EP3526459A1 - Method to determine fuel pump phasing - Google Patents

Method to determine fuel pump phasing

Info

Publication number
EP3526459A1
EP3526459A1 EP17784618.5A EP17784618A EP3526459A1 EP 3526459 A1 EP3526459 A1 EP 3526459A1 EP 17784618 A EP17784618 A EP 17784618A EP 3526459 A1 EP3526459 A1 EP 3526459A1
Authority
EP
European Patent Office
Prior art keywords
pressure
crankshaft
pump
pumping
stroke
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
EP17784618.5A
Other languages
German (de)
French (fr)
Other versions
EP3526459B1 (en
Inventor
Pedro LOQUAIS
Anthony MICHOU
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.)
Borgwarner US Technologies LLC
Original Assignee
Delphi Technologies IP Ltd
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
Publication date
Application filed by Delphi Technologies IP Ltd filed Critical Delphi Technologies IP Ltd
Publication of EP3526459A1 publication Critical patent/EP3526459A1/en
Application granted granted Critical
Publication of EP3526459B1 publication Critical patent/EP3526459B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/38Controlling fuel injection of the high pressure type
    • F02D41/3809Common rail control systems
    • F02D41/3836Controlling the fuel pressure
    • F02D41/3845Controlling the fuel pressure by controlling the flow into the common rail, e.g. the amount of fuel pumped
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/009Electrical control of supply of combustible mixture or its constituents using means for generating position or synchronisation signals
    • 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
    • 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
    • F02M63/02Fuel-injection apparatus having several injectors fed by a common pumping element, or having several pumping elements feeding a common injector; Fuel-injection apparatus having provisions for cutting-out pumps, pumping elements, or injectors; Fuel-injection apparatus having provisions for variably interconnecting pumping elements and injectors alternatively
    • F02M63/0225Fuel-injection apparatus having a common rail feeding several injectors ; Means for varying pressure in common rails; Pumps feeding common rails
    • 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
    • F02M63/02Fuel-injection apparatus having several injectors fed by a common pumping element, or having several pumping elements feeding a common injector; Fuel-injection apparatus having provisions for cutting-out pumps, pumping elements, or injectors; Fuel-injection apparatus having provisions for variably interconnecting pumping elements and injectors alternatively
    • F02M63/0225Fuel-injection apparatus having a common rail feeding several injectors ; Means for varying pressure in common rails; Pumps feeding common rails
    • F02M63/0265Pumps feeding common rails
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D1/00Controlling fuel-injection pumps, e.g. of high pressure injection type
    • F02D2001/0085Arrangements using fuel pressure for controlling fuel delivery in quantity or timing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/22Safety or indicating devices for abnormal conditions
    • F02D2041/224Diagnosis of the fuel system
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D2200/00Input parameters for engine control
    • F02D2200/02Input parameters for engine control the parameters being related to the engine
    • F02D2200/06Fuel or fuel supply system parameters
    • F02D2200/0602Fuel pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D2250/00Engine control related to specific problems or objectives
    • F02D2250/14Timing of measurement, e.g. synchronisation of measurements to the engine cycle

