Digital valve

Information

  • Patent Grant
  • 6662783
  • Patent Number
    6,662,783
  • Date Filed
    Wednesday, March 27, 2002
    22 years ago
  • Date Issued
    Tuesday, December 16, 2003
    21 years ago
Abstract
A control valve for a fuel injector generally includes a valve body and a spool positioned within a bore of said valve body. The spool is slideable between a first and second position. The control valve also comprises a first bore in fluid communication with a rail inlet of the fuel injector, a cross bore positioned within the valve body and offset from the first bore, and a groove located about the spool. The groove provides fluid communication between the cross bore and the first bore when the spool is in the first position, and seals fluid communication when the spool is in the second position. At least two solenoids are provided on opposing sides of the spool for moving the spool between the first and second positions, and a non-magnetic barrier is provided between the solenoids and the spool.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention generally relates to an oil activated fuel injector. More particularly, the present invention relates to a digital control valve used with an oil activated, electronically or mechanically controlled fuel injector.




2. Background Description




There are many types of fuel injectors designed to inject fuel into a combustion chamber of an engine. For example, fuel injectors may be mechanically, electrically, or hydraulically controlled in order to inject fuel into the combustion chamber of the engine. In the hydraulically actuated systems, a control valve body may be provided with two-, three-, or four-way valve systems, each having grooves or orifices that allow fluid communication between working ports, high pressure ports, and venting ports of the control valve body of the fuel injector and the inlet area. The working fluid is typically engine oil or other types of suitable hydraulic fluid that is capable of providing a pressure within the fuel injector in order to begin the process of injecting fuel into the combustion chamber.




In current designs, a driver will deliver a current or voltage to an open side of an open coil solenoid. The magnetic force generated in the open coil solenoid will shift a spool into the open position so as to align grooves or orifices (hereinafter referred to as “grooves”) of the control valve body and the spool. The alignment of the grooves permits the working fluid to flow into an intensifier chamber from an inlet portion of the control valve body (via working ports). The high pressure working fluid then acts on an intensifier piston to compress an intensifier spring and hence compress fuel located within a high pressure plunger chamber. As the pressure in the high pressure plunger chamber increases, the fuel pressure will begin to rise above a needle check valve opening pressure. At the prescribed fuel pressure level, the needle check valve will shift against the needle spring and open the injection holes in a nozzle tip. The fuel will then be injected into the combustion chamber of the engine.




However, in such a conventional system, a response time between the injection cycles may be slow, thus decreasing the efficiency of the fuel injector. This is mainly due to the slow movement of the control valve spool. More specifically, the slow movement of the control valve may result in a slow activation response time to begin the injection cycle. To remedy this inadequacy, additional pressurized working fluid may be needed; however, additional energy from the high pressure oil pump must be expended in order to provide this additional working fluid. This leads to an inefficiency in the operations of the fuel injector itself. Also, the working fluid at an end of an injection cycle may not be vented at an adequate response rate due to the slow movement of the control valve spool.




Other prior art systems use a small step at the end of the spool to reduce the area where the spool and the solenoid are in contact. However, these steps introduce wear due to impact between parts and reduced magnetic force between the spool and the solenoids.




SUMMARY OF THE INVENTION




According to a first aspect of the invention, a control valve for a fuel injector generally includes a valve body and a spool positioned within a bore of said valve body. The spool is slideable between a first and second position. The control valve also comprises a first bore in fluid communication with a rail inlet of the fuel injector, a cross bore positioned within the valve body and offset from the first bore, and a groove located about the spool. The cross bore, in embodiments, leads to ambient, and the first bore may be located within the valve body. The groove provides fluid communication between the cross bore and the first bore when the spool is in the first position, and seals fluid communication when the spool is in the second position. At least two solenoids are provided on opposing sides of the spool for moving the spool between the first and second positions, and a non-magnetic barrier is provided for controlling latching forces between the spool and at least one of the at least two solenoids when the spool is in the first position or the second position. The latching forces are created by a current pulse of one of the at least two solenoids. In embodiments, the solenoids are provided in end caps. The non-magnetic barrier may be a non-magnetic shim or a non-magnetic coating, and is preferably selected based upon the required or developed latching forces between the spool and the solenoids.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

shows an oil activated fuel injector used with a control valve according to the present invention;





