FIELD OF THE INVENTION
[0001] The present invention is directed to a regenerative pump, sometimes referred to as
a toric pump, especially designed for economical mass production which is capable
of developing higher pressures and flow rates at higher efficiencies than other pumps
of comparable design and operating speed, by modifications made to the impeller and/or
housing.
BACKGROUND OF THE INVENTION
[0002] In an automotive emission control system, a pump supplies air as required to the
exhaust system between the manifold and the catalytic converter. In conventional regenerative
pumps intended for use in an automotive emission control system, the impeller has
straight radially extending blades at its outer periphery and is driven in rotation
between a pump housing and a cover formed with a pump chamber. The pump chamber is
formed symmetrical with respect to the rotatable impeller, and the surfaces of the
housing and the cover. Further descriptions of toric pumps of this construction can
be obtained from U.S. Patent No. 5,302,081; No. 5,205,707 and No. 5,163,810.
[0003] The features of the preamble of claim 1 are known from US 5,302,081.
[0004] Document DE 876 285 C discloses an impeller that is an integral unit. It consists
of a housing including a closed ring-shaped working area having a circular or elliptical
like cross-section. A blade wheel rotates within a semi-circular blade wheel channel
of the working area transporting fluid in axial direction. A very dramatic taper is
required for this single channel closed vane system.
[0005] AU 128 026 B discloses a blower in which an axially constant width chamber is varied
along the radial direction from an inlet to an outlet.
[0006] EP-A-0 602 558 discloses a centrifugal pump that utilizes centrifugal force to circulate
a fluid from a fluid inlet to a fluid outlet.
[0007] Over time, industry needs have changed as restrictions on emissions have changed.
It is now desirable to provide more air to an automotive emission control system than
was previously required. Currently, it is desirable to provide at least between 32
und 34 m
3/h (19 and 20 cubic feet per minute (cfm)). It is also desirable to meet the minimum
fluid flow requirements while maintaining the same size housing. To meet these new
fluid flow requirements, it has been necessary to double, and in some instances quadruple,
the currently existing fluid flow rates of regenerative single stage pumps. Up to
this point in time, the typical regenerative pump used in automotive emission control
system applications has been capable of achieving a fluid flow rate of only 6,8 m
3/h (4 cubic feet per minute (cfm)) at approximately 111 000 Pa (40 inches (H
2O) head), and therefore, it is desirable in the present invention to provide a greater
fluid flow output at the same or greater pressure for a given size housing configuration.
[0008] The invention provides a regenerative pump according to claim 1.
SUMMARY OF THE INVENTION
[0009] In a regenerative pump the rotor vanes of the peripheral regenerative pump are arcuate
when viewed from the side, with the upper and lower portions curved forward in the
direction of rotation. Preferably, a chamfer, or similar relief is formed on the convex
side of the inner portion of all vanes. Bending the root portion of the vane to face
forward and the addition of the chamfer are aimed at reducing pressure energy losses
in the fluid entry region. Energy losses in the fluid entry region are the dominant
loss in this type of regenerative pump. Prototypes of an impeller have been produced
and tested. The test results have indicated a pressure increase, for the same rotational
speed, of no less than 60% over the whole operating range and no less than 100% over
a substantial portion of the whole operating range. In the tests, flow also increases
over the operating range. Such dramatic increases in pressure and flow were unexpected.
