US20040101427A1 - Gerotor fuel pump having primary and secondary inlet and outlet portings - Google Patents
Gerotor fuel pump having primary and secondary inlet and outlet portings Download PDFInfo
- Publication number
- US20040101427A1 US20040101427A1 US10/306,585 US30658502A US2004101427A1 US 20040101427 A1 US20040101427 A1 US 20040101427A1 US 30658502 A US30658502 A US 30658502A US 2004101427 A1 US2004101427 A1 US 2004101427A1
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- Prior art keywords
- porting
- outlet
- inlet
- primary
- gear
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 89
- 239000002828 fuel tank Substances 0.000 claims abstract description 12
- 230000003247 decreasing effect Effects 0.000 claims 6
- 230000007423 decrease Effects 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000010349 pulsation Effects 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C15/00—Component parts, details or accessories of machines, pumps or pumping installations, not provided for in groups F04C2/00 - F04C14/00
- F04C15/06—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C15/00—Component parts, details or accessories of machines, pumps or pumping installations, not provided for in groups F04C2/00 - F04C14/00
- F04C15/0042—Systems for the equilibration of forces acting on the machines or pump
- F04C15/0049—Equalization of pressure pulses
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2/00—Rotary-piston machines or pumps
- F04C2/08—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C2/10—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of internal-axis type with the outer member having more teeth or tooth-equivalents, e.g. rollers, than the inner member
- F04C2/102—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of internal-axis type with the outer member having more teeth or tooth-equivalents, e.g. rollers, than the inner member the two members rotating simultaneously around their respective axes
Definitions
- the present invention relates to a gear assembly of a gerotor fuel pump for improved efficiency in supplying fuel to an automotive engine from a fuel tank.
- Gerotor fuel pumps that have a gear assembly with a ring slidably disposed around the outer diameter have been widely used in automotive applications. Such fuel pumps have been used because of their low cost and relatively high efficiency.
- gerotor fuel pump for improved efficiency in supplying fuel to an automotive engine from a fuel tank, wherein the gerotor fuel pump includes an improved porting system to reduce local velocity acceleration within the fuel pump for avoiding potential cavitations, pressure pulsations, and relatively high noise.
- the gear assembly includes an inner gear and an outer gear matingly cooperating with the inner gear for rotation about an axis.
- the assembly further includes a pump cover having a cover surface adjacent the inner and outer gears and a pump body having a body surface adjacent the inner and outer gears opposite the pump cover.
- the cover surface has an inlet aperture formed therethrough.
- the cover surface further has a primary inlet porting and a secondary outlet porting formed thereon wherein the primary inlet porting is formed from the inlet aperture at a first inlet end and radially extends therealong at a second inlet end.
- the secondary outlet porting radially extends between first and second outlet ends.
- the gerotor or gear assembly having a porting system includes an inlet porting and an outlet porting, wherein the inlet porting has a greater length than the outlet porting to reduce inlet fuel velocity, prevent potential cavitations, and reduce noise.
- the body surface of the pump body has an outlet aperture formed therethrough.
- the body surface further has a primary outlet porting and a secondary inlet porting formed thereon.
- the primary outlet porting is formed at the outlet aperture.
- the primary and secondary inlet portings are configured to allow fuel to pass therethrough at a rate at which the gear assembly moves.
- the primary outlet porting radially extends therealong in alignment with the secondary outlet porting.
- the secondary inlet porting is in alignment with the primary inlet porting.
- the present invention allows for improved efficiency by allowing fuel to pass therethrough at a rate corresponding to the rate at which the gear assembly moves.
- the fuel pump comprises a pump housing and a motor mounted within the housing and having a shaft extending therefrom.
- the fuel pump further includes the gear assembly mentioned above.
- the primary outlet porting is formed at the outlet aperture and in alignment with the secondary outlet porting.
- the primary and secondary inlet portings are configured to allow fuel to pass therethrough at a rate at which the gear assembly rotates.
- the primary and secondary outlet portings are configured to allow fuel to pass therethrough at a rate corresponding to the rate at which the gear assembly rotates.
- the primary outlet porting radially extends therealong in alignment with the secondary outlet porting.
- the secondary inlet porting is in alignment with the primary inlet porting.
- FIG. 1 is a cross-sectional view of a fuel pump having a gear assembly in accordance with one embodiment of the present invention
- FIG. 2 a is an exploded inlet view of the gear assembly in FIG. 1;
- FIG. 2 b is an exploded exit view of the gear assembly in FIG. 1;
- FIG. 3 a is a cover surface view of a pump cover of the gear assembly in accordance with one embodiment of the present invention.
- FIG. 3 b is a cross-sectional view of the pump cover taken along lines 3 b - 3 b in FIG. 3 a;
- FIG. 3 c is another cross-sectional view of the pump cover taken along lines 3 c - 3 c in FIG. 3 a ;
- FIG. 3 d is yet another cross-sectional view of the pump cover taken along lines 3 d - 3 d in FIG. 3 a;
- FIG. 4 a is a body surface view of a pump cover of the gear assembly in accordance with one embodiment of the present invention.
- FIG. 4 b is a cross-sectional view of the pump body taken along lines 4 b - 4 b in FIG. 4 a;
- FIG. 4 c is another cross-sectional view of the pump body taken along lines 4 c - 4 c in FIG. 4 a;
- FIG. 4 d is yet another cross-sectional view of the pump body taken along lines 4 d - 4 d in FIG. 4 a;
- FIG. 5 a is a first view of an inner gear (cover side) of the gear assembly in accordance with one embodiment of the present invention
- FIG. 5 b is a second view of the inner gear (body side) in accordance with the present invention.
- FIG. 5 c is a cross-sectional view of the inner gear taken along lines 5 c - 5 c in FIG. 5 b;
- FIG. 6 a is a first view of the outer gear (cover side) of the gear assembly in accordance with one embodiment of the present invention.
- FIG. 6 b is a cross-sectional view of the outer gear taken along lines 6 b - 6 b in FIG. 6 a;
- FIG. 7 a is a cover side view of the gear assembly in accordance with the present invention.
- FIG. 7 b is a cross-sectional view of the gear assembly taken along lines 7 b - 7 b in FIG. 7 a.
- a fuel pump of the present invention is generally shown at 10 .
- the fuel pump 10 includes a housing 12 and a motor 14 mounted within the housing 12 .
- the motor 14 is an electric motor with a shaft 18 extending therefrom.
- a gerotor or gear assembly 20 having inner and outer gears is fitted onto the shaft 18 and is encased within the pump housing 12 between a pump body 22 and a pump cover 24 .
- the gerotor assembly 20 fits onto the shaft 18 such that the assembly is free to move axially along the shaft 18 and rotates with the shaft 18 . Therefore, the gerotor assembly “float” between the pump cover 24 and the pump body 22 .
