly.
The present invention provides improved control of several fluid injection parameters resulting in improved engine performance and lower emissions, noise, and wear.
In the accompanying drawings:
Fig. 1 is a diagrammatic general schematic view of an electronicallycontrolled fuel injector system of the present invention.
Fig. 2 is a diagrammatic partial cross-sectional view of one embodiment of an injector of the present invention as installed in an exemplary internal combustion engine; Fig. 3 is a diagrammatic isolated enlarged crosssectional view of the injector shown in Fig. 2; Fig. 4 is a diagrammatic enlarged cross-sectional partial view of a first or upper portion of the injector shown in Fig. 3; Fig. 5 is a diagrammatic further enlarged crosssectional partial view of a second or intermediate portion of the injector shown in Fig. 3; Fig. 6 is a diagrammatic enlarged cross-sectional partial view of shown in Fig. 3; Fig. 7 is a diagrammatic enlarged cross-sectional partial view of Fig. 2 taken generally along line 7-7; Fig. 8 is a diagrammatic approximate graph of fuel injection pressure, P measured in megapascals, versus time, T measured in seconds, comparing predicted operation of a computer-simulated exemplary injector of the present invention versus actual operation of a bench-tested conventional electronically-controlled injector; Fig. 9 is a diagrammatic approximate graph of fuel injection pressure P versus time T comparing predicted a third or lower portion of the injector 4 operations of a computer-simulated exemplary injector of the present invention operating at three different exemplary injection pressures but delivering approximately the same quantity of fuel per injection; Fig. 10 is a diagrammatic approximate graph of cumulative fuel quantity Q versus time T showing predicted dual-type segmented injection operation during an injection cycle of a computer-simulated exemplary injector of the present invention; Fig. 11 is a diagrammatic approximate graph of fuel injection pressure P versus time T showing predicted operation corresponding to Fig. 10.
Fig. 12 is a diagrammatic approximate graph of cumulative fuel quantity Q versus time T showing predicted triple-type segmented injection operation during an injection cycle of a computer-simulated exemplary injector of the present invention; Fig. 13 is a diagrammatic approximate graph of fuel injection pressure P versus time T showing predicted operation corresponding to Fig. 12.
Referring to Figs. 1-7, wherein similar reference numerals designate similar elements or features throughout the Figs., there is shown an embodiment of an electronically-controlled fuel injection system 10 of the present invention (hereinafter referred to as an EUI-II fuel system).
The exemplary EUI-II fuel system 10 is shown in Figs. 1-2 as adapted for a direct-injection diesel-cycle reciprocating internal combustion engine 12. However, it should be understood that the present invention is also applicable to other types of engines, such as rotary engines or modified-cycle engines, and that the engine may contain one or more engine combustion chambers 14 or cylinders. The engine 12 has at least one cylinder head 16 wherein each cylinder head 16 defines one or more separate injector bores 18. The EUI-II fuel system 10 includes one or more electronically-controlled injectors 20 adapted to be positioned in a respective injector bore 18.
The EUI-II fuel system 10 further includes apparatus or means 22 for supplying fuel to each injector 20, apparatus or means 24 for actuating each injector, and apparatus or means 26 for electronically controlling each injector.
The fuel supplying means 22 preferably includes a fuel tank 28, a fuel supply passage 30 arranged in fluid communication between the fuel tank and the injector(s), a relatively low pressure fuel transfer pump 32, one or more fuel filters 34, and a fuel drain passage 36 arranged in fluid communication between the injector(s) 20 and the fuel tank 28. Preferably, each cylinder head 16 defines an internal fuel supply passage 38 which communicates with the annular fuel inlet 40 of each injector 20 associated with the cylinder head 16. Preferably, each cylinder head 16 defines an internal fuel drain passage 42 which communicates with the fuel outlet 44 of each injector associated with the cylinder head 16. Alternatively, the fuel supply passage 38 and the fuel drain passage 42 defined in the cylinder head 16 may be a single passage.
optionally, a sleeve 46 may be sealedly positioned in the injector bore 18 between the injector 20 and the cylinder head 16 to separate internal coolant chambers 48 of the cylinder head 16 from the injector 20.
