Two stage intensifier

Information

  • Patent Grant
  • 6830202
  • Patent Number
    6,830,202
  • Date Filed
    Friday, March 22, 2002
    22 years ago
  • Date Issued
    Tuesday, December 14, 2004
    19 years ago
Abstract
A two stage intensifier capable of multiple intensification rates comprises a stepped top portion and a shoulder portion, each being actuated by separate fluid passages. A stepped top portion is received into an upper bore of a piston bore and a shoulder is received into a lower bore. The stepped top forms a seal with the upper bore to prevent direct fluid communication between a first actuation cavity above the stepped top and a second actuation cavity above the shoulder.
Description




TECHNICAL FIELD




The present invention relates generally to an intensifier piston capable of multiple intensification rates.




BACKGROUND




Intensifier pistons can be used in a variety of applications in which it is necessary to intensify the pressure of a fluid from a first pressure to a second pressure. For example, intensifier pistons are very common in valve actuators and fuel injectors. Specifically, in a fuel injector, the intensifier is used to increase the fuel pressure from low or medium pressure to high pressure for fuel injection.




Intensifier pistons in a fuel injector can be cam operated or hydraulically operated. With a hydraulically operated intensifier, the top of the intensifier piston is exposed to a pressurized fluid causing the piston to move downward, thereby moving a plunger and pressurizing low pressure fuel in a pressurization chamber. The rate of intensification depends upon the pressure of the actuation fluid on top of the intensifier piston as well as the area of the intensifier piston exposed to the actuation fluid.




When intensifiers were first used in fuel injection systems, they were only able to provide one rate of intensification per injection event. This initial problem was solved with a development of a stepped top piston as illustrated in U.S. Pat. No. 5,826,562 issued Chen et al. The stepped top piston allows two different intensification rates during a single injection event. Actuation fluid is exposed to a first area, on the stepped top, causing a first intensification rate. As the piston moves downward, the stepped top comes out of its bore exposing a second actuation area, the shoulder of the intensifier, to actuation fluid and increasing the intensification ratio. Although this is a beneficial design, improvements can be made. First, there is no ability to choose intensification rates; every injection event gets both intensification profiles. Second, the design is inefficient with its actuation fluid usage because the second area must be filled with fluid as the piston moves down before the second area becomes effective. This results in the need for extra actuation fluid in the cavity, a slight delay in increased pressurization and difficulty in fully returning the plunger between injections, especially in cold conditions.




The present invention is designed at overcoming one or more of the above problems.




SUMMARY OF THE INVENTION




In the first embodiment of the present invention, a fuel injector comprises a barrel defining a first fluid passage, a second fluid passage, and a piston bore with an upper bore and a lower bore. An intensifier piston includes a shoulder and a stepped top. A first actuation cavity is defined by the upper bore, the stepped top and the first fluid passage and a second actuation cavity is defined by the lower bore, the shoulder and the second fluid passage. The piston is slidably received in the piston bore, wherein the shoulder is received in the lower bore and the stepped top is received in the upper bore. The stepped top has a first surface open to fluid pressure in the first actuation cavity and the shoulder has a second surface open to the fluid pressure in the second actuation cavity. The piston is movable between the first position and the second piston and the stepped top is sealable with the upper bore when the piston moves between the first position and the second position. Additionally, the fuel injector comprises a source of actuation fluid, a drain passage, and a control valve to open and close fluid communication between the first and second fluid passages and the source of actuation fluid and the drain.




In a second embodiment of the present invention, a method for operating an intensifier piston, having a first effective area and a second effective area, comprises delivering a first fluid flow from a common fluid source to the first area, moving the intensifier piston a first pre-selected distance, delivering a second fluid flow from the common fluid source to the second area, moving the intensifier piston a second pre-selected distance, and maintaining the first area in direct fluid isolation from the second area.




In the third embodiment of the present invention, a method for operating an intensifier piston system includes delivering a first signal, moving a valve to a first position response to the first signal, allowing fluid flow to a first effective area of an intensifier piston, delivering a second signal, moving the valve to a second position response to the second signal and allowing the fluid flow to a second effective area of the intensifier piston.




