The present disclosure is directed to a manifold for a filter assembly. The manifold includes a first base which may define a first inlet configured to direct fuel flow to a first filter element, and a first outlet configured to direct fuel flow from the first filter element to the second filter ele
The present disclosure is directed to a manifold for a filter assembly. The manifold includes a first base which may define a first inlet configured to direct fuel flow to a first filter element, and a first outlet configured to direct fuel flow from the first filter element to the second filter element. The manifold includes a second base operably coupled to the first base. The second base may define a barrier which prevents the fuel flow from flowing from the first inlet to the second filter element without passing through the first filter element. The second base may also define a second inlet configured to receive fuel flow from the first outlet and direct the fuel flow to the second filter element, and a second outlet configured to receive the fuel flow from the second filter element.
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1. A manifold for a filter assembly, the manifold comprising: a first base defining a first inlet configured to direct fuel flow to a first filter element,a first outlet configured to direct fuel flow from the first filter element to a second filter element, anda coupling configured to receive the f
1. A manifold for a filter assembly, the manifold comprising: a first base defining a first inlet configured to direct fuel flow to a first filter element,a first outlet configured to direct fuel flow from the first filter element to a second filter element, anda coupling configured to receive the first filter element;a second base operably coupled to the first base, the second base defining a barrier configured to prevent the fuel flow from flowing from the first inlet to the second filter element without passing through the first filter element,a second inlet configured to receive fuel flow from the first outlet and to direct the fuel flow to the second filter element via a passage formed by the second base, wherein the passage terminates at a location internal to the second base,a second outlet configured to receive the fuel flow from the second filter element, anda coupling configured to receive the second filter element; anda vent passage configured to permit flow of vapor between the first base and the second base. 2. The manifold of claim 1, wherein the first base and the second base define at least one of protrusions and recesses configured to align the first base and the second base when operably coupled to one another. 3. The manifold of claim 1, wherein at least one of the first base and the second base includes at least one flange configured to operably couple the first base and the second base to one another. 4. The manifold of claim 1, wherein at least one of the first base and the second base includes a boss configured to operably couple the manifold in operational relation to an engine. 5. The manifold of claim 1, wherein at least one of the first base and the second base defines a vent opening configured to permit flow of vapor from at least one of the first base and the second base to the vent passage. 6. The manifold of claim 1, further including a third base operably coupled to the first base, the third base defining a third inlet configured to direct fuel flow to at least one of a third filter element and the first filter element,a third outlet configured to direct fuel flow from the third filter element to at least one of the first base and the second base, anda coupling configured to receive the third filter element. 7. A filter assembly comprising: a first filter element configured to filter fuel;a second filter element configured to filter fuel; anda manifold configured to direct fuel to the first and the second filter elements,the manifold including a first base defining a first inlet configured to direct fuel flow to at least one of the first filter element,a first outlet configured to direct fuel flow from the first filter element to the second filter element,a coupling receiving the first filter element, anda second base operably coupled to the first base, the second base defining a barrier configured to prevent the fuel flow from flowing from the first inlet to the second filter element without passing through the first filter element,a second inlet configured to receive fuel flow from the first outlet and to direct the fuel flow to the second filter element via a passage formed by the second base, wherein the passage terminates at a location internal to the second base,a second outlet configured to receive the fuel flow from the second filter element, anda coupling receiving the second filter element; anda vent passage configured to permit flow of vapor between the first base and the second base. 8. The filter assembly of claim 7, wherein the first filter element is configured to remove particulate matter having a first size greater than a first size dimension, and the second filter element is configured to remove particulate matter having a second size greater than a second size dimension, and wherein the first size dimension and the second size dimension are about equal. 9. The filter assembly of claim 7, wherein at least one of the first filter element and the second filter element includes a spin-on type fuel filter. 10. The filter assembly of claim 7, wherein the first base and the second base define at least one of protrusions and recesses configured to align the first base and the second base when operably coupled to one another. 11. The filter assembly of claim 7, wherein at least one of the first base and the second base includes at least one flange configured to operably couple the first base and the second base to one another. 12. The filter assembly of claim 7, wherein at least one of the first base and the second base includes a boss configured to operably couple the manifold in operational relation to an engine. 13. The filter assembly of claim 7, wherein at least one of the first base and the second base defines a vent opening configured to permit flow of vapor from at least one of the first filter element and the second filter element to the vent passage. 14. The filter assembly of claim 7, further including a third base operably coupled to the first base, the third base defining a third inlet configured to direct fuel flow to at least one of a third filter element and the first filter element,a third outlet configured to direct fuel flow from the third filter element to at least one of the first base and the second base, anda coupling configured to receive the third filter element. 15. A fuel system comprising: a tank configured to contain a supply of fuel;a low pressure pump configured to route the supply of fuel to a high pressure pump;a high pressure pump configured to raise the pressure of the supply of fuel;a primary fuel filter assembly including a primary filter element configured to remove at least one of undesired fluid and particulate matter from the supply of fuel; anda secondary fuel filter assembly comprising a first filter element configured to filter fuel;a second filter element configured to filter fuel; anda manifold configured to direct fuel to the first and the second filter elements, the manifold including a first base defining a first inlet configured to direct fuel flow to the first filter element, a first outlet configured to direct fuel flow from the first filter element to the second filter element, a coupling receiving the first filter element, anda second base operably coupled to the first base, the second base defining a barrier configured to prevent the fuel flow from flowing from the first inlet to the second filter element without passing through the first filter element, a second inlet configured to receive fuel flow from the first outlet and to direct the fuel flow to the second filter element via a passage formed by the second base, wherein the passage terminates at a location internal to the second base, a second outlet configured to receive the fuel flow from the second filter element, and a coupling receiving the second filter element; anda vent passage configured to permit flow of vapor between the first base and the second base. 16. The fuel system of claim 15, wherein the first base and the second base define at least one of protrusions and recesses configured to align the first base and the second base when operably coupled to one another. 17. The fuel system of claim 15, wherein at least one of the first base and the second base includes at least one flange configured to operably couple the first base and the second base to one another. 18. The fuel system of claim 15, wherein at least one of the first base and the second base includes a boss configured to operably couple the manifold in operational relation to an engine. 19. The fuel system of claim 15, wherein at least one of the first base and the second base defines a vent opening configured to permit flow of vapor from at least one of the first filter element and the second filter element to the vent passage. 20. The fuel system of claim 15, further including a third base operably coupled to the first base, the third base defining a third inlet configured to direct fuel flow to at least one of a third filter element and the first filter element,a third outlet configured to direct fuel flow from the third filter element to at least one of the first base and the second base, anda coupling configured to receive the third filter element. 21. The manifold of claim 1, wherein the second outlet receives the fuel flow from the second filter element via an additional passage terminating at an additional location internal to the second base. 22. The manifold of claim 1, wherein the passage terminates at an inlet of the second filter element.
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이 특허에 인용된 특허 (14)
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