Definitions

  • the invention relates to fuel pumps for internal combustions engines which are driven by a crankshaft drive. It has particular application to piston (plunger type) fuel pumps, where typically a pump plunger is driven by a pump cam mechanism driven by the crankshaft.
  • the invention relates to a method of accurately and reliably determining the pump phase i.e. in relation to the crankshaft.
  • Modern engines use high pressure pumps to supply fuel to a accumulator volume such as a common rail which supplies fuel in turn to one or more fuel injectors.
  • a fuel injector volume such as a common rail which supplies fuel in turn to one or more fuel injectors.
  • Such pumps are piston or plunger type pumps which reciprocate as a result of an (e.g. offset) cam mechanism driven by the camshaft, to pressurize fuel in a fuel chamber.
  • inlet metering valve and outlet valves are provided adjacent to the fuel chamber.
  • Pump phasing is defined as the angle (phase offset) between Top Dead Center (TDC) of one (or more) cylinder and pump TDC (i.e. when the pump plunger reaches the top position at the end of the pumping stroke).
  • TDC Top Dead Center
  • the pressure control of the common rail by e.g. the use of a digital Inlet valve requires the pump TDC to be accurately known (in relation to the crankshaft position).
  • the digital inlet valve behavior is linked to the pump cycle with an angular timing command.
  • the usual method to phase the pump is a mechanical indexation by a pin between pump shaft and engine timing pulley.
  • this phasing method is not enough accurate and other mechanical dispersion are not taken into account (timing belt, crank wheel, sensor location, etc.) It is an object of the invention to provide a method to determine the pump phasing and thus also to control more precisely the pump phase and to reduce the scatter.
  • a method of determining the relative phasing between a crankshaft and a crankshaft driven high pressure piston pump via a cam mechanism, said piston pump adapted to provide high pressure fuel to a common rail comprising: a) measuring the pressure PI in said common rail at a time before a pumping stroke/event;
  • step b) measuring the pressure P2 in said common rail at a time after the pumping stroke/event; c) determining the average pressure of said measured pressure from steps a) and b); d) determining the time point where the measured pressure reaches the average pressure determined form step c) e) correlating said time point with from d) with crankshaft position to determine said relative phasing.
  • Said time point in d) may be assumed to be the mid-stroke in a pumping event of said piston pump.
  • Said correlation may include determining the phase difference between the top dead centre after the pumping stroke from said assumed mid-stroke time point and cam geometry.
  • Step e) may comprise correlating said time point with a crankshaft signal, said crankshaft signal including a phasing reference point.
  • Said crankshaft signal may comprise a series of pulses generated as crankshaft teeth pass in proximity to a sensor, and said reference point comprises a tooth having an irregular pitch or gap.
  • Said pressure PI may be that measured during a first plateau phase before a pumping stroke and the pressure P2 is measured during a second higher plateau phase after said pumping stroke.
  • Said pressure PI may be the average pressure Pavl over a timespan in said first plateau phase and said pressure P2 is the average pressure Pav2 over a timespan of said sensor plateau phase.
  • relative phasing can mean the phase difference or relative position. In examples it is the phasing between the TDC of the crankshaft (e.g. in relation to one or more cylinders) and TDC of the pumping stroke of the piston/plunder of the high pressure pump.
  • Figure 1 shows a schematic figure of a high pressure piston pump system to supply pressurized fuel to an accumulator volume such as a common rail;
  • Figure 2 shows a diagram representing high pressure piston pump phasing dispersion
  • Figure 3 shows a chart of crankshaft output pulse against common rail pressure and illustrates an example of how the method can be implemented.
  • Figure 1 shows a schematic figure of a piston pump system 1 to supply pressurized fuel to an accumulator volume such as a common rail.
  • the piston pump includes plunger 2 driven by cam mechanism 4 and is adapted to pressurise fuel in a chamber 3.
  • Located between the chamber outlet and the common rail 5 is an outlet valve 10.
  • IMV inlet metering valve
  • the actuator which drives the pump flow can be an IMV or a DIV (DIV drives the inlet valve closure).
  • a further valve /head cap 10 is normally provided integral with the pump.
  • the cam is driven from the camshaft 8 (shown by the dotted line) which comprises a toothed wheel.
  • FIG. 1 shows a diagram representing pump phasing dispersion.
  • the cylinder top dead centre (Cyl TDC), for a particular cylinder is at a phase difference to the pump TDC; usually this angle is 44°.
  • the figure shows the typically scatter which is about +/- 20° about a nominal ideal phase angle.
  • the typically the phase difference between pump (TDC) and crankshaft (TDC) should be e.g. 44°.
  • examples of the invention can be applied to engines having any number of cylinders. In one example, as single revolution of the crank will result in a single full pumping stroke/period.
  • the frequency of a reciprocation of a piston in a cylinder will be the same as the pumping plunger in the high pressure fuel pump.
