Control unit for a fuel injector
A control unit ( 2 ) for a fuel injector ( 3 ) comprising a solenoid actuator ( 31 ) having an armature ( 33 ), the control unit configured to drive a current through an electromagnet coil ( 34 ) of the solenoid actuator in a voltage mode during at least a portion of an injection cycle.
1. A control unit for a fuel injector used or to be used in an internal combustion engine, the fuel injector comprising a solenoid actuator comprising an armature which can travel between first and second positions, the control unit configured to drive current through an electromagnet coil of the solenoid actuator to controllably position and hold the armature at a third position between the first and second positions so as to provide partial lift, wherein the control unit is configured to apply a voltage or current drive waveform such that any residual magnetic fields decay quickly at the end of the injection.
2. A control unit according to claim 1 , wherein the control unit is configured to apply the voltage or current drive waveform such that the injection results in substantially zero net magnetic flux in the solenoid actuator at the end of the injection.
3. A control unit according to claim 1 , wherein the voltage or current drive waveform comprises positive pulse(s) and negative pulse(s).
4. A control unit according to claim 1 , wherein the control unit is configured to apply the voltage or current drive waveform which results in a negative current.
5. A control unit according to claim 1 , wherein the voltage or current drive waveform is a first voltage or current drive waveform and the injection is a first injection, wherein the control unit is configured to apply a second voltage or current drive waveform for a second, next injection and to trim the second voltage or current drive waveform so as to take account of residual magnetic flux in the solenoid actuator arising from the first injection.
6. A control unit according to claim 1 , comprising:
a waveform source having an output;
an adder having first and second inputs and an output, wherein the output of the waveform source is coupled to the first input of the adder;
a drive amplifier having an input and a rectified output, wherein the output of the adder is coupled to the input of the drive amplifier;
an error amplifier having first and second inputs and an output, wherein the output of the waveform source is coupled to the first input of the error amplifier and the rectified output of the drive amplifier is coupled to the second input of the error amplifier via a pre-scaler;
a filter having an input and an output, wherein the output of the error amplifier is coupled to the input of the filter and the output of the filter is coupled to the second input of the adder,
wherein the rectified output of the drive amplifier is coupled to an output terminal for coupling to the electromagnetic coil of the solenoid actuator.
7. A control unit according to claim 1 , comprising:
a switching driver configured to employ an error signal to shorten the duration of a boost pulse by delaying its start.
8. A control unit according to claim 1 , wherein an integral of voltage applied across the electromagnet coil over the voltage or current drive waveform is substantially zero.
9. A control unit according to claim 1 , wherein the control unit is configured to apply the voltage or current drive waveform which results in partial lift.
10. A control unit according to claim 1 , wherein the control unit is configured to vary pulse widths, inter-pulse gaps, number of pulses in a pulse train and pulse amplitudes in the voltage or current drive waveform.
11. A control unit for a fuel injector used or to be used in an internal combustion engine, the fuel injector comprising a solenoid actuator comprising an armature which can travel between first and second positions, the control unit configured to drive current through an electromagnet coil of the solenoid actuator to controllably position and hold the armature at a third position between the first and second positions so as to provide partial lift, wherein the control unit is configured to apply a first voltage or current drive waveform for a first injection and to apply a second voltage or current waveform for a second, next injection, wherein the control unit is configured to trim the second voltage or current drive waveform so as to take account of residual magnetic flux in the solenoid actuator arising from the first injection.
12. A control unit according to claim 11 , comprising:
a waveform source having an output;
an adder having first and second inputs and an output, wherein the output of the waveform source is coupled to the first input of the adder;
a drive amplifier having an input and a rectified output, wherein the output of the adder is coupled to the input of the drive amplifier;
an error amplifier having first and second inputs and an output, wherein the output of the waveform source is coupled to the first input of the error amplifier and the rectified output of the drive amplifier is coupled to the second input of the error amplifier via a pre-scaler;
a filter having an input and an output, wherein the output of the error amplifier is coupled to the input of the filter and the output of the filter is coupled to the second input of the adder,
wherein the rectified output of the drive amplifier is coupled to an output terminal for coupling to the electromagnetic coil of the solenoid actuator.
13. A control unit according to claim 11 comprising:
a switching driver configured to employ an error signal to shorten the duration of the boost pulse by delaying its start.
14. A control unit according to claim 11 , wherein the control unit is configured to trim the second voltage or current drive waveform such that the second voltage or current waveform uses only a positive current.
15. A control unit according to claim 11 , wherein the control unit is configured to vary pulse widths, inter-pulse gaps, number of pulses in a pulse train and pulse amplitudes in the voltage or current drive waveform.
16. A GDI drive stage comprising the control unit according to claim 1 .
17. A GDI drive stage comprising the control unit according to claim 11 .
18. A fuel injection system comprising:
a fuel injector comprising a solenoid actuator which comprises:
at least one pole piece;
an armature;
at least one electromagnet coil arranged, in response to energisation, to cause travel of the armature between first and second positions; and
at least one spring arranged to bias the armature; and
the control unit according to claim 1 coupled to the solenoid actuator.
19. A fuel injection system comprising:
a fuel injector comprising a solenoid actuator which comprises:
at least one pole piece;
an armature;
at least one electromagnet coil arranged, in response to energisation, to cause travel of the armature between first and second positions; and
at least one spring arranged to bias the armature; and
the control unit according to claim 11 coupled to the solenoid actuator.
20. A fuel injection system according to claim 18 , wherein the solenoid actuator further comprises:
at least one permanent magnet positioned and orientated so as to latch the armature in the first and second positions when the armature is in the first and second positions respectively,
wherein the spring is arranged to bias the armature and configured to provide sufficient force so as to prevent the armature from latching in the second position.
21. A fuel injection system according to claim 19 , wherein the solenoid actuator further comprises:
at least one permanent magnet positioned and orientated so as to latch the armature in the first and second positions when the armature is in the first and second positions respectively,
wherein the spring is arranged to bias the armature and configured to provide sufficient force so as to prevent the armature from latching in the second position.
22. A fuel injection system according to claim 18 , wherein the solenoid actuator:
does not comprise any permanent magnet or
comprises at least one permanent magnet, which does not latch the armature in the first and second positions when the armature is in the first and second positions respectively.
23. A fuel injection system according to claim 19 , wherein the solenoid actuator:
does not comprise any permanent magnet or
comprises at least one permanent magnet, which do not latch the armature in the first and second positions when the armature is in the first and second positions respectively.
24. A computer program product comprising a non-transitory computer-readable medium storing a computer program which, when executed by a control unit, causes the control unit to drive current through an electromagnet coil of a solenoid actuator, used or to be used in an internal combustion engine and which comprises an armature which can travel between first and second positions, to controllably position and hold the armature at the third position between the first and second positions so as to provide partial lift and, for closely spaced injections, to apply a voltage or current drive waveform such that such that any residual magnetic fields decay quickly at the end of the injection.
25. A computer program product comprising a non-transitory computer-readable medium storing a computer program which, when executed by a control unit, causes the control unit to drive current through an electromagnet coil of a solenoid actuator, used or to be used in an internal combustion engine and which comprises an armature which can travel between first and second positions, to controllably position and hold the armature at a third position between the first and second positions so as to provide partial lift and, for closely spaced injections, to apply a first voltage or current drive waveform for a first injection and to apply a second voltage or current drive waveform for a second, next injection, wherein the control unit is configured to trim the second voltage or current drive waveform so as to take account of residual magnetic flux in the solenoid actuator arising from the first injection.