The present invention generally relates to an automotive fuel pump for use with an automobile engine.
Regenerative fuel pumps with a ring impeller are well known in the industry and are especially used for lower voltage, high pressure applications. However, this type of regenerative fuel pump that has an impeller with a ring extending around the outer diameter exhibits “disadvantageous” characteristics when used in an Electrical Returnless Fuel System (ERFS). When the vehicle is at idle, the fuel pump of an ERFS typically spins at approximately 3,000 to 4,000 revolutions per minute (rpm), while the fuel pump of a traditional system spins at approximately 8,000-9,000 rpm. At the lower rpm rate, the impeller exhibits pressure pulsation noise in the fuel pump.
Therefore, there is a need for a fuel pump that will dampen the pressure pulsation within the fuel pump while maintaining the efficiency advantages of the ring impeller.
a is a cross sectional view of a flat bottomed radial groove;
b is a cross sectional view of an ellipitical bottomed radial groove; and
c is a cross sectional view of a circular radial groove.
The following description of the preferred embodiments of the invention is not intended to limit the scope of the invention to these preferred embodiments, but rather to enable any person skilled in the art to make and use the invention.
Referring to
The pump cover 24 is mounted within the housing 12 and has a first side that has a fuel inlet orifice 26 and a second side that defines a sealing surface. The second side further includes a first flow channel 28 formed therein. The fuel inlet orifice 26 extends through the pump cover 24 and is in fluid communication with the first flow channel 28.
The pump body 22 is also mounted within the housing 12, adjacent the pump cover 24. The pump body 22 has a first side that has a fuel outlet orifice 30 and a second side that has a second flow channel 32 formed therein. The first flow channel 28 and the second flow channel 32 define a pumping chamber. The fuel outlet orifice 30 extends through the pump body 22 and is in fluid communication with the second flow channel 32.
The impeller 20 fits onto the shaft 18 such that the impeller 20 is free to move axially along the shaft 18 and rotates with the shaft 18. Therefore, the impeller 20 “floats” between the pump cover 24 and the pump body 22. The fuel pump 10 is of a conventional type which is further described in U.S. Pat. Nos. 6,210,102; 6,296,439; and 6,299,406, which are all commonly assigned to the same assignee as the present application and are hereby incorporated by reference into the present application.
The impeller 20 has a central axis which is coincident with the axis of the shaft 18. The shaft 18 passes through a shaft opening 34 in the pump body 22, through the impeller 20, into a cover recess 36, and abuts a thrust button 38. The shaft 18 is journalled within a bearing 40. The pumping chamber is formed along the periphery of the impeller 20 by the first flow channel 28 of the pump cover 24 and the second flow channel 32 of the pump body 22. Pressurized fuel is discharged through the fuel outlet orifice 30 and cools the motor 14 while passing over the motor 14 to a pump outlet 42 at an end of the pump 10 which is axially opposite the fuel inlet orifice 26.
Referring to
Preferably, the vanes 50 are un-evenly spaced around the outer circumference of the impeller 20. In other words, the distance between any two adjacent vanes 50 is not a constant, and varies in a non-repeating pattern about the circumference of the impeller 20. By spacing the vanes 50 un-evenly, harmonic pulsations are reduced within the impeller 20. Also, the pattern of the spacing of the vanes 50 is a non-repeating pattern to further reduce harmonic pulsations.
Referring to
Referring to
Preferably, the stripper areas 56, 62 of both the pump cover 24 and the pump body 22 have at least one radially extending groove 70 formed therein. The stripper areas 56, 62 can have one radial groove 70, as shown in
Preferably, if more than one radial groove 70 is present, the radial grooves 70 within either of the stripper areas 56, 62 are spaced apart from one another a distance that is not less than the distance between any two adjacent vanes 50 of the impeller 20. This way, no one vane groove 52 can simultaneously be in fluid communication with more than one of the radial grooves 70. This will prevent leakage between the vane grooves 52 as the vane grooves 52 move over the radial grooves 70.
The radial grooves 70 can be straight, as shown in
Referring to
Referring again to
Referring to
The foregoing discussion discloses and describes three preferred embodiments of the invention. One skilled in the art will readily recognize from such discussion, and from the accompanying drawings and claims, that changes and modifications can be made to the invention without departing from the scope of the invention as defined in the following claims. The invention has been described in an illustrative manner, and it is to be understood that the terminology which has been used is intended to be in the nature of words of description rather than of limitation.
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Number | Date | Country |
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2220706 | Jan 1990 | GB |
Number | Date | Country | |
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20040062634 A1 | Apr 2004 | US |