Title of Invention	AN IMPROVED FEED PUMP WITH A DRIVEN IMPELLER
Abstract	In a feed pump (2) designed as a side-channel pump, a blade chamber (12, 13) of an impeller (5) has a contour which fs formed by a radius (R) and In which, as seen from the contour, the origin of the radius ( R) is located behind a center line of the blade chamber (12, 13). A circulation flow thereby passes into the blade chamber (12, 13) with particularly low turbulences. The feed pump (2) has particularly high efficiency as a result.

Title of Invention

AN IMPROVED FEED PUMP WITH A DRIVEN IMPELLER

Abstract

In a feed pump (2) designed as a side-channel pump, a blade chamber (12, 13) of an impeller (5) has a contour which fs formed by a radius (R) and In which, as seen from the contour, the origin of the radius ( R) is located behind a center line of the blade chamber (12, 13). A circulation flow thereby passes into the blade chamber (12, 13) with particularly low turbulences. The feed pump (2) has particularly high efficiency as a result.

Full Text	This invention relates to an improved feed pump with a driven impeller. Description The invention relates to a feed pump with a driven impeller which rotates in a pump casing and has in its end faces at least one ring of guide blades delimiting blade chambers and in which the blade chambers have an inflow region and an outflow region for the medium to be fed, and with at least one part-annular channel which is arranged in the region of the guide blades in the pump casing and which forms with the blade chambers a feed chamber from an inlet channel to an outlet channel, the contour of the blade chambers being formed by at least one radius with an origin within the feed chamber. Such feed pumps are often used for feeding fuel in a fuel tank or for feeding washing fluid in a shield washing system of a motor vehicle and are known from practice. The known feed pump has a ring of blade chambers in each of the two end faces of the impeller. The blade chambers are delimited in the radially outer direction by a straight wall arranged perpendicularly to the end faces of the impeller. The contour of the blade chambers which points in the radially inner direction of the impeller is generated by a radius. The origin of the radius is located on the center line arranged perpendicularly to the end faces of the impeller. This origin is at the same time the origin of a second radius forming the part-annular channel. One disadvantage of the known feed pump is that it generates turbulences in the medium to be fed. These turbulences lead to the feed pump having lowj efficiency. Moreover, in the case of media which are near the boiling point, such as, for example, "hot gasoline fuel, there is the risk that vapor bubbles will be formed within the feed chamber. The vapor bubbles lead to a sharp reduction in the volume flow fed by the feed pump. - 3- The problem on which the invention is based is to design a feed pump of the type initially mentioned, in such a way that it has as high an efficiency as possible and reliably prevents the formation of vapor bubbles. This problem is solved, according to the invention,, in that, as seen from the blade chamber contour determined by the radius, the origin of the radius is located in the region opposite a center line of the blade chamber, said center line running perjpendicjjJLar-l-y-to-the-end face of the impeller. By virtue of this design, the blade chamber has, in its region formed by the radius, a contour which ascends at a very low inclination. A circulation flow in the feed chamber alternates between the impeller and the pump casing via this low-inclination contour. Since the circulation flow undergoes only slight deflection in this region, the risk of turbulences is kept particularly low. The formation of vapor bubbles is also avoided as a result. According to an advantageous development of the invention, the impeller can be manufactured cost-effectively if the origins of a plurality of radii for blade chamber contours opposite one another are located on a common plane within the impeller, said plane running parallel to the end face of the impeller. Turbulences often occur in the region in which the circulation flow alternates between the blade chamber and the part-annular channel. According to another advantageous development of the invention, the circulation flow set in turbulence here can be calmed again quickly if, from the plane running parallel to the end face of the impeller as far as the end face, the blade chambers have, in their regions adjacent to the guide blades, boundaries guided perpendicularly to the end face of the impeller. According to another advantageous development of the invention, the impeller has simply constructed blade chambers and can therefore be manufactured -4- particularly cost-effectively if the origins of two radii generating in each case contours opposite one anther are arranged mirror-symmetrically to the center line of the blade chamber. As a result, the center line can be designed as a bisecting line for the contour pointing toward- the center of the impeller and for the contour pointing away from the center of the impeller. The feed pump according to the invention has particularly high efficiency if the distance of the origins of the radii from the center line is approximately the same amount as their distance from the end face. As in the known feed pump, blade chambers arranged opposite one another could be connected to one another in a radially outer region of the impeller. However, a contribution to a further increase in the efficiency of the feed pump according to the invention is made if blade chambers arranged opposite one another mirror-symmetrically in the two end