Method and system of intensifier piston control

Information

  • Patent Grant
  • 6663014
  • Patent Number
    6,663,014
  • Date Filed
    Friday, June 28, 2002
    22 years ago
  • Date Issued
    Tuesday, December 16, 2003
    21 years ago
Abstract
The movement of the intensifier piston in a fuel injector, to control the pressurization of fuel, can be controlled with a flow control valve. The flow control valve provides different flow rates depending upon the direction of flow. In a first direction, flow control valve has a first rate of flow and in the second direction flow control valve allows a second different rate of flow. Typically, this can be applied to a intensifier piston as follows: flow traveling to the intensifier piston, in the first direction, has a first flow rate, allowing the intensifier to move downward and pressurize fuel. When injection is over, and the intensifier piston is vented, the flow control valve allows a second flow rate which is greater than the first flow rate, allowing the intensifier piston to vent quickly and reset for another injection.
Description




TECHNICAL FIELD




The present invention relates to fuel injection and specifically to the ability to control flow rates to and from an intensifier piston and the ability to reset the intensifier piston quickly.




BACKGROUND




Reducing emissions is a top priority for today's engine manufacturers. As the government continues to tighten emission requirements, manufacturers must find new ways to reduce engine emissions while still providing powerful, economic engine operation. One area that engine manufacturers have focused on is fuel injection.




Fuel injection plays a crucial role in the amount of emissions created during combustion. Numerous fuel injection variables, including fuel pressure, spray pattern, droplet size, number of injections and injection timing impact emissions. In order to properly control these parameters, fuel injectors have become more complicated and more precise. For example, one exemplary design of a fuel injector is a hydraulically actuated electronically controlled unit injector such as a Caterpillar HEUT™ B unit injector. This unit injector uses actuation fluid to pressurize fuel for injection. Specifically, a control valve and spool valve control the timing of high pressure actuation fluid acting upon an intensifier piston. When high pressure actuation fluid acts on the intensifier piston, the hydraulic force overcomes a biasing force from a piston spring and moves the piston downward, also moving a plunger, which pressurizes fuel in the pressurization cavity for injection. When injection is over, the control valve allows the high pressure actuation fluid acting on the intensifier piston to vent. This allows a piston spring to push the intensifier piston and plunger back to their original position and reset them for the next injection




As emissions regulations have increased, injection strategies have become more complicated. For example, multiple injections, including pilots and posts, reduce emissions during combustion. However, it can be difficult for the Injector to cycle quickly enough to perform multiple injections during a single combustion event. In the hydraulically actuated electronically controlled unit injector described above, multiple injections can be performed by cycling the control valve but depending on the dwell time between injections and the desired injection profile, the intensifier piston may not properly reset between injections.




The present invention is intended to overcome one or more of the above problems.




SUMMARY OF THE INVENTION




A fuel injector comprises a high pressure actuation fluid source, a lower pressure drain, at least one fluid line selectively to one of high pressure actuation fluid source and lower pressure drain, an intensifier piston fluidly connected to the fluid line and a flow control valve. The flow control valve is in fluid communication with the fluid line and the intensifier piston and position to control the rate of flow to and from the intensifier piston. The flow control valve has a first flow rate in the first direction and a second flow rate in a second direction, the second rate being different from the first.




In another embodiment, a fuel injector comprises a high pressure actuation fluid source, a low pressure drain, flow control valve connected with the high pressure actuation fluid source and the low pressure drain and intensifier piston connected to flow control valve. The control flow valve controls the flow rate between the flow control valve and the intensifier piston and has a first flow rate in the first direction and a second flow rate in the second direction.




In another embodiment, a method of controlling intensifier piston comprises pressurizing the intensifier piston at a first flow rate and venting the intensifier piston at a second flow rate, wherein the second flow rate is different than the first flow rate.




In another embodiment of the present invention, a fuel injector comprises a high pressure actuation fluid source, low pressure drain, at least one fluid line selectively connected to one of the high pressure actuation fluid source and low pressure drain, and intensifier piston fluidly connected to the fluid line, and a flow control valve. The flow control is in fluid communication with the fluid line and the intensifier piston and position to control flow to and from the intensifier piston. Further, the flow control valve has a flow in a first direction and a second direction having a flow control valve having a flow restriction for flow in the first direction.