  • the cam mechanism used to drive the plunger may comprise various mechanisms; e.g. it having various numbers of lobes. In this case there may be any number of pumping cycles per crank revolution; thus the invention is also applicable to any of these; there may be for example two lobes and two pumping cycles per one crank revolution.
  • the bottom plot shows the signal 10 obtained from a toothed crank wheel which e.g. has 60 teeth. This signal is derived from e.g. a proximity sensor such as a Hall effect sensor, where a pulse is obtained every time a tooth of the wheel passes.
  • the signal is a rectangular (pulsed) waveform.
  • one of the pulses has a larger pitch or period than the others (shown by the arrow A) - this is from/corresponds to the reference tooth 9 of figure 1- the longer tooth or gap machined into the toothed wheel and in the examples is used as a reference. So thus, typically in order to provide a reference, one tooth has a larger pitch or period that the others.
  • this indexing tooth or tooth gap is located as shown by the arrow A and is considered a reference point. It is assumed that the phase difference (if any) between this and the crankshaft TDC (e.g. in respect of one or more cylinders) is fixed/known.
  • the top plot 11 shows the pressure in the common rail 9 as a result of pressurisation of fluid therein resulting from a pumping stroke of the high pressure pump via the cam mechanism driven by the correspondingly rotating crankshaft corresponding to signal 11.
  • the pump plunger moves to the TDC position, it acts to pressurize fuel in the fuel rail.
  • the pressure of the fluid is generally at first generally pressure level PI (see plateau 12) and after the pumping stroke the pressure is increased to a higher pressure P2 (see plateau 13).
  • a common rail includes a pressure sensor; pressures can be thus be determined by the pressure sensor already present on the common rail. Finding the exact end of the pumping event on the rail pressure signal is difficult because the end of pressure increase is very slow (due to pump cam profile).
  • the pressures before and after the pumping stroke are measured and the average is determined.
  • the mid-point of the pumping stroke is assumed to be at the point where the pressure is at this value.
  • the pressure PI and P2 may be also averaged, or the pressure over the plateau regions 12, 13 are determined and this averaged.
  • the values of averages pressure values Pavl and average pressure value Pav2 over a period in the plateaus may be determined and the averages of these averages pressures determined. This is illustrated by the boxes designated for Pavl and Pav2 where, within the time span in the box, the average value of pressure is determined.
  • one aspect the point at which the pressure reaches the average value of averages Pavl and Pav2 is used to determine phasing and this point is assumed to be the point at which the pump is half way throught he pumping stroke i.e. in the mid-stroke (pressurization) position.
  • This point is illustrated by X in the figure.
  • the average of the averages Pavl and Pav2 is determined to be Px equivalent to point X. This point is assumed to be the mid-point of the pumping stroke and can be used to determine pump phasing.
  • the tooth number corresponding to the time at which the mid-point in terms of pressure is noted and the phase between that and the reference is noted.
  • the phase (difference) between the absolute reference point A and the mid stroke pressurisation point is given by arrow B.
  • the point of top dead-centre of the pump plunger would be at point CI , effectively and the phase between this point and the absolute reference point is shown by arrow C.
  • This point and thus the phase difference between pump TDC and crank reference (and hence crank TDC) can be determined from the cam profile. From the cam design the difference between the mid-point and the TDC can be easily determined or is already known. So for example with a single lobe cam the point of mid stroke may be 90° ahead of TDC.
  • geometries may vary. There may be more than one lobe e.g. two lobes or more or the geometry may perform two or more pumping operations per cam revolution.
  • pump cam profile may not be symmetric; the filling phase may cover 85°, pumping phase 95°deg.
  • absolute reference point is the nominal TDC of the crankshaft.
  • crank TDC the reference point
  • a method learns the phasing between the high pressure fuel pump and the engine (crankshaft).
  • the principle of the pump phasing measurement chosen is to position the middle of the pumping where the pressure increase slope is high in relation to the engine crank wheel.
  • the middle of the rail pressure increase during a pumping event corresponds to half of the pumped volume.
  • the end of the pumping event e.g. the plunger TDC
  • examples of the invention allow accurate rail Pressure control by a digital inlet valve (DIV) and then to increase rail pressure control performances and accuracy.
  • the present invention allows to control the rail pressure by a e.g. digital inlet valve (DIV) without adding any manufacturing process constraints (machining tolerance).
  • This method by learning allows diagnosis of a faulty operating pump assembly on engine. This method allow to take into account scatter of chain rattling from pump TDC to software angle reference.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)