The actuating means 24 may be any mechanically actuating-device or hydraulically-actuating device. In the embodiment shown, a tappet and plunger assembly 50 associated with the injector 20 is mechanically actuated indirectly or directly by a rotatable cam or cam lobe 52 mounted on an engine-driven camshaft 54.
The profile of the cam surface depends upon, inter alia, the desired timing of plunger movement, plunger stroke, type of cam follower, engine speed, and range of operating injection pressure. For example, the profile may include a plurality of segments including i) a f irst 6 segment 56 extending between points A to B for moving the pressurization member from its first position toward its second position; ii) a second segment 58 extending between points B to C for actuating the pressurization member during injection, iii) a third segment 60 extending between points C to D for moving the pressurization member from its second position toward its first position, and iv) a fourth segment 62 for maintaining the pressurization member at its f irst position D to A. In the embodiment shown, the cam 52 drives a rocker arm assembly 64 which in turn reciprocates tappet associated with the injector 20. Alternatively, pushrod (not shown) may be positioned between the cam 52 and the rocker arm assembly 64. Alternatively, a pushrod (not shown) may be positioned between the rocker arm assembly 64 and the tappet.
The electronic controlling means 26 or apparatus preferably includes a electronic control module 66 which controls 1) the fuel injection timing, 2) the total fuel injection quantity during an injection cycle, 3) the fuel injection pressure, 4) the number of separate injections or injection segments during an injection cycle, 5) the time interval (s) between the injection segment (s), 6) the fuel quantity of each injection segment during an injection cycle; and 7) any combination of the above parameter(s) between a plurality of injectors 20. Each of the above parameters are variably controllable independent of engine speed and loading.
Preferably, each injector 20 is a unit injector wherein both a fuel pressurization device 68 and a fuel injection device 70 are housed in the same unit. Although shown here as a unitized injector 20, alternatively, the injector could be of a modular construction with the fuel injection device 70 positioned separate from the fuel pressurization device 68. The injector 20 includes an imaginary longitudinal centreline axis 72 for reference purposes.
7 The injector 20 includes a housing portion 74, a nozzle portion 76, an electrical actuation means or device(s) 78, an electronically-controlled first pressure control valve 80, a reciprocal fuel pressurization member 82, a direct-operated check 84, a first biasing device 86, an electronically-controlled second pressure control valve 88, and a second biasing device 90.
The housing portion 74 defines a fuel control passage 92 and an integral fuel storage chamber 94. The internal fluid volume of the storage chamber 94 is preferably fixed and sized depending upon, inter alia, the desired maximum fuel quantity injected during an injection cycle, the desired peak fuel injection pressure during an injection cycle, the desired fuel injection pressure decay or drop during an injection cycle, the bulk modulus of the fuel, and the displacement of the pressurization member 82 (i.e., stroke and effective area). The control passage 92 generally refers to either a relatively-low pressure fuel supply passage 96 or a relatively-low pressure fuel drain passage 98 defined in the injector 20.
The electrical actuation means 78 is provided for controlling the positions of the first and second valves 80,88. The electrical actuation means 78 is selectively de-energized or energized. For example, the electrical actuation means 78 may include a single solenoid or a plurality of solenoids. Alternatively, the means 78 may include a piezoelectric device. The f irst valve 80 is preferably positioned in the storage chamber 94 and selectively movable between a first position, at which the electrical actuation means 78 is de-energized, and an second position at which the electrical actuation means 78 is either energized or deenergized as explained below. At its first position, the first valve 80 opens fluid communication between the storage chamber 94 and the control passage 96. The f irst valve 80 is energized to move from its first (opened) position to its second (closed) position. At its closed position, the first valve 8 blocks fluid communication between the storage chamber 94 and the control passage 96.
