Advance arrangement

Information

  • Patent Grant
  • 6244252
  • Patent Number
    6,244,252
  • Date Filed
    Tuesday, November 23, 1999
    25 years ago
  • Date Issued
    Tuesday, June 12, 2001
    23 years ago
Abstract
An advance arrangement comprising an advance piston slidable within a bore under the action of fuel pressure within a control chamber, a surface associated with the piston being exposed to the fuel pressure within the control chamber. The control chamber communicates, through a restricted flow passage, with a low pressure fuel volume. A valve is operable to vary the restriction to flow formed by the restricted flow passage.
Description




This invention relates to an advance arrangement for use in controlling the timing of fuel delivery by a high pressure fuel pump.




A rotary distributor high pressure fuel pump conveniently includes an advance arrangement for use in controlling the timing of fuel delivery by the pump, and hence for controlling the timing of commencement of fuel injection through injectors associated with the pump. The advance arrangement typically comprises an angularly adjustable cam ring having a cam surface with which one or more plungers cooperate, in use. The position of the cam ring is adjustable by means of an advance piston which cooperates with a peg secured to the cam ring such that axial movement of the piston causes angular movement of the cam ring. The advance piston may be spring biased towards a first position, fuel under pressure being applied to the piston to move the piston against the spring biasing towards a second position. In a more complex arrangement, the advance piston may be of the servo-advance type. The fuel pressure applied to the advance piston is typically associated with engine speed, thus the timing of fuel injection is associated with engine speed.




It is an object of the invention to provide an advance arrangement in which corrections for other factors, for example air temperature or density, altitude or fuel cetane number, can be made to the timing of fuel delivery.




According to the present invention there is provided an advance arrangement comprising an advance piston slidable within a bore under the action of the fuel pressure within a control chamber, a surface associated with the piston being exposed to the fuel pressure within the control chamber, the control chamber communicating, through a restricted flow passage, with a low pressure fuel volume, and a valve operable to vary the restriction to flow formed by the restricted flow passage.




Conveniently, the valve may be a solenoid actuable valve.




The advance piston may simply comprise a piston slidable within a bore, or may comprise a servo-advance piston having a servo piston slidable within the advance piston controlling the position of the advance piston.











The invention will further be described, by way of example, with reference to the accompanying diagrammatic view of an advance arrangement in accordance with an embodiment of the invention.




The advance arrangement illustrated, diagrammatically, in the accompanying drawing comprises a metering valve arrangement


10


arranged to control the rate at which fuel is supplied from an inlet passage


11


which communicates with the outlet of a low pressure transfer pump (not shown) to an outlet passage


12


which communicates with the inlet of a high pressure fuel pump (not shown). The metering valve arrangement


10


comprises a valve member


13


provided with a recess, the valve member


13


being angularly adjustable within a bore to control the degree by which the end of the outlet passage


12


which communicates with the bore is obscured by the valve member


13


, thereby controlling the rate of fuel flow to the high pressure pump. The recess of the valve member


13


further communicates through a relatively small diameter drilling


14


and a recess


15


with a passage


16


. The drilling


14


, recess


15


and passage


16


are located so that the rate at which fuel flows to the passage


16


is varied when the valve member


13


is moved.




The passage


16


communicates with a control chamber


17


of an advance piston arrangement


18


. The advance piston arrangement


18


comprises an advance piston


19


slidable within a bore


20


, the control chamber


17


being defined by an end surface


19




a


of the advance piston


19


and part of the bore


20


. A spring


21


is provided within the bore


20


, the spring


21


urging the piston


19


towards a position in which the volume of the control chamber


17


is relatively small. It will be appreciated that the position adopted by the piston


19


, in use, is dependent upon the fuel pressure applied to the control chamber


17


.




The advance piston


19


is provided with a recess


22


which receives, in use, a peg or tooth attached to or forming part of a cam ring of the high pressure fuel pump, the cam ring being angularly adjustable to vary the timing of fuel delivery, the position of the cam ring being dependent upon the axial position of the piston


19


within the bore


20


.




The passage


16


further communicates with a restricted flow passage


23


which includes a first, variable flow restriction


24


, a second flow restriction


25


and a third flow restriction


26


. The restricted flow passage


23


opens into a low pressure fuel volume, for example the cam box of the high pressure fuel pump.




Intermediate the second and third flow restrictions


25


,


26


, the restricted flow passage


23


communicates with a bypass passage


27


. The bypass passage


27


opens into a chamber


28


which communicates with a further passage


29


. A valve member


30


of a solenoid actuable valve


31


is located within the chamber


28


and is moveable under the influence of the solenoid actuator of the valve


31


between a rest position (as illustrated) and an actuated position in which the end of the further passage


29


which opens into the chamber


28


is closed by the valve member


30


. It will be appreciated that, in this position, communication between the bypass passage


27


and the further passage


29


is broken. The further passage


29


also communicates with the low pressure fuel volume, for example the cam box of the high pressure fuel pump.