Abstract

A method of determining the relative phasing between a crankshaft and a crankshaft driven high pressure piston pump via a cam mechanism, said piston pump adapted to provide high pressure fuel to a common rail, comprising: a) measuring the pressure P1 in said common rail at a time before a pumping stroke/event; b) measuring the pressure P2 in said common rail at a time after the pumping stroke/event; c) determining the average pressure of said measured pressure from steps a) and b); d) determining the time point where the measured pressure reaches the average pressure determined form step c) e) correlating said time point with from d) with crankshaft position to determine said relative phasing.

Description

Method to Determine Fuel Pump Phasing
Field of the Invention
The invention relates to fuel pumps for internal combustions engines which are driven by a crankshaft drive. It has particular application to piston (plunger type) fuel pumps, where typically a pump plunger is driven by a pump cam mechanism driven by the crankshaft. The invention relates to a method of accurately and reliably determining the pump phase i.e. in relation to the crankshaft.
Background to the Invention
Modern engines use high pressure pumps to supply fuel to a accumulator volume such as a common rail which supplies fuel in turn to one or more fuel injectors. Typically such pumps are piston or plunger type pumps which reciprocate as a result of an (e.g. offset) cam mechanism driven by the camshaft, to pressurize fuel in a fuel chamber. Typically inlet metering valve and outlet valves are provided adjacent to the fuel chamber.
Pump phasing is defined as the angle (phase offset) between Top Dead Center (TDC) of one (or more) cylinder and pump TDC (i.e. when the pump plunger reaches the top position at the end of the pumping stroke). The pressure control of the common rail by e.g. the use of a digital Inlet valve requires the pump TDC to be accurately known (in relation to the crankshaft position). The digital inlet valve behavior is linked to the pump cycle with an angular timing command.
Typically actual pump TDC scatter (that is the variation in phase the pump in operation) can be up to +/- 20° and DIV control requires a precision of +/-3°.
The usual method to phase the pump is a mechanical indexation by a pin between pump shaft and engine timing pulley. However this phasing method is not enough accurate and other mechanical dispersion are not taken into account (timing belt, crank wheel, sensor location, etc.) It is an object of the invention to provide a method to determine the pump phasing and thus also to control more precisely the pump phase and to reduce the scatter.
Statement of the Invention
In one aspect is provided a method of determining the relative phasing between a crankshaft and a crankshaft driven high pressure piston pump via a cam mechanism, said piston pump adapted to provide high pressure fuel to a common rail, comprising: a) measuring the pressure PI in said common rail at a time before a pumping stroke/event;
b) measuring the pressure P2 in said common rail at a time after the pumping stroke/event; c) determining the average pressure of said measured pressure from steps a) and b); d) determining the time point where the measured pressure reaches the average pressure determined form step c) e) correlating said time point with from d) with crankshaft position to determine said relative phasing.
Said time point in d) may be assumed to be the mid-stroke in a pumping event of said piston pump.
Said correlation may include determining the phase difference between the top dead centre after the pumping stroke from said assumed mid-stroke time point and cam geometry.
Step e) may comprise correlating said time point with a crankshaft signal, said crankshaft signal including a phasing reference point.
Said crankshaft signal may comprise a series of pulses generated as crankshaft teeth pass in proximity to a sensor, and said reference point comprises a tooth having an irregular pitch or gap. Said pressure PI may be that measured during a first plateau phase before a pumping stroke and the pressure P2 is measured during a second higher plateau phase after said pumping stroke. Said pressure PI may be the average pressure Pavl over a timespan in said first plateau phase and said pressure P2 is the average pressure Pav2 over a timespan of said sensor plateau phase.