The nozzle portion 76 defines a bore 100, an injection chamber 102 integral with or arranged in fluid communication with the storage chamber 94, a pressure control chamber 104 separate from the injection chamber 102 and storage chamber 94, a tip seat 106, and at least one fuel injection orifice 108.
In the embodiment shown, the pressurization member 82 preferably includes a reciprocal plunger 110. The plunger 110 is preferably positioned in the storage chamber 94 and is selectively movable between a first position and a second position. When the first valve 80 is opened (i.e., its first position), the plunger 110 is operable during movement from its first to second positions for displacing a first variably-selected volume of fuel from the storage chamber 94 to the control passage 96. When the first valve 80 is closed (i.e., its second position) the plunger 110 is operable during movement from its first to second positions for displacing a second variably-selected volume of fuel in the storage chamber 94 thereby pressurizing such fuel to a selected variable pressure. Stated differently, after the first valve 80 is closed, the plunger 110 compresses the fuel to a controlled volume which is less than the fixed volume. To control or minimize torsional loads in a mechanical drivetrain which actuates the plunger 110, the cam profile is preferably chosen to begin movement of the plunger 110 from its first to second positions before initial fuel injection begins in an injection cycle. This also provides a variably selected injection pressure at the beginning of injection. In order to increase the mean effective injection pressure produced by the injector 20, the cam profile is preferably chosen as generally shown in Fig. 2 to continue moving the plunger 110 from its first to second positions (A to B) during fuel injection of an injection cycle. Alternatively as shown in Fig. 1, the cam profile can be chosen to complete movement of the plunger 9 from its first position to its second position prior to initial fuel injection of an injection cycle.
The check 84 is preferably positioned in the bore of the nozzle portion and selectively movable between a first position blocking fluid communication between the injection chamber 102 and the fuel injection orifice 108 and a second position opening fluid communication between the injection chamber 102 and the fuel injection orifice 108. The check 84 has a f irst end portion 112 and a second end portion 114. The first end portion 112 defines a first effective area arranged in partial fluid communication with the injection chamber 102 when the check 84 is closed (i.e., its first position). The first effective area is arranged to be in complete f luid communication with the injection chamber 102 when the check 84 is opened (i.e., its second position). The second end portion 114 def ines a second effective area arranged in fluid communication with the pressure control chamber 104. The first biasing device 86 preferably includes a first mechanical spring 116 operable for biasing the check 84 towards its closed or first position.
The second valve 88 is selectively movable between a de-energized first position and an energized second position. Preferably, the second valve 88 is a three-way valve such as a poppet valve or spool valve. The second valve 88 at its first position blocks fluid communication between the pressure control chamber 104 and the control passage 98 and opens fluid communication between the pressure control chamber 104 and the injection chamber 102.
The second valve 88 at its second position opens fluid communication between the pressure control chamber 104 and the fuel control passage 98 and blocks fluid communication between the pressure control chamber 104 and the injection chamber 102. When the check 84 is closed and the second valve 88 is at its second position, the first and second effective areas are operable for hydraulically moving the check 84 towards its second (opened) position. When the check 84 is at its second (opened) position and the second valve 88 is at its first position, the first and second effective areas are operable for balancing opposing hydraulic forces acting on such effective areas thereby allowing the first biasing device 86 to move the check 84 towards its first (closed) position.
The second biasing device 90 preferably includes a second mechanical spring 118 for biasing both the first and second valves 80,88 towards their respective first positions. Alternatively, the second biasing device 90 may be a plurality of springs biasing the respective first and second valves towards their respective first positions.
