Method of calibrating an integrated pressure management apparatus

Information

  • Patent Grant
  • 6484555
  • Patent Number
    6,484,555
  • Date Filed
    Wednesday, April 5, 2000
    24 years ago
  • Date Issued
    Tuesday, November 26, 2002
    22 years ago
Abstract
A method of calibrating an integrated pressure management apparatus having a chamber with an interior volume varying in response to fluid pressure in the chamber. A diaphragm partially defining the chamber is displaceable between first and second configurations in response to fluid pressure variations around a certain pressure level. A resilient element applies a force biasing the diaphragm a first configuration and a switch is actuated by the diaphragm in the second configuration. The method includes connecting the chamber to a pressure source at a known pressure level, and adjusting resilient element such that the switch is actuated at the known pressure level.
Description




FIELD OF INVENTION




The present invention relates to a method of calibrating an integrated pressure management system that manages pressure and detects leaks in a fuel system. The present invention also relates to a method of calibrating an integrated pressure management system that performs a leak diagnostic for the headspace in a fuel tank, a canister that collects volatile fuel vapors from the headspace, a purge valve, and all associated hoses.




BACKGROUND OF INVENTION




In a conventional pressure management system for a vehicle, fuel vapor that escapes from a fuel tank is stored in a canister. If there is a leak in the fuel tank, canister or any other component of the vapor handling system, some fuel vapor could exit through the leak to escape into the atmosphere instead of being stored in the canister. Thus, it is desirable to detect leaks.




In such conventional pressure management systems, excess fuel vapor accumulates immediately after engine shutdown, thereby creating a positive pressure in the fuel vapor management system. Thus, it is desirable to vent, or “blow-off,” through the canister, this excess fuel vapor and to facilitate vacuum generation in the fuel vapor management system. Similarly, it is desirable to relieve positive pressure during tank refueling by allowing air to exit the tank at high flow rates. This is commonly referred to as onboard refueling vapor recovery (ORVR).




SUMMARY OF THE INVENTION




A sensor or switch signals that a predetermined pressure exists. In particular, the sensor/switch signals that a predetermined vacuum exists. As it is used herein, “pressure” is measured relative to the ambient atmospheric pressure. Thus, positive pressure refers to pressure greater than the ambient atmospheric pressure and negative pressure, or “vacuum,” refers to pressure less than the ambient atmospheric pressure.




The present invention is achieved by providing a method.











BRIEF DESCRIPTION OF THE DRAWINGS




The accompanying drawings, which are incorporated herein and constitute part of this specification, illustrate the present invention, and, together with the general description given above and the detailed description given below, serve to explain features of the invention. Like reference numerals are used to identify similar features.





FIG. 1

is a schematic illustration showing the operation of an apparatus according to the present invention.





FIG. 2

is a cross-sectional view of a first embodiment of the apparatus according to the present invention.





FIG. 3

is a cross-sectional view of a second embodiment of the apparatus according to the present invention.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT




Referring to

FIG. 1

, a fuel system


10


, e.g., for an engine (not shown), includes a fuel tank


12


, a vacuum source


14


such as an intake manifold of the engine, a purge valve


16


, a charcoal canister


18


, and an integrated pressure management system (IPMA)


20


.




The IPMA


20


performs a plurality of functions including signaling


22


that a first predetermined pressure (vacuum) level exists, relieving pressure


24


at a value below the first predetermined pressure level, relieving pressure


26


above a second pressure level, and controllably connecting


28


the charcoal canister


18


to the ambient atmospheric pressure A.




In the course of cooling that is experienced by the fuel system


10


, e.g., after the engine is turned off, a vacuum is created in the tank


12


and charcoal canister


18


. The existence of a vacuum at the first predetermined pressure level indicates that the integrity of the fuel system


10


is satisfactory. Thus, signaling


22


is used for indicating the integrity of the fuel system


10


, i.e., that there are no leaks. Subsequently relieving pressure


24


at a pressure level below the first predetermined pressure level protects the integrity of the fuel tank


12


, i.e., prevents it from collapsing due to vacuum in the fuel system


10


. Relieving pressure


24


also prevents “dirty” air from being drawn into the tank


12


.




Immediately after the engine is turned off, relieving pressure


26


allows excess pressure due to fuel vaporization to blow off, thereby facilitating the desired vacuum generation that occurs during cooling. During blow off, air within the fuel system


10


is released while fuel molecules are retained. Similarly, in the course of refueling the fuel tank


12


, relieving pressure


26


allows air to exit the fuel tank


12


at high flow.




While the engine is turned on, controllably connecting


28


the canister


18


to the ambient air A allows confirmation of the purge flow and allows confirmation of the signaling


22


performance. While the engine is turned off, controllably connecting


28


allows a computer for the engine to monitor the vacuum generated during cooling.