In a fourth embodiment of the present invention, an intensifier assembly comprises a barrel defining a first fluid passage, a second fluid passage and a piston bore having an upper bore and a lower bore. An intensifier piston includes a shoulder and a stepped top. A first actuation cavity is defined by the upper bore, the stepped top and the first fluid passage. A second actuation cavity is defined by the lower bore, shoulder and the second fluid passage. The piston is slidably received in the piston bore, wherein the shoulder is received in the lower bore and the stepped top is received in the upper bore. The stepped top has a first surface open to fluid pressure in the first actuation cavity and a shoulder has a second surface open to fluid pressure in the second actuation cavity. Finally, the piston is movably between a first position and a second position wherein the stepped top is sealable with the upper bore when the piston moves between the first position and the second position.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a diagrammatic cross-section of a fuel injector according to the present invention.





FIG. 2

is a diagrammatic illustration of a rate shape according to one embodiment of the present invention.





FIG. 3

is a diagrammatic illustration of a rate shape according to one embodiment of the present invention.





FIG. 4

is a diagrammatic illustration of a rate shape according to one embodiment of the present invention.











DETAILED DESCRIPTION





FIG. 1

is a diagrammatic cross-section of a fuel injector


20


according to the present invention. Fuel injector


20


includes a control valve


22


an upper body


24


and a nozzle assembly


26


. Supply line


28


provides actuation fluid through upper body


24


to control valve


22


.




Control valve


22


includes a valve body


30


, a three position spool


32


and first valve spring


34


and second valve spring


36


. Spool


32


is actuated by solenoid


38


against the biasing force of first and second valve springs


34


and


36


. Spool valve


32


controls fluid communication of actuation fluid between supply line


28


or drain


40


and first pressure passage


42


and second pressure passage


44


.




First pressure passage


42


and second pressure passage


44


carry actuation fluid from control valve


22


through barrel


46


, in the upper body


24


, to piston


48


. Piston


48


is the intensifier piston which intensifies fuel within injector


20


. Piston


48


includes a stepped top


50


, with a first actuation area


52


, and a shoulder


53


, with a second actuation area


54


. Piston


48


is slidably received within piston bore


55


, which has an upper bore


56


and a lower bore


57


. The stepped top


50


is received in upper bore


56


and shoulder


53


is received in lower bore


57


. A first actuation cavity


58


is formed by stepped top


50


, upper bore


56


, and first pressure passage


42


. A second actuation cavity


59


is formed by shoulder


53


, lower bore


56


and second pressure passage


44


. Finally, stepped top


50


forms a seal with upper bore


56


to prevent direct fluid communication between first actuation cavity


58


and second actuation cavity


59


.




When first or second actuation areas are exposed to actuation fluid from first or second pressure passages


42


and


44


, piston


48


is moved downward, actuating plunger


60


. When actuated, plunger


60


pressurizes fuel in pressurization chamber


62


. Piston


48


is generally biased in its upward position by piston return spring


63


and piston return spring


63


returns piston


48


to it upward position when first and second pressure passages


42


and


44


are vented to drain


40


.




Fuel for injection enters the injector through fuel fill line


64


and passes through ball check


65


into pressurization chamber


62


. Pressurized fuel from pressurization chamber


62


moves through fuel passage


66


and into fuel chamber


68


. Check valve


70


, biased in the close position by check spring


72


, controls fluid communication of fuel between fuel chamber


68


and orifice


74


. Check valve


70


is moved into the open position when fuel in fuel chamber


68


exceeds the spring force of check spring


72


; called the valve opening pressure (VOP). When check valve


70


is open, fuel injection into the combusting chamber (not shown) can occur. When pressurization stops and the fuel pressure in chamber


68


decreases, check valve


70


is closed by check spring


72


and injection is stopped.




Industrial Applicability




Intensifier piston


48


provides great flexibility during injection events by allowing for a first pressurization rate, a second pressurization rate or multiple pressurization rates during a single injection event. Different pressurization rates are achieved by controlling how much area of piston


48


is exposed to pressurized fluid. Control valve


22


plays an important role in controlling the flow of actuation fluid between the stepped top


50


and the shoulder


53


. As illustrated in

FIG. 1

, a single solenoid and a three position spool


32


are is used to control first pressure passage


42


and second pressure passage


44


; however, alternative control valve embodiments could be used. For example, a multiple control valve scheme could be used in which two solenoids are used to control two, two position spool or poppet valves.