The term "relative phasing" can mean the phase difference or relative position. In examples it is the phasing between the TDC of the crankshaft (e.g. in relation to one or more cylinders) and TDC of the pumping stroke of the piston/plunder of the high pressure pump.
Brief Description of Drawings
The invention will now be described by way of example and with reference to the following figures of which:
Figure 1 shows a schematic figure of a high pressure piston pump system to supply pressurized fuel to an accumulator volume such as a common rail;
Figure 2 shows a diagram representing high pressure piston pump phasing dispersion; Figure 3 shows a chart of crankshaft output pulse against common rail pressure and illustrates an example of how the method can be implemented. Detailed Description of Drawings
Figure 1 shows a schematic figure of a piston pump system 1 to supply pressurized fuel to an accumulator volume such as a common rail. The piston pump includes plunger 2 driven by cam mechanism 4 and is adapted to pressurise fuel in a chamber 3. Located between the chamber outlet and the common rail 5 is an outlet valve 10. Located between the fuel supply and the inlet to the pumping chamber, is an inlet metering valve (IMV) 6. The actuator which drives the pump flow can be an IMV or a DIV (DIV drives the inlet valve closure). A further valve /head cap 10 is normally provided integral with the pump. The cam is driven from the camshaft 8 (shown by the dotted line) which comprises a toothed wheel. Typically one of the teeth 9 has a longer tooth pitch or tooth gap and this is used for reference, i.e. for timing purposes. Figure 2 shows a diagram representing pump phasing dispersion. The cylinder top dead centre (Cyl TDC), for a particular cylinder is at a phase difference to the pump TDC; usually this angle is 44°. The figure shows the typically scatter which is about +/- 20° about a nominal ideal phase angle. Again the typically the phase difference between pump (TDC) and crankshaft (TDC) should be e.g. 44°. It should be noted that examples of the invention can be applied to engines having any number of cylinders. In one example, as single revolution of the crank will result in a single full pumping stroke/period. In other words the frequency of a reciprocation of a piston in a cylinder will be the same as the pumping plunger in the high pressure fuel pump. However the cam mechanism used to drive the plunger may comprise various mechanisms; e.g. it having various numbers of lobes. In this case there may be any number of pumping cycles per crank revolution; thus the invention is also applicable to any of these; there may be for example two lobes and two pumping cycles per one crank revolution. In Figure 3, the bottom plot shows the signal 10 obtained from a toothed crank wheel which e.g. has 60 teeth. This signal is derived from e.g. a proximity sensor such as a Hall effect sensor, where a pulse is obtained every time a tooth of the wheel passes. As can be seen the signal is a rectangular (pulsed) waveform. Note that one of the pulses has a larger pitch or period than the others (shown by the arrow A) - this is from/corresponds to the reference tooth 9 of figure 1- the longer tooth or gap machined into the toothed wheel and in the examples is used as a reference. So thus, typically in order to provide a reference, one tooth has a larger pitch or period that the others. In the example of the figure this indexing tooth or tooth gap is located as shown by the arrow A and is considered a reference point. It is assumed that the phase difference (if any) between this and the crankshaft TDC (e.g. in respect of one or more cylinders) is fixed/known.
The top plot 11 shows the pressure in the common rail 9 as a result of pressurisation of fluid therein resulting from a pumping stroke of the high pressure pump via the cam mechanism driven by the correspondingly rotating crankshaft corresponding to signal 11. Thus, as the pump plunger moves to the TDC position, it acts to pressurize fuel in the fuel rail. Before the pumping stroke the pressure of the fluid is generally at first generally pressure level PI (see plateau 12) and after the pumping stroke the pressure is increased to a higher pressure P2 (see plateau 13). Typically a common rail includes a pressure sensor; pressures can be thus be determined by the pressure sensor already present on the common rail. Finding the exact end of the pumping event on the rail pressure signal is difficult because the end of pressure increase is very slow (due to pump cam profile).