- the fuel pump is of a conventional type which is further described in U.S. Pat. No. 6,113,360 and U.S. patent application Ser. No. 10/256,359 which are assigned to the same assignee as the present application and are hereby incorporated by reference into the present application.
- the gerotor assembly 20 has a central axis which is coincident with the axis of the shaft 18 .
- the shaft 18 passes through a shaft opening 26 in the pump body 22 , through the gear assembly 20 , into a cover recess 28 , and abuts a thrust button 30 .
- the shaft 18 is journalled within a bearing 32 .
- the pump body 22 has a fuel outlet (not shown) leading from an outlet porting 82 . Pressurized fuel is discharged through the fuel outlet (not shown) to 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 a fuel inlet 44 .
- the gear assembly 20 has a lifting and lubricating feature for the fuel pump 10 .
- the gear assembly 10 includes an inner gear 50 and an outer gear 52 which is disposed about the outer diameter of the inner gear 50 .
- the inner gear 50 and the outer gear 52 are in camming relationship to cooperate with each other for supplying fuel to the automotive engine from the fuel tank.
- the inner and outer gears 50 , 52 are both toothed.
- the inner gear 50 is toothed along its outer diameter and the outer gear 52 is toothed along an inner wall to cooperate with the inner gear 50 .
- the gear assembly further includes a cram ring 54 which is slideably disposed about the outer diameter of the outer gear. As shown, the height of the cram ring 54 determines the distance between the pump body 22 and the pump cover 24 .
- FIGS. 2 a and 2 b illustrate an exploded view of the gear assembly 20 .
- the pump cover 24 generally includes a primary inlet porting 84 , seal areas 49 and 51 , and a secondary outlet porting 86 .
- the primary inlet porting 84 is a low pressure fuel side of the pump cover 24 and may be defined by the configuration of the gear assembly.
- the secondary outlet porting 86 is a high pressure fuel side of the pump cover.
- each of the seal areas 49 , 51 is formed between one of the portings 84 , 86 .
- the pump cover 24 includes a cover surface 25 adjacent the inner and outer gears 50 , 52 .
- the cover surface 25 is adjacent the inner gear cover face and the outer gear cover face.
- the cover surface 25 has an inlet aperture 27 and has a primary inlet porting 84 and a secondary outlet porting 86 formed thereon.
- the primary inlet porting 84 is formed from the inlet aperture 27 at a first inlet end 31 and radially extends therealong at a second inlet end 33 .
- the secondary outlet porting 86 radially extends between first and second outlet ends 35 , 37 .
- the primary inlet porting 84 has a radial width which increases toward the second inlet end 33 .
- the primary inlet porting 84 further has a first depth at the first inlet end 31 and decreases toward the second inlet end 33 to a second depth as it extends along the cover surface.
- the primary inlet porting 84 has a varying width and a varying depth.
- the primary inlet porting 84 has a depth of about 4.0 millimeters at the first inlet end 31 and tapers or decreases to about 2.0 millimeters at the second inlet end 33 .
- the secondary outlet porting 86 has a depth of about 1.0 millimeters, having a substantially constant depth. As shown, the primary inlet porting 84 and the secondary outlet porting 86 of the pump cover 24 are separated by seal areas 88 , 89 .
- the pump body 22 generally includes a secondary inlet porting 80 , seal areas 47 and 48 , and a primary outlet porting 82 formed on the pump body surface.
- the secondary inlet porting 80 is a low pressure fuel side of the pump body 22 and may be defined by the configuration of the gear assembly.
- the primary outlet porting 82 is a high pressure fuel side of the pump body 22 .
- each of the seal areas 47 , 48 is formed between one of the portings 80 , 82 .
- the pump body 22 includes a body surface 41 adjacent the inner and outer gears 50 , 52 opposite the pump cover 24 .
- the body surface 41 is adjacent the inner gear body face and the outer gear body face.
- the body surface 41 has an outlet aperture 43 formed therethrough.
- the body surface 41 further has a primary outlet porting 82 and a secondary inlet porting 80 formed thereon.
- the primary outlet porting 82 is formed at the outlet aperture 43 and is in alignment with the secondary outlet porting 86 .
- the primary and secondary inlet portings 84 , 80 are configured to allow fuel to pass therethrough at a rate corresponding to the rate at which the gear assembly moves or rotates.
- the primary outlet porting 82 radially extends therealong in alignment with the secondary outlet porting 86 .
- the secondary inlet porting 80 is in alignment with the primary inlet porting 84 .
- the primary and secondary outlet portings 82 , 86 are configured to allow fuel to pass therethrough at a rate corresponding to the rate at which the gear assembly rotates.
- the primary outlet porting 82 has a radial width which decreases toward the second outlet end 37 .
- the primary outlet porting also has a first depth at the first outlet end 35 and flares or increases to the second outlet end 37 to a second depth.
- the primary outlet porting 82 has a varying width and a varying depth as it extends along the body surface.
- the primary outlet porting 82 has a depth of about 2.0 millimeters at the first outlet end 35 and increases to about 4.0 millimeters at the second outlet end 37 .
- the primary outlet porting and the secondary inlet porting cooperate to allow fuel to pass therethrough at a rate at which the gear assembly rotates.
- the secondary inlet porting 80 has a depth of about 1.0 millimeters, having a substantially constant depth.
- each of the seal areas mentioned above is about 0.93 pitch length of the inner gear or less than 1.0 pitch length of the inner gear.
- the inlet portings and the outlet portings have predetermined pitch values so that during normal operations, the fuel pump allows fuel to pass therethrough at a rate corresponding to the rate at which the gear assembly rotates.
- the inlet portings have a greater pitch value than the outlet portings.
- the inlet and outlet portings have a pitch value ratio of approximately 3:2, wherein the pitch value ratio is based on the pitch of the inner gear.
- the inlet portings have a pitch value of 2.54 and the outlet portings have a pitch value of 1.60.
- the inner gear 50 has a substantially disc shape with an outside camming surface 56 which is a first toothed surface.
- the inner gear further includes an inner cover face 58 and an inner body face 60 .
- the inner gear 50 further has a center aperture 62 formed therethrough to define an axis A of rotation which is perpendicular to the inner cover face 58 and the inner body face 60 .
- the inner cover face 58 has a plurality of inner concave grooves 64 radially formed thereon and spaced apart from each other to provide lifting or floating of the inner gear 50 when rotating about axis A.
- the plurality of inner concave grooves 64 are radially aligned with each other on the inner cover face 58 of the inner gear 50 .
- each of the inner concave grooves 64 is radially formed on the inner cover face 58 and extends, for example about 30°-120° and preferably about 90°, thereabout based on the number of inner concave grooves.