[0010] The present invention also concerns double channel regenerative pumps of the type
embodying a central rotor with vanes extending generally radially, either in a straight
radial fashion, or in an arcuate fashion. Previously, it has been difficult to achieve
a proper matching of the output of such a regenerative pump or compressor to the requirements
of a particular application. Although some matching could be achieved by judicial
choice of shaft rotational speed, pump efficiency can suffer in the process. Typically,
a pump of this type includes a housing means for mounting a drive motor and one of
the side channels, a rotor with generally radially extending vanes at its outer region
on one or more axial sides of the rotor, and a cover sealingly engaged with the housing
and a second side channel. The present invention allows matching of a pump's capacity
to the requirements of a particular application without changing shaft rotational
speed. Previously the channels and the housing and cover have been equal, or symmetrical
in cross-section, and differ only at the channel ends where it is common to place
transfer inlet and delivery passages from the housing channel to ducts in the cover
or housing. In the present invention, the channels of the housing and cover are formed
in a manner which is not symmetrical. The cover, which is freely accessible, can be
replaced by alternative covers having channels of various depths, or the cover can
be spaced axially outwardly from the impeller by insertable spacers of various depths
to change the effective depth of the channel in the cover. Thereby, the specific output
of the pump may be varied to suit different fluid flow requirements by providing the
appropriate asymmetrical depth of channel. Prototypes of asymmetrical side channels
have been constructed and tested. These tests show that a change in capacity of at
least 20% can be achieved by varying the axial depth of the channel without loss in
the overall efficiency of the regenerative pump. The prototype of the present invention
that was tested included a spacer plate inserted between the housing and the cover.
The plate increased one of the side channels by a depth according to the thickness
of the plate. Thus, a deeper channel can be provided without requiring the costly
and time consuming measure of manufacturing a new cover. The magnitude of enhancement
to pump performance was unexpected.
[0011] A regenerative pump for adding energy to a fluid includes an impeller having an axis
of rotation and axially spaced, radially extending first and second surfaces. A radially
split casing encloses the impeller and has a fluid inlet and a fluid outlet separated
by a stripper. The stripper generally has a close clearance to a periphery of the
impeller. The casing has axially spaced, radially extending first and second side
walls facing the first and second surfaces respectively. Axially and radially extending
blade means is formed on an outer radial periphery of the pump for driving fluid from
the inlet toward the outlet as the impeller rotates about the axis of rotation. Means,
formed in at least one side wall of the casing, directs fluid back toward the impeller.
[0012] The blade means preferably includes a plurality of vanes spaced circumferentially
around the outer radial periphery of the impeller. Each vane has a radially inward
base portion extending in a generally trailing direction with respect to rotation
of the impeller and a radially outward tip portion extending in a generally leading
direction with respect to rotation of the impeller.
[0013] Chamfer means is preferably formed on the base portion of each vane for deflecting
fluid from the inlet toward the pocket defined between two adjacent vanes and the
casing. Preferably, the chamfer means is formed on a trailing edge of the base portion
of each vane. The chamfer means may be formed at an angle with respect to a radially
extending plane normal to the axis of rotation of the impeller at a range selected
from between 10° and 45° inclusive. Alternatively, the chamfer means may be formed
as a curved surface having a predetermined radius connecting a generally radially
extending surface of each vane to a generally axially extending surface of the respective
vane along a trailing edge.
[0014] The blade means may include a plurality of vanes spaced circumferentially around
the outer radial periphery of the impeller, where each vane is bent in radial direction
with respect to the axis of rotation of the impeller about an axis generally parallel
with the axis of rotation of the impeller. Alternatively, the blade means may include
at least one set of radially bent vanes with respect to the axis of rotation, where
the set of vanes is defined by at least two circumferentially spaced vanes collaborating
with one another to form a single circular annulus.
[0015] The base portion of each vane preferably forms an entry angle with respect to a radially
extending plane normal to the axis of rotation of the impeller in a range selected
from between 20° and 30° inclusive. The tip portion preferably forms an exit angle
with respect to a radially extending plane normal to the axis of rotation of the impeller
in a range selected from between 20° and 45° inclusive.
[0016] The impeller has a generally radially extending plane or web normal to the axis of
rotation and connected to the blade means. The web extends radially into the blade
means to a position generally midway between the base and the tip of each vane. Preferably,
the right angle surfaces, formed by the web and an annular hub of the impeller supporting
the base of each vane, is filled in to provide an angled, stepped, or preferably radially
curved transition between the axially extending hub portion of the impeller and the
radially extending web between each adjacent set of vanes.
