Fuel-air separator and pulse dampener

• US 9,366,206 B2
• Filed: 12/17/2012
• Issued: 06/14/2016
• Est. Priority Date: 12/17/2012
• Status: Active Grant

• Current Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Original Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Inventors: Myers, Eric, Zhang, Yi, Ali, Syed K., Dong, Mike, Armesto, Carlos
• Primary Examiner(s): DALLO, JOSEPH J
• Application Number:
  US13/717,402
• Publication Number:
  US 20140165971A1
• Time in Patent Office: 1,275 Days
• Field of Search: 123516-520, 962/08, 962/09, 962/16, 952/61, 554/591
• US Class Current: 1/1
• CPC Class Codes: B01D 17/0217 by centrifugal force
• CPC Class Codes: B01D 19/0042 modifying the liquid flow B01D19/0021 takes precedence
• CPC Class Codes: B01D 19/0057 the centrifugal movement being caused by a vortex, e.g. using a cyclone, or by a tangential inlet
• CPC Class Codes: B01D 21/267 by using a cyclone
• CPC Class Codes: B01D 45/12 by centrifugal forces centrifuges B04B; cyclones B04C
• CPC Class Codes: B04C 3/06 Construction of inlets or outlets to the vortex chamber
• 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 37/20 characterised by means for preventing vapour lock

Abstract

A fuel-air separator includes a chamber with an interior side-wall surface and adjacent interior top and bottom surfaces. An inlet of the fuel-air separator opens to the interior side-wall surface to admit fuel and air and to cause the fuel and air to flow helically down and along the interior side-wall surface. A diptube opens to the bottom surface and extends along an axis of the interior side-wall surface to a fuel outlet, while the separated air is released to the atmosphere.

Claims

1. A fuel-air separator comprising:

a chamber with an interior side-wall surface and adjacent interior top and bottom surfaces;

an inlet opening to the side-wall surface to admit fuel and air and to cause the fuel and air to flow helically down and along the side-wall surface;

a diptube opening to the bottom surface and extending along an axis of the side-wall surface to a fuel outlet, wherein a distance between the side-wall surface and the diptube along the entire length of the diptube is unobstructed, wherein the diptube extends below a steady-state level of fuel and wherein the fuel outlet is at the top surface; and

an air outlet at the top surface.

2. The fuel-air separator of claim 1 wherein the diptube is oriented vertically.

3. The fuel-air separator of claim 1 wherein the interior side-wall surface is cylindrical.

4. The fuel-air separator of claim 3 wherein the interior top surface is directly above the interior bottom surface.

5. The fuel-air separator of claim 1 wherein the inlet is adjacent the interior top surface.

6. The fuel-air separator of claim 1 wherein the inlet is aligned to a tangent of the interior side-wall surface.

7. The fuel-air separator of claim 1 wherein the interior top surface is larger in diameter than the interior bottom surface.

8. The fuel-air separator of claim 1 wherein the interior bottom surface is larger in diameter than the interior top surface.

9. The fuel-air separator of claim 1 wherein the chamber is resiliently deformable under the influence of a pressure pulsation of the fuel and air admitted to the inlet.

10. An engine system comprising:

a fuel-air separator having a chamber with an interior side-wall surface and adjacent interior top and bottom surfaces, an inlet opening to the side-wall surface to admit fuel and air and to cause the fuel and air to flow helically down and along the side-wall surface, a diptube opening to the bottom surface and extending along an axis of the side-wall surface to a fuel outlet at the top surface, the fuel outlet at the top surface delivering fuel with less entrained air than at the inlet, wherein a distance between the side-wall surface and the diptube along the entire length of the diptube is unobstructed, wherein the diptube extends below a steady-state level of fuel and an air outlet at the top surface; and

a fuel tank.

11. The engine system of claim 10 wherein the fuel-air separator is coupled in the fuel tank, with the diptube coupled to an outlet line that exits the fuel tank.

12. The engine system of claim 10 further comprising:

a fuel pump coupled to the inlet; and

a fuel injector coupled to the fuel outlet, the air outlet being vented to the atmosphere.

13. The engine system of claim 12 wherein the fuel injector is coupled to a combustion chamber of the engine system.

14. The engine system of claim 12 wherein the fuel injector is coupled to an intake manifold or cylinder port of the engine system.

15. A method to separate air from fuel in a fuel-air separator of a motor-vehicle fuel system, the method comprising:

admitting fuel and air tangentially onto an interior side-wall surface of a chamber of the fuel-air separator;

separating the air from the fuel under a centrifugal force caused by a helical flow of the fuel and air down and along the interior side-wall surface;

pooling the fuel at an interior bottom surface of the chamber;

releasing the fuel through a diptube opening to the interior bottom surface of the chamber and extending parallel to an axis of the interior side-wall surface to a fuel outlet at a top surface of the chamber, wherein a distance between the side-wall surface and the diptube along the entire length of the diptube is unobstructed, wherein the diptube extends below a steady-state level of fuel and

releasing the air through an outlet at an interior top surface of the chamber and fuel through the fuel outlet at the top surface.

16. The method of claim 15 further comprising exposing a column of air inside the chamber to a pressure pulsation of the admitted fuel and air to dampen the pressure pulsation.

17. The method of claim 15 wherein the fuel and air are admitted from a pressurized fuel line of a motor-vehicle engine system, the method further comprising delivering the fuel released through the diptube to a fuel injector of the fuel system.

18. The method of claim 17 wherein the air released is vented to the atmosphere, rather than being returned to the fuel system.

19. The method of claim 18 wherein the air is vented to the atmosphere via an adsorbent canister.

20. The method of claim 15 wherein the fuel is diesel fuel.