- each of the inner concave grooves 64 is separated by a flat or planar surface in each end, for example about 5°-20° and preferably about 10°, thereabout on the inner cover face 58 of the inner gear 50 depending on the number of inner concave grooves.
- the inner body face 60 has a plurality of inner convex grooves 66 radially formed thereon and spaced apart from each other.
- Each of the inner convex grooves 66 is opposite with a respective inner concave groove 64 of the inner cover face 58 .
- each of the inner convex grooves 66 is formed on the inner body face 60 of the inner gear 50 and radially extends, for example about 30°-120 and preferably about 90°, thereabout depending of the number of inner convex grooves.
- Each of the inner convex grooves 66 are convexly formed, for example about 5°-60° and preferably about 30° on the each end with about 30° flat on the middle (see FIG. 5 c ), on the inner body face 60 of the inner gear 50 based on the number of inner convex grooves.
- the inner gear includes three inner concave grooves and three inner convex grooves.
- the plurality of inner concave grooves and the plurality of inner convex grooves may include any number of groove greater than one groove formed on the inner gear without falling beyond the scope or spirit of the present invention.
- the inner gear 52 further includes a plurality of exit holes 68 formed therethrough and spaced apart between each of the inner concave grooves 64 .
- each of the exit holes 68 is formed through one of the inner convex grooves 66 and extends, for example about 30°, thereabout.
- the outer gear 52 has a substantially planar shape.
- the outer gear 52 includes an annular wall 70 having an inside camming surface 72 .
- Inside camming surface 72 cammingly engages about the outside camming surface 56 of the inner gear 50 to matingly cooperate with the inner gear 50 for rotation about the axis A.
- the inside camming surface 72 is a second toothed surface which matingly cooperates with the first toothed surface of the outside camming surface 56 .
- the outer gear has one more tooth than the inner gear.
- the inner gear and the outer gear are off-center from each other. In this embodiment, during normal use when the gears rotate, the camming surfaces of the gears cooperate such that the cavities 38 changes the volume between the inlet and outlet and that the number of separate cavities are equal to the number of the teeth of the inner gear.
- the outer gear 52 has an outer cover surface 74 and an outer body surface 76 .
- the outer cover surface 74 has a plurality of outer concave grooves 78 radially formed thereon and spaced apart from each other to provide improved lifting or floating of the outer gear 52 when rotating about the axis A.
- each of the outer concave grooves 78 extends about 17° about the outer cover surface 74 .
- each of the outer concave grooves 78 is concavely formed on the outer cover surface 74 of the outer gear 52 and extends about 17° thereabout.
- the plurality of the outer concave grooves are radially aligned with each other on the outer cover surface of the outer gear.
- the outside camming surface 56 has teeth formed radially thereon and the inside camming surface 72 has teeth formed radially thereon.
- the teeth of the inner gear 50 is configured to matingly cooperate with the teeth of the outer gear 52 for rotation of the axis A.
- the teeth of the outer gear 52 is greater in number than the teeth of the inner gear 52 .
- the inner gear has six teeth while the outer gear has seven teeth. This allows rotation of the outer gear 52 about the inner gear 50 during normal operation of the fuel pump.
- the cram ring 54 is slidably disposed about the outer gear 52 .
- pumping cavities 38 are formed between inside camming surface 72 of outer gear 52 and outside camming surface 56 of the inner gear 50 .
- the primary inlet porting 84 of the pump cover and the secondary inlet porting 80 of the pump body feed fuel to the cavities at which volumes increase.
- the primary outlet porting 82 of the pump body and the secondary outlet porting 86 of the pump cover receive fuel from the cavities, at which volumes are decreases, and deliver fuel to the outlet.
- the gerotor assembly is preferably made of powered metal, or sintered metal, for example, sintered Nickel steel. It is to be understood that the gerotor assembly could also be made from other non-plastic materials known to those skilled in the art such as aluminum or steel.
- the fuel pump can be mounted within a fuel tank (not shown) or, alternatively, can be mounted in-line between the fuel tank and the engine of the vehicle.
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- Details And Applications Of Rotary Liquid Pumps (AREA)
Abstract
The present invention involves a gear assembly of a fuel pump for improved supply of fuel to an automotive engine from a fuel tank. The assembly includes an inner gear and an outer gear matingly cooperating with the inner gear for rotation about an axis. The assembly further includes a pump cover including a cover surface adjacent the inner and outer gears and a pump body including a body surface adjacent the inner and outer gears opposite the pump cover. The cover surface has a primary inlet porting and a secondary outlet porting formed thereon and separated between seal areas. The body surface of the pump body includes a primary outlet porting and a secondary inlet porting separated between seal areas. In use, the inlet portings and the outlet portings of the pump body and the pump cover cooperate together, respectively, such that fuel entering through the inlet portings pass therethrough at a rate at which the gear assembly moves. Also, the outlet portings of the pump body and the pump cover cooperate together to allow fuel to pass therethrough at the rate at which the gear assembly moves.
Description
- The present invention relates to a gear assembly of a gerotor fuel pump for improved efficiency in supplying fuel to an automotive engine from a fuel tank.
- Gerotor fuel pumps that have a gear assembly with a ring slidably disposed around the outer diameter have been widely used in automotive applications. Such fuel pumps have been used because of their low cost and relatively high efficiency.
- However, the efficiency of many such fuel pumps and problems associated therewith can still further be improved. For example, many current gerotor fuel pumps experience pressure pulsation at an inlet area adjacent the bottom of the fuel tank of a vehicle. As a result, relatively high noise is experienced between the tank and the fuel pump. Additionally, in many situations, such gerotor fuel pumps may experience relatively high acceleration and pressure fluctuations therethrough potentially resulting in cavitations and reduced efficiency. Moreover, manufacturers of fuel pumps are also concerned about avoiding potential hydraulic lock when the fuel is at a high pressure within the pump.
- Thus, it is one aspect of the present invention to provide a gerotor fuel pump for improved efficiency in supplying fuel to an automotive engine from a fuel tank, wherein the gerotor fuel pump includes an improved porting system to reduce local velocity acceleration within the fuel pump for avoiding potential cavitations, pressure pulsations, and relatively high noise.
- It is another aspect of the present invention to provide a gerotor or gear assembly having a porting system for improved supply of fuel to an automotive engine from a fuel tank. In one embodiment, the gear assembly includes an inner gear and an outer gear matingly cooperating with the inner gear for rotation about an axis. The assembly further includes a pump cover having a cover surface adjacent the inner and outer gears and a pump body having a body surface adjacent the inner and outer gears opposite the pump cover. The cover surface has an inlet aperture formed therethrough. The cover surface further has a primary inlet porting and a secondary outlet porting formed thereon wherein the primary inlet porting is formed from the inlet aperture at a first inlet end and radially extends therealong at a second inlet end. The secondary outlet porting radially extends between first and second outlet ends.