In the embodiment shown in Figs. 1-7, the injector also includes a tappet 120, a first retainer 122 positioned between the plunger 110 and the tappet 120, a tappet return spring 124, a barrel 126 defining a bore 128 in which the plunger 110 reciprocates according to a predetermined tight clearance, a second retainer 130 positioned between the barrel 126 and the tappet 120, a housing 132 connected to the barrel 126 and defining a bore 134 in which the first valve 80 reciprocates according to a relatively loose clearance, a sleeve 136 sealedly positioned between the barrel 126 and the housing 132, an electrical connector 138 electrically connected to the electrical actuation device 78, an upper seal 140, an upper stop 142 defining a bore 144 in which the second valve 88 reciprocates according to a predetermined tight clearance, a spacer 146, a lower stop 148, a poppet sleeve 150 positioned between the spacer 146 and the lower stop 148, a body 152 defining the bore 100 in which the check 84 reciprocates according to a preselected tight clearance, a tip 154 which defines the tip seat 106 and the injection orifice(s) 108, and a case 156 connected to the housing 132.
The housing 132 and first valve 80 each define a seat 158,160 which sealedly contact one another when the first valve 80 is closed.
The upper stop 142 and second valve 88 each define a seat 162, 164 which sealedly contact one another when the second valve 88 is at its second position. The poppet sleeve 150 and second valve 88 each define a separate seat 168,170 which sealedly contact one another when the second valve 88 is at its first position.
Preferably, the poppet sleeve 150 defines a bore 166 in which the second valve 88 reciprocates according to a predetermined tight clearance. Preferably, the poppet sleeve 150 is loosely positioned, in the axial and radial directions, between the spacer 146 and the lower stop 148.
Preferably, the electrical actuation device 78 is connected to the housing 132. The upper stop 142, spacer 146, lower stop 148, body 152, and tip 154 are retained between the case 156 and the housing 132.
Industrial Applicability
In operation, before an injection cycle begins, the electrical actuation device 78 or solenoid is normally deenergized so that the first valve 80 is opened and the second valve 88 is at its first position. The check 84 is at its first (closed) position. The opened first valve 80 allows the---fuelstorage chamber 94 and the injection chamber 102 to be filled with relatively low pressure fuel provided by the pressure control passage 96.
The plunger 110, driven by the first segment 56 (A-B) of the cam 52, begins its stroke from its retracted first position A. At a selected amount of plunger stroke, the solenoid 78 is energized causing closure of the first valve 80 and movement of the second valve 88 to its second position. The solenoid 78 preferably remains energized until the fuel pressure in the storage chamber 94 reaches a level sufficient to hydraulically hold the first valve 80 closed. The solenoid 78 is then deenergized allowing the second spring 118 to return the second valve 88 to its first position. The fuel pressure in the storage chamber 94 and the injection chamber 102 continues to increase to a variably selected pressure due to continued stroking of 12 the plunger 110. With the second valve 88 at its f irst position, high pressure fuel communicates with the pressure control chamber 104 from the injection chamber 102 between opened seats 162,164.
With the check 84 seated, the second effective area exposed to high fuel pressure is greater than the first effective area exposed to high fuel pressure thereby preventing the check 84 from opening.
To start injection, the solenoid 78 is again energized thereby moving the second valve 88 to its second position and also compressing the second spring. This closes seats 164,162 of the second valve and upper stop. This also opens seats 170,168 of the second valve 88 and the poppet sleeve 150 communicating the pressure control chamber 104 with the control pressure passage 98. By reducing the pressure in the pressure control chamber 104 and having high pressure in the injection chamber 102, the check 84 opens to begin fuel injection through the injection orifice(s) 108 and into the engine combustion chamber 14.
To end fuel injection, the solenoid 78 is again deenergized allowing the compressed second spring 118 to return the second valve 88 back to its first position and closing seats 170,168 of the second valve 88 and the poppet sleeve 150 to block fluid communication between the pressure control chamber 104 and the control pressure passage 98. Moreover, seats 164,162 of the second valve 88 and the upper stop 142 are opened communicating the pressure control chamber 104 with the injection chamber 102 thereby introducing high pressure fuel back into the pressure control chamber 104.