faces of the impeller are connected to one another solely in the region of the center line. The circulation flow can thereby flow from one feed chamber over into the other feed chamber with particularly low turbulences. Moreover, the risk of the formation of vapor bubbles is likewise kept particularly low as a result. The invention permits numerous embodiments. In order to make its basic principle even clearer, one of these is illustrated in the drawing and is described below. In the/drawing: ' O -__/ Figure 1 shows a sectional illustration through a feed pump according to the invention, Figure 2 shows an enlarged illustration of the feed pump from Figure 1 in the region of feed chambers. Figur-e 1 shows a longitudinal section through a feed pump 2 which is driven by an electric motor 1 and is designed as an axial-throughf'low side-channel pump and which may be provided, for example, for feeding fuel out of a fuel tank, not illustrated, of a motor vehicle. The feed pump 2 has a pump casing 3, in which is arranged an impeller 5 fastened fixedly in terms of rotation on a shaft 4 of the electric motor 1. The pump casing 3 has an inlet channel 6 on its face facing away from the electric motor 1 and an outlet channel 7 on the side facing the electric motor 1. The inlet channel 6 opens into a feed chamber 8. A second feed chamber 9 opens into the outlet channel 7. The feed chambers 8, 9 have in each case part-annular channels 10, 11 incorporated in the pump casing 3 and blade chambers 12, 13 arranged in the impeller 5. The blade chambers 12, 13 are delimited in each case by guide blades 14, 15 and in each case have an inflow region 16, 17 for the inflow of the medium to be fed and an outflow region 18, 19. Blade chambers 12, 13 opposite one another are connected to one another between the inflow region 16, 17 and the outflow region 18, 19. When the impeller 5 rotates, circulation flows occur in each case in the feed chambers 8, 9. A part stream is branched off from the circulation flow of the inlet-side feed chamber 8 and flows over into the outlet-side feed chamber 9. The flows are identified by arrows in the drawing. Figure 2 shows, greatly enlarged, the feed pump 2 from Figure 1 in the region of the feed chambers 8, 9. It can be seen, here, that the blade chambers 12, 13 are in each case designed symmetrically to a center line running perpendicularly to one end face. The blade chambers 12, 13 have, in the inflow regions 16, 17 and in the outflow regions 18, 19, in each case a contour formed by radii R. The radii R have, in this case, an origin located behind the center line, as seen from the respective contour. Moreover, the origins of the radii R are located in a common plane arranged parallel to the end face of the impeller 5. For clarity, the planes of the blade chambers 12, 13 are illustrated by dashes 43 and dots in the drawing. As a result, the circulation flow passes from the part-annular channels 10, 11 into the blade chambers 12, 13 with particularly low turbulences. The plane of the origins of the radii R is at approximately the same distance from the end face of the impeller 5 as the origins of the radii R are from the center line. -7- WE CLAIM: 1. An improved feeipump with a driven impeller which rotates in a pump casing and has in its end faces at least one ring of guide blades delimiting blade chambers and in which the blade chambers have an Inflow region and an outflow region for the medium to be fed, and with at least one part- annular channel which is arranged in the region of the guide blades in the pump casing and which forms with the blade chambers a feed chamber from an inlet channel to an outlet channel, the contour of the blade chambers being formed by at least one radius with an origin within the feed chamber, characterized In that, as seen from the blade chamber (12, 13) contour determined by the radius ( R), the origin of the radius ( R) is located In the region opposite a center line of the blade chamber (12, 13), said center line running perpendicularly to the end face of the impeller (5). 2. The feed pump as claimed In claim 1, wherein the origins of a plurality of radii ( R) for blade chamber (12, 13) contours opposite one another are located on a common plane within the impeller (5), said plane 3. The feed pump as claimed in claim 1 or 2, wherein from the plane running parallel to the end face of the impeller (5) as far as the end face, the blade chambers (12, 13) have, in their regions adjacent to the guide blades (14, 15), boundaries guided perpendicularly to the end face of the impeller (5). 4. The feed pump as claimed in any one of the preceeding claims wherein the origins of two radii (R) generating in each case contours opposite one another are arranged mirror-symmetrically to the center line of the blade chambers (12,13). 5. The feed pump as claimed in any one of the preceeding claims, wherein the distance of the origins of the radii (R ) from the center^line is approximately the same amount as their distance from the end face. -8- 6. The feed pump as claimed in any one of the proceeding claims, wherein blade chambers (12, 13) arranged opposite one another mirror-symmetricalry in the two end faces of the impeller (5) are connected to one another solely in the region of the center line. In a feed pump (2) designed as a side-channel pump, a blade chamber (12, 13) of an impeller (5) has a contour which fs formed by a radius (R) and In which, as seen from the contour, the origin of the radius ( R) is located behind a center line of the blade chamber (12, 13). A circulation flow thereby passes into the blade chamber (12, 13) with particularly low turbulences. The feed pump (2) has particularly high efficiency as a result.

