Reference has already been made to
Referring to
The Applicant has identified that it is possible to compensate for the pressure wave effects in the injector 2 and guard against substantial variation between pilot injections by modifying the pilot injection voltage discharge waveform.
The proposed solution is to minimise the delivery volume variation to control two aspects of the discharge profile:
The above aspects are shown in
As a result of the above steps, during the second pilot injection P2, the valve needle opening duration is approximately equal to the time period for a single pressure oscillation. Thus, the fuel pressure at the nozzle outlets increases to a relatively high pressure and a relatively low pressure during the same pilot delivery period. The result is that the area under the second pilot injection delivery profile (Area B) is substantially equal to the area under the first pilot injection delivery profile (Area A). Put another way, the total delivery volume is substantially unaffected by the standing wave set up in the injector nozzle and the pilot injection separation.
The above voltage discharge waveform is applicable to a ‘de-energise to inject’ injector. However, it should be appreciated that the invention is also applicable to a so-called ‘energise to inject’ injector. In such an injector, an injection event is initiated by applying a voltage charge pulse to the actuator rather than a voltage discharge pulse.
In other words, in the “de energise to inject” case the “activating voltage component” of the voltage drive profile is a voltage discharge pulse and the “deactivating voltage component” is a voltage charge pulse. In the “energise to inject case” the “activating voltage component” of the voltage drive profile is a voltage charge pulse and the “deactivating voltage component” is a voltage discharge pulse
It is to be appreciated that that the injector on time TON need not be selected to be equal to the pressure wave time period. In another embodiment, the injector on time TON may be selected to be greater than the pressure wave time period.
It is noted that the effect of the present invention will be to reduce the delivery error as depicted in
The pressure wave time period may be calculated with reference to the geometry and dimensions of the fuel injection system or alternatively can be measured on a test rig. In either case, the pressure wave time period for a given engine operating parameter may conveniently be stored in a function map 30 within the controller 20 (as indicated in
It will be understood that the embodiments described above are given by way of example only and are not intended to limit the invention, the scope of which is defined in the appended claims. It will also be understood that the embodiments described may be used individually or in combination.
Number | Date | Country | Kind |
---|---|---|---|
0610230.5 | May 2006 | GB | national |
0621156.9 | Oct 2006 | GB | national |