[0017] The fluid directing means preferably includes a fixed shaped surface. The fluid directing
means may include at least one of the first and second side walls having a generally
ring-shaped, side channel portion formed in the casing around the axis of rotation
for directing fluid helically back into contact with the blade means as the impeller
rotates. Preferably, the side channel portion is generally perpendicular to and along
an arc of constant radius centered on the axis of rotation. In the preferred embodiment,
the fluid directing means includes each of the first and second side walls having
a generally ring-shaped side channel portion formed therein around the axis of rotation
of the impeller for directing fluid helically back into contact with the blade means
as the impeller rotates. Preferably, the fluid directing side channel portion of one
of the first and second side walls is enlarged with respect to the other fluid directing
side channel portion. Preferably, the enlarged one of the side channel portions is
enlarged in the axial direction. The fluid directing means preferably is formed asymmetrically
in the first and second side walls of the casing around the axis of rotation of the
impeller.
[0018] According to the invention a means for defining a flow path between the fluid inlet
and the fluid outlet is formed in at least one of the first and second side walls
of the casing. The flow path defining means is tapered so that the cross-sectional
area at the fluid inlet is greater than the cross-sectional area at the fluid outlet.
The flow path defining means may include the side channel portions wherein the side
channel portions preferably taper axially inward toward said impeller at a constant
slope from said fluid inlet to said fluid outlet.
[0019] Regenerative pumps have traditionally been constructed, when there are two channels,
with side channels equal in cross-section. The present invention demonstrates that
unequal channels cause no significant loss in efficiency or other deleterious effects.
The option of using unequal channels facilitates convenient capacity modifications
so that a single pump design may have its pumping characteristics modified to satisfactorily
meet more than one specific application requirement. The asymmetric channels according
to the present invention may be used with a standard configuration impeller for a
regenerative pump, or may be used in combination with the arcuate vane impeller configuration
according to the present invention for further performance enhancement. The rear swept
lower, or entry, or base portion of the vane with forward swept tip approximately
midway up from the root of the vane, as previously described with respect to the present
invention, can advantageously be used in combination with the asymmetric channels.
The arcuate vane configuration, as previously described, can also include the modification
of chamfer means for easing entry of fluid, particularly where the entry angle is
large relative to the impeller axis. As the flow rate is reduced and the pressure
rises, the ease of entry for fluid into the impeller is a feature that is associated
with results that reveal improved maximum pressure for a given shaft speed and higher
efficiency. As previously described, the chamfer means may also take an alternative
curvilinear profile.
[0020] Other objects, advantages and applications of the present invention will become apparent
to those skilled in the art when the following description of the best mode contemplated
for practicing the invention is read in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
[0021] The description herein makes reference to the accompanying drawings wherein like
reference numerals refer to like parts throughout the several views, and wherein:
Figure 1 is a front end view, with certain parts broken away, of a conventional toric
pump;
Figure 2 is a detailed cross sectional view of the pump of Figure 1 taken on line
2-2 of Figure 1;
Figure 3 is a front end view of the impeller housing of the pump of Figure 1;
Figure 4 is a detailed cross sectional view of the impeller housing taken on line
4-4 of Figure 3;
Figure 5 is a detailed cross sectional view of the impeller housing taken on line
5-5 of Figure 3;
Figure 6 is a front end view of the impeller cover of the pump of Figure 1;
Figure 7 is a rear end view of the impeller cover;
Figure 8 is a detailed cross sectional view taken on the line 8-8 of Figure 6;
Figure 9 is a detailed cross sectional view of the impeller cover taken on line 9-9