In order to achieve only a first pressurization rate during a single injection event, high pressure actuation fluid is supplied through supply line


28


to control valve


22


. It should be noted that the high pressure actuation fluid is preferably lubrication oil but other fluids, such as diesel fuel or another engine fluid, could be used as well. In between injection events, spool


32


is at rest in its first position in which supply line


28


is blocked and both first pressure passage


42


and second pressure passage


44


are open to drain


40


. In order to begin injection at the first pressurization rate, solenoid


38


is energized at a first current level causing spool


32


to move to a second position in which first pressure passage


42


is open to actuation fluid within supply line


28


and second pressure passage


44


is still blocked from supply line


28


and open to drain


40


. In this configuration, actuation fluid travels through first pressure passage


42


into first actuation cavity


58


where it can act upon the first area


52


of stepped top


50


. This causes piston


48


, and therefore plunger


60


, to move downwards, against the force of piston return spring


63


, and pressurize fuel located in pressurization chamber


62


. The pressurized fuel travels through fuel passage


66


into fuel chamber


68


. The pressurized fuel then acts upon check valve


70


, and pushes check valve


70


up against the force of check spring


72


. When the check


70


moves upward, orifice


74


is open allowing fluid communication between fuel chamber


68


and the combustion chamber (not shown). When it is desirable to stop injection, solenoid


38


is de-energized, moving spool


32


back to its first position in which supply line


28


is blocked and both first pressure passage and second pressure passage first pressure passage


42


and second pressure passage


44


are open to drain


40


. When first pressure passage


42


is open to drain, the first actuation fluid cavity


58


is also open to drain and the force of piston return spring


63


pushes piston back to its original or upward position. Additionally, the fuel pressure in fuel chamber


68


is decreased and check spring


72


forces check valve


70


down, closing orifice


74


.




In order to maintain only the first pressurization rate through the injection event, the stepped top


50


must remain within upper bore


56


for the entire duration of the injection event. If stepped top


50


were to leave upper bore


56


, actuation fluid from first actuation cavity


58


would be in direct communication with second actuation cavity


59


, allowing actuation fluid to act upon second area


54


of shoulder


53


. This would expose a larger area of piston


48


to actuation fluid and cause piston


48


to increase its pressurization rate. Additionally, it is important that stepped top


50


form an adequate seal with upper bore


56


to prevent direct fluid communication between first actuation cavity


58


and second actuation cavity


59


even when stepped top


50


is in upper bore


56


.




In order to obtain only a second pressurization rate during a single injection event, solenoid


38


is energized only with a second current level causing spool


32


to move from its first position, in which both first pressure passage


42


and second pressure passage


44


are open to drain and supply line


28


is blocked, to a third position in which drain


40


is blocked and both first pressure passage


42


and second pressure passage


44


are open to actuation fluid in supply line


28


. In this configuration, actuation fluid travels through both first pressure passage


42


and second pressure passage


44


, exposing first actuation cavity


58


and second actuation cavity


59


to actuation fluid. Therefore, first area


52


of stepped top


50


and second area


54


of shoulder


53


are exposed to high pressure fluid within first actuation cavity


58


and second actuation cavity


59


. This causes piston


48


, and subsequently plunger


60


, to move downward, against the force of piston return spring


63


at a second pressurization rate. This pressurization rate is greater than the first pressurization rate because a greater area of piston


48


is exposed to high pressure actuation fluid. Injection of the fuel and the termination of the injection event are similar to that described above.