Full Text

This invention relates to an improved feed pump with a driven impeller.
Description

The invention relates to a feed pump with a driven impeller which rotates in a pump casing and has in its end faces at least one ring of guide blades delimiting blade chambers and in which the blade chambers have an inflow region and an outflow region for the medium to be fed, and with at least one part-annular channel which is arranged in the region of the guide blades in the pump casing and which forms with the blade chambers a feed chamber from an inlet channel to an outlet channel, the contour of the blade chambers being formed by at least one radius with an origin within the feed chamber.
Such feed pumps are often used for feeding fuel in a fuel tank or for feeding washing fluid in a shield washing system of a motor vehicle and are known from practice. The known feed pump has a ring of blade chambers in each of the two end faces of the impeller. The blade chambers are delimited in the radially outer direction by a straight wall arranged perpendicularly to the end faces of the impeller. The contour of the blade chambers which points in the radially inner direction of the impeller is generated by a radius. The origin of the radius is located on the center line arranged perpendicularly to the end faces of the impeller. This origin is at the same time the origin of a second radius forming the part-annular channel.
One disadvantage of the known feed pump is that it generates turbulences in the medium to be fed. These turbulences lead to the feed pump having lowj efficiency. Moreover, in the case of media which are near the boiling point, such as, for example, "hot gasoline fuel, there is the risk that vapor bubbles will be formed within the feed chamber. The vapor bubbles lead to a sharp reduction in the volume flow fed by the feed pump.

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The problem on which the invention is based is to design a feed pump of the type initially mentioned, in such a way that it has as high an efficiency as possible and reliably prevents the formation of vapor bubbles.
This problem is solved, according to the invention,, in that, as seen from the blade chamber contour determined by the radius, the origin of the radius is located in the region opposite a center line of the blade chamber, said center line running perjpendicjjJLar-l-y-to-the-end face of the impeller.
By virtue of this design, the blade chamber has, in its region formed by the radius, a contour which ascends at a very low inclination. A circulation flow in the feed chamber alternates between the impeller and the pump casing via this low-inclination contour. Since the circulation flow undergoes only slight deflection in this region, the risk of turbulences is kept particularly low. The formation of vapor bubbles is also avoided as a result.
According to an advantageous development of the invention, the impeller can be manufactured cost-effectively if the origins of a plurality of radii for blade chamber contours opposite one another are located on a common plane within the impeller, said plane running parallel to the end face of the impeller.
Turbulences often occur in the region in which the circulation flow alternates between the blade chamber and the part-annular channel. According to another advantageous development of the invention, the circulation flow set in turbulence here can be calmed again quickly if, from the plane running parallel to the end face of the impeller as far as the end face, the blade chambers have, in their regions adjacent to the guide blades, boundaries guided perpendicularly to the end face of the impeller.
According to another advantageous development of the invention, the impeller has simply constructed blade chambers and can therefore be manufactured

-4-

particularly cost-effectively if the origins of two radii generating in each case contours opposite one anther are arranged mirror-symmetrically to the center line of the blade chamber. As a result, the center line can be designed as a bisecting line for the contour pointing toward- the center of the impeller and for the contour pointing away from the center of the impeller.
The feed pump according to the invention has particularly high efficiency if the distance of the origins of the radii from the center line is approximately the same amount as their distance from the end face.
As in the known feed pump, blade chambers arranged opposite one another could be connected to one another in a radially outer region of the impeller. However, a contribution to a further increase in the efficiency of the feed pump according to the invention is made if blade chambers arranged opposite one another mirror-symmetrically in the two end faces of the impeller are connected to one another solely in the region of the center line. The circulation flow can thereby flow from one feed chamber over into the other feed chamber with particularly low turbulences. Moreover, the risk of the formation of vapor bubbles is likewise kept particularly low as a result.
The invention permits numerous embodiments. In order to make its basic principle even clearer, one of these is illustrated in the drawing and is described below. In the/drawing: ' O -__/
Figure 1 shows a sectional illustration through a feed pump according to the invention,
Figure 2 shows an enlarged illustration of the feed pump from Figure 1 in the region of feed chambers.
Figur-e 1 shows a longitudinal section through a feed pump 2 which is driven by an electric motor 1 and is