FIG. 2

shows an embodiment of the present invention;





FIG. 3



a


shows an exploded view of the control valve of the present invention;





FIG. 3



b


shows an exploded view of an embodiment of the control valve body of the present invention;





FIG. 4

shows an exploded view of the control valve of the present invention in a closed position;





FIG. 5

shows an exploded view of the control valve of the present invention in an open position;





FIG. 6

shows an embodiment of the valve body with a spool in a first position used with the control valve of the present invention; and





FIG. 7

shows the embodiment of the valve body with a spool in a second position used with the control valve of the present invention.











DETAILED DESCRIPTION OF A PREFERRED EMBODIMENT OF THE INVENTION




The present invention is directed to an oil activated, electronically, mechanically, or hydraulically controlled fuel injector, and more particularly to a digital control valve used with an oil activated fuel injector. The digital control valve of the present invention is capable of providing a short control valve stroke that, in turn, translates into a fast response time for the outflow of the inlet rail pressure. The oil activated fuel injector of the present invention will thus increase efficiency of the injection cycle.




Embodiments of the Oil Activated Fuel Injector of the Present Invention




Referring now to

FIG. 1

, the fuel injector is generally depicted as reference numeral


100


and includes an inlet port


102


, which receives working fluid, for example engine lubricant, from an inlet rail (not shown). The fuel injector


100


also includes a body


104


having a flat body area


106


and a central bore


108


. The central bore


108


includes a first diameter


108




a


and a second diameter


108




b


. In embodiments, the first diameter


108




a


is slightly smaller than the second diameter


108




b


. A spool


110


is slidably positioned within the central bore


108


and includes a groove


112


positioned within the first diameter


108




a


. The groove includes a first leading edge


112




a


and a second leading edge


112




b


, and provides fluid communication between the inlet port


102


and the bore or working port


114


, which leads to the intensifier chamber. A venting space


107


is developed between the first leading edge


112




a


and the flat body area


106


in the position of the spool


110


of FIG.


1


. It should be recognized by those of ordinary skill in the art that the venting space


107


is sealed when the spool


110


is moved in the direction of arrow “A.” As discussed in more detail below, the working fluid in the intensifier chamber is allowed to vent via the space


107


at the termination of the injection cycle.




The spool


110


further includes a throttle


116


, which provides fluid communication between the inlet port


102


and a pressure chamber


118


. The pressure chamber


118


is defined by a partial bore


118




a


within the spool


110


and a servo piston


119


. The servo piston


119


is partly located within the partial bore


118




a


and further includes a central bore


119




a


. The central bore


119




a


is in fluid communication with the pressure chamber


118


, which provides, in part, a mechanism for the working fluid to be vented to ambient during an initial stage of the injection cycle.




Still referring to

FIG. 1

, a control valve


120


includes a spool body


124


(also referred to as a control valve body or valve body) having a bore


122


in axial alignment with the central bore


119




a


of the servo piston


119


. The spool body


124


also includes a cross bore


125


leading to ambient. A spool


126


, slidably positioned within the spool body


124


, includes a groove


126




a


, which, in a first, or activated, position of the spool


126


, overlaps with the bore


122


and the cross bore


125


to provide fluid communication therebetween. In turn, this position of the groove


126




a


(that is, when the spool


126


is activated) provides a flow path for the working fluid from the inlet port


102


to ambient via (i) the inlet port


102


; (ii) the throttle


116


; (iii) the pressure chamber


118


; (iv) the central bore


119




a


; (v) the bore


122


; (vi) the groove


126




a


; (vii) the cross bore


125


; and (viii) ambient. At this pressure stage, the pressure within the pressure chamber


118


will be substantially equal to that of the inlet rail pressure.