Preferably, the first and second effective areas of the check 84 are sized such that when the check 84 is opened and the second valve 88 is at its first position, the net hydraulic forces acting on the check 84 are effectively zero. In other words, the net opposing fluid pressures are equal and also the first and second effective areas on which such pressures act are equal. When the 13 is check 84 is opened, the force of the first spring 116 is preferably the only unbalanced force acting on the check 84, consequently biasing the check 84 toward its f irst (closed) position. At the end of a fuel injection cycle or injection segment, the force of the first spring 116 urges the check 84 from its opened position to its closed position at a selected velocity. The first spring force is preferably chosen to be sufficiently high for adequate check response yet sufficiently low to gently move the check 84 toward the tip seat 106 so that the check 84 does not overstress the tip 154 upon initial contact. Advantageously, the end of fuel injection during an injection cycle or segment is more precisely controlled since the velocity of the check 84 in the closing direction is primarily determined only by the force of the first spring 116 with minimal affect by the fuel injection pressure.
Fig. 8 is a diagrammatic approximate graph of fuel injection pressure, P measured in megapascals, versus time, T measured in seconds, comparing predicted operation of a computer- simulated exemplary injector 172 of the present invention versus actual operation of a bench-tested conventional electranical ly-contro 1 led injector 174 adapted for a same engine. Fig. 8 shows that the subject invention produces a higher mean injection pressure 176 compared to the mean injection pressure 178 of the conventional injector for approximately the same peak injection pressure 180 and total fuel quantity. Moreover, a higher initial injection pressure 182 is available with the subject invention at the beginning of fuel injection. Moreover,the subject invention produces a sharper or more abrupt end of injection 184 compared to the end of injection 186 of the conventional injector.
Fig. 9 is a diagrammatic approximate graph of fuel injection pressure, P measured in megapascals, versus time, T measured in seconds, comparing predicted operations of a computer-simulated exemplary injector of the present 14 invention operating at three different exemplary injection pressures 188, 190, 192 but delivering approximately the same quantity of fuel per injection. Fig. 9 shows the subject invention is capable of varying peak fuel injection pressure independent of engine speed and load.
Fig. 10 is a diagrammatic approximate graph of cumulative fuel quantity, Q measured in cubic millimetres, versus time, T measured in seconds, showing predicted dualtype segmented injection operation of a computer- simulated exemplary injector of the present invention. Fig. 11 is a diagrammatic approximate graph of fuel injection pressure, P measured in megapascals, versus time, T measured in seconds, showing predicted operation corresponding to Fig. 10. In Fig. 11, a f irst injection segment 194 and a separate second injection segment 196 are shown. The subject invention is capable of variably controlling the fuel quantity, Q 1 and/or Q 2 of each separate fuel injection segment 194,196 during an injection cycle. The subject invention is also capable of variably controlling each time interval, delta T 3-2' between each separate fuel injection segment 194,196 during an injection cycle.
Fig. 12 is a diagrammatic approximate graph of cumulative fuel quantity, Q measured in cubic millimetres, versus time, T measured in seconds, showing predicted triple-type segmented injection operation of a computersimulated exemplary injector of the present invention. Fig. 13 is a diagrammatic approximate graph of fuel injection pressure, P measured in megapascals, versus time, T measured in seconds, showing predicted operation corresponding to Fig. 12. In Fig. 13, a first injection segment 198, a separate second injection segment 200, and a separate third injection segment 202 are shown. The subject invention is capable of variably controlling the f JI fuel quantity. for example, Q 1 and/or Q 2 and/or Q 3 of each separate fuel injection segment 198,200,202 during an injection cycle. The subject invention is also capable of variably controlling each time interval, for example, delta V 3-2 and/or delta T S-V between each fuel injection segment during an injection cycle. Moreover, the solenoid 78 can be energized and de-energized once or a selected plurality of times during an injection cycle to produce one or a variably-selected plurality of injection segments.