FIG. 2

, shows a first embodiment of the IPMA


20


mounted on the charcoal canister


18


. The IPMA


20


includes a housing


30


that can be mounted to the body of the charcoal canister


18


by a “bayonet” style attachment


32


. A seal


34


is interposed between the charcoal canister


18


and the IPMA


20


. This attachment


32


, in combination with a snap finger


33


, allows the IPMA


20


to be readily serviced in the field. Of course, different styles of attachments between the IPMA


20


and the body


18


can be substituted for the illustrated bayonet attachment


32


, e.g., a threaded attachment, an interlocking telescopic attachment, etc. Alternatively, the body


18


and the housing


30


can be integrally formed from a common homogenous material, can be permanently bonded together (e.g., using an adhesive), or the body


18


and the housing


30


can be interconnected via an intermediate member such as a pipe or a flexible hose.




The housing


30


can be an assembly of a main housing piece


30




a


and housing piece covers


30




b


and


30




c


. Although two housing piece covers


30




b


,


30




c


have been illustrated, it is desirable to minimize the number of housing pieces to reduce the number of potential leak points, i.e., between housing pieces, which must be sealed. Minimizing the number of housing piece covers depends largely on the fluid flow path configuration through the main housing piece


30




a


and the manufacturing efficiency of incorporating the necessary components of the IPMA


20


via the ports of the flow path. Additional features of the housing


30


and the incorporation of components therein will be further described below.




Signaling


22


occurs when vacuum at the first predetermined pressure level is present in the charcoal canister


18


. A pressure operable device


36


separates an interior chamber in the housing


30


. The pressure operable device


36


, which includes a diaphragm


38


that is operatively interconnected to a valve


40


, separates the interior chamber of the housing


30


into an upper portion


42


and a lower portion


44


. The upper portion


42


is in fluid communication with the ambient atmospheric pressure through a first port


46


. The lower portion


44


is in fluid communication with a second port


48


between housing


30


the charcoal canister


18


. The lower portion


44


is also in fluid communicating with a separate portion


44




a


via first and second signal passageways


50


,


52


. Orienting the opening of the first signal passageway toward the charcoal canister


18


yields unexpected advantages in providing fluid communication between the portions


44


,


44




a


. Sealing between the housing pieces


30




a


,


30




b


for the second signal passageway


52


can be provided by a protrusion


38




a


of the diaphragm


38


that is penetrated by the second signal passageway


52


. A branch


52




a


provides fluid communication, over the seal bead of the diaphragm


38


, with the separate portion


44




a


. A rubber plug


50




a


is installed after the housing portion


30




a


is molded. The force created as a result of vacuum in the separate portion


44




a


causes the diaphragm


38


to be displaced toward the housing part


30




b


. This displacement is opposed by a resilient element


54


, e.g., a leaf spring. The bias of the resilient element


54


can be adjusted by a calibrating screw


56


such that a desired level of vacuum, e.g., one inch of water, will depress a switch


58


that can be mounted on a printed circuit board


60


. In turn, the printed circuit board is electrically connected via an intermediate lead frame


62


to an outlet terminal


64


supported by the housing part


30




c


. An O-ring


66


seals the housing part


30




c


with respect to the housing part


30




a


. As vacuum is released, i.e., the pressure in the portions


44


,


44




a


rises, the resilient element


54


pushes the diaphragm


38


away from the switch


58


, whereby the switch


58


resets.




According to the present invention, a certain desired level of vacuum is calibrated by connecting the IPMA


20


to a pressure source at a known level of vacuum. This calibration can be performed in-situ, i.e., while the IPMA


20


is mounted on a vehicle. This calibration can also be an iterative process wherein the calibrating screw


56


is adjusted between occurrences of connecting the IPMA


20


to the pressure source at the known level of vacuum, i.e., calibrating screw


56


can be turned when the IPMA


20


is disconnected from the pressure source, with activation of the switch


58


being determined for a subsequent connection of the IPMA to the pressure source.




Pressure relieving


24


occurs as vacuum in the portions


44


,


44




a


increases, i.e., the pressure decreases below the calibration level for actuating the switch


58


. Vacuum in the charcoal canister


18


and the lower portion


44


will continually act on the valve


40


inasmuch as the upper portion


42


is always at or near the ambient atmospheric pressure A. At some value of vacuum below the first predetermined level, e.g., six inches of water, this vacuum will overcome the opposing force of a second resilient element


68


and displace the valve


40


away from a lip seal


70


. This displacement will open the valve


40


from its closed configuration, thus allowing ambient air to be drawn through the upper portion


42


into the lower the portion


44


. That is to say, in an open configuration of the valve


40


, the first and second ports


46


,


48


are in fluid communication. In this way, vacuum in the fuel system


10


can be regulated.