In more particularity, in a first, or activated, position of the spool


126


, the groove


126




a


overlaps both the bore


122


and the cross bore


125


. In this position, the pressure within the pressure chamber


118


will be lower than that of the inlet rail pressure, which, in turn, allows the slideable spool


110


to move in the direction of arrow “A.” At this spool


110


position, the first leading edge


112




a


is positioned within the inside edge of the flat body area


106


(that is, within the central bore


108


), thus sealing the venting space


107


. This allows working fluid to flow from the inlet port


102


through the bore


114


and into the intensifier body in order to begin an injection cycle.




In a second, or deactivated, position of the spool


126


, the groove


126




a


no longer overlaps with the bore


122


and the cross bore


125


, and hence will not lead the working fluid to ambient. In this spool


110


position, the working fluid will flow from the inlet port


102


to the pressure chamber


118


via the throttle


116


. This will increase the pressure within the pressure chamber


118


to a pressure which is substantially equal to that of the inlet rail pressure. In turn, this increased or higher pressure will force the slideable spool


110


to move in the direction of arrow “B” to a second position, thus moving the first leading edge


112




a


beyond the outside edge of the flat body area


106


, and hence forming the venting space


107


. The working fluid within the intensifier chamber will be vented to ambient via the venting space


107


, thus ending the injection cycle.





FIG. 1

further shows the remaining portions of the fuel injector


100


used with the control valve


120


of the present invention. It should be understood by one skilled in the art that the control valve


120


of the present invention may equally be used with other configurations of fuel injector


100


. By way of example only, and without limitation, these other configurations may include a ball valve mechanism at the fuel inlet or other angled or straight bores leading to the nozzle of the injector


100


.




An intensifier body


128


is mounted to the body


104


via any conventional mounting mechanism. A seal


130


, for example, an o-ring, may be positioned between the mounting surfaces of the intensifier body


128


and the body


104


. A piston


131


is slidably positioned within the intensifier body


128


and is in contact with an upper end of a plunger


132


. An intensifier spring


133


surrounds a portion (e.g., shaft) of the plunger


132


and is further positioned between the piston


131


and a flange or shoulder formed on an interior portion of the intensifier body


128


. The intensifier spring


133


urges the piston


131


and the plunger


132


in a first position proximate to the body


104


.




As further seen in

FIG. 1

, a fuel inlet


134


is formed within the intensifier body


128


proximate an end portion


132




a


of the plunger


132


. The fuel inlet


134


provides fluid communication between a high pressure chamber


136


and a fuel area (not shown). This fluid communication allows fuel to flow into the high pressure chamber


136


from the fuel area during an up-stroke of the plunger


132


. A check disk


135


is positioned below the intensifier body


128


remote from the inlet port


102


. The combination of an upper surface


135




a


of the check disk


135


, the end portion


132




a


of the plunger


132


, and an interior wall


128




a


of the intensifier body


128


forms the high pressure chamber


136


. The check disk


135


also includes a fuel bore


138


in fluid communication with the high pressure chamber


136


.





FIG. 1

further shows a nozzle


140


and a spring cage


142


. The spring cage


142


is positioned between the nozzle


140


and the check disk


135


, and includes a fuel bore


144


in fluid communication with the fuel bore


138


of the check disk


135


. The spring cage


142


also includes a centrally located bore


148


having a first bore diameter


148




a


and a second, smaller bore diameter


148




b


. A spring


150


and a spring seat


151


are positioned within the first bore diameter


148




a


of the spring cage


142


, and a pin


154


is positioned within the second, smaller bore diameter


148




b.






The nozzle


140


includes an angled bore


146


in alignment with the bore


144


of the spring cage


142


. A needle


156


is preferably centrally located within the nozzle


140


and is urged downwards by the spring


150


via the pin


154


. A fuel heart chamber


152


surrounds the needle


156


and is in fluid communication with the bore


146


. In embodiments, a nut


160


is threaded about the intensifier body


128


, the check disk


135


, the nozzle


140


, and the spring cage


142


.





