Dual fuel delivery module system for bifurcated automotive fuel tanks

• US 6,283,142 B1
• Filed: 02/04/2000
• Issued: 09/04/2001
• Est. Priority Date: 02/04/2000
• Status: Expired due to Term

• Current Assignee: Robert Bosch Corporation (Robert Bosch GmbH)
• Original Assignee: Robert Bosch Corporation (Robert Bosch GmbH)
• Inventors: Wickett, Paul, Fischerkeller, Rolf, Wheeler, Tony Joe
• Primary Examiner(s): RIVELL, JOHN A
• Application Number:
  US09/498,313
• Time in Patent Office: 578 Days
• Field of Search: 137/265, 137/565.22, 137/565.3, 137/565.33, 137/574, 137/576, 123/509, 123/514
• US Class Current: 137/265
• CPC Class Codes: F02M 37/0094 Saddle tanks; Tanks having partition walls
• CPC Class Codes: F02M 37/025 Feeding by means of a liquid fuel-driven jet pump jet pumps per se F04F
• CPC Class Codes: F02M 37/106 the pump being installed in a sub-tank
• CPC Class Codes: Y10T 137/4841 With cross connecting passage
• CPC Class Codes: Y10T 137/86075 And jet-aspiration type pump
• CPC Class Codes: Y10T 137/86163 Parallel

Abstract

A fuel system including first and second tank portions communicating with each other such that the first and second tank portions have a substantially equal vapor pressure, first and second fuel pumps in the first and second tank portions, respectively, and a crossover fuel line for transferring fuel in either direction between the first and second tank portions, the direction of transfer depending on the relative level of fuel in the first and second tank portions. Respective first and second shuttle valves control the direction of fuel flow through the single crossover line to maintain substantially equal fuel levels in both bifurcated portions until the tank is empty. First and second jet pumps communicate with the crossover fuel line and provide the suction needed for fuel transfer.

Claims

1. A fuel system comprising:

first and second tank portions communicating with each other such that the first and second tank portions have a substantially equal vapor pressure;

first and second fuel pumps in the first and second tank portions, respectively; and

a crossover fuel line for transferring fuel in either direction between the first and second tank portions, the direction of transfer depending on the relative level of fuel in the first and second tank portions.

2. The fuel system of claim 1, wherein the first and second tank portions define a saddle tank.

3. A fuel system comprising:

first and second tank portions communicating with each other such that the first and second tank portions have a substantially equal vapor pressure;

first and second fuel pumps in the first and second tank portions, respectively;

a crossover fuel line for transferring fuel in either direction between the first and second tank portions, the direction of transfer depending on the relative level of fuel in the first and second tank portions;

a first jet pump in the first tank portion communicating with the crossover fuel line for pulling fuel through the crossover fuel line; and

a second jet pump in the second tank portion communicating with the crossover fuel line for pulling fuel through the crossover fuel line.

4. The fuel system of claim 3, further comprising:

a first fuel reservoir in the first tank portion from which the first fuel pump draws fuel; and

a second fuel reservoir in the second tank portion from which the second fuel pump draws fuel.

5. The fuel system of claim 4, wherein the first and second jet pumps include respective first and second outlets communicating with the first and second reservoirs, respectively.

6. The fuel system of claim 5, wherein the crossover fuel line transfers fuel from the first tank portion to the second reservoir or from the second tank portion to the first reservoir depending on the relative level of fuel in the first and second tank portions.

7. The fuel system of claim 3, further comprising:

a first fuel pickup tube in the first tank portion, the first fuel pickup tube having a first inlet, a first outlet communicating with the first jet pump and a first valve between the first inlet and the first outlet for opening when the level of fuel in the first tank is sufficient and for closing when the level of fuel in the first tank is insufficient; and

a second fuel pickup tube in the second tank portion, the second fuel pickup tube having a second inlet, a second outlet communicating with the second jet pump and a second valve between the second inlet and the second outlet for opening when the level of fuel in the second tank is sufficient and for closing when the level of fuel in the second tank is insufficient.

8. The fuel system of claim 7, wherein the first and second valves include respective first and second blocking members and the first and second valves are in an open position, allowing fuel to enter the respective inlets, when the respective blocking members are in a raised position in the presence of fuel, and the first and second valves are in a closed position, preventing air and air vapor from entering the respective inlets, when the respective blocking members are in a lowered position in the absence of fuel.

9. The fuel system of claim 8, wherein the first and second valves are also in the closed position when the fuel system is not in operation.

10. The fuel delivery system of claim 8, wherein the crossover fuel line transfers fuel between the first and second tank portions when one of either the first or second valves is in the closed position.

11. The fuel delivery system of claim 10, wherein the crossover fuel line transfers fuel from the first tank portion to the second tank portion when the second valve is in the closed position.

12. The fuel delivery system of claim 10, wherein the crossover fuel line transfers fuel from the second tank portion to the first tank portion when the first valve is in the closed position.