According to one example, the pressures before and after the pumping stroke are measured and the average is determined. The mid-point of the pumping stroke is assumed to be at the point where the pressure is at this value. Thus the pressure PI and P2 may be also averaged, or the pressure over the plateau regions 12, 13 are determined and this averaged. In an example the values of averages pressure values Pavl and average pressure value Pav2 over a period in the plateaus may be determined and the averages of these averages pressures determined. This is illustrated by the boxes designated for Pavl and Pav2 where, within the time span in the box, the average value of pressure is determined.
So, one aspect the point at which the pressure reaches the average value of averages Pavl and Pav2 (or PI and P2) is used to determine phasing and this point is assumed to be the point at which the pump is half way throught he pumping stroke i.e. in the mid-stroke (pressurization) position. This point is illustrated by X in the figure. So in the figure the average of the averages Pavl and Pav2 is determined to be Px equivalent to point X. This point is assumed to be the mid-point of the pumping stroke and can be used to determine pump phasing.
In one example the tooth number corresponding to the time at which the mid-point in terms of pressure is noted and the phase between that and the reference (e.g. crankshaft reference tooth/gap is noted is noted. Thus the phase (difference) between the absolute reference point A and the mid stroke pressurisation point is given by arrow B.
The point of top dead-centre of the pump plunger would be at point CI , effectively and the phase between this point and the absolute reference point is shown by arrow C. This point and thus the phase difference between pump TDC and crank reference (and hence crank TDC) can be determined from the cam profile. From the cam design the difference between the mid-point and the TDC can be easily determined or is already known. So for example with a single lobe cam the point of mid stroke may be 90° ahead of TDC. Of course geometries may vary. There may be more than one lobe e.g. two lobes or more or the geometry may perform two or more pumping operations per cam revolution.
So to recap, the method determines the mid pressure value. At this mid pressure value, the angle in relation to crankshft is determined. With the pump cam profile, the angle between the pump top dead center and the mid lift pump position ("angle2") is known. So we can calculate the position of the pump TDC relative to crankshaft (phase) is Pump TDC angle = angle 1 - angle2
In one example there are 2 pumping events per pump revolution, and so 1 pumping event = 180°. Furthermore the pump cam profile may not be symmetric; the filling phase may cover 85°, pumping phase 95°deg. As the pump may also not be symmetric during pumping, plunger mid point may not be is not 95/2=47.5 but 48.2deg from pump TDC. It is to be noted that in the example the absolute reference point is the nominal TDC of the crankshaft. Of course it may be that there is a known phase difference between crank TDC and the reference point (i.e. that denoted by the larger tooth period/pitch).
Thus according to aspects, a method learns the phasing between the high pressure fuel pump and the engine (crankshaft). As a result, the principle of the pump phasing measurement chosen is to position the middle of the pumping where the pressure increase slope is high in relation to the engine crank wheel. Indeed, the middle of the rail pressure increase during a pumping event corresponds to half of the pumped volume. So in a simple method the end of the pumping event (e.g. the plunger TDC) is identified from the rail pressure and the crank events during the engine starting. As a consequence, examples of the invention allow accurate rail Pressure control by a digital inlet valve (DIV) and then to increase rail pressure control performances and accuracy. The present invention allows to control the rail pressure by a e.g. digital inlet valve (DIV) without adding any manufacturing process constraints (machining tolerance). This method by learning allows diagnosis of a faulty operating pump assembly on engine. This method allow to take into account scatter of chain rattling from pump TDC to software angle reference.