of Figure 6;
Figure 10 is a detailed cross sectional view of the impeller cover taken on line 10-10
of Figure 6;
Figure 11 is a perspective view of an impeller according to the present invention;
Figure 12 is a detailed view of a portion of an impeller according to the present
invention;
Figure 13 is a cross-sectional detailed view of the impeller taken on line 13-13 of
Figure 12;
Figure 14 is a cross-sectional detailed view of the impeller taken on line 14-14 of
Figure 13;
Figure 15 is a cross-sectional detailed view of an asymmetrical pump chamber formed
with a spacer according to the present invention;
Figure 16 is a cross-sectional detailed view of an asymmetrical pump chamber according
to the present invention formed integrally in the impeller cover;
Figure 17 is a graph of overall efficiency versus flow rate in cubic feet per minute
at 40 inches of water back pressure showing various curves for different size spacers;
Figure 18 is a graph of flow rate in cubic feet per minute versus back pressure in
inches of water showing flow lines comparing pump chambers with and without spacers,
and corresponding electrical current lines of the pump with and without a spacer;
Figure 19 is a graph of overall efficiency versus flow in standard cubic feet per
minute showing curves comparing pump chambers with and without a spacer;
Figure 20 is a rear end view of the impeller cover with the side wall channels tapered;
Figure 21 is a detailed cross-sectional view of the impeller cover taken on line 21-21
of Figure 20 showing the tapered side wall channels of the impeller cover;
Figure 22 is a graph of the airflow in kilograms per hour versus discharge pressure
in millibars showing curves comparing the taper applied to the impeller cover, impeller
housing and neither the impeller cover nor impeller housing; and
Figure 23 is a graph of overall pump efficiency versus discharge pressure in millibars
showing curves comparing the taper applied to the impeller cover, impeller housing
and neither the impeller cover nor impeller housing.
DESCRIPTION OF THE PREFERRED EMBODIMENT
[0022] The interrelationship of the various parts of a conventional toric pump or regenerative
pump are best seen in the assembly views of Figures 1 and 2, while details of the
individual parts are shown in Figures 3-10.
[0023] Referring first to Figures 1 and 2, a pump includes an impeller housing designated
generally 20, an impeller cover designated generally 22 mounted upon the front of
housing 20, and a filter cover designated generally 24 mounted on the front of impeller
cover 22. A pump impeller 26 is mounted in operative relationship with a pump chamber
designated generally 28 cooperatively defined by the assembled impeller housing 20
and impeller cover 22, the impeller 26 being fixedly coupled to the drive shaft 30
(Figure 2) of an electric motor 32 mounted or integrated with the rear of the impeller
housing. An inlet port or fitting 34 opens through filter cover 24 into a filter chamber
36 defined by the assembled impeller cover and filter cover. A passage or opening
in impeller cover 22 places the filter chamber 36 in communication with pump chamber
20, a sponge-like block of filter media 40 being fitted in filter chamber 36 between
inlet port 34 and passage 38 to filter air passing into the pump through inlet port
34 before the air passes through passage 38 into pump chamber 28.
[0024] For purposes of the present application, the conventional pump impeller 26 and the
configuration of pump chamber 28 may be assumed to be identical to the impeller and
pump chamber disclosed in U.S. Patent No. 5,302,081, No. 5,205,707 and/or No. 5,163,810,
and further details of the impeller and pump operation of a conventional pump may
be had from those patents, whose disclosure is incorporated herein by reference. The
invention of the present application is especially concerned with modifications to
the configuration and interrelationship of the impeller and the side channel in the
casing, details of which are set forth in detail below with respect to Figures 11-19.
[0025] The construction of impeller housing 20 is best seen in Figures 3, 4 and 5. Housing
20 is initially formed as a metal casting with a portion of pump chamber 28 and an
impeller receiving recess formed in the casting. Impeller housing 20, if die cast
from a suitable material such as SAE 413 aluminum, will require, the machined finishing
of only two surfaces and the drilling and tapping of four holes for the reception
of mounting bolts.