In another embodiment, fuel injector comprises high pressure actuation fluid source, low pressure drain, at least one fluid line, means for selectively connecting the fluid line to one of the high pressure actuation fluid source and low pressure drain, an intensifier piston fluidly connected to the fluid line, and a flow control. The flow control valve is in fluid communication with the fluid line and the intensifier piston and in position to control a rate of flow to and from the intensifier piston. Further, the flow control valve has a first flow rate in the first direction and a second flow rate, different from the first flow rate, in the second direction.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a diagrammatic illustration of a cross section of a fuel injector according to one embodiment of the present invention.





FIG. 2

is a diagrammatic illustration of a bottom view of a damper plate according to the embodiment of FIG.


1


.





FIG. 3

is a diagrammatic illustration of a cross section of a flow control valve along line


3





3


of the embodiment illustrated in FIG.


1


.





FIG. 4

is a diagrammatic illustration of a cross section of a flow control valve along line


3





3


of the embodiment illustrated in FIG.


1


.





FIG. 5

is a diagrammatic illustration of a cross section of a flow control valve along line


5





5


of the embodiment illustrated in FIG.


1


.





FIG. 6

is an enlarged diagrammatic illustration of a cross section of a flow control valve according to another embodiment of the present invention.











DETAILED DESCRIPTION





FIG. 1

is a diagrammatic illustration of a hydraulically actuated electronically controlled unit injector


10


. Fuel enters injector


10


through fuel inlet passage


12


, passes ball check


14


and enters fuel pressurization chamber


16


. High pressure actuation fluid enters injector


10


through actuation fluid inlet passage


18


. Actuation fluid then travels to control valve


20


and spool valve


22


.




Control valve


20


controls the overall operation of injector


10


and operates as a pilot valve for spool valve


22


. Control valve


20


includes an armature


24


and a seated pin


26


. A solenoid (not shown) in control valve


20


controls movement of armature


24


and therefore the position of the seated pin


26


. In a first position, seated pin


26


allows high pressure actuation fluid to travel through upper check passage


28


and lower check passage


32


to check control cavity


34


. When seated pin


26


is in the first position, high pressure actuation fluid also travels through upper check passage


28


to spool passage


36


to balance spool valve


22


in its first position. When seated pin


26


is in its second position, high pressure actuation fluid from actuation fluid inlet passage is blocked and upper check passage


28


, lower check passage


32


, check control cavity


34


and spool passage


36


are open to low pressure drain


38


.




When seated pin


26


is moved to its second position, the spool passage


36


is open to low pressure drain


38


, which unbalances spool valve


22


and allows high pressure actuation fluid to travel through upper intensifier passage


40


, into damper plate


42


where the flow is split in to two passages; middle intensifier passage


44


and upper rate shaping passage


46


. High pressure actuation fluid in middle intensifier passage


44


proceeds to lower intensifier passage


48


, in central body


50


where it acts upon piston hat


52


of intensifier piston


54


. Flow also travels from upper rate shaping passage


46


through flow control valve


56


to lower rate shaping passage


58


where the high pressure actuation fluid acts on the shoulder


60


of intensifier piston


54


.




When high pressure actuation fluid acts upon intensifier piston


54


, intensifier piston


54


moves downward, against the force of piston spring


62


, causing plunger


64


to move downward and pressurize fuel in fuel pressurization chamber


16


. Fuel in fuel pressurization chamber


16


is pressurized to injection pressure and is directed through high pressure fuel passage


66


and into fuel cavity


68


.




Check


70


is located in the nozzle assembly of injector


10


and controls the flow of fuel through orifices


72


, in nozzle tip


74


, into the combustion chamber (not shown). Check


70


is biased in the closed position by check spring


76


. High pressure fuel in fuel cavity


68


acts on an opening surface


78


of check


70


and pushes it upwards, against check spring


76


, into the open position, allowing injection through orifice


72


. Check opening and closing is also hydraulically controlled by check control cavity


34


. When high pressure actuation fluid is present in check control cavity


34


, it helps keep check


70


closed even when high pressure fuel is present in fuel cavity


68


. High pressure actuation fluid acts upon a closing surface


80


of check piston


82


and hydraulically offsets and, in fact overcomes, the pressure from the high pressure fuel in fuel cavity


68


. The high pressure actuation fluid helps close check


70


in combination with check spring


76


. Injection occurs when check control cavity


34


is opened to low pressure drain


38


, leaving the pressurized fuel to overcome only the check spring's


76


force. By controlling the high pressure actuation fluid in check control cavity


34


, injection timing and duration can be more accurately controlled.