- In another aspect of the present invention, the gerotor or gear assembly having a porting system includes an inlet porting and an outlet porting, wherein the inlet porting has a greater length than the outlet porting to reduce inlet fuel velocity, prevent potential cavitations, and reduce noise.
- The body surface of the pump body has an outlet aperture formed therethrough. The body surface further has a primary outlet porting and a secondary inlet porting formed thereon. The primary outlet porting is formed at the outlet aperture. The primary and secondary inlet portings are configured to allow fuel to pass therethrough at a rate at which the gear assembly moves. The primary outlet porting radially extends therealong in alignment with the secondary outlet porting. The secondary inlet porting is in alignment with the primary inlet porting.
- In another aspect, the present invention allows for improved efficiency by allowing fuel to pass therethrough at a rate corresponding to the rate at which the gear assembly moves.
- It is yet another aspect of the present invention to provide a gerotor fuel pump for improved supply of fuel to an automotive engine from a fuel tank. The fuel pump comprises a pump housing and a motor mounted within the housing and having a shaft extending therefrom. The fuel pump further includes the gear assembly mentioned above. The primary outlet porting is formed at the outlet aperture and in alignment with the secondary outlet porting. The primary and secondary inlet portings are configured to allow fuel to pass therethrough at a rate at which the gear assembly rotates. The primary and secondary outlet portings are configured to allow fuel to pass therethrough at a rate corresponding to the rate at which the gear assembly rotates. The primary outlet porting radially extends therealong in alignment with the secondary outlet porting. The secondary inlet porting is in alignment with the primary inlet porting.
- The following description of the preferred embodiment of the present invention is not intended to limit the scope of the invention to this preferred embodiment, but rather enable any person skilled in the art to make and use the invention.
- FIG. 1 is a cross-sectional view of a fuel pump having a gear assembly in accordance with one embodiment of the present invention;
- FIG. 2a is an exploded inlet view of the gear assembly in FIG. 1;
- FIG. 2b is an exploded exit view of the gear assembly in FIG. 1;
- FIG. 3a is a cover surface view of a pump cover of the gear assembly in accordance with one embodiment of the present invention;
- FIG. 3b is a cross-sectional view of the pump cover taken along lines 3 b-3 b in FIG. 3a;
- FIG. 3c is another cross-sectional view of the pump cover taken along
lines 3 c-3 c in FIG. 3a; - FIG. 3d is yet another cross-sectional view of the pump cover taken along lines 3 d-3 d in FIG. 3a;
- FIG. 4a is a body surface view of a pump cover of the gear assembly in accordance with one embodiment of the present invention;
- FIG. 4b is a cross-sectional view of the pump body taken along lines 4 b-4 b in FIG. 4a;
- FIG. 4c is another cross-sectional view of the pump body taken along
lines 4 c-4 c in FIG. 4a; - FIG. 4d is yet another cross-sectional view of the pump body taken along lines 4 d-4 d in FIG. 4a;
- FIG. 5a is a first view of an inner gear (cover side) of the gear assembly in accordance with one embodiment of the present invention;
- FIG. 5b is a second view of the inner gear (body side) in accordance with the present invention;
- FIG. 5c is a cross-sectional view of the inner gear taken along lines 5 c-5 c in FIG. 5b;
- FIG. 6a is a first view of the outer gear (cover side) of the gear assembly in accordance with one embodiment of the present invention;
- FIG. 6b is a cross-sectional view of the outer gear taken along lines 6 b-6 b in FIG. 6a;
- FIG. 7a is a cover side view of the gear assembly in accordance with the present invention; and
- FIG. 7b is a cross-sectional view of the gear assembly taken along lines 7 b-7 b in FIG. 7a.
- Referring to FIG. 1, a fuel pump of the present invention is generally shown at10. The
fuel pump 10 includes ahousing 12 and amotor 14 mounted within thehousing 12. Preferably, themotor 14 is an electric motor with ashaft 18 extending therefrom. A gerotor orgear assembly 20 having inner and outer gears is fitted onto theshaft 18 and is encased within thepump housing 12 between apump body 22 and apump cover 24. Thegerotor assembly 20 fits onto theshaft 18 such that the assembly is free to move axially along theshaft 18 and rotates with theshaft 18. Therefore, the gerotor assembly “float” between thepump cover 24 and thepump body 22. The fuel pump is of a conventional type which is further described in U.S. Pat. No. 6,113,360 and U.S. patent application Ser. No. 10/256,359 which are assigned to the same assignee as the present application and are hereby incorporated by reference into the present application. - The
gerotor assembly 20 has a central axis which is coincident with the axis of theshaft 18. Theshaft 18 passes through ashaft opening 26 in thepump body 22, through thegear assembly 20, into acover recess 28, and abuts athrust button 30. Theshaft 18 is journalled within abearing 32. Thepump body 22 has a fuel outlet (not shown) leading from an outlet porting 82. Pressurized fuel is discharged through the fuel outlet (not shown) to and cools themotor 14 while passing over themotor 14 to apump outlet 42 at an end of thepump 10 which is axially opposite afuel inlet 44. - As shown in FIGS. 2a and 2 b, the
gear assembly 20, in this embodiment, has a lifting and lubricating feature for thefuel pump 10. Thegear assembly 10 includes aninner gear 50 and anouter gear 52 which is disposed about the outer diameter of theinner gear 50. Theinner gear 50 and theouter gear 52 are in camming relationship to cooperate with each other for supplying fuel to the automotive engine from the fuel tank. As will be described in greater detail below, the inner andouter gears inner gear 50 is toothed along its outer diameter and theouter gear 52 is toothed along an inner wall to cooperate with theinner gear 50. The gear assembly further includes acram ring 54 which is slideably disposed about the outer diameter of the outer gear. As shown, the height of thecram ring 54 determines the distance between thepump body 22 and thepump cover 24. - FIGS. 2a and 2 b illustrate an exploded view of the
gear assembly 20. As shown, thepump cover 24 generally includes a primary inlet porting 84,seal areas pump cover 24 and may be defined by the configuration of the gear assembly. The secondary outlet porting 86 is a high pressure fuel side of the pump cover. As shown, each of theseal areas portings - As shown in FIGS. 2a-3 d, the
