The present invention relates to a fluid pump; more particularly to a fuel pump; even more particularly to a multi-channel fuel pump; and still even more particularly to a multi-channel fuel pump in which the channels are synchronized.
Fluid pumps, and more particularly fuel pumps for pumping fuel, for example, from a fuel tank of a motor vehicle to an internal combustion engine of the motor vehicle, are known. U.S. Pat. No. 5,338,151 shows one type of fuel pump which includes an impeller with two arrays of blades that are concentric to each other such that one array of blades radially surrounds the other array of blades. An inlet plate is disposed adjacent to one face of the impeller and includes first and second inlet plate flow channels that are arranged in series to each other. One inlet plate flow channel is aligned with the first array of blades while the other inlet plate flow channel is aligned with the second array of blades, accordingly, one inlet plate flow channel is disposed radially outward of the other inlet plate flow channel. An outlet plate is disposed adjacent to the face of the impeller that is opposite the inlet plate. The outlet plate includes first and second outlet plate flow channels that are arranged in series to each other. One outlet plate flow channel is aligned with the first array of blades while the other outlet plate flow channel is aligned with the second array of blades, accordingly, one outlet plate flow channel is disposed radially outward of the other outlet plate flow channel. Rotation of the impeller by an electric motor pumps fuel from an inlet of the fuel pump, through one or more of the inlet and outlet plate flow channels, and subsequently to an outlet of the fuel pump. The pumping efficiency of each inlet and outlet flow channel is affected by the radial distance of the flow channel from the center of rotation of the impeller, the cross-sectional area of the flow channel, and the rotational rate of impeller. Without consideration to the geometry of each of the flow channels relative to each other, the maximum pumping efficiency for each flow channel may occur at different rotational rates of the impeller which reduces the overall efficiency of the fuel pump.
What is needed is a fuel pump which minimizes or eliminates one or more of the shortcomings as set forth above.
Briefly described, a fluid pump includes an outlet for discharging fluid from the fluid pump, a housing, and a motor with a shaft that rotates about an axis. The fluid pump also includes an impeller having a first array of blades radially surrounding the axis and a second array of blades radially surrounding the first array of blades. The impeller is rotatable by the shaft of the motor. The fluid pump also includes an inlet plate adjacent to the impeller and has an inlet for introducing fluid into the fluid pump, a first inlet plate flow channel aligned with the first array of blades and having a first inlet plate flow channel cross-sectional area, and a second inlet plate flow channel aligned with the second array of blades and having a second inlet plate flow channel cross-sectional area. Rotation of the impeller pumps fluid from the inlet to the outlet. The second inlet plate flow channel cross-sectional area is synchronized with the first inlet plate flow channel cross-sectional area.
This invention will be further described with reference to the accompanying drawings in which:
Reference will be made to
Motor section 14 includes electric motor 20 which is disposed within housing 18. Electric motor 20 includes a shaft 22 extending therefrom into pump section 12. Shaft 22 rotates about axis 24 when an electric current is applied to electric motor 20. Electric motors and their operation are well known, consequently, electric motor 20 will not be discussed further herein.
With continued reference to
Inlet plate 26 is generally planer and circular in shape, i.e. disk shaped, and includes an inlet 34 that extends through inlet plate 26 in the same direction as axis 24. Inlet 34 is a passage which introduces fuel into fuel pump 10. Inlet plate 26 also includes an inlet plate first flow channel 36 and an inlet plate second flow channel 38 that are both formed in the face of inlet plate 26 that faces toward impeller 28. Inlet plate first flow channel 36 and inlet plate second flow channel 38 are joined together in series by inlet plate transition channel 40. Inlet plate first flow channel 36 is defined by an inner wall 42, an outer wall 44, and a bottom 46 such that inner wall 42 is radially inward of outer wall 44. Inlet plate first flow channel 36 has a width WIP1 and a depth DIP1 such that outer wall 44 has a radius RIP1 with a center at axis 24. Preferably, the ratio of width WIP1 to depth DIP1 is about 2.5:1. Inlet plate first flow channel 36 has a cross-sectional area AIP1 defined by a plane passing through and parallel to axis 24 as viewed in
Inlet plate second flow channel 38 is defined by an inner wall 48, an outer wall 50, and a bottom 52. Inlet plate second flow channel 38 has a width WIP2 and a depth DIP2 such that outer wall 50 has a radius RIP2 with a center at axis 24 such that inner wall 48 is radially inward of outer wall 50. Preferably, the ratio of width WIP2 to depth DIP2 is about 2.5:1. Inlet plate second flow channel 38 has a cross-sectional area AIP2 defined by a plane passing through and parallel to axis 24 as viewed in