When injection is finished, seated pin


26


is returned to its first position, allowing high pressure actuation fluid into check control cavity


34


and spool passage


36


. As stated above, high pressure actuation fluid in check control cavity


34


closes check


70


. Further, high pressure actuation fluid in spool passage


36


causes spool valve


22


to return to its original position, stopping the flow of high pressure actuation fluid to the intensifier piston


54


and allowing the high pressure actuation fluid acting on the intensifier piston


54


from upper, middle, and lower intensifier passages


40


,


44


,


48


and upper and lower rate shaping passages


46


,


58


to drain, allowing intensifier piston


54


and plunger


64


to return to their original positions.




Flow control valve


56


controls the rate of flow through upper and lower rate shaping passages


46


,


58


.

FIGS. 2-5

are enlarged diagrammatic cross sections of flow control valve


56


illustrated in FIG.


1


. In this embodiment, flow control valve


56


includes rate shaping orifice plate


84


and grooved damper plate


42


. Rate shaping orifice plate


84


is a circular disk that defines rate shaping orifice


86


through the center of plate


84


. Damper plate


42


defines a circular annulus


88


and a center passage


90


that is in fluid communication with circular annulus


88


. When high pressure fluid is moving from upper rate shaping passage


46


to lower rate shaping passage


58


, as illustrated in

FIG. 4

, rate shaping orifice plate


84


is pushed down, forming a seal with central body


50


and only allowing flow through rate shaping orifice


86


. When fluid is moving from lower rate shaping passage


58


to upper rate shaping passage


46


, as illustrated in

FIG. 3

, rate shaping orifice plate


84


is moved up, away from central body


50


, allowing flow through rate shaping orifice


86


and around rate shaping orifice plate


84


in annular plate passage


91


. This allows for a higher flow rate. As illustrated in this embodiment, flow control valve


56


results in a first flow rate to pressurize intensifier piston


54


and a faster flow rate for venting the fluid acting on intensifier piston


54


.




Alternative flow control valve configurations can be implemented. Flow control valve


56


must simply allow different flow rates depending on the direction of the flow.

FIG. 6

illustrates an alternative embodiment for flow control valve


56


. Thins embodiment comprises a flow orifice


92


, located in damper plate


42


, and a flow ball check


94


located in central body


50


. When flow is moving in the first direction, from upper rate shaping passage


46


to lower rate shaping passage


58


, actuation fluid travels through flow orifice


92


but flow ball check


94


is closed. This results in a slower flow rate and less pressure on shoulder


60


. When flow is moving in the second direction, from lower rate shaping passage


58


to upper rate shaping passage


46


, venting the cavity acting on shoulder


60


, flow travels through flow orifice


92


and also through flow ball check


94


, due to the ball coming of its seat. This allows a faster venting flow rate than filling flow rate.




Industrial Applicability




Controlling injection pressure and timing is important to reducing emissions. Further, multiple injections per engine cycle, such as pilots and posts, can also have a significant impact in emissions controls. Multiple injections could include two injections per cycle or as many as five or more. As the number of injections increase, injector speed must also increase. Unfortunately, many current injectors may have a difficult time cycling or resetting fast enough to allow multiple injections per engine cycle. For example, depending on the timing of the injection events and the desired quantity per event, an intensifier piston, used to pressurize fuel for injection, may not be able to reset quickly enough to perform all necessary injections.




Flow control valve


56


allows different flow rates to and from the intensifier piston


54


. For example, flow control valve


56


allows a first flow rate to intensifier piston


54


to pressurize fuel at a desired rate (Note that this rate can adjusted and tuned by those skilled in the art by including rate shaping features, such as piston hats and rate shaping orifices.) Flow control valve


56


allows a second, faster flow rate away from intensifier piston


54


when the actuation passages are open to drain. This allows for quicker venting, allowing intensifier piston


54


to reset quicker. This allows the intensifier to handle multiple injection in the same engine cycle.