designed as an axial-throughf'low side-channel pump and which may be provided, for example, for feeding fuel out of a fuel tank, not illustrated, of a motor vehicle. The feed pump 2 has a pump casing 3, in which is arranged an impeller 5 fastened fixedly in terms of rotation on a shaft 4 of the electric motor 1. The pump casing 3 has an inlet channel 6 on its face facing away from the electric motor 1 and an outlet channel 7 on the side facing the electric motor 1. The inlet channel 6 opens into a feed chamber 8. A second feed chamber 9 opens into the outlet channel 7. The feed chambers 8, 9 have in each case part-annular channels 10, 11 incorporated in the pump casing 3 and blade chambers 12, 13 arranged in the impeller 5. The blade chambers 12, 13 are delimited in each case by guide blades 14, 15 and in each case have an inflow region 16, 17 for the inflow of the medium to be fed and an outflow region 18, 19. Blade chambers 12, 13 opposite one another are connected to one another between the inflow region 16, 17 and the outflow region 18, 19. When the impeller 5 rotates, circulation flows occur in each case in the feed chambers 8, 9. A part stream is branched off from the circulation flow of the inlet-side feed chamber 8 and flows over into the outlet-side feed chamber 9. The flows are identified by arrows in the drawing.
Figure 2 shows, greatly enlarged, the feed pump 2 from Figure 1 in the region of the feed chambers 8, 9. It can be seen, here, that the blade chambers 12, 13 are in each case designed symmetrically to a center line running perpendicularly to one end face. The blade chambers 12, 13 have, in the inflow regions 16, 17 and in the outflow regions 18, 19, in each case a contour formed by radii R. The radii R have, in this case, an origin located behind the center line, as seen from the respective contour. Moreover, the origins of the radii R are located in a common plane arranged parallel to the end face of the impeller 5. For clarity, the planes of the blade chambers 12, 13 are illustrated by dashes

43 and dots in the drawing. As a result, the circulation flow passes from the part-annular channels 10, 11 into the blade chambers 12, 13 with particularly low turbulences. The plane of the origins of the radii R is at approximately the same distance from the end face of the impeller 5 as the origins of the radii R are from the center line.

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WE CLAIM:
1. An improved feeipump with a driven impeller which rotates in a pump
casing and has in its end faces at least one ring of guide blades delimiting
blade chambers and in which the blade chambers have an Inflow region
and an outflow region for the medium to be fed, and with at least one part-
annular channel which is arranged in the region of the guide blades in the
pump casing and which forms with the blade chambers a feed chamber
from an inlet channel to an outlet channel, the contour of the blade
chambers being formed by at least one radius with an origin within the
feed chamber, characterized In that, as seen from the blade chamber (12,
13) contour determined by the radius ( R), the origin of the radius ( R) is
located In the region opposite a center line of the blade chamber (12, 13),
said center line running perpendicularly to the end face of the impeller (5).
2. The feed pump as claimed In claim 1, wherein the origins of a plurality of
radii ( R) for blade chamber (12, 13) contours opposite one another are
located on a common plane within the impeller (5), said plane
3. The feed pump as claimed in claim 1 or 2, wherein from the plane running
parallel to the end face of the impeller (5) as far as the end face, the blade
chambers (12, 13) have, in their regions adjacent to the guide blades (14,
15), boundaries guided perpendicularly to the end face of the impeller (5).
4. The feed pump as claimed in any one of the preceeding claims wherein
the origins of two radii (R) generating in each case contours opposite one
another are arranged mirror-symmetrically to the center line of the blade
chambers (12,13).
5. The feed pump as claimed in any one of the preceeding claims, wherein
the distance of the origins of the radii (R ) from the center^line is
approximately the same amount as their distance from the end face.

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6. The feed pump as claimed in any one of the proceeding claims, wherein blade chambers (12, 13) arranged opposite one another mirror-symmetricalry in the two end faces of the impeller (5) are connected to one another solely in the region of the center line.
In a feed pump (2) designed as a side-channel pump, a blade chamber (12, 13) of an impeller (5) has a contour which fs formed by a radius (R) and In which, as seen from the contour, the origin of the radius ( R) is located behind a center line of the blade chamber (12, 13). A circulation flow thereby passes into the blade chamber (12, 13) with particularly low turbulences. The feed pump (2) has particularly high efficiency as a result.

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Patent Number

202587

Indian Patent Application Number

IN/PCT/2001/00443/KOL

PG Journal Number

09/2007

Publication Date

02-Mar-2007

Grant Date

02-Mar-2007

Date of Filing

19-Apr-2001

Name of Patentee

MANNESMANN VDO AG

Applicant Address

KRUPPSTRASSE 105, 60338 FRANKFURT, GERMANY

Inventors:

#	Inventor's Name	Inventor's Address
1	STAAB MATTHIAS	AHORNSTRASSE 4, 36211 ALHEIM, GERMANY.
2	WILHELM HANS-DIETER	HATTSTEINER WEG 6, 61267 NEU-ANSPACH, GERMANY
3	BARTH HOLGER	RHONBLICK 21, 36289 FRIEDEWALD, GERMANY.

PCT International Classification Number

F 04D 29/18

PCT International Application Number

PCT/EP00/08334

PCT International Filing date

2000-08-26

PCT Conventions:

#	PCT Application Number	Date of Convention	Priority Country
1	19943261.9	1999-09-10	Germany