FIG. 2

shows an embodiment of the present invention. In this embodiment, the high pressure chamber


118


is positioned between the end of the spool


110


and the valve body


124


. That is, a portion of the central bore


108


forms the high pressure chamber


118


between the spool


110


and the valve body


124


. The bore


119




a


is located within the spool


110


and provides fluid communication between the high pressure chamber


118


and the throttle


116


. The embodiment of

FIG. 2

further shows the high pressure chamber


118


in fluid communication with the bore


122


, with all of the remaining features and advantages substantially the same ad the embodiment of FIG.


1


.




As to the advantages and remaining features, it is noted by way of example only that in a first, or activated, position of the spool


126


, the slidable spool


110


will move in the direction of arrow “A” such that the first leading edge


112




a


is positioned within the inside edge of the flat body area


106


. As previously discussed, this allows working fluid to flow in to the intensifier body in order to begin an injection cycle. In a second, or deactivated, position of the spool


126


, working fluid will flow into the pressure chamber


118


, thus increasing the pressure therein to a higher pressure than that of the inlet rail pressure. This is due to the fact that the groove


126




a


is no longer overlapping with the bore


122


and the cross bore


125


, and hence will not lead to ambient. In turn, this higher pressure will force the slidable spool


110


top move in the direction of arrow “B,” thus allowing the working fluid to vent from the intensifier chamber to ambient via the space


107


provided between the flat body


106


and the first leading edge


112




a.







FIG. 3



a


is an exploded view of the control valve


120


of the present invention. In this view, it is readily seen that the control valve


120


of the present invention includes the valve body


124


having the bore


122


and the cross bore


125


. Also, the spool


126


is slidably positioned within the spool body


124


, and includes a groove


126




a


that provides fluid communication between the bore


122


and the cross bore


125


when the spool


126


is in the first position. The control valve body also includes end caps


123


mounted to the control valve body


124


via a nut and bolt mechanism


127


or other mounting mechanism. A pair of coils


141


(e.g., solenoids) are used to activate and deactivate the spool


126


between the first, or open, position and the second, or closed, position, respectively. By a short current pulse of a coil


141


, the spool


126


will change positions, moving towards the activated coil


141


and remaining there by latching forces. A high latching force will delay the switching process, while a very low latching force will not guarantee that the spool


126


will stay in position.




In embodiments, the valve control body (spool body)


124


is further provided with non-magnetic shims


300


and


301


between the spool


126


and the coils


141


. Preferably, non-magnetic shims


300


,


301


are made of stainless steel and are between 10 and 60 microns in thickness. Alternatively, a non-magnetic coating (e.g., ceramic, chrome, etc.) could be used at ends of the spool


126


or on the inner pole of the coils


141


(

FIG. 3



a


). In further embodiments, as shown in

FIG. 3



b


, the non magnetic coatings or shims


300


,


301


may be on the outer pole between the end cap


124




a


and the spool body


124


. In this case, the non magnetic coating would no longer be required at ends of the spool


126


or on the inner pole of the coils. Thus, the present invention provides a large contact surface between the spool


126


and the coils


141


. This allows for less wear and improved durability of the control valve


120


. Furthermore, greater control over the latching forces is advantageously achieved, as the thickness of nonmagnetic shims


300


,


301


or non-magnetic coatings is easily controlled in response to variations in the developed or required latching force.





FIGS. 4 and 5

are exploded views of circle


45


in FIG.


3


. In

FIG. 4

, the groove


126




a


is offset from the cross bore


125


by a distance “a” when the spool


126


is in the closed, or deactivated, position. In

FIG. 5

, the groove


126




a


overlaps with the cross bore


125


by a distance “b” when the spool


126


is in the activated, or open, position. In the activated position, the groove


126




a


is also in fluid communication with the bore


122


. As seen in

FIGS. 4 and 5

, the groove


126




a


moves a total distance “s” between the open and closed positions of the spool


126


.





