Apparatus and method for pulsation damping and flow measurement in liquid fuel system

• US 4,590,796 A
• Filed: 01/23/1985
• Issued: 05/27/1986
• Est. Priority Date: 01/23/1985
• Status: Expired due to Fees

• Current Assignee: FloScan Instrument Co., Inc.
• Original Assignee: FloScan Instrument Co., Inc.
• Inventors: Baatz, Wilfried
• Primary Examiner(s): Myracle, Jerry W.
• Assistant Examiner(s): Raevis, Robert R.
• Application Number:
  US06/693,875
• Time in Patent Office: 489 Days
• Field of Search: 73/113, 73/114, 73/119 A, 137/593, 137/207, 417/540, 417/542, 417/543
• US Class Current: 73/114.42
• CPC Class Codes: F02D 33/003 Controlling the feeding of liquid fuel from storage containers to carburettors or fuel-injection apparatus control of electrical fuel pumps F02D41/3082, controlling fuel flow to a common rail F02D41/3845; Failure or leakage prevention; Diagnosis or detection of failure; Arrangement of sensors in the fuel system; Electric wiring; Electrostatic discharge
• CPC Class Codes: F02M 37/0041 Means for damping pressure pulsations equalisation of pulses in positive displacement pumps F04B1/00; devices for damping fluid pulsations in pipes F16L55/04
• CPC Class Codes: F02M 37/0047 Layout or arrangement of systems for feeding fuel fuel injection apparatus characterised by their conduits and venting means F02M55/00; fuel injection apparatus having a common rail F02M63/0225; arrangement of fuel conduits of low pressure fuel injection apparatus F02M69/462
• CPC Class Codes: G01F 1/72 Devices for measuring pulsing fluid flows
• CPC Class Codes: Y10T 137/3118 Surge suppression

Abstract

An apparatus and method are disclosed for reducing flow pulsations and measuring fuel flow in a fuel system for a liquid fuel engine. The engine (54) has associated with it a fuel tank (30) and a pump (32) for causing fuel to flow through a fuel flow path from the fuel tank through the pump to the engine. In one embodiment, the invention comprises a flow sensor (50), gas inlet means (62), and a pulsation damper (46) that includes a chamber (70) in communication with the fuel flowing through the pulsation damper. The flow sensor is positioned in the fuel flow path (44, 48, 52) between the pump and the engine, and serves to measure the rate of fuel flowing to the engine. The gas inlet means introduces gas into the fuel flow path, and preferably directly into the chamber. The pulsation damper is located in the fuel flow path (44, 48) between the pump and the flow sensor, and operates to damp flow pulsations in the fuel and separate the gas introduced by the gas inlet means from the fuel such that the gas does not reach the engine.

Claims

1. An apparatus for reducing flow pulsations in a fuel system for a liquid fuel engine, the fuel system comprising a fuel tank and a pump for causing fuel to flow through a fuel flow path from the fuel tank through the pump to the engine, the apparatus comprising:

gas inlet means for introducing gas into the fuel flow path; and

damping means located in the fuel flow path between the pump and the engine for damping flow pulsations in the fuel, the damping means including means for containing a volume of gas in communication with the fuel flowing through the damping means such that flow pulsations in the fuel are transmitted to and damped by the gas, and separation means for automatically removing gas from the damping means at approximately the same rate as the gas is introduced by the gas inlet means, such that said volume of gas is substantially constant over time and such that the fuel flowing from the damping means towards the engine is substantially free of gas.

2. The apparatus of claim 1, wherein the damping means comprises a first conduit for receiving fuel that has passed through the pump, container means forming a chamber in communication with the first conduit, a second conduit in communication with the chamber for carrying fuel from the chamber towards the engine, and wherein the separation means comprises a third conduit for carrying fuel and gas from the chamber and means forming an orifice positioned within the chamber for allowing fuel and gas to flow from the chamber into the third conduit.

3. The apparatus of claim 2, wherein the gas inlet means is operative to introduce the gas into the chamber.

4. The apparatus of claim 2, wherein the orifice has a fixed size that is selected to produce a maximum fuel flow rate through the orifice of 2-4 gallons per hour.

5. The apparatus of claim 2, wherein the damping means is adapted to cause fuel to flow from the first conduit into the chamber at an entry level positioned near the bottom of the chamber, and to cause fuel to flow from the chamber into the second conduit at an exit level positioned above the entry level, and wherein the orifice is positioned above the entry and exit levels.

6. The apparatus of claim 5, wherein the third conduit comprises a hollow tube positioned partially within the second conduit and extending to a level above the second conduit, the orifice being positioned in the tube at a level above the exit level, the height of the orifice above the exit level being sufficient to avoid entrainment of gas in the fuel flowing out of the container through the second conduit, and being further selected such that there is a sufficient volume of gas above the orifice to provide adequate damping of flow pulsations.

7. The apparatus of claim 1, wherein the gas inlet means is operative to introduce gas into the fuel flow path at a rate of approximately 1 cubic foot per hour at 28 psi.

8. The apparatus of claim 1, wherein the gas inlet means is positioned to introduce gas into the fuel flow path upstream of the damping means, wherein the damping means comprises a first conduit for receiving fuel that has passed through the pump, container means forming a chamber in communication with the first conduit, and a second conduit in communication with the chamber for carrying fuel from the chamber towards the engine, and wherein the separation means is operative to remove from the damping means gas that enters the damping means through the first conduit.