16 claims 1. A method of operating an electronical ly-control led unit fuel pump injector comprising the steps of: opening fluid communication between a fixed-volume fuel storage chamber and a control passage; closing fluid communication between the storage chamber and at least one fuel injection orifice; displacing a variably- selected volume of fuel from the storage chamber to the control passage; closing fluid communication between the storage chamber and the control passage; displacing anothervariably-selected volume of fuel in the storage chamber and thereby pressurizing the fuel to a selected pressure; opening fluid communication between the storage chamber and the fuel injection orifice to begin fuel injection; and closing fluid communication between the storage chamber and the fuel injection orifice to end fuel injection.
2. A method of operating an electronica 1 ly-control led unit fuel pump injector comprising the steps of: opening fluid communication between a fixed-volume fuel storage chamber and a control passage; closing a check to block fluid communication between the storage chamber and at least one fuel injection orifice; 30 displacing a variably- se 1 ected volume of fuel from the storage chamber to the control passage; closing fluid communication between the storage chamber and the control passage; displacing another variably-selected volume of fuel in the storage chamber and thereby pressurizing the fuel to a selected pressure; 17 biasing the check towards a closed position blocking f luid communication between the storage chamber and the fuel injection orifice; hydraulically-unbalancing the check for movement towards an opened position opening f luid communication between the storage chamber and the fuel injection orifice; and hydraulically-balancing the check and allowing the biased check to move to the closed position.
GB9801389A 1994-05-13 1995-03-27 Electronically-controlled fluid injector system having pre-injection pressurizable fluid storage chamber and direct-operated check Expired - Fee Related GB2320292B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US24250194A 1994-05-13 1994-05-13
GB9506193A GB2289313B (en) 1994-05-13 1995-03-27 Fluid injector system

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GB9801389D0 GB9801389D0 (en) 1998-03-18
GB2320292A true GB2320292A (en) 1998-06-17
GB2320292A8 GB2320292A8 (en) 1998-07-08
GB2320292B GB2320292B (en) 1998-09-30

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GB9801383A Expired - Fee Related GB2320290B (en) 1994-05-13 1995-03-27 Electronically-controlled fluid injector system having pre-injection pressurizable fluid storage chamber and direct-operated check
GB9801379A Expired - Fee Related GB2320289B (en) 1994-05-13 1995-03-27 Electronically-controlled fluid injector system having pre-injection pressurizable fluid storage chamber and direct-operated check
GB9801387A Expired - Fee Related GB2320291B (en) 1994-05-13 1995-03-27 Electronically-controlled fluid injector system having pre-injection pressurizale fluid storage chamber and direct-operated check
GB9801375A Expired - Fee Related GB2320288B (en) 1994-05-13 1995-03-27 Electronically-controlled fluid injector system having pre-injection pressurizable fluid storage chamber and direct-operated check
GB9801389A Expired - Fee Related GB2320292B (en) 1994-05-13 1995-03-27 Electronically-controlled fluid injector system having pre-injection pressurizable fluid storage chamber and direct-operated check

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GB9801383A Expired - Fee Related GB2320290B (en) 1994-05-13 1995-03-27 Electronically-controlled fluid injector system having pre-injection pressurizable fluid storage chamber and direct-operated check