As explained above, injector


10


starts in a closed or no-injection state. Control valve


20


is in its first position providing high pressure actuation fluid to the check control cavity


34


. This insures that check


70


remains closed, preventing any fuel from entering the combustion chamber (not shown) through orifice


72


. Control valve


20


also provides high pressure actuation fluid to spool passage


36


, thereby biasing spool valve


22


in its first position, which prevents high pressure actuation fluid from acting on intensifier piston


54


and pressurizing fuel.




When injection is desired, control valve


20


is actuated causing seated pin


26


to move to its second position. This opens spool passage


36


to low pressure drain


38


, allowing spool valve


22


to move to its second position. In its second position, spool valve


22


allows high pressure actuation fluid to act upon intensifier piston


54


, which causes intensifier piston


54


and subsequently plunger


64


to move downward and pressurize fuel in fuel pressurization chamber


16


. Specifically, high pressure actuation fluid travels through upper, middle and lower intensifier passages


40


,


44


, and


48


to act upon the piston hat


52


. High pressure actuation fluid also travels through upper rate shaping passage


46


, flow control valve


56


and lower rate shaping passage


58


to act upon shoulder


60


. As the high pressure actuation fluid travels through flow control valve


56


, rate shape orifice plate


84


is pushed downward, forming a seal with central body


50


. This allows flow to only travel through rate shaping orifice


86


.




The high pressure actuation fluid acting on hat


52


and shoulder


60


causes intensifier piston


54


to move downward, moving plunger


64


, and pressurize fuel at the desired rate. (Note the rate of pressurization can change if and when the piston hat


52


comes out of the bore.) Pressurized fuel from pressurization chamber


16


then moves to fuel cavity


68


where it acts on check


70


, trying to push check


70


up, into the open position, so that injection can occur. When seated pin


26


is in the second position, check control cavity


34


is also opened to low pressure drain


38


. This results in check spring


76


being the only thing that keeps check


70


closed; however, as fuel is pressurized, the force of pressurized fuel overcomes the force of the check spring


76


and moves check


70


to its open position.




When end of injection is desired, control valve


20


is de-actuated and seated pin


26


is moved back to its first position. This results in high pressure actuation fluid traveling back in to spool passage


36


to bias spool valve


22


in its first position. Moving back to its first position, spool valve


22


blocks the high pressure actuation fluid and opens upper, middle and lower intensifier passages


40


,


44


,


48


to drain. Lower rate shaping passage


58


and upper rate shaping passage


46


are also opened to drain. As actuation fluid travels in this direction, back through flow control valve


56


, the flow rate is increased. Rate shape orifice plate


84


moves off of central body


50


allowing flow through rate shaping orifice


86


and around plate


84


in the annular plate passage


91


. By venting the high pressure actuation fluid acting on intensifier piston


54


, piston spring


62


can reset intensifier piston


54


back in its original, up position.




Additionally, when the seated pin


26


moves back to its first position, high pressure actuation fluid is again directed through upper and lower check passages


28


,


32


and back into check control cavity


34


to insure check closure.




It should be noted that the valve arrangement in the injector shown provides a fast moving control valve


20


and a slow moving spool valve


22


. This can impact the rate shaping capabilities of the injector


10


. For example, it may be possible to cycle control valve


20


quickly enough to stop and start injection without spool valve


22


ever really changing positions. In this scenario, flow control valve


56


does not play much of a role, instead it just acts as a conventional rate shaping orifice. However, when multiple injections are sufficiently spaced apart, such that spool valve


22


has time to react, flow control valve


56


allows intensifier piston


54


to reset quickly.




As illustrated above, flow control valve


56


could have alternative embodiments. Further, depending on the embodiment, more or less body parts could be used. For example, the flow control valve embodiment shown in

FIG. 6

could be implemented in one piece. Further, the size of the valve and its passages and orifices can be sized according to each injector's specific design. Those skilled in the art will understand that modeling and experimentation on valve and orifice sizes will achieve desired results.