Multiple pressurization rates can also be achieved during a single injection event. Initially, when solenoid


38


is not energized, spool


32


is in its first position in which actuation fluid from supply line


28


is blocked in both first pressure passage


42


and second pressure passage


44


are open to drain


40


. Solenoid


38


is then energized to a first current level causing spool


32


to move to a second position in which first pressure passage


42


is open to actuation fluid in supply line


28


and second pressure passage


44


is still blocked from supply line


28


and open to drain


40


. As described above, this creates a first pressurization rate for the fuel within the pressurization chamber


62


. As the injection event progresses, solenoid


38


can be energized to a second current level causing spool


32


to move from its second position to its third position in which both first pressure passage


42


and second pressure passage


44


are open to actuation fluid in supply line


28


and drain


40


is blocked. This increases the area of piston


48


that is exposed to actuation fluid causing piston


48


to move downward at a greater rate and increase its pressurization rate of the fuel within pressurization chamber


62


. Injection is stopped when solenoid


38


is de-energized, causing spool


32


to move from its third position back to its first position in which supply line


28


is blocked and both first pressure passage


42


and second pressure passage


44


are opened to drain


40


. By venting first actuation cavity


58


and second actuation cavity


59


, allowing piston return spring


63


moves piston


48


back to its original upward position.




Multiple pressurization rates during a single injection event gives the injector flexibility in the injection rate shape.

FIGS. 2-4

illustrate different possible rate shapes. In

FIGS. 2-4

, (


a


) is the current level to the solenoid


28


, (


b


) is the spool


32


motion (spool position) and (


c


) is the injection rate. In all cases the variables are plotted on the vertical axis against time on the horizontal axis.

FIG. 2

illustrates a boot injection.

FIG. 3

illustrates a pilot and a square and

FIG. 4

illustrates a pilot, boot and a post. It should be noted that

FIGS. 2-4

illustrate current levels for a spool valve that has initial pull current levels and then a decreased holding level. For example, in

FIG. 2



a


a first current level is applied to move spool


32


from its first position to its second position. The current level is then reduced to a holding current which increases efficiency but still holds spool


32


in the second position. A third current level is then applied to move spool


32


from the second position to the third position. Again, after moving the spool, the current level is reduced to a fourth current level to hold the spool in the third position. Finally, current is stopped to move the spool


32


back to the first position. As stated previously, the exact workings of the valve are not critical to the piston's


48


operation. In the previous descriptions, differentiating between pulling and holding currents was ignored to simplify the description but these current levels as illustrated in

FIGS. 2-4

could be used to control spool


32


and ultimately piston


48


.




By having two separate areas of piston


48


exposed to actuation fluid through separate means, first actuation cavity


58


and second actuation cavity


59


, plunger


60


return is improved. In previous designs all the actuation fluid acting on the piston needed to be pushed out of the main fluid passage (on top of the stepped piston) or through a rate shaping orifice, which restricted flow to and from the shoulder of the piston. With the present design, both stepped top


50


and shoulder


53


are associated with actuation cavities


58


and


59


that have full sized fluid passages in communication with drain


40


. This allows piston return spring


63


to quickly and smoothly return piston


48


to its original, upward position because the actuation cavities


58


and


59


vent quickly. This in turn, helps the injector during cold starts by insuring piston


48


is quickly returned even though the actuation fluid may be more viscous than normal.




The present description has illustrated a conventional check valve nozzle that opens or closes depending upon when fuel pressure is greater than the valve opening pressure (the force of the check spring


72


). However, the present invention could be used with a direct operated check nozzle as well. A direct operated check would open or close independently when fuel is pressurized. Typically a direct operated check would have its own control valve associated with it, allowing independent pressurization and injection signals to be delivered to the injector.




The present invention has also been illustrated as a way to obtain multiple pressurization rates within a hydraulically actuated electronically controlled fuel injector; however, the present intensifier configuration can be used anywhere multiple pressurization rates are necessary including intensified common rail systems and general hydraulic valve actuators. For example, this intensifier design could be implemented in an actuation valve in which different opening positions are achieved based upon pressurization of an actuation fluid.




It should be understood that the above description be intended for illustrative purposes only and is not intended to limit the scope of the present invention in anyway. Thus, those skilled in the art will appreciate that other aspects, objects and advantages of the invention can be obtained from a study of the drawings, the disclosure and the claims.