GB9801379A Expired - Fee Related GB2320289B (en) 1994-05-13 1995-03-27 Electronically-controlled fluid injector system having pre-injection pressurizable fluid storage chamber and direct-operated check
GB9801387A Expired - Fee Related GB2320291B (en) 1994-05-13 1995-03-27 Electronically-controlled fluid injector system having pre-injection pressurizale fluid storage chamber and direct-operated check
GB9801375A Expired - Fee Related GB2320288B (en) 1994-05-13 1995-03-27 Electronically-controlled fluid injector system having pre-injection pressurizable fluid storage chamber and direct-operated check

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0987431A2 (en) * 1998-09-18 2000-03-22 Lucas Industries Limited Fuel injector
EP1081373A2 (en) * 1999-08-28 2001-03-07 Delphi Technologies, Inc. Fuel injector

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5947380A (en) * 1997-11-03 1999-09-07 Caterpillar Inc. Fuel injector utilizing flat-seat poppet valves
US5934559A (en) * 1997-11-03 1999-08-10 Caterpillar Inc., Electronic fuel injector with internal single-pole solenoid and center flow post
DE19839581A1 (en) * 1997-11-04 1999-05-06 Lucas Ind Plc Fuel injector
US5971300A (en) * 1997-11-04 1999-10-26 Caterpillar, Inc. Fuel injector employing center fuel flow and pressure-assisted check closing

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4211202A (en) * 1977-09-21 1980-07-08 Daimler-Benz Aktiengesellschaft Pump nozzle for air-compressing injection internal combustion engine
EP0174718A1 (en) * 1984-08-06 1986-03-19 General Motors Corporation Electromagnetic unit fuel injector
EP0269289A2 (en) * 1986-11-28 1988-06-01 Diesel Technology Corporation Diesel unit fuel injector with spill assist injection needle valve closure
EP0675282A1 (en) * 1994-03-03 1995-10-04 Lucas Industries Public Limited Company Fuel systems

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4129256A (en) * 1977-09-12 1978-12-12 General Motors Corporation Electromagnetic unit fuel injector
US4538576A (en) * 1983-07-21 1985-09-03 Allied Corporation Diesel fuel injector with double dump configuration
US4572433A (en) * 1984-08-20 1986-02-25 General Motors Corporation Electromagnetic unit fuel injector
JPH0759919B2 (en) * 1986-04-04 1995-06-28 日本電装株式会社 Fuel injection controller for diesel engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4211202A (en) * 1977-09-21 1980-07-08 Daimler-Benz Aktiengesellschaft Pump nozzle for air-compressing injection internal combustion engine
EP0174718A1 (en) * 1984-08-06 1986-03-19 General Motors Corporation Electromagnetic unit fuel injector
EP0269289A2 (en) * 1986-11-28 1988-06-01 Diesel Technology Corporation Diesel unit fuel injector with spill assist injection needle valve closure
EP0675282A1 (en) * 1994-03-03 1995-10-04 Lucas Industries Public Limited Company Fuel systems

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0987431A2 (en) * 1998-09-18 2000-03-22 Lucas Industries Limited Fuel injector
EP0987431A3 (en) * 1998-09-18 2001-01-24 Lucas Industries Limited Fuel injector
US6267306B1 (en) 1998-09-18 2001-07-31 Lucas Industries Fuel injector including valve needle, injection control valve, and drain valve
EP1081373A2 (en) * 1999-08-28 2001-03-07 Delphi Technologies, Inc. Fuel injector
EP1081373A3 (en) * 1999-08-28 2002-04-10 Delphi Technologies, Inc. Fuel injector
US6502555B1 (en) 1999-08-28 2003-01-07 Delphi Technologies, Inc. Fuel injector

Also Published As

Publication number Publication date
GB9801383D0 (en) 1998-03-18
GB2320290A (en) 1998-06-17
GB2320292B (en) 1998-09-30
GB2320288B (en) 1998-09-30
GB2320290B (en) 1998-09-30
GB2320288A (en) 1998-06-17
GB9801389D0 (en) 1998-03-18
GB9801379D0 (en) 1998-03-18
GB2320289B (en) 1998-09-30
GB2320291A (en) 1998-06-17
GB9801375D0 (en) 1998-03-18
GB2320289A (en) 1998-06-17
GB2320291B (en) 1998-09-30
GB2320292A8 (en) 1998-07-08
GB9801387D0 (en) 1998-03-18

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