[0026] Referring to Figure 4, two surfaces which require precise machining are what will
be referred to as the front end surface 50 of housing 20 and a parallel surface 52
which defines the bottom of an impeller receiving recess in impeller housing 20. Surfaces
50 and 52 are finished accurately flat and parallel with each other and are spaced
axially from each other by a distance which only slightly exceeds the axial thickness
of the impeller 26 used. The amount by which the spacing between surfaces 50 and 52
exceeds the impeller thickness establishes the clearance between surface 52 and one
side 26A (Figure 2) of the impeller and between the opposite side 26B of the impeller
and an opposed surface 56 of the impeller cover when the impeller, impeller housing
and impeller cover are assembled as in Figure 2. These clearances must be sufficient
to avoid rubbing between the impeller sides and housing elements during rotation of
the impeller, while at the same time being small enough to minimize any flow of air
between the last mentioned opposed surfaces.
[0027] A central bore 58 through the impeller housing serves to pilot the front motor boss
32a of motor 32 which carries a shaft bearing, not shown, which locates the axis of
motor shaft relative to the impeller housing. The location and diameter of bore 58
and the radius of stripper surface 74a are the other dimensions (other than surfaces
50 and 52) of housing 20 which must be machined to tight tolerances. The radial outer
surface 28a of the pump chamber portion of the recess may be established with sufficient
precision by the die casting process. Alternatively, bore 58 may receive a shaft bearing
directly, rather than a boss on the motor housing in which the shaft bearing is located.
Bore 58 establishes the location of the motor shaft axis relative to the housing,
stripper surface 74a is machined at a precise distance from and concentric to this
axis to establish radial clearance between impeller and housing across the stripper.
The diameter of bore 58 is such as to receive the motor boss (or shaft bearing) with
a transition or locational interference fit. The motor housing is fixedly attached
to the rear side of the impeller housing as by bolts 60 (Fig. 2) which pass through
bores 62 at the bottom of a central recess 64. Mounting lugs 66 may be integrally
formed on housing 20 to enable the pump to be mounted on a suitable mounting bracket.
Tapped bores 68 (Figs. 3 and 5) are formed in housing 20 to accommodate mounting bolts
employed to mount impeller cover 22 on impeller housing 20.
[0028] As is conventional in toric pumps, the punp chamber 28 extends circumferentially
about the axis of the impeller from an inlet end 70 (Fig. 3) to an outlet end 72.
The recessed inlet and outlet ends 70, 72 are separated from each other by a stripper
portion 74 of surface 52 which, when the impeller is in place, cooperates with the
adjacent side surface of the impeller to form a flow restriction between the two surfaces
functionally equivalent to a seal between the inlet and outlet. This prevents high
pressure air at outlet 72 from flowing across the stripper portion 74 to the low pressure
region at inlet end 70.
[0029] The structure of impeller cover 22 is best seen in Figs. 6. Impeller cover 22 is
a molded one-piece part of a suitable thermoplastic material. The flat surface 56
referred to above is formed on the rear side of impeller cover 22 to be seated in
face to face engagement with the machined surface 50 of impeller housing 20. An annular
recess 28c in the flat rear surface 56 forms a pump chamber portion in the rear surface
of impeller housing 20 which is coextensive with and matched to pump chamber 28 of
housing 20. As best seen in Figs. 9 and 10, the flat rear surface 56 of the impeller
cover is recessed slightly to form an axially projecting peripheral flange 76 which
fits over the front end of impeller housing 20 to locate the housing and cover relative
to each other upon assembly. As best seen in Figure 2, bolts 78 passing through bores
80 in impeller cover 22 are received in the tapped bore 68 in impeller housing 20
to fixedly secure housing 20 and cover 22 into assembled relationship with each other.
As best seen in Figures 7 and 9, the outlet end 72a of the pump chamber portion 28C
communicates with a passage 82 extending through a nipple 84 on impeller cover 22
to define an outlet port for the pump chamber 28, 28A, 28C of the pump.
[0030] At the front side of impeller cover 22, a cup shaped recess 86, best seen in Figs.