In use, fuel is supplied by the transfer pump to the metering valve


10


and from the metering valve to the high pressure fuel pump at a rate governed by the angular position of the valve member


13


. Fuel is also supplied through the drilling


14


and recess


15


to the passage


16


at a rate governed by the angular position of the metering valve member


13


. The fuel supplied to the passage


16


acts to pressurize the control chamber


17


, applying a force to the end surface


19




a


of the piston


19


acting against the spring


21


and urging the piston


19


towards a position governed by the fuel pressure within the control chamber


17


. The position adopted by the advance piston


19


determines the angular position of the cam ring of the high pressure fuel pump, and thus determines the timing of fuel delivery by the pump.




The fuel pressure within the control chamber


17


is not only dependent upon the rate at which fuel is supplied to the passage


16


through the valve member


13


, but is also dependent upon the rate at which fuel can flow from the passage


16


through the restricted flow passage


23


. With the solenoid actuable valve


31


in the position illustrated, the rate at which fuel is able to escape from the passage


16


through the restricted flow passage


23


is governed by the first and second restrictions


24


,


25


, the relatively unrestricted fuel flow path through the bypass passage


27


, chamber


28


and further passage


29


resulting in the third restriction


26


having little effect upon the rate of fuel flow from the passage


16


. The setting of the first restriction


24


is chosen to achieve the desired timing of fuel delivery when the valve


31


occupies its rest position, the second restriction


25


being provided to desensitise the arrangement so that small changes in the setting of the first restriction


24


have little impact upon the operation of the arrangement.




If, in use, the position of the metering valve changes to alter the fuel supply to the high pressure pump and the engine, then the fuel flow rate to the passage


16


will also vary. The fuel pressure applied to the control chamber


17


will thus change leading to a shift in the position of the piston


19


and to a change in the timing of fuel delivery by the pump.




If it is determined that the timing of fuel injection should be advanced, for example as a result of the engine operating under low ambient temperature conditions, then the actuator of the solenoid actuable valve


31


may be energized to move the valve member


30


to its alternative position in which communication between the bypass passage


27


and further passage


29


is broken. It will be appreciated that in these circumstances, fuel flowing through the restricted flow passage


23


must flow through the third restriction


26


in order to escape to the low pressure fuel volume. As a result, the rate at which fuel can escape from the passage


16


is reduced, and the fuel pressure within the control chamber


17


will rise. The increase in fuel pressure within the control chamber


17


will urge the advance piston


19


to adopt a position in which the timing of fuel delivery by the high pressure fuel pump is advanced compared to the position which would otherwise be adopted by the piston. The effect of actuating the valve


31


does not effect the maximum level of advance of the timing of fuel delivery of the timing of fuel delivery under full load conditions.




In the embodiment illustrated, the fuel pressure applied to the control chamber


17


through the metering valve


13


is arranged to vary in such a manner that fuel can flow towards the control chamber


17


at an increased rate when the engine is operating at low speed. It will be appreciated, however, that, if desired, the rate at which fuel is supplied towards the control chamber


17


may be arranged to increase with increasing engine speed.




The solenoid actuator arrangement


31


may be actuable in response to the ambient air temperature as described hereinbefore, or alternatively may be responsive to changes in air density, altitude or cetane number of the fuel.




Although in the description hereinbefore, the advance arrangement is described with reference to a fuel pump of the rotary distributor type including an angularly adjustable cam ring, it will be appreciated that the invention is also applicable to other types of fuel pump in which the timing of fuel injection can be altered. Further, although in the description hereinbefore, a simple advance piston is described, it will be appreciated that the invention is also suitable for use with servo-advance type arrangements.



Claims
  • 1. An advance arrangement comprising an advance piston slidable within a bore under the action of fuel pressure within a control chamber, a surface associated with said piston being exposed to said fuel pressure within said control chamber, said control chamber communicating, through a restricted flow passage, with a low pressure fuel volume, a valve being operable to vary the restriction to flow formed by said restricted flow passage, wherein said advance arrangement further comprises a metering valve arrangement arranged to control the rate at which fuel is supplied to an outlet in communication with a high pressure fuel pump and the rate at which fuel is supplied to said control chamber.
  • 2. The advance arrangement as claimed in claim 1, wherein said valve is a solenoid actuable valve.
  • 3. The advance arrangement as claimed in claim 1, wherein said valve includes a valve member located within a chamber and movable under the influence of an actuator.
  • 4. The advance arrangement as claimed in claim 1, wherein said advance piston comprises a piston slidable within a bore.
  • 5. The advance arrangement as claimed in claim 1, wherein said restricted flow passage comprises one or more restrictions to flow.
  • 6. The advance arrangement as claimed in claim 5, wherein said restricted flow passage comprises a variable restriction to flow.
  • 7. The advance arrangement as claimed in claim 5, wherein said restricted flow passage communicates with a by-pass passage which provides a relatively unrestricted fuel flow path between said restricted passage and said low pressure volume when said valve occupies an open position.
  • 8. The advance arrangement as claimed in claim 1, wherein said valve is operable in response to any one of the ambient air temperature, changes in air density, changes in altitude or changes in the cetane number of fuel.
  • 9. The advance arrangement as claimed in claim 1, wherein said metering valve arrangement comprises a valve member which is angularly adjustable within a bore to control said rate of fuel supply to said outlet and to said control chamber.
Priority Claims (1)
Number Date Country Kind
9826348 Feb 1998 GB
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5263457 Konrath et al. Nov 1993
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