Outlet plate 30 is generally planer and circular in shape, i.e. disk shaped, and includes an outlet plate outlet plate passage 54 that extends through outlet plate 30 in the same direction as axis 24. Outlet plate outlet passage 54 is in fluid communication with outlet section 16 as will be describe in more detail later. Outlet plate 30 also includes an outlet plate first flow channel 56 and an outlet plate second flow channel 58 that are both formed in the face of outlet plate 30 that faces toward impeller 28. Outlet plate first flow channel 56 and outlet plate second flow channel 58 are joined together in series by outlet plate transition channel 60. Outlet plate first flow channel 56 is defined by an inner wall 62, an outer wall 64, and a bottom 66 such that inner wall 62 is radially inward of outer wall 64. Outlet plate first flow channel 56 has a width WOP1 and a depth DOP1 such that outer wall 64 has a radius ROP1 with a center at axis 24. Preferably, the ratio of width WOP1 to depth DOP1 is about 2.5:1. Outlet plate first flow channel 56 has a cross-sectional area AOP1 defined by a plane passing through and parallel to axis 24 as viewed in
Outlet plate second flow channel 58 is defined by an inner wall 68, an outer wall 70, and a bottom 72 such that inner wall 68 is radially inward of outer wall 70. Outlet plate second flow channel 58 has a width WOP2 and a depth DOP2 such that outer wall 70 has a radius ROP2 with a center at axis 24. Preferably, the ratio of width WOP2 to depth DOP2 is about 2.5:1. Outlet plate second flow channel 58 has a cross-sectional area AOP2 defined by a plane passing through and parallel to axis 24 as viewed in
Impeller 28 includes a first plurality of blades 76 arranged in a polar array radially surrounding and centered about axis 24 such that blades 76 are aligned with inlet plate first flow channel 36 and outlet plate first flow channel 56. Blades 76 are each separated from each other by a first blade chamber 78 that passes through impeller 28 in the general direction of axis 24. Impeller 28 also includes a second plurality of blades 80 arranged in a polar array radially surrounding and centered about axis 24 and first array of blades 76 such that blades 80 are aligned with inlet plate second flow channel 38 and outlet plate second flow channel 58. Blades 80 are each separated from each other by a second blade chamber 82 that passes through impeller 28 in the general direction of axis 24. The first plurality of blades 76 are radially separated from the second plurality of blades 80 by a blade separation wall 84 that is located radially between the first plurality of blades 76 and the second plurality of blades 80. Impeller 28 may be made, for example only, by a plastic injection molding process in which the preceding features of impeller 28 are integrally molded as a single piece of plastic.
Outlet section 16 includes outlet 86 for discharging fuel from fuel pump 10. Outlet 86 may be connected to, for example, a conduit (not shown) for supplying fuel to an internal combustion engine (not shown). Outlet 86 is in fluid communication with outlet plate outlet passage 54 of outlet plate 30 for receiving fuel that has been pumped by pump section 12.
In operation, inlet 34 is exposed to a volume of fuel (not shown) which is to be pumped to, for example, an internal combustion engine (not shown). An electric current is supplied to electric motor 20 in order to rotate shaft 22 and impeller 28. As impeller 28 rotates, fuel is drawn through inlet 34 into inlet plate first flow channel 36, inlet plate second flow channel 38, and inlet plate transition channel 40. First blade chambers 78 and second blade chambers 82 allow fuel from inlet plate first flow channel 36, inlet plate second flow channel 38, and inlet plate transition channel 40 to flow to outlet plate first flow channel 56, outlet plate second flow channel 58, and outlet plate transition channel 60. Impeller 28 subsequently discharges the fuel through outlet plate outlet passage 54 and consequently through outlet 86.
In order to improve the pumping efficiency of fuel pump 10, inlet plate first flow channel 36 is synchronized with inlet plate second flow channel 38, i.e. area AIP1 is synchronized with area AIP2, to provide maximum or near maximum pumping efficiency of inlet plate first flow channel 36 and inlet plate second flow channel 38 for a desired rate of rotation of impeller 28. Similarly, outlet plate first flow channel 56 is synchronized with outlet plate second flow channel 58, i.e. area AOP1 is synchronized with area AOP2, to provide maximum or near maximum efficiency of outlet plate first flow channel 56 and outlet plate second flow channel 58 at the desired rate of rotation of impeller 28. As related to inlet plate first flow channel 36, inlet plate second flow channel 38, outlet plate first flow channel 56 and outlet plate second flow channel 58, the term “synchronized” signifies that the geometry of inlet plate first flow channel 36 and the geometry of inlet plate second flow channel 38 have been given consideration relative to each other in order to provide maximum or near maximum pumping efficiency at a common rotational rate of impeller 28 and that the geometry of outlet plate first flow channel 56 and the geometry of outlet plate second flow channel 58 have been given consideration relative to each other in order to provide maximum or near maximum pumping efficiency at a common rotational rate of impeller 28. In the paragraphs that follow, the synchronization will be described in further detail.