Controllably connecting


28


to similarly displace the valve


40


from its closed configuration to its open configuration can be provided by a solenoid


72


. At rest, the second resilient element


68


displaces the valve


40


to its closed configuration. A ferrous armature


74


, which can be fixed to the valve


40


, can have a tapered tip that creates higher flux densities and therefore higher pull-in forces. A coil


76


surrounds a solid ferrous core


78


that is isolated from the charcoal canister


18


by an O-ring


80


. The flux path is completed by a ferrous strap


82


that serves to focus the flux back towards the armature


74


. When the coil


76


is energized, the resultant flux pulls the valve


40


toward the core


78


. The armature


74


can be prevented from touching the core


78


by a tube


84


that sits inside the second resilient element


68


, thereby preventing magnetic lock-up. Since very little electrical power is required for the solenoid


72


to maintain the valve


40


in its open configuration, the power can be reduced to as little as 10% of the original power by pulse-width modulation. When electrical power is removed from the coil


76


, the second resilient element


68


pushes the armature


74


and the valve


40


to the normally closed configuration of the valve


40


.




Relieving pressure


26


is provided when there is a positive pressure in the lower portion


44


, e.g., when the tank


12


is being refueled. Specifically, the valve


40


is displaced to its open configuration to provide a very low restriction path for escaping air from the tank


12


. When the charcoal canister


18


, and hence the lower portions


44


, experience positive pressure above ambient atmospheric pressure, the first and second signal passageways


50


,


52


communicate this positive pressure to the separate portion


44




a


. In turn, this positive pressure displaces the diaphragm


38


downward toward the valve


40


. A diaphragm pin


39


transfers the displacement of the diaphragm


38


to the valve


40


, thereby displacing the valve


40


to its open configuration with respect to the lip seal


70


. Thus, pressure in the charcoal canister


18


due to refueling is allowed to escape through the lower portion


44


, past the lip seal


70


, through the upper portion


42


, and through the second port


46


.




Relieving pressure


26


is also useful for regulating the pressure in fuel tank


12


during any situation in which the engine is turned off. By limiting the amount of positive pressure in the fuel tank


12


, the cool-down vacuum effect will take place sooner.





FIG. 3

shows a second embodiment of the present invention that is substantially similar to the first embodiment shown in

FIG. 2

, except that the first and second signal passageways


50


,


52


have been eliminated, and the intermediate lead frame


62


penetrates a protrusion


38




b


of the diaphragm


38


, similar to the penetration of protrusion


38




a


by the second signal passageway


52


, as shown in FIG.


2


. The signal from the lower portion


44


is communicated to the separate portion


44




a


via a path that extends through spaces between the solenoid


72


and the housing


30


, through spaces between the intermediate lead frame


62


and the housing


30


, and through the penetration in the protrusion


38




b.






While the invention has been disclosed with reference to certain preferred embodiments, numerous modifications, alterations, and changes to the described embodiments are possible without departing from the sphere and scope of the invention, as defined in the appended claims and their equivalents thereof. Accordingly, it is intended that the invention not be limited to the described embodiments, but that it have the full scope defined by the language of the following claims.



Claims
  • 1. A method of calibrating an integrated pressure management apparatus, the method comprising:providing a chamber having an interior volume varying in response to fluid pressure in the chamber, the chamber including a diaphragm displaceable between a first configuration in response to fluid pressure above a certain pressure level and a second configuration in response to fluid pressure below the certain pressure level; providing a resilient element applying a force biasing the diaphragm toward the first configuration, the providing a resilient element includes providing a leaf spring having a first end fixed with respect to the chamber and a second end contiguously engaging the diaphragm; providing a switch actuated by the diaphragm in the second configuration; providing an adjuster contiguously engaging the resilient element, the providing an adjuster including providing a calibrating screw threadably mounted with respect to the chamber; connecting the chamber to a pressure source at the certain pressure level; and adjusting the biasing force such that the switch is actuated at the certain pressure level, the adjusting includes turning the calibrating screw in contiguous engagement with an intermediate portion of the leaf spring between the first and second ends.
  • 2. A method of calibrating an integrated pressure management apparatus, the method comprising:providing a chamber having an interior volume varying in response to fluid pressure in the chamber, the chamber including a diaphragm displaceable between a first configuration in response to fluid pressure above a certain pressure level and a second configuration in response to fluid pressure below the certain pressure level; providing an adjuster contiguously engaging the resilient element, the providing an adjuster including providing a calibrating screw threadably mounted with respect to the chamber; providing a resilient element applying a force biasing the diaphragm toward the first configuration, the providing a resilient element includes providing a leaf spring having a first end fixed with respect to the housing and the calibrating screw connecting a second end of the leaf spring with respect to the chamber; providing a switch actuated by the diaphragm in the second configuration; connecting the chamber to a pressure source at the certain pressure level; and adjusting the biasing force such that the switch is actuated at the certain pressure level, the adjusting includes turning the calibrating screw to adjust spacing between the first and second ends.
CROSS REFERENCE TO RELATED APPLICATIONS

This application claims the benefit of the earlier filing date of U.S. Provisional Application No. 60/166,404, filed Nov. 19 1999, which is incorporated by reference herein in its entirety.

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Provisional Applications (1)
Number Date Country
60/166404 Nov 1999 US