13. A fuel system having a first fuel transfer unit with a total pressure H_total1, and a second fuel transfer unit with a total pressure H_total2, the fuel system comprising:

first and second tank portions communicating with each other such that the first and second tank portions have a substantially equal vapor pressure and include first and second fuel levels creating pressures H_f1 and H_f2, respectively;

first and second fuel pumps in the first and second tank portions, respectively;

a crossover fuel line for transferring fuel in either direction between the first and second tank portions, the direction of transfer depending on the relative level of fuel in the first and second tank portions;

a first jet pump in the first tank portion communicating with the crossover fuel line and creating a pressure H_s1;

a second jet pump in the second tank portion communicating with the crossover fuel line and creating a pressure H_s2;

a first fuel pickup tube in the first tank portion, the first fuel pickup tube having a first inlet, a first outlet communicating with the first jet pump and a first valve between the first inlet and the first outlet for opening when the level of fuel in the first tank is sufficient and for closing when the level of fuel in the first tank is insufficient, the first valve having a first blocking member calibrated such that a pressure of H_b1 is required to lift the blocking member to an open position; and

a second fuel pickup tube in the second tank portion, the second fuel pickup tube having a second inlet, a second outlet communicating with the second jet pump and a second valve between the second inlet and the second outlet for opening when the level of fuel in the second tank is sufficient and for closing when the level of fuel in the second tank is insufficient, the second valve having a second blocking member calibrated such that a pressure of H_b2 is required to lift the blocking member to an open position;

wherein the total pressure for the first fuel transfer unit is H_total1=H_s1+H_f1−

H_b1, and the total pressure for the second fuel transfer unit is H_total2=H_s2+H_f2−

H_b2.

14. The fuel system of claim 13, wherein fuel is transferred through the crossover line from the first tank portion to the second tank portion when H_total1>

H_total2.

15. The fuel system of claim 13, wherein fuel is transferred through the crossover line from the second tank portion to the first tank portion when H_total2>

H_total1.

16. The fuel system of claim 13, wherein the first and second valves are in the open position, allowing fuel to enter the respective inlets, when H_s1+H_f1>

H_b1 and H_s2+H_f2>

H_b2, and the first and second valves are in a closed position, preventing air and air vapor from entering the respective inlets, when H_s1+H_f1<

H_b1 and H_s2+H_f2<

H_b2.

17. The fuel system of claim 13, wherein H_s1<

H_b1 and H_s2<

H_b2, such that the first and second valves are in the closed position when the fuel level in the respective tank portions is insufficient.

18. The fuel system of claim 13, wherein the first and second blocking members have a weight/area value and H_b1 and H_b2 are calibrated by changing the weight/area value.

19. The fuel system of claim 13, wherein H_s1=0 and H_s2=0 when the fuel system is not in operation, and H_f1<

H_b1 and H_f2<

H_b2 such that the first and second valves are in the closed position when the fuel system is not in operation.

20. A fuel system comprising:

first and second tank portions communicating with each other such that the first and second tank portions have a substantially equal vapor pressure;

first and second fuel pumps in the first and second tank portions, respectively;

a first fuel reservoir in the first tank portion from which the first fuel pump draws fuel;

a second fuel reservoir in the second tank portion from which the second fuel pump draws fuel;

a crossover fuel line for transferring fuel in either direction between the first and second tank portions, the direction of transfer depending on the relative level of fuel in the first and second tank portions;

a first jet pump in the first tank portion communicating with the crossover fuel line for pulling fuel through the crossover fuel line, the first jet pump having a first outlet communicating with the first reservoir;

a second jet pump in the second tank portion communicating with the crossover fuel line for pulling fuel through the crossover fuel line, the second jet pump having a second outlet communicating with the second reservoir;

a first fuel pickup tube in the first tank portion, the first fuel pickup tube having a first inlet, a first outlet communicating with the first jet pump and a first valve between the first inlet and the first outlet for opening when the level of fuel in the first tank is sufficient and for closing when the level of fuel in the first tank is insufficient, the first valve having a first blocking member such that the first valve is in an open position, allowing fuel to enter the first inlet, when the first blocking member is in a raised position in the presence of fuel, and the first valve is in a closed position, preventing air and air vapor from entering the first inlet, when the first blocking member is in a lowered position in the absence of fuel; and

a second fuel pickup tube in the second tank portion, the second fuel pickup tube having a second inlet, a second outlet communicating with the second jet pump and a second valve between the second inlet and the second outlet for opening when the level of fuel in the second tank is sufficient and for closing when the level of fuel in the second tank is insufficient, the second valve having a second blocking member such that the second valve is in an open position, allowing fuel to enter the second inlet, when the second blocking member is in a raised position in the presence of fuel, and the second valve is in a closed position, preventing air and air vapor from entering the second inlet, when the second blocking member is in a lowered position in the absence of fuel.