Let us assume that fuel pump 10 is to have a maximum efficiency at a rotational rate of impeller 28 of ω radians per second while delivering a volumetric flow rate Q m3/s at pressure P pascals. The non-dimensional pressure ψ and non-dimensional flow φ follow the characteristic equation ψ=ƒ(φ) where ƒ is a known function. Maximum pumping efficiency of fuel pump 10 occurs at φ=φ0≈0.7. At this point, ψ=ψ0=ƒ(φ0) where ψ may be obtained from empirical data.
In the following equations, let P1 be the pressure generated by inlet plate first flow channel 36 and outlet plate first flow channel 56, let P2 be the pressure generated by inlet plate second flow channel 38 and outlet plate second flow channel 58, let R1 be equal to RIP1 and ROP1, let R2 be equal to RIP2 and ROP2, and let ρ be the fluid density in kg/m3 of the fuel being pumped.
The total pressure P generated by the fuel pump 10 equals the sum of pressures generated by inlet plate first flow channel 36 and outlet plate first flow channel 56, inlet plate second flow channel 38, and outlet plate second flow channel 58 as indicated by the following equation:
P=P
1
+P
2 equation 3
It may be desirable to minimize leakage between inlet plate first flow channel 36 and inlet plate second flow channel 38 and between outlet plate first flow channel 56 and outlet plate second flow channel 58. In order to minimize this leakage, a separation ε, for example about 0.006 m, is provided between inlet plate first flow channel 36 and inlet plate second flow channel 38 and between outlet plate first flow channel 56 and outlet plate second flow channel 58 such that ε is equal to the radial dimension of inlet plate separation surface 53 plus WIP2 and also equal to the radial dimension of outlet plate separation surface 73 plus WOP2. Consequently, inlet plate second flow channel 38 is related to inlet plate first flow channel 36 as shown by equation 4 below. Similarly, outlet plate second flow channel 58 is related to outlet plate first flow channel 56 as shown by equation 4.
R
2
=R
1+ε equation 4
The four equations; equation 1, equation 2, equation 3, and equation 4; can now be solved for the four unknowns: P1, P2, R1, R2. Having determined R1 and R2, the cross section areas AIP1, AIP2, AOP1, and AOP2 can be determined from the following equations where AIP1=AOP1, A1=AIP1+AOP1, AIP2=AOP2, and A2=AIP2+AOP2:
By using equations 5 and 6, the cross section areas AIP1, AIP2, AOP1, and AOP2 can be determined such that inlet plate first flow channel 36 and inlet plate second flow channel 38 are synchronized with each other and such that outlet plate first flow channel 56 and outlet plate second flow channel 58 are synchronized with each other. In this way, the pumping efficiency of inlet plate first flow channel 36, inlet plate second flow channel 38, outlet plate first flow channel 56, and outlet plate second flow channel 58 are all substantially the same. Consequently, the overall pumping efficiency of fuel pump 10 is the same as each of inlet plate first flow channel 36, inlet plate second flow channel 38, outlet plate first flow channel 56, and outlet plate second flow channel 58. This synchronization is illustrated in
In contrast to
While fuel pump 10 has been shown having impeller 28 with first and second arrays of blades 76, 80, it should now be understood that fuel pump 10 may have an impeller with a greater number of arrays of blades, such that in general, there are N arrays of blades where N≧2. It should also be understood that the inlet plate and the outlet plate will each have flow channels that correspond to the number of arrays of blades in the impeller and that the flow channels of the inlet plate will be synchronized with each other and the flow channels of the outlet plate will be synchronized with each other. In this arrangement, the flow channels are synchronized by determining the cross-sectional area of each pair of flow channels corresponding to one array of blades of the impeller, e.g. the cross sectional area of the flow channels of the inlet and outlet plates corresponding to the first array of blades of the impeller, from the following equation which is similar to equations 5 and 6 above where n is the number representing the flow channel as counted from the inside moving radially outward:
In equation 7, N is the number of arrays of blades of the impeller, and consequently, the number of flow channels in each of the inlet plate and the outlet plate, i.e. the inlet plate has N flow channels and the outlet plate has N flow channels.
Equations 1-4 can also be expressed generically in order to determine Rn used in equation 7 above. The equations expressed generically are as follows:
While fuel pump 10 has been described as having flow channels in both inlet plate 26 and outlet plate 30, it should now be understood that the equations set forth herein are equally applicable to fluid pumps that have multiple flow channels in only one plate. Consequently, in such a fluid pump having multiple flow channels in only one plate, An in equation 7 will determine the area of each nth flow channel in the plate having multiple flow channels.
While this invention has been described in terms of preferred embodiments thereof, it is not intended to be so limited.