The present invention relates to fuel supply systems. Fuel supply systems (sometimes called “fuel pump modules” typically include a pump unit and a filter unit and are located inside a fuel tank in a vehicle or other device. The pump unit pumps fuel from the tank through the filter unit and out through a supply outlet to a fuel burning device, such as an internal combustion engine. A check valve at the outlet of the pump unit ensures one-way flow through the pump unit.
In one aspect, the invention provides a fuel supply system including a fuel pump having a bottom inlet end configured to pick up fuel and a top discharge end configured to discharge fuel at a pressure higher than that of the inlet end. A housing defines a pressure vessel in fluid communication with the discharge end of the fuel pump. The fuel pump is secured with respect to the housing so that the pressure vessel is laterally adjacent the fuel pump and the pressure vessel and the fuel pump have overlapping heights. Exactly one check valve is positioned between the discharge end of the fuel pump and the pressure vessel, and the check valve is spaced laterally away from the discharge end of the fuel pump at an inlet to the pressure vessel.
In another aspect, the invention provides a fuel supply system including a fuel pump having a bottom inlet end configured to pick up fuel and a top discharge end configured to discharge fuel at a pressure higher than that of the inlet end. A housing defines a pressure vessel in fluid communication with the discharge end of the fuel pump. The fuel pump is secured in a receptacle area of the housing so that the pressure vessel is laterally adjacent the fuel pump and the pressure vessel and the fuel pump have overlapping heights. A channel is defined by the housing and is configured to receive 100 percent of the flow from the fuel pump. The channel terminates at a manifold feeding exactly two further flow paths, including a first flow path through a check valve and into the pressure vessel, and a second flow path through a jet pump configured to draw fuel from a remote location.
Before any embodiments of the invention are explained in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the following drawings. The invention is capable of other embodiments and of being practiced or of being carried out in various ways.
As shown in
The housing 32 defines a pressure vessel 40 receiving the fuel pressurized by the pump unit 24. The pressure vessel 40 can constitute a majority portion of the housing 32. The pressure vessel 40 can be utilized for defining a volume directly surrounding a filter 42. Thus, the pressure vessel 40 can be part of a “filter unit” 44 positioned alongside the pump unit 24. Because the housing 32 defines both the pressure vessel 40 and the receptacle area 30 for the pump unit 24, the filter unit 44 and the pump unit 24 are commonly housed by a single shell or housing 32. As shown in the drawings, the pressure vessel 40 and the pump unit 24 are positioned side-by-side, having overlapping heights such that a horizontal plane (i.e., transverse to the axial direction defined by the pump unit 24 intersects both the pump unit 24 and the pressure vessel 40 at at least one height. As illustrated, a majority of the height of the pump unit 24 overlaps with a majority of the height of the pressure vessel 40. Fuel is pumped via the pump unit 24 through the pressure vessel 40 and out to the engine or other device via an outlet port 52 or primary supply outlet. The illustrated outlet port 52 is formed integrally as a single piece with a cover 56 located at an upper end of the pressure vessel 40.
In order to minimize the axial height for better packaging in demanding applications, there is no check valve at the upper end B of the pump unit 24. Rather, fuel is sent from the pump unit 24 directly into a hydraulic channel 60 formed in the housing 32 as shown in
From the manifold 62, without first being directed through the check valve 64, or any check valve whatsoever, a portion of the flow from the pump unit 24 can also drive a jet pump 76 to draw fuel toward the immediate area of the pump module 20 from a remote tank area. Thus, any portion of the pumped fuel not directed through the check valve 64 to the pressure vessel 40 is directed through the jet pump 76, and vice versa.
Pressure regulation/relief is achieved with a pressure regulation valve 80 located in communication with an outlet passage positioned between the pressure vessel 40 and the outlet port 52. The housing 32 includes a receptacle 82 integrally formed as a single piece therewith and configured to receive the pressure regulation valve 80. The pressure regulation valve 80 is fluidly coupled with the outlet port 52 via a connection pipe 86, which is coupled between the regulator receptacle 82 at a lower end and a receptacle port 88 of the outlet passage adjacent the outlet port 52 at an upper end as shown in
The pump module 20 as described above enables a lower overall height compared to conventional pump modules. This can be particularly advantageous as the increase of technical content on new vehicles (hybridization and electrification places greater packaging demands on a vehicle's fuel tank, typically resulting in less available tank height than previous applications. Historically, achieving a low set up height requires the fuel pump to be oriented horizontally rather than vertically. This has obvious height advantages, however it complicates the assembly process as the fuel pump module becomes longer than the tank opening and a complicated method must be used to guide the module through the tank opening. The pump module 20 allows simple vertical installation, while still reducing the set up height by 20 percent.
The present application claims priority to U.S. Provisional Patent Application No. 61/650,254, filed May 22, 2012, the entire contents of which are hereby incorporated by reference.
Number | Date | Country | |
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61650254 | May 2012 | US |