pump cover 24 includes acover surface 25 adjacent the inner andouter gears cover surface 25 is adjacent the inner gear cover face and the outer gear cover face. Thecover surface 25 has aninlet aperture 27 and has a primary inlet porting 84 and a secondary outlet porting 86 formed thereon. The primary inlet porting 84 is formed from theinlet aperture 27 at afirst inlet end 31 and radially extends therealong at asecond inlet end 33. The secondary outlet porting 86 radially extends between first and second outlet ends 35, 37. The primary inlet porting 84 has a radial width which increases toward thesecond inlet end 33. The primary inlet porting 84 further has a first depth at thefirst inlet end 31 and decreases toward thesecond inlet end 33 to a second depth as it extends along the cover surface. Thus, the primary inlet porting 84 has a varying width and a varying depth. In this embodiment, the primary inlet porting 84 has a depth of about 4.0 millimeters at thefirst inlet end 31 and tapers or decreases to about 2.0 millimeters at thesecond inlet end 33. The secondary outlet porting 86 has a depth of about 1.0 millimeters, having a substantially constant depth. As shown, the primary inlet porting 84 and the secondary outlet porting 86 of thepump cover 24 are separated byseal areas - As shown in FIGS. 4a-4 d, the
pump body 22 generally includes a secondary inlet porting 80,seal areas pump body 22 and may be defined by the configuration of the gear assembly. The primary outlet porting 82 is a high pressure fuel side of thepump body 22. As shown, each of theseal areas portings - The
pump body 22 includes abody surface 41 adjacent the inner andouter gears pump cover 24. Specifically, thebody surface 41 is adjacent the inner gear body face and the outer gear body face. Thebody surface 41 has anoutlet aperture 43 formed therethrough. Thebody surface 41 further has a primary outlet porting 82 and a secondary inlet porting 80 formed thereon. The primary outlet porting 82 is formed at theoutlet aperture 43 and is in alignment with the secondary outlet porting 86. The primary and secondary inlet portings 84, 80 are configured to allow fuel to pass therethrough at a rate corresponding to the rate at which the gear assembly moves or rotates. The primary outlet porting 82 radially extends therealong in alignment with the secondary outlet porting 86. The secondary inlet porting 80 is in alignment with the primary inlet porting 84. - In this embodiment, the primary and secondary outlet portings82, 86 are configured to allow fuel to pass therethrough at a rate corresponding to the rate at which the gear assembly rotates. The primary outlet porting 82 has a radial width which decreases toward the
second outlet end 37. The primary outlet porting also has a first depth at thefirst outlet end 35 and flares or increases to thesecond outlet end 37 to a second depth. Thus, the primary outlet porting 82 has a varying width and a varying depth as it extends along the body surface. In this embodiment, the primary outlet porting 82 has a depth of about 2.0 millimeters at thefirst outlet end 35 and increases to about 4.0 millimeters at thesecond outlet end 37. The primary outlet porting and the secondary inlet porting cooperate to allow fuel to pass therethrough at a rate at which the gear assembly rotates. The secondary inlet porting 80 has a depth of about 1.0 millimeters, having a substantially constant depth. In this embodiment, each of the seal areas mentioned above is about 0.93 pitch length of the inner gear or less than 1.0 pitch length of the inner gear. - The inlet portings and the outlet portings have predetermined pitch values so that during normal operations, the fuel pump allows fuel to pass therethrough at a rate corresponding to the rate at which the gear assembly rotates. The inlet portings have a greater pitch value than the outlet portings. For example, the inlet and outlet portings have a pitch value ratio of approximately 3:2, wherein the pitch value ratio is based on the pitch of the inner gear. In this embodiment, the inlet portings have a pitch value of 2.54 and the outlet portings have a pitch value of 1.60.
- As shown in FIGS. 2a and 2 b, the
inner gear 50 has a substantially disc shape with anoutside camming surface 56 which is a first toothed surface. The inner gear further includes aninner cover face 58 and aninner body face 60. Theinner gear 50 further has acenter aperture 62 formed therethrough to define an axis A of rotation which is perpendicular to theinner cover face 58 and theinner body face 60. - In this embodiment, the
inner cover face 58 has a plurality of innerconcave grooves 64 radially formed thereon and spaced apart from each other to provide lifting or floating of theinner gear 50 when rotating about axis A. In this embodiment, the plurality of innerconcave grooves 64 are radially aligned with each other on the inner cover face 58 of theinner gear 50. As shown in FIGS. 5a-5 c, each of the innerconcave grooves 64 is radially formed on theinner cover face 58 and extends, for example about 30°-120° and preferably about 90°, thereabout based on the number of inner concave grooves. In this embodiment, each of the innerconcave grooves 64 is separated by a flat or planar surface in each end, for example about 5°-20° and preferably about 10°, thereabout on the inner cover face 58 of theinner gear 50 depending on the number of inner concave grooves. - As shown, the
inner body face 60 has a plurality of innerconvex grooves 66 radially formed thereon and spaced apart from each other. Each of the innerconvex grooves 66 is opposite with a respective innerconcave groove 64 of theinner cover face 58. In this embodiment, each of the innerconvex grooves 66 is formed on the inner body face 60 of theinner gear 50 and radially extends, for example about 30°-120 and preferably about 90°, thereabout depending of the number of inner convex grooves. Each of the innerconvex grooves 66 are convexly formed, for example about 5°-60° and preferably about 30° on the each end with about 30° flat on the middle (see FIG. 5c), on the inner body face 60 of theinner gear 50 based on the number of inner convex grooves. - In this embodiment, the inner gear includes three inner concave grooves and three inner convex grooves. However, it is to be understood that the plurality of inner concave grooves and the plurality of inner convex grooves may include any number of groove greater than one groove formed on the inner gear without falling beyond the scope or spirit of the present invention.