The present example has only illustrated a single injection event but multiple injections per engine cycle could be employed. Further, actuation fluid is preferably lubrication oil but could be any variety of other engine fluids, including fuel, coolant, or steering fluid.




The present example also illustrates the use of the flow control valve in a hydraulically actuated electronically controlled unit injector; however, the flow control valve could be used in a variety of other injector types, including common rail systems, or other hydraulic devices.




Other aspects, features, and advantages of the present invention may be obtained from a study of this disclosure and the drawings, along with the appended claims.



Claims
  • 1. A fuel injector comprising:a high pressure actuation fluid source; a low pressure drain; at least one fluid line selectively connected to one of said high pressure actuation fluid source and said low pressure drain; an intensifier piston fluidly connected to said fluid line; a flow control valve in fluid communication with said fluid line and said intensifier piston and positioned to control a rate of flow to and from said intensifier piston; and said flow control valve having a first flow rate in a first direction and a second rate, different from said first rate in a second direction.
  • 2. The fuel injector of claim 1 further including:a control valve to selectively connect said fluid line to one of said high pressure actuation fluid source and said low pressure drain.
  • 3. The fuel injector of claim 1 wherein said control valve and said flow control valve are a single valve.
  • 4. The fuel injector of claim 1 wherein:said first direction includes flow from said high pressure source to said intensifier piston; and said second direction includes flow from said intensifier piston to said low pressure drain.
  • 5. The fuel injector of claim 4 wherein:said first flow rate is less than said second flow rate.
  • 6. The fuel injector of claim 1 wherein said flow control valve is passively operated.
  • 7. The fuel injector of claim 1 wherein said flow control valve includes a rate shape orifice plate.
  • 8. The fuel injector of claim 1 wherein said flow control valve includes a flow orifice and a flow ball check.
  • 9. A fuel injector comprising:a high pressure actuation fluid source; a low pressure drain; a flow control valve connected with said high pressure actuation fluid source and said low pressure drain; an intensifier piston connected to said flow control valve; said flow control valve controlling the flow rate between said flow control valve and said intensifier piston and having a first flow rate in a first direction and a second flow rate, different from said first flow rate, in a second direction.
  • 10. The fuel injector of claim 9 further including:a control valve connected to said high pressure actuation fluid source and said low pressure drain; and said control valve selectively connecting said flow control valve to one of said high pressure actuation fluid source and said low pressure drain.
  • 11. The fuel injector of claim 9 wherein:said first direction includes flow from said flow control valve to said intensifier piston; and said second direction includes flow from said intensifier piston to said flow control valve.
  • 12. The fuel injector of claim 11 wherein:said first flow rate is less than said second flow rate.
  • 13. The fuel injector of claim 9 wherein said flow control valve is passively operated.
  • 14. The fuel injector of claim 9 wherein said flow control valve includes a rate shape orifice plate.
  • 15. The fuel injector of claim 9 wherein said flow control valve includes a flow orifice and a flow ball check.
  • 16. A fuel injector comprising:a high pressure actuation fluid source; a low pressure drain; at least one fluid line selectively connected to one of said high pressure actuation fluid source and said low pressure drain; an intensifier piston fluidly connected to said fluid line; a flow control valve in fluid communication with said fluid line and said intensifier piston and positioned to control flow to and from said intensifier piston; and said flow control valve having a flow in a first direction and a second direction and said flow control valve having a flow restriction for said flow in said first direction.
  • 17. A fuel injector comprising:a high pressure actuation fluid source; a low pressure drain; at least one fluid line; means for selectively connecting said fluid line to one of said high pressure actuation fluid source and said low pressure drain; an intensifier piston fluidly connected to said fluid line; a flow control valve in fluid communication with said fluid line and said intensifier piston and positioned to control a rate of flow to and from said intensifier piston; and said flow control valve having a first flow rate in a first direction and a second rate, different from said first rate in a second direction.
US Referenced Citations (4)
Number Name Date Kind
6024296 Wear et al. Feb 2000 A
6050497 Cotton Apr 2000 A
6113000 Tian Sep 2000 A
6119960 Graves Sep 2000 A