9 and 10, is formed. A flow passage 88 leads rearwardly from the bottom of recess
86 to open through the flat rear surface 56 of the impeller cover. Passage 88 opens
into the inlet end 70a of the pump chamber portion 28C in impeller cover 22 and constitutes
the inlet to the combined pump chamber 28, 28A, 28C of the pump defined by the assembled
housing 20 and cover 22. A central post 90 is integrally formed on cover 22 within
the recess 86 and projects forwardly to a flat front end 92 co-planar with the front
end edge 94 of cover 22. A bore 96 for receiving a self tapping mounting screw extends
rearwardly into post 90, with a square recess 98 at the front end of bore 96. A radially
extending web 100 (Figs. 6 and 8) projects radially from central post 100 entirely
across recess 86 to be integrally joined to the side wall 102 of the recess. The forward
edge 104 (Fig. 8) of web 100 is co-planar with the front edge 94 of the impeller cover.
Other stiffening webs such as 106 may be formed at appropriate locations in recess
86 but, as best seen in Figure 8, these other webs 106 have edges which are spaced
well rearwardly of front edge 94. Recess 86 constitutes a portion of a filter chamber
adapted to receive filter 40 (see Fig. 2). Cover 24 is of a generally cup shaped configuration,
the recess 110 of the cup opening rearwardly. The recess 110 in filter cover 24 is
conformed to mate with and form an extension of the filter receiving recess 86 of
impeller cover 22, as seen in Figure 2. Like impeller cover 22, a central post 112
is formed in the filter receiving recess 110. A bore through post 112 receives a mounting
bolt 118 threaded into bore 96 in the impeller cover to hold the filter cover seated
on the impeller cover 22. The filter element designated generally 40 is formed from
a block of a sponge-like material, such as a reticulated polyester foam. The axial
thickness of filter element 40 is chosen to slightly exceed the axial dimension of
the filter chamber defined by the mated filter receiving recesses 86, 110 of the impeller
cover 22 and filter cover 24 when the two covers are assembled. Filter element 40
is formed with a central bore 130 adapted to receive central posts 90 and 112, as
seen in Figure 2.
[0031] The pump impeller 26 can be modified from the conventional straight radially extending
vanes to a bent shape of vane as illustrated in Figure 11 or a curvilinear form as
illustrated in Figures 12-14. In any case, the pump impeller 26 includes axially and
radially extending blade means 140 formed on an outer radial periphery 142 of the
impeller 26 for driving fluid from the inlet end 70 toward the outlet end 72 as the
impeller 26 rotates about the axis of rotation. The blade means 140 includes a plurality
of vanes 144 spaced circumferentially around the outer radial periphery 142 of the
impeller 26. Each vane 144 has a radially inward base portion 146 connected to an
axially extending cylindrical sidewall or hub 148 of the impeller 26. The base portion
146 extends in a generally trailing direction with respect to rotation of the impeller
26. As illustrated in Figure 11, the impeller would rotate in a counter-clockwise
direction. A radially outward tip portion 150 of each vane 144 extends in a generally
leading direction with respect to rotation of the impeller 26. The base portion 146
forms an entry angle φ
1 with respect to a radially extending plane containing the axis of rotation of the
impeller 26 in a range selected from between 20° and 30° inclusive, with a preferable
range selected from between 26° and 30° inclusive, and a most preferred angle of 26°.
The tip portion 150 forms an exit angle φ
2 with respect to a radially extending plane containing the axis of rotation of the
impeller 26 in a range selected from between 20° and 45° inclusive, with a preferable
range selected from between 20° and 30° inclusive, and a most preferred angle of 20°.