- As shown, the
inner gear 52 further includes a plurality of exit holes 68 formed therethrough and spaced apart between each of the innerconcave grooves 64. In this embodiment, each of the exit holes 68 is formed through one of the innerconvex grooves 66 and extends, for example about 30°, thereabout. - As shown in FIGS. 2, 6, and7, the
outer gear 52 has a substantially planar shape. Theouter gear 52 includes anannular wall 70 having aninside camming surface 72. Insidecamming surface 72 cammingly engages about theoutside camming surface 56 of theinner gear 50 to matingly cooperate with theinner gear 50 for rotation about the axis A. As shown, theinside camming surface 72 is a second toothed surface which matingly cooperates with the first toothed surface of theoutside camming surface 56. In this embodiment, the outer gear has one more tooth than the inner gear. As shown, the inner gear and the outer gear are off-center from each other. In this embodiment, during normal use when the gears rotate, the camming surfaces of the gears cooperate such that thecavities 38 changes the volume between the inlet and outlet and that the number of separate cavities are equal to the number of the teeth of the inner gear. - The
outer gear 52 has anouter cover surface 74 and anouter body surface 76. In this embodiment, theouter cover surface 74 has a plurality of outerconcave grooves 78 radially formed thereon and spaced apart from each other to provide improved lifting or floating of theouter gear 52 when rotating about the axis A. In this embodiment, each of the outerconcave grooves 78 extends about 17° about theouter cover surface 74. As shown, each of the outerconcave grooves 78 is concavely formed on theouter cover surface 74 of theouter gear 52 and extends about 17° thereabout. In this embodiment, the plurality of the outer concave grooves are radially aligned with each other on the outer cover surface of the outer gear. - Thus, the
outside camming surface 56 has teeth formed radially thereon and theinside camming surface 72 has teeth formed radially thereon. The teeth of theinner gear 50 is configured to matingly cooperate with the teeth of theouter gear 52 for rotation of the axis A. As shown, the teeth of theouter gear 52 is greater in number than the teeth of theinner gear 52. For example in this embodiment, the inner gear has six teeth while the outer gear has seven teeth. This allows rotation of theouter gear 52 about theinner gear 50 during normal operation of the fuel pump. As shown, thecram ring 54 is slidably disposed about theouter gear 52. - As shown in FIGS. 2 and 7, pumping
cavities 38 are formed betweeninside camming surface 72 ofouter gear 52 andoutside camming surface 56 of theinner gear 50. In operation, when the gear assembly rotates, the primary inlet porting 84 of the pump cover and the secondary inlet porting 80 of the pump body feed fuel to the cavities at which volumes increase. Moreover, the primary outlet porting 82 of the pump body and the secondary outlet porting 86 of the pump cover receive fuel from the cavities, at which volumes are decreases, and deliver fuel to the outlet. - The gerotor assembly is preferably made of powered metal, or sintered metal, for example, sintered Nickel steel. It is to be understood that the gerotor assembly could also be made from other non-plastic materials known to those skilled in the art such as aluminum or steel. The fuel pump can be mounted within a fuel tank (not shown) or, alternatively, can be mounted in-line between the fuel tank and the engine of the vehicle.
- It is to be understood that the inner gear and the outer gear are mentioned above in accordance with one embodiment of the present invention. It is understood that the lifting feature mentioned above of the inner and outer gears are not required in the present invention. Thus, other embodiments without concave and convex grooves do not fall beyond the scope or spirit of the present invention.
- The foregoing discussion discloses and describes two 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.
Claims (52)
1. A gear assembly of a fuel pump for supplying fuel to an automotive engine from a fuel tank, the assembly comprising:
an inner gear;
an outer gear matingly cooperating with the inner gear for rotation about an axis;
a pump cover including a cover surface adjacent the inner and outer gears, the cover surface having an inlet aperture formed therethrough, the cover surface having a primary inlet porting and a secondary outlet porting formed thereon, the primary inlet porting being formed from the inlet aperture at a first inlet end and radially extending therealong at a second inlet end, the secondary outlet porting radially extending between first and second outlet ends;
a pump body including a body surface adjacent the inner and outer gears opposite the pump cover, the body surface having an outlet aperture formed therethrough, the body surface having a primary outlet porting and a secondary inlet porting formed thereon, the primary outlet porting being formed at the outlet aperture and in alignment with the secondary outlet porting, the primary and secondary inlet portings being configured to allow fuel to pass therethrough at a rate at which the gear assembly moves, the primary outlet porting radially extending therealong in alignment with the secondary outlet porting, the secondary inlet porting being in alignment with the primary inlet porting.
2. The assembly of claim 1 wherein the primary and secondary outlet portings are configured to allow fuel to pass therethrough at the rate at which gear assembly rotates.
3. The assembly of claim 1 wherein the inner gear has a substantially disc shape with an outside camming surface and having an inner gear cover face and an inner gear body face.
4. The assembly of claim 3 wherein the outer gear has an annular wall having an inside camming surface to matingly cooperate with the outside camming surface of the inner gear for rotation about an axis, the outer gear having an outer gear cover face and an outer gear body face.
5. The assembly of claim 4 wherein the cover surface is adjacent the inner gear cover face and the outer gear cover face.
6. The assembly of claim 1 wherein the inner gear has a substantially disc shape with an outside camming surface and having an inner gear cover face and an inner gear body face, the inner gear having a center aperture formed therethrough defining an axis of rotation perpendicular to the inner gear cover face and the inner gear body face.
7. The assembly of claim 6 wherein the outer gear has a substantially planar shape, the outer gear including an annular wall having an inside camming surface slidably engaging about the outside camming surface to matingly cooperate with the inner gear for rotation about the axis, the outer gear having an outer gear cover face and an outer gear body face.
8. The assembly of claim 1 wherein the primary inlet porting has a radial width increasing toward the second inlet end.
9. The assembly of claim 8 wherein the primary inlet porting has a first depth at the first inlet end and decreasing toward the second inlet end to a second depth.
10. The assembly of claim 1 wherein the primary inlet porting has a first varying width and a first varying depth.
11. The assembly of claim 1 wherein the primary inlet porting has a depth of about 4.0 millimeters at the first inlet end and decreasing to about 2.0 millimeters at the second inlet end.
12. The assembly of claim 1 wherein the secondary outlet porting has a depth of about 1.0 millimeters.
13. The assembly of claim 1 wherein the secondary outlet porting has a substantially constant depth.
14. The assembly of claim 4 wherein the body surface is adjacent the inner gear body face and the outer gear body face.
15. The assembly of claim 1 wherein the primary outlet porting has a radial width decreasing toward the second outlet end.
16. The assembly of claim 15 wherein the primary outlet porting has a third depth at the first outlet end and increasing to the second outlet end to a fourth depth.
17. The assembly of claim 1 wherein the primary outlet porting has a second varying width and a second varying depth.
18. The assembly of claim 1 wherein the primary outlet porting has a depth of about 2.0 millimeters at the first outlet end and increasing to about 4.0 millimeters at the second outlet end.
19. The assembly of claim 1 wherein the secondary inlet porting has a depth of about 1.0 millimeters.
20. The assembly of claim 1 wherein the secondary inlet porting has a substantially constant depth.
21. The assembly of claim 1 wherein the primary inlet porting and the secondary outlet porting of the pump cover and the primary outlet porting and the secondary inlet porting of the pump body are separated by seal areas.
