The present invention relates to a filtering system and more particularly to a wash filter therefor.
Engine systems often contain contamination sensitive components. These components are sensitive to contamination and require a filtration system which protects the clearances against contamination within the fuel.
Pumps that supply pressure and flow are typically fixed displacement pumps—that is, the flow varies linearly with speed. During steady-state operation, excess pump flow is bypassed and recirculated. Conventional fixed geometry wash filters utilize this excess flow as wash flow. The range of wash flow over the pump operating envelope supplies sufficient washing action to clean a traditional wash filter filtration system.
A variable wash flow filter assembly according to an exemplary aspect of the present invention includes: a housing which defines an inlet, at least one filtered flow port, and at least one outlet port; a wash filter within the housing adjacent to at least one filtered flow port; and a wash velocity control cone biased within the housing relative to the wash filter, the wash velocity control cone is movable between a minimal position and a maximum position.
A fuel system according to an exemplary aspect of the present invention includes: a main fuel pump; and a variable wash flow filter assembly in fluid communication with the main fuel pump. The variable wash flow filter assembly comprises a wash velocity control cone movable relative to a wash filter, the wash velocity control cone movable between a minimal position and a maximum position to split a fuel flow from the fuel pump into thru flow to the demand system and a filtered flow. The thru flow serves as a wash flow to carry away contaminate trapped by the wash filter within said variable wash flow filter assembly.
A method of filtering a fuel flow according to an exemplary aspect of the present invention includes: biasing a wash velocity control cone relative to a wash filter within a variable wash flow filter assembly the wash velocity control cone movable between a minimal position and a maximum position, the variable wash flow filter assembly splits inlet flow into a thru flow to a demand system and a filtered flow. The thru flow operable as a wash flow to carry away contaminate trapped by the wash filter within the variable wash flow filter assembly.
The various features and advantages of this invention will become apparent to those skilled in the art from the following detailed description of the disclosed non-limiting embodiment. The drawings that accompany the detailed description can be briefly described as follows:
As the filtered flow FF supplies only the flow required for contaminate sensitive devices 56, there is no excess flow to supply wash flow within the variable wash flow filter assembly 54. The burn flow GG is thereby utilized as the wash flow, however, the burn flow GG may have a relatively high “turn down ratio” or the ratio of max flow to min flow. This high turn down ratio would not allow a conventional fixed geometry wash filter to meet a standard wash velocity range for a fixed geometry wash filter. The variable wash flow filter assembly 54 maintains the wash velocity within a desired range for effective operation.
Referring to
The wash filter 74 is of conical shape to receive the wash velocity control cone 68 which has a generally equivalent shape such that, at the minimum position (
The gap between the wash velocity control cone 68 and the wash filter 74 has a relatively high fluid velocity which may causes a drop in the static fluid pressure that may result in a closing pressure load and a net closing force on the wash velocity control cone 68. To avoid this potential closing force, at least one deltaP window 78 is located within the guide 76 downstream of the conical gap between the wash velocity control cone 68 and the wash filter 74. The window 78 may be located through a sleeve section 80 of the guide 76. One or more windows 78 may be located and contoured to optimize the deltaP for various flow conditions which provide net positive forces for controlling cone position.
Fuel flow F from the main fuel pump 52 enters the variable wash flow filter assembly 54 through the inlet 62. The fuel is guided to flow between the wash velocity control cone 68 and the wash filter 74. Movement of the wash velocity control cone 68 relative the wash filter 74 operates to vary the flow area relative to the stroke of the wash velocity control cone 68. A portion of the inlet flow will pass through the wash filter 74 and into the filtered flow FF port 64 to become filtered flow FF. The balance of the fuel becomes system demand flow and will carry away contaminate trapped by the wash filter 74. System demand flow passes essentially though the variable wash flow filter assembly 54, while the filtered flow FF is directed generally perpendicular to the axis F through the wash filter assembly 54.
Referring to
Fuel flow from the centrifugal main fuel pump 52′ enters the variable wash flow filter assembly 54A through the inlet 62′. The fuel is guided through the stability valve 90 which creates the proper backpressure for stable pump operation, then flows between the wash velocity control cone 68′ and the wash filter 74′ as described above. The wash velocity control cone 68′ that integrates the stability valve 90 are fixed together to move as a unit and therefore have the same stroke to flow relationship.
Referring to
It should be understood that relative positional terms such as “forward,” “aft,” “upper,” “lower,” “above,” “below,” and the like are with reference to the normal operational attitude of the vehicle and should not be considered otherwise limiting.
It should be understood that although a particular component arrangement is disclosed in the illustrated embodiment, other arrangements will benefit from the instant invention.
Although particular step sequences are shown, described, and claimed, it should be understood that steps may be performed in any order, separated or combined unless otherwise indicated and will still benefit from the present invention.
The foregoing description is exemplary rather than defined by the limitations within. Many modifications and variations are possible in light of the above teachings. Non-limiting embodiments are disclosed herein, however, one of ordinary skill in the art would recognize that certain modifications would come within the scope of this invention. It is, therefore, to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described. For that reason the following claims should be studied to determine the true scope and content of this invention.
This invention was made with Government support under N00019-02-C-3003 awarded by The United States Air Force. The Government has certain rights in this invention.
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