FIG. 6

shows an embodiment of the valve body used with the control valve of the present invention. In this embodiment, the body


104


includes a larger diameter central bore


108


, which provides more flow area for the working fluid. The body


104


further includes a cross bore


200


(leading to ambient), which has a connection to groove


202


. A front portion


204


of the spool


110


acts as a guide with a small passage to prevent piston effects. Control edges


206


and


208


of the spool


110


and control edges


210


and


212


of the body


104


are also provided. A ledge or stepped portion


214


is also provided in the valve body


108


.




As shown in

FIG. 6

, the control edge


206


is aligned with an edge of the groove


202


, and the control edge


212


is aligned with the working port


114


. In this position (that is, a second position), the return oil from the intensifier piston is in fluid communication with ambient via the bore


114


, the spool control edge


206


, the body control edge


210


to the groove


202


, and cross bore


200


. As shown in

FIG. 7

, to activate, the injection control valve opens to ambient so that the pressure in the space


118


drops. The spool then moves to the right, providing a connection between the inlet port


102


and the working port


114


by the control edges


212


of the body


104


and the control edge


208


of the spool


110


. The advantage of this embodiment is a larger flow area for given dimensions and less oil consumption to control the spool


110


. Additionally, the stop position (

FIG. 6

) is better defined with the stepped portion


214


. The closed position can also be more easily adjusted using shims (not shown).




Operation of the Oil Activated Fuel Injector of the Present Invention




In operation, a driver (not shown) will first energize a coil


141


. The energized coil


141


will then shift the spool


126


to an open position. In the open position, the groove


126




a


will overlap with the bore


122


and the cross bore


125


. This provides a fluid path for the working fluid to flow from the inlet port to ambient. In this position, the working fluid pressure within the pressure chamber


118


should be much lower than the rail inlet pressure. At this pressure stage, the spool


110


moves in the direction of arrow “A,” thus sealing the venting space


107


. This will allow the working fluid to flow between the inlet port


102


and the intensifier chamber via the working port


114


.




Once the pressurized working fluid is allowed to flow into the working port


114


, it begins to act on the piston


131


and the plunger


132


. That is, the pressurized working fluid will begin to push the piston


131


and the plunger


132


downwards, thus compressing the intensifier spring


133


. As the piston


131


is pushed downwards, fuel in the high pressure chamber


136


will begin to be compressed via the end portion


132




a


of the plunger


132


. A quantity of compressed fuel will be forced through e bores


138


,


144


,


146


into the heart chamber


152


surrounding the needle


156


. As the pressure increases further still, the fuel pressure will rise above a needle check valve opening pressure until the needle spring


150


is urged upwards. At this stage, the injection holes are open in the nozzle


140


, thus allowing a main fuel quantity to be injected into the combustion chamber of the engine.




To end the injection cycle, the driver will energize the closed coil


141


. The magnetic forced generated in the coil


141


will shift the spool


126


into the closed position, which, in turn, will offset the groove


126




a


from the cross bore


125


(FIG.


4


). At this stage, the pressure will begin to increase in the pressure chamber


118


, forcing the spool


110


in the direction of arrow “B.” This will open the venting space


107


between the flat body area


106


and the leading edge


112




a


of the spool


110


. Also, the inlet port


102


will no longer be in fluid communication with the working port


114


and intensifier chamber. The working fluid within the intensifier chamber will then be vented to ambient, and the needle spring


150


will urge the needle


156


downward towards the injection holes of the nozzle


140


, thereby closing the injection holes. Similarly, the intensifier spring


133


will urge the plunger


132


and the piston


131


into the closed, or first, position adjacent to the control valve


120


. As the plunger


132


moves upwards, fuel will again begin to flow into the high pressure chamber


136


of the intensifier body.




While the invention has been described in terms of its preferred embodiment, those skilled in the art will recognize that the invention can be practiced with modifications within the spirit and scope of the appended claims. Thus, it is intended that all matter contained in the foregoing description or shown in the accompanying drawings shall be interpreted as illustrative rather than limiting, and the invention should be defined only in accordance with the following claims and their equivalents.