22. The assembly of claim 21 wherein each of the seal areas is about 0.93 pitch length of the inner gear.
23. A gear assembly for a fuel pump for supplying fuel to an automotive engine from a fuel tank, the assembly comprising:
an inner gear including a substantially disc shape with an outside camming surface and having an inner gear cover face and an inner gear body face;
an outer gear including an annular wall having an inside camming surface to matingly cooperate with the outside camming surface of the inner gear for rotation about an axis, the outer gear having an outer gear cover face and an outer gear body face;
a pump cover including a cover surface adjacent the inner gear cover face and the outer gear cover face, the cover surface having an inlet aperture formed therethrough, the cover surface having a primary inlet porting and a secondary outlet porting formed thereon, the primary inlet porting being formed from the inlet aperture at a first inlet end and radially extending therealong at a second inlet end, the secondary outlet porting radially extending between first and second outlet ends; and
a pump body including a body surface adjacent the inner gear body face and the outer gear body face, the body surface having an outlet aperture formed therethrough, the body surface having a primary outlet porting and a secondary inlet porting formed thereon, the primary outlet porting being formed at the outlet aperture and in alignment with the secondary outlet porting, the primary outlet porting radially extending therealong in alignment with the second outlet end, the secondary inlet porting being in alignment with the primary inlet porting, the primary and secondary inlet portings being configured to allow fuel to pass therethrough at a rate at which the gear assembly rotates;
24. The assembly of claim 22 wherein the primary and secondary outlet portings are configured to allow fuel to pass therethrough at the rate at which the gear assembly rotates.
25. A gerotor fuel pump for supplying fuel to an automotive engine from a fuel tank, the fuel pump comprising:
a pump housing;
a motor mounted within the housing and having a shaft extending therefrom;
an inner gear disposed within the housing;
an outer gear disposed within the housing and matingly cooperating with the inner gear for rotation about an axis;
a pump cover mounted within an end of the housing and including a cover surface adjacent the inner and outer gears, the cover surface having an inlet aperture formed therethrough, the cover surface having a primary inlet porting and a secondary outlet porting formed thereon, the primary inlet porting being formed from the inlet aperture at a first inlet end and radially extending therealong at a second inlet end, the secondary outlet porting radially extending between first and second outlet ends;
a pump body mounted within the housing and having a bore through which the shaft extends, the pump body including a body surface adjacent the inner and outer gears opposite the pump cover, the body surface having an outlet aperture formed therethrough, the body surface having a primary outlet porting and a secondary inlet porting formed thereon, the primary outlet porting being formed at the outlet aperture and in alignment with the secondary outlet porting, the primary and secondary inlet portings being configured to allow fuel to pass therethrough at a rate at which the gear assembly rotates, the primary outlet porting radially extending therealong in alignment with the secondary outlet porting, the secondary inlet porting being in alignment with the primary inlet porting.
26. The fuel pump of claim 25 wherein the primary and secondary outlet portings are configured to allow fuel to pass therethrough at the rate at which the gear assembly rotates.
27. The fuel pump of claim 25 wherein the inner gear has a substantially disc shape with an outside camming surface and having an inner gear cover face and an inner gear body face.
28. The fuel pump of claim 27 wherein the outer gear has an annular wall having an inside camming surface to matingly cooperate with the outside camming surface of the inner gear for rotation about an axis, the outer gear having an outer gear cover face and an outer gear body face.
29. The fuel pump of claim 28 wherein the cover surface is adjacent the inner gear cover face and the outer gear cover face.
30. The fuel pump of claim 25 wherein the inner gear has a substantially disc shape with an outside camming surface and having an inner gear cover face and an inner gear body face, the inner gear having a center aperture formed therethrough defining an axis of rotation perpendicular to the inner gear cover face and the inner gear body face.
31. The fuel pump of claim 30 wherein the outer gear has a substantially planar shape, the outer gear including an annular wall having an inside camming surface slidably engaging about the outside camming surface to matingly cooperate with the inner gear for rotation about the axis, the outer gear having an outer gear cover face and an outer gear body face.
32. The fuel pump of claim 25 wherein the primary inlet porting has a radial width increasing toward the second inlet end.
33. The fuel pump of claim 32 wherein the primary inlet porting has a first depth at the first inlet end and decreasing toward the second inlet end to a second depth.
34. The fuel pump of claim 25 wherein the primary inlet porting has a first varying width and a first varying depth.
35. The fuel pump of claim 25 wherein the primary inlet porting has a depth of about 4.0 millimeters at the first inlet end and decreasing to about 2.0 millimeters at the second inlet end.
36. The fuel pump of claim 25 wherein the secondary outlet porting has a depth of about 1.0 millimeters.
37. The fuel pump of claim 25 wherein the secondary outlet porting has a substantially constant depth.
38. The fuel pump of claim 28 wherein the body surface is adjacent the inner gear body face and the outer gear body face.
39. The fuel pump of claim 25 wherein the primary outlet porting has a radial width decreasing toward the second outlet end.
40. The fuel pump of claim 39 wherein the primary outlet porting has a third depth at the first outlet end and increasing to the second outlet end to a fourth depth.
41. The fuel pump of claim 25 wherein the primary outlet porting has a second varying width and a second varying depth.
42. The fuel pump of claim 25 wherein the primary outlet porting has a depth of about 2.0 millimeters at the first outlet end and increasing to about 4.0 millimeters at the second outlet end.
43. The fuel pump of claim 25 wherein the secondary inlet porting has a depth of about 1.0 millimeters.
44. The fuel pump of claim 25 wherein the secondary inlet porting has a substantially constant depth.
45. The fuel pump of claim 25 wherein the primary inlet porting and the secondary outlet porting of the pump cover and the primary outlet porting and the secondary inlet porting of the pump body are separated by seal areas.
46. The fuel pump of claim 45 wherein each of the seal areas is about 0.93 pitch length of the inner gear.
47. The assembly of claim 1 wherein the inlet portings have a first pitch value and the outlet portings have a second pitch value, wherein the first pitch value is greater than the second pitch value.
48. The assembly of claim 47 wherein the first pitch value and the second pitch value are at a pitch value ratio of about 3:2.
49. The gear assembly of claim 23 wherein the inlet portings have a first pitch value and the outlet portings have a second pitch value, the first pitch value being greater than the second pitch value.
50. The gear assembly of claim 49 wherein the first pitch value and the second pitch value are at a pitch value ratio of about 3:2.
51. The gerotor fuel pump of claim 25 wherein the inlet portings have a first pitch value and the outlet portings have a second pitch value, the first pitch value being greater than the second pitch value.
