Fuel system having a valve upstream of a jet pump
A fuel system includes a fuel reservoir configured to be located within the fuel tank such that the fuel reservoir defines a fuel reservoir volume which is a subset of a fuel tank volume; a fuel pump configured to pump fuel from within the fuel reservoir volume to the fuel consuming device through a fuel supply line; a jet pump configured to 1) receive excess fuel, through a fuel return line, which had been supplied to the fuel consuming device through the fuel supply line and 2) aspirate fuel into the fuel reservoir volume from the fuel tank volume; and a valve which allows fuel flow in both directions between the fuel return line and the jet pump when a differential pressure across the valve is greater than or equal to a predetermined threshold.
1. A fuel system for supplying fuel from a fuel tank defining a fuel tank volume to a fuel consuming device, said fuel system comprising:
a fuel reservoir configured to be located within said fuel tank such that said fuel reservoir defines a fuel reservoir volume which is a subset of said fuel tank volume;
a fuel pump configured to pump fuel from within said fuel reservoir volume to said fuel consuming device through a fuel supply line;
a jet pump configured to 1) receive excess fuel, through a fuel return line, which had been supplied to said fuel consuming device through said fuel supply line and 2) aspirate fuel into said fuel reservoir volume from said fuel tank volume; and
a valve which allows fuel flow from said fuel return line to said jet pump when a differential pressure across said valve is greater than or equal to a predetermined threshold and which also allows fuel flow from said jet pump to said fuel return line when said differential pressure across said valve is greater than or equal to said predetermined threshold.
2. A fuel system as in claim 1 , wherein said predetermined threshold is a 15 cm column of E85.
3. A fuel system as in claim 1 , wherein said valve includes an annular wall with a central passage therein and an end wall with a slit extending therethrough such that 1) said end wall closes said central passage when said differential pressure across said valve is less than said predetermined threshold, thereby preventing fluid communication between said fuel return line and said jet pump and 2) said end wall elastically deforms when said differential pressure across said valve is greater than or equal to said predetermined threshold, thereby opening said central passage and allowing fluid communication from said fuel return line to said jet pump.
4. A fuel system for supplying fuel to a fuel consuming device, said fuel system comprising:
a fuel tank which defines a fuel tank volume which is configured to hold fuel;
a fuel reservoir located within said fuel tank such that said fuel reservoir defines a fuel reservoir volume which is a subset of said fuel tank volume;
a fuel pump configured to pump fuel from within said fuel reservoir volume to said fuel consuming device through a fuel supply line;
a jet pump configured to 1) receive excess fuel, through a fuel return line, which had been supplied to said fuel consuming device through said fuel supply line and 2) aspirate fuel into said fuel reservoir volume from said fuel tank volume; and
a valve which allows fuel flow from said fuel return line to said jet pump when a differential pressure across said valve is greater than or equal to a predetermined threshold and which also allows fuel flow from said jet pump to said fuel return line when said differential pressure across said valve is greater than or equal to said predetermined threshold.
5. A fuel system as in claim 4 , wherein said predetermined threshold is a 15 cm column of E85.
6. A fuel system as in claim 4 , wherein said valve includes an annular wall with a central passage therein and an end wall with a slit extending therethrough such that 1) said end wall closes said central passage when said differential pressure across said valve is less than said predetermined threshold, thereby preventing fluid communication between said fuel return line and said jet pump and 2) said end wall elastically deforms when said differential pressure across said valve is greater than or equal to said predetermined threshold, thereby opening said central passage and allowing fluid communication from said fuel return line to said jet pump.