9. An apparatus for measuring the fuel consumed by a liquid fuel engine, the engine having associated with it a fuel tank and a pump for causing fuel to flow through a fuel flow path from the fuel tank through the pump to the engine, the apparatus comprising:

a flow sensor positioned in the fuel flow path between the pump and the engine;

gas inlet means for introducing gas into the fuel flow path; and

damping means located in the fuel flow path between the pump and the flow sensor for damping flow pulsations in the fuel, the damping means including means for containing a volume of gas in communication with the fuel flowing through the damping means such that flow pulsations in the fuel are transmitted to and damped by the gas, and separation means for automatically removing gas from the damping means at approximately the same rate as the gas is introduced by the gas inlet means, such that said volume of gas is substantially constant over time and such that the fuel flowing from the damping means towards the engine is substantially free of gas.

10. The apparatus of claim 9, wherein the damping means comprises a first conduit for receiving fuel that has passed through the pump, container means forming a chamber in communication with the first conduit, a second conduit in communication with the chamber for carrying fuel from the chamber towards the engine, and wherein the separation means comprises a third conduit for carrying fuel and gas from the chamber and means forming an orifice positioned within the chamber for allowing fuel and gas to flow from the chamber into the third conduit.

11. The apparatus of claim 10, wherein the gas inlet means is operative to introduce the gas into the chamber.

12. The apparatus of claim 10, wherein the orifice has a fixed size that is selected to produce a maximum fuel flow rate through the orifice of 2-4 gallons per hour.

13. The apparatus of claim 10, wherein the damping means is adapted to cause fuel to flow from the first conduit into the chamber at an entry level positioned near the bottom of the chamber, and to cause fuel to flow from the chamber into the second conduit at an exit level positioned above the entry level, and wherein the orifice is positioned above the entry and exit levels.

14. The apparatus of claim 13, wherein the third conduit comprises a hollow tube positioned partially within the second conduit and extending to a level above the second conduit, the orifice being positioned in the tube at a level above the exit level, the height of the orifice above the exit level being sufficient to avoid entrainment of gas in the fuel flowing out of the container through the second conduit, and being further selected such that there is a sufficient volume of gas above the orifice to provide adequate damping of flow pulsations.

15. The apparatus of claim 9, wherein the gas inlet means is operative to introduce gas into the fuel flow path at a rate of approximately 1 cubic foot per hour at 28 psi.

16. The apparatus of claim 9, wherein the gas inlet means is positioned to introduce gas into the fuel flow path upstream of the damping means, wherein the damping means comprises a first conduit for receiving fuel that has passed through the pump, container means forming a chamber in communication with the first conduit, and a second conduit in communication with the chamber for carrying fuel from the chamber towards the engine, and wherein the separation means is operative to remove from the damping means gas that enters the damping means through the first conduit.

17. A method for reducing flow pulsations in a fuel system for a liquid fuel engine, the fuel system comprising a fuel tank and a pump for causing fuel to flow through a fuel flow path from the fuel tank through the pump to the engine, the method comprising:

providing a chamber in the fuel flow path between the pump and the engine;

introducing a gas into the fuel flow path such that the gas flows into the chamber and forms therein a volume of gas in communication with the fuel flowing through the chamber, such that flow pulsations in the fuel are transmitted to and damped by the gas in the chamber; and

removing gas from the chamber at approximately the same rate as the gas is introduced into the fuel flow path, such that the volume of gas in the chamber is substantially constant over time and such that fuel flowing from the chamber towards the engine is substantially free of gas.

18. The method of claim 17, further comprising providing an orifice positioned within the chamber for allowing gas and fuel to flow from the chamber.

19. The method of claim 18, wherein the orifice has a fixed size that is selected to produce a maximum fuel flow rate through the orifice of 2-4 gallons per hour.

20. The method of claim 17, wherein the gas is introduced into the fuel flow path at a rate of approximately 1 cubic foot per hour at 28 psi.

21. A method for measuring the fuel consumed by a liquid fuel engine, the engine having associated with it a fuel tank and a pump for causing fuel to flow through a fuel flow path from the fuel tank through the pump to the engine, and the method comprising:

measuring the rate of fuel flow to the engine by means of a flow sensor positioned in the fuel flow path between the pump and the engine;

providing a chamber in the fuel flow path between the pump and the flow sensor;

introducing a gas into the fuel flow path such that the gas flows into the chamber and forms therein a volume of gas in communication with the fuel flowing through the chamber, such that flow pulsations in the fuel are transmitted to and damped by the gas in the chamber; and

removing gas from the chamber at approximately the same rate as the gas is introduced into the fuel flow path, such that the volume of gas in the chamber is substantially constant over time and such that fuel flowing from the chamber towards the engine is substantially free of gas.

22. The method of claim 21, wherein the engine has associated with it a return flow line for carrying unused fuel from the engine back to the fuel tank, the method further comprising measuring the rate of fuel flow from the engine by means of a return flow sensor positioned in the return flow line.

23. The method of claim 22, further comprising providing an orifice positioned within the chamber for allowing gas and fuel to flow from the chamber.

24. The method of claim 23, wherein the orifice has a fixed size that is selected to produce a maximum fuel flow rate through the orifice of 2-4 gallons per hour.

25. The method of claim 22, wherein the gas inlet means is operative to introduce gas into the fuel flow path at a rate of approximately 1 cubic foot per hour at 28 psi.