Claims

Claims
1. A method of determining the relative phasing between a crankshaft and a crankshaft driven high pressure piston pump via a cam mechanism, said piston pump adapted to provide high pressure fuel to a common rail, comprising:
a) measuring the pressure PI in said common rail at a time before a pumping stroke/event;
b) measuring the pressure P2 in said common rail at a time after the pumping stroke/event;
c) determining the average pressure of said measured pressure from steps a) and b);
d) determining the time point where the measured pressure reaches the average pressure determined form step c)
e) correlating said time point with from d) with crankshaft position to determine said relative phasing.
2. A method as claimed in claim 1 wherein said time point in d) is assumed to be the mid-stroke in a pumping event of said piston pump.
3. A method as claimed in claim 2 wherein said correlation includes determining the phase difference between the top dead centre after the pumping stroke from said assumed mid-stroke time point and cam geometry.
4. A method as claimed in claims 1 to 3 wherein step e) comprises correlating said time point with a crankshaft signal, said crankshaft signal including a phasing reference point.
5. A method as claimed in claims 1 to 4 wherein said crankshaft signal comprises a series of pulses generated as crankshaft teeth pass in proximity to a sensor, and said reference point comprises a tooth having an irregular pitch or gap.
6. A method as claimed in any preceding claim wherein said pressure PI is that measured during a first plateau phase before a pumping stroke and the pressure P2 is measured during a second higher plateau phase after said pumping stroke.
7. A method as claimed in claim 6 wherein said pressure PI is the average pressure Pavl over a timespan in said first plateau phase and said pressure P2 is the average pressure Pav2 over a timespan of said sensor plateau phase.
EP17784618.5A 2016-10-14 2017-10-11 Method to determine fuel pump phasing Active EP3526459B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1617450.0A GB2554917B (en) 2016-10-14 2016-10-14 Method to determine fuel pump phasing
PCT/EP2017/075898 WO2018069377A1 (en) 2016-10-14 2017-10-11 Method to determine fuel pump phasing

Publications (2)

Publication Number Publication Date
EP3526459A1 true EP3526459A1 (en) 2019-08-21
EP3526459B1 EP3526459B1 (en) 2020-12-09

Family

ID=57680824

Family Applications (1)

Application Number Title Priority Date Filing Date
EP17784618.5A Active EP3526459B1 (en) 2016-10-14 2017-10-11 Method to determine fuel pump phasing

Country Status (3)

Country Link
EP (1) EP3526459B1 (en)
GB (1) GB2554917B (en)
WO (1) WO2018069377A1 (en)

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10023227A1 (en) * 2000-05-12 2001-11-22 Bosch Gmbh Robert System to determine the position of a high-pressure fuel injection piston in relation to the crankshaft angle establishes the piston top and bottom dead points from the variation in the stored pressure
DE10115262C2 (en) * 2001-03-28 2003-04-24 Bosch Gmbh Robert Method for determining the rotational position of the camshaft of an internal combustion engine
JP3965098B2 (en) * 2002-09-30 2007-08-22 ヤンマー株式会社 Fuel pressure detection device for common rail type fuel injection device and common rail type fuel injection device provided with the fuel pressure detection device
JP2005307747A (en) * 2004-04-16 2005-11-04 Mitsubishi Electric Corp Fuel supply device for internal combustion engine
JP2005337031A (en) * 2004-05-24 2005-12-08 Mitsubishi Electric Corp High pressure fuel system abnormality diagnosis device for in-cylinder fuel injection internal combustion engine
EP2042720B1 (en) * 2007-09-26 2010-03-10 Magneti Marelli S.p.A. Control method of a direct injection system of the common rail type provided with a high-pressure fuel pump
EP2634407A1 (en) * 2012-02-29 2013-09-04 Volvo Car Corporation Camshaft position determination system
GB2526323A (en) * 2014-05-20 2015-11-25 Gm Global Tech Operations Inc An electronic control unit for an internal combustion engine
FR3035684B1 (en) * 2015-04-28 2019-07-12 Continental Automotive France METHOD FOR DETERMINING THE ANGULAR TIMING RELATING TO A COMBUSTION ENGINE AND A FUEL SUPPLY PUMP