The blade means 140 preferably includes a plurality of vanes spaced circumferentially
around the outer radial periphery 142 of the impeller 26 with each vane 144 bent or
curved in radial direction with respect to the axis of rotation of the impeller 26
about an axis generally parallel with the axis of rotation. The blade means 140 may
include at least one set of radially bent vanes 144 with respect to the axis of rotation,
where the set of vanes 144 is defined by at least two circumferentially spaced vanes
144 cooperating with one another to form a single circular annulus. As best seen in
Figures 11-14, the impeller 26 preferably includes a generally radially extending
planar web 152 disposed normal to the axis of rotation and connected to the blade
means 140. The web 152 extends at least radially outwardly from the axially extending,
cylindrical sidewall or hub 148 of the impeller 26. Preferably, the transition surface
154 formed between the web 152 and the annular hub 148 of the impeller 26 is filled
in to provide an angled, stepped, or most preferably a radially curved transition
surface 154 between the axially extending hub 148 of the impeller 26 and the radially
extending web 152 between each adjacent set of vanes 144. The web 152 preferably extends
radially into the blade means 140 to a position generally midway between the base
portion 146 and the tip portion 150 of each vane 144. If the web 152 is extended radially
outwardly to the outer radial periphery 142 of the impeller 26 (not shown), each vane
144 can be axially separated or isolated from one another if desired for a particular
application. It has been found that optimum performance characteristics are achieved
if the web 152 is maintained at a position located between the base portion 146 and
a tip portion 150 of each vane, and preferably at a position generally midway between
the base portion 146 and the tip portion 150. It should be recognized that the base
portion 146 may be of the same, or a differing length, with respect to the tip portion
150 of each vane 144. Preferably, the base portion 146 forms a percentage of the overall
radial length of each vane 144 in a range selected from between 30% and 70% inclusive,
with a preferable range of 40% to 60% inclusive and a most preferable value of approximately
50%. Preferably, each vane 144 is identical with the other corresponding vanes 144
formed on the outer radial periphery 142 of the impeller 26.
[0032] Chamfer means 158 is preferably formed on the base portion 146 of each vane 144 for
deflecting fluid from the inlet toward a pocket 160 defined between two adjacent vanes
144 and the casing sidewalls defining the pump chamber 28. The chamfer means 158 is
preferably formed on a trailing edge of the base portion 146. The chamfer means 158
can be formed at an angle φ
3 with respect to a radially extending plane normal to the axis of rotation of the
impeller at a range selected from between 10° and 45° inclusive, with a preferred
value of approximately 45°. The chamfer means 158 could also be formed as a curved
or radial surface (not shown) having a predetermined radius connecting a generally
radially extending surface 162 of the vane 144 to a generally axially extending surface
164 of the vane 144 along a trailing edge.
[0033] Fluid directing means 166 is preferably formed in at least one sidewall of the casing
defining the pump chamber 28 for directing fluid back toward the impeller 26. The
fluid directing means 166 preferably takes the form of a fixed surface 168 defining
a portion of the pump chamber 28. The fluid directing means 166 can include at least
one of the first and second sidewalls 52, 56 having a generally ring-shaped, side
channel portion 28A, 28C formed in the casing around the axis of rotation for directing
fluid helically back into contact with the blade means 140 as the impeller 26 rotates.
The side channel portion 28A or 28C is generally perpendicular to the axis of rotation
and extends along an arc of constant radius centered on the axis of rotation. The
fluid directing means 166 may also include each of the first and second sidewalls
52, 56 having generally ring-shaped side channel portion 28A, 28C respectively formed
therein around the axis of rotation for directing fluid helically back into contact
with the blade means 140 as the impeller 26 rotates. In the preferred configuration,
as best seen in Figures 15 and 16, the fluid directing side channel portion 28C of
one of the first and second sidewalls 52, 56 is enlarged with respect to the other
fluid directing side channel portion 28A. Preferably, the enlarged fluid directing
side channel portion 28C is enlarged in the axial direction. The axial enlargement
can be accomplished by placing a spacer 170 between the impeller housing 20 and the
impeller cover 22, as best seen in Figure 15. The spacer 170 is formed to extend the
wall defining the side channel portion 28C in axial direction with sidewall extension
172. The sidewall extension 172 is formed to closely follow the contour of the side
channel portion 28C of the pump chamber 28 formed in the impeller cover 22. Of course,
it should be recognized that the combination of the spacer 170 and impeller cover
22 can be replaced with a unitary impeller cover 22 formed with the appropriate enlarged
side channel portion 28C, as is illustrated in Figure 16. The fluid directing means
166 preferably is formed asymmetrically in the first and second side walls 52, 56
of the casing.