Claims
  • 1. A control valve for a fuel injector, comprising:a valve body; a spool positioned within a bore of said valve body and slidable between a first position and a second position; a first bore in fluid communication with a rail inlet of the fuel injector; a cross bore positioned within said valve body and offset from said first bore; a groove located about the spool, said groove providing fluid communication between said cross bore and said first bore when said spool is in the first position and sealing fluid communication between said first bore and said cross bore when said spool is in the second position; at least two solenoids on opposing sides of said spool for moving said spool between the first and second positions; and a non-magnetic barrier for controlling latching forces between said spool and at least one of said at least two solenoids when said spool is in the first position or the second position, said latching forces being created by a current pulse of one of said at least two solenoids.
  • 2. The control valve according to claim 1, wherein said cross bore leads to ambient.
  • 3. The control valve according to claim 1, wherein said at least two solenoids are provided in at least two end caps.
  • 4. The control valve according to claim 1, wherein said first bore is located within said valve body.
  • 5. The control valve according to claim 1, wherein said control valve controls a flow of working fluid to the fuel injector.
  • 6. The control valve according to claim 1, wherein said non-magnetic barrier is a non-magnetic shim located between said at least two solenoids and said spool.
  • 7. The control valve according to claim 6, wherein said non-magnetic shim is stainless steel.
  • 8. The control valve according to claim 1, wherein said non-magnetic barrier is a non-magnetic coating on at least one of said at least two solenoids and said spool.
  • 9. The control valve according to claim 8, wherein said non-magnetic coating is selected from the group consisting of ceramic and chrome.
  • 10. The control valve according to claim 1, wherein a thickness of said non-magnetic barrier is selected based upon latching forces between said at least two solenoids and said spool.
  • 11. The control valve according to claim 10, wherein the thickness of said non-magnetic barrier is between 10 and 60 microns.
  • 12. The control valve according to claim 1, wherein said non-magnetic barrier is provided between one of (i) said at least two solenoids and said spool and (ii) between end caps and said valve body.
  • 13. A fuel injector, comprising:a fuel injector body portion; and a control valve for controlling a flow of a working fluid to said fuel injector body portion, said control valve comprising: a valve body; a spool positioned within a bore of said valve body and slidable between a first position and a second position; a first bore in fluid communication with a rail inlet of the fuel injector; a cross bore positioned within said valve body and offset from said first bore; a groove located about the spool, said groove providing fluid communication between said cross bore and said first bore when said spool is in the first position and sealing fluid communication between said first bore and said cross bore when said spool is in the second position; at least two solenoids for moving said spool between the first and second positions; and a non-magnetic barrier for controlling latching forces between said spool and at least one of said at least two solenoids when said spool is in the first position or the second position, said latching forces being created by a current pulse of one of said at least two solenoids.
  • 14. The fuel injector of claim 13, wherein said non-magnetic barrier is provided between said at least two solenoids and said spool.
  • 15. The fuel injector of claim 13, wherein said non-magnetic barrier is provided between end caps associated with the at least two solenoids and said valve body.
CROSS-REFERENCE TO RELATED APPLICATIONS

This application claims priority under 35 U.S.C. §§119(e) and 120 of U.S. Provisional Patent Application Ser. No. 60/336,708, filed Dec. 7, 2001, and is a continuation-in-part of U.S. patent application Ser. No. 09/983,037, filed Oct. 22, 2001, the contents of which are hereby incorporated by reference.

US Referenced Citations (7)
Number Name Date Kind
3792390 Boyd Feb 1974 A
4247052 Gray Jan 1981 A
4559511 Basnett et al. Dec 1985 A
4928028 Leibovich May 1990 A
5954030 Sturman et al. Sep 1999 A
6163239 Ozawa et al. Dec 2000 A
6494187 Giavi et al. Dec 2002 B2
Provisional Applications (1)
Number Date Country
60/336708 Dec 2001 US
Continuation in Parts (1)
Number Date Country
Parent 09/983037 Oct 2001 US
Child 10/106123 US