Also Published As

Publication number Publication date
GB2554917B (en) 2020-04-08
EP3526459B1 (en) 2020-12-09
GB201617450D0 (en) 2016-11-30
GB2554917A (en) 2018-04-18
WO2018069377A1 (en) 2018-04-19

Similar Documents

Publication Publication Date Title
CN101994575B (en) For the controlling method of common rail fuel pump and the device for performing the method
US9371794B2 (en) Method and control unit for controlling an internal combustion engine
US9347413B2 (en) Method and control unit for controlling an internal combustion engine
CN108350824B (en) Method for combined identification of stroke phase difference of piston, inlet valve and outlet valve of internal combustion engine
EP3199788B1 (en) Control device for internal combustion engine
EP2835518A1 (en) Method to Determine Bulk Modulus of a Fuel
CN107013352B (en) Control device for internal combustion engine
JP5858793B2 (en) Fuel supply device for internal combustion engine
JP2016196866A (en) Engine control system
CN102644519A (en) Fuel injection system for internal combustion engine
US9562504B2 (en) Fuel pump for an internal combustion engine
US10125749B2 (en) Pump, in particular a high-pressure fuel pump
JP5892649B2 (en) High pressure fuel pump reference point detection method and common rail fuel injection control device
US10837383B2 (en) Method for estimating a top dead centre for a high-pressure pump of a fuel injection system in an automotive vehicle engine
EP3526459B1 (en) Method to determine fuel pump phasing
RU2681560C1 (en) Method for determining actual stroke in cylinder of engine with progressively moving pistons
CN108026857B (en) Method for controlling rail pressure in an injection system
JP5556209B2 (en) High-pressure fuel pump reference time calculation device
WO2015052909A1 (en) Control device for internal combustion engine
JP5825266B2 (en) Fuel supply system
EP2143913A1 (en) High-pressure pump cam top position detecting device
JP4650449B2 (en) Fuel supply device
JP5314078B2 (en) Control device for internal combustion engine
JPH01116271A (en) Fuel injection quantity control device
WO2019216337A1 (en) Engine control device and engine

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: UNKNOWN

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20190514

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20200703

RIN1 Information on inventor provided before grant (corrected)

Inventor name: LOQUAIS, PEDRO

Inventor name: MICHOU, ANTHONY

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1343688

Country of ref document: AT

Kind code of ref document: T

Effective date: 20201215

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602017029345

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210310

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210309

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1343688

Country of ref document: AT

Kind code of ref document: T

Effective date: 20201209

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210309

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20201209

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210409

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602017029345

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210409

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

26N No opposition filed

Effective date: 20210910

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20210409

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20211031

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211011

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211031

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211031

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211031

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20211011

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230327

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20171011

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 602017029345

Country of ref document: DE

Owner name: PHINIA DELPHI LUXEMBOURG SARL, LU

Free format text: FORMER OWNER: DELPHI TECHNOLOGIES IP LIMITED, SAINT MICHAEL, BB

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

REG Reference to a national code

Ref country code: GB

Ref legal event code: 732E

Free format text: REGISTERED BETWEEN 20240725 AND 20240731

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20250911

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20250912

Year of fee payment: 9

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20201209

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20250912

Year of fee payment: 9