Claims
  • 1. A fuel injector comprising:a barrel defining a first fluid passage, a second fluid passage and a piston bore including an upper bore and a lower bore; an intensifier piston including a shoulder and a stepped top; a first actuation cavity defined by said upper bore, said stepped top and said first fluid passage; a second actuation cavity defined by said lower bore, said shoulder and said second fluid passage; said piston being slidably received in said piston bore wherein said shoulder is received in said lower bore and said stepped top is received in said upper bore; said stepped top having a first surface open to fluid pressure in said first actuation cavity and said shoulder having a second surface open to fluid pressure in said second actuation cavity; said piston being moveable between a first position and a second position; said stepped top being sealable with said upper bore when said piston moves between said first position and said second position; a source of actuation fluid; a drain passage; a control valve to open and close fluid communication between said first and second fluid passages and said source of actuation fluid and said drain passage.
  • 2. The fuel injector of claim 1 whereinsaid first surface defines a first area open to fluid pressure in said first actuation cavity; and said second surface defines a second area open to fluid pressure in said second actuation cavity.
  • 3. The fuel injector of claim 2 wherein said first area is smaller than said second area.
  • 4. The fuel injector of claim 2 wherein said first surface and said second surface are axially aligned.
  • 5. The fuel injector of claim 1 wherein said second surface is annular in shape.
  • 6. The fuel injector of claim 1 wherein said piston isolates said upper bore from fluid communication from said lower bore.
  • 7. The fuel injector of claim 1 further including a piston return spring.
  • 8. The fuel injector of claim 1 further including a plunger actuated by said piston.
  • 9. The fuel injector of claim 1 wherein said control valve includes a three position spool.
  • 10. The fuel injector of claim 9 wherein said control valve opens said first and second fluid passages to said drain when said control valve is in a first position.
  • 11. The fuel injector of claim 9 wherein said control valve isolates said first fluid passage from said drain and opens fluid communication between said first fluid passage and said source of actuation fluid when said control valve is in a second position.
  • 12. The fuel injector of claim 9 said control valve isolates said first and said second fluid passages from said drain and opens fluid communication between said first and second fluid passages and said source of actuation fluid when said control valve is where in a third position.
  • 13. The fuel injector of claim 1 wherein said control valve includes a solenoid.
  • 14. A method of operating an intensifier piston arrangement, an intensifier piston having a first effective area partially defining a first actuation cavity and a second effective area partially defining a second actuation cavity, the method comprising:delivering a first fluid flow from a common fluid source to said first actuation cavity; moving said intensifier piston a first preselected distance; delivering a second fluid flow from said common fluid source to said second actuation cavity; moving said intensifier piston a second preselected distance; maintaining said first area in direct fluid isolation from said second actuation cavity.
  • 15. The method of claim 14 further including sending a first signal and moving a valve from a first position to a second position.
  • 16. The method of claim 15 further including sending a second signal and moving said valve to a third position.
  • 17. The method of claim 16 further including sending a third signal and moving said valve to a first position and draining said fluid flow from said first and second actuation cavities.
  • 18. The method of claim 15 further including sending a second signal and moving a second valve from a first position to a second position.
  • 19. A method of operating a intensifier piston system comprising:delivering a first signal; moving a valve to a first position in response to said first signal; allowing fluid flow to a first effective area of an intensifier piston, said first area partially defining a first actuation cavity; delivering a second signal; moving said valve to a second position in response to said second signal; allowing a fluid flow to a second effective area of said intensifier piston, said second area partially defining a second actuation cavity.
  • 20. The method of claim 19 wherein moving a valve to a first position includes moving a three position spool valve to said first position.
  • 21. The method of claim 19 further including allowing said fluid flow to a stepped top of said intensifier piston.
  • 22. The method of claim 19 further including allowing said fluid flow to a shoulder of said intensifier piston.
  • 23. The method of claim 19 further including maintaining said first actuation cavity in direct fluid isolation from said second actuation cavity.
  • 24. The method of claim 19 further including:delivering a third signal; moving said valve to a third position in response to said third signal; and draining said fluid flow from said first and second actuation cavities.
US Referenced Citations (4)
Number Name Date Kind
5826562 Chen et al. Oct 1998 A
6047899 Graves Apr 2000 A
6053421 Chockley Apr 2000 A
6113000 Tian Sep 2000 A
Foreign Referenced Citations (1)
Number Date Country
WO 0070216 Nov 2000 WO