52. The gerotor fuel pump of claim 51 wherein the first pitch value and the second pitch value have a pitch value ratio of about 3:2.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/306,585 US20040101427A1 (en) | 2002-11-27 | 2002-11-27 | Gerotor fuel pump having primary and secondary inlet and outlet portings |
GB0327225A GB2396385B (en) | 2002-11-27 | 2003-11-24 | Gerotor fuel pump |
DE10355774A DE10355774A1 (en) | 2002-11-27 | 2003-11-26 | Rotor fuel pump with internally toothed rotor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/306,585 US20040101427A1 (en) | 2002-11-27 | 2002-11-27 | Gerotor fuel pump having primary and secondary inlet and outlet portings |
Publications (1)
Publication Number | Publication Date |
---|---|
US20040101427A1 true US20040101427A1 (en) | 2004-05-27 |
Family
ID=29780426
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/306,585 Abandoned US20040101427A1 (en) | 2002-11-27 | 2002-11-27 | Gerotor fuel pump having primary and secondary inlet and outlet portings |
Country Status (3)
Country | Link |
---|---|
US (1) | US20040101427A1 (en) |
DE (1) | DE10355774A1 (en) |
GB (1) | GB2396385B (en) |
Cited By (11)
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US20080031760A1 (en) * | 2006-08-15 | 2008-02-07 | Arvinmeritor Technology, Llc | Gerotor pump |
WO2009135714A1 (en) * | 2008-05-09 | 2009-11-12 | Robert Bosch Gmbh | Internal gear pump |
US20120020820A1 (en) * | 2009-03-24 | 2012-01-26 | Inergy Automotive Systems Research Societe Anonyme | Rotary pump |
WO2013081784A1 (en) * | 2011-11-30 | 2013-06-06 | Walbro Engine Management, L.L.C. | Fuel pump assembly |
WO2013110037A3 (en) * | 2012-01-19 | 2014-04-24 | Parker-Hannifin Corporation | Hollow gerotor |
US20140119963A1 (en) * | 2008-11-07 | 2014-05-01 | Magna Powertrain Inc. | Submersible Integrated Electric Pump |
CN104863846A (en) * | 2014-02-25 | 2015-08-26 | Lg伊诺特有限公司 | Electric pump |
US20160230772A1 (en) * | 2013-09-17 | 2016-08-11 | Denso Corporation | Fuel pump |
US20170009625A1 (en) * | 2015-07-10 | 2017-01-12 | Mgi Coutier | Liquid delivery module, a method for assembling such a delivery module and a tank set comprising such a delivery module |
WO2018149551A1 (en) * | 2017-02-15 | 2018-08-23 | Magpumps Limited | Pump and method |
JP2020148127A (en) * | 2019-03-13 | 2020-09-17 | 株式会社ジェイテクト | Pump device |
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2002
- 2002-11-27 US US10/306,585 patent/US20040101427A1/en not_active Abandoned
-
2003
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- 2003-11-26 DE DE10355774A patent/DE10355774A1/en not_active Ceased
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US5096398A (en) * | 1990-11-13 | 1992-03-17 | Stackpole Limited | Pulse tuned optimized positive displacement porting |
US5797734A (en) * | 1996-11-26 | 1998-08-25 | Chrysler Corporation | Pump for hot and cold fluids |
US6089842A (en) * | 1996-12-16 | 2000-07-18 | Schwabische Huttenwerke Gmbh | Gear oil pump with internal rotor, comprising extensions of reniform suction and pressure elements |
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7670122B2 (en) | 2006-08-15 | 2010-03-02 | Arvinmeritor Technology, Llc | Gerotor pump |
US20080031760A1 (en) * | 2006-08-15 | 2008-02-07 | Arvinmeritor Technology, Llc | Gerotor pump |
WO2009135714A1 (en) * | 2008-05-09 | 2009-11-12 | Robert Bosch Gmbh | Internal gear pump |
US9581158B2 (en) * | 2008-11-07 | 2017-02-28 | Magna Powertrain Inc. | Submersible electric pump having a shaft with spaced apart shoulders |
US20140119963A1 (en) * | 2008-11-07 | 2014-05-01 | Magna Powertrain Inc. | Submersible Integrated Electric Pump |
US20120020820A1 (en) * | 2009-03-24 | 2012-01-26 | Inergy Automotive Systems Research Societe Anonyme | Rotary pump |
CN102365460A (en) * | 2009-03-24 | 2012-02-29 | 因勒纪汽车系统研究公司 | Rotary pump |
US20140271282A1 (en) * | 2009-03-24 | 2014-09-18 | Inergy Automotive Systems Research (Societe Anonyme) | Rotary pump with rotor and stator arrangement |
WO2013081784A1 (en) * | 2011-11-30 | 2013-06-06 | Walbro Engine Management, L.L.C. | Fuel pump assembly |
US8939736B2 (en) | 2011-11-30 | 2015-01-27 | Walbro Engine Management, L.L.C. | Fuel pump assembly |
US9617991B2 (en) | 2012-01-19 | 2017-04-11 | Parker-Hannifin Corporation | Hollow gerotor |
WO2013110037A3 (en) * | 2012-01-19 | 2014-04-24 | Parker-Hannifin Corporation | Hollow gerotor |
US20160230772A1 (en) * | 2013-09-17 | 2016-08-11 | Denso Corporation | Fuel pump |
US10408219B2 (en) * | 2013-09-17 | 2019-09-10 | Denso Corporation | Fuel pump |
US20150240811A1 (en) * | 2014-02-25 | 2015-08-27 | Lg Innotek Co., Ltd. | Electric pump |
CN104863846A (en) * | 2014-02-25 | 2015-08-26 | Lg伊诺特有限公司 | Electric pump |
US10190584B2 (en) * | 2014-02-25 | 2019-01-29 | Lg Innotek Co., Ltd. | Electric pump |
US20170009625A1 (en) * | 2015-07-10 | 2017-01-12 | Mgi Coutier | Liquid delivery module, a method for assembling such a delivery module and a tank set comprising such a delivery module |
US10895185B2 (en) * | 2015-07-10 | 2021-01-19 | Akwel | Liquid delivery module, a method for assembling such a delivery module and a tank set comprising such a delivery module |
WO2018149551A1 (en) * | 2017-02-15 | 2018-08-23 | Magpumps Limited | Pump and method |
JP2020148127A (en) * | 2019-03-13 | 2020-09-17 | 株式会社ジェイテクト | Pump device |
JP7251227B2 (en) | 2019-03-13 | 2023-04-04 | 株式会社ジェイテクト | pumping equipment |
Also Published As
Publication number | Publication date |
---|---|
DE10355774A1 (en) | 2004-06-17 |
GB2396385A (en) | 2004-06-23 |
GB0327225D0 (en) | 2003-12-24 |
GB2396385B (en) | 2004-11-03 |
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AS | Assignment |
Owner name: VISTEON GLOBAL TECHNOLOGIES, INC., MICHIGAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:YU, DEQUAN;CASTLE, HAROLD L.;KEMPFER, STEPHEN T.;REEL/FRAME:013546/0908 Effective date: 20021122 |
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STCB | Information on status: application discontinuation |
Free format text: EXPRESSLY ABANDONED -- DURING EXAMINATION |