[0034] Figure 17 is a graph of an extended range electrical air pump according to the present
invention showing overall pump efficiency versus flow rate in 0,028 m
3/min (standard cubic feet per minute) at 111000 Pa (40 inches H
2O) back pressure with an 85 mm diameter impeller, no filter and powered by 13.5 volt
power source. The various curves show operating characteristics for different sizes
of spacers placed between the impeller housing 20 and the impeller cover 22. The first
curve 174 illustrates the device with no spacer interposed between the impeller housing
20 and the impeller cover 22. The second curve 176 illustrates the performance characteristics
of the modified pump with a spacer having a thickness of 1.0 mm. The third curve 178
illustrates the performance characteristics of the pump with a 1.5 mm spacer interposed
between the housing 20 and the cover 22 disclosed as illustrated in Figure 15. The
fourth curve 180 illustrates the performance characteristics of the pump with a 2.5
mm spacer between the impeller housing 20 and the impeller cover 22. Each of these
curves were obtained through the use of a prototype configuration including the arcuate
vanes 144 as described in greater detail above with an entry angle of 26°, an exit
angle of 30° and a 45° chamfer on the trailing edge of the base portion of the vane.
The test results are summarized in the table below.
| SCFM FLOW AT 40 INCH H2O |
BEST CHOICE SPACER |
OVERALL EFFICIENCY |
RPM |
AMPS |
| 10 |
1.0 mm |
20.75 |
13,460 |
16.8 |
| 16 |
1.0 mm |
21.5 |
16,430 |
28.5 |
| 20 |
1.5 mm |
20.3 |
18,300 |
33.5 |
[0035] Figure 18 is a graph of flow in 0,028m
3/min (cubic feet per minute) versus back pressure in 250 Pa (inches of water) and
further showing the current in amps versus back pressure in 250 Pa (inches of water).
The first line 182 shows flow characteristics of a pump according to the present invention
without a spacer, while the second line 184 shows the fluid flow characteristics of
the pump with a spacer of 2.5 mm in size. The third line 186 depicts the current used
by the pump when operated without a space corresponding to the fluid flow of the first
line 182 while the fourth line 188 corresponds to the current flow through the pump
with a spacer corresponding to the fluid flow characteristics of the second line 184.
The data obtained for a back pressure of 104 000 Pa (10 inches of water) was at 15,337
revolutions per minute (RPM), while the data points for approximately 107 600 Pa (25
inches) back pressure were at 15,075 revolutions per minute (RPM). The data points
corresponding to 111 000 Pa (40 inches) of back pressure and 116 300 Pa (60 inches)
of back pressure were obtained at 14,860 revolutions per minute (RPM) and 14,319 revolutions
per minute (RPM) respectively. Each of these curves were obtained through the use
of a prototype configuration including the arcuate vanes 144 as described in greater
detail above with an entry angle of 26°, an exit angle of 30° and a 45° chamfer on
the trailing edge of the base portion of the vane, with an 85 mm diameter impeller,
no filter and powered by 13.5 volt power source.
[0036] Figure 19 is a graph depicting overall efficiency in percent versus flow in 0,028
m
3/min (standard cubic feet per minute) The first or lower curve 190 illustrates the
pump characteristics without a spacer, while the upper or second curve 192 illustrates
the pump characteristics with a spacer of a size of 2.5 mm. The plotted data points
along each curve starting from the right or highest flow rate proceeding toward the
lower flow rate correspond to 104 000 Pa (10 inches), 107 600 Pa (25 inches) and 111
000 Pa (40 inches (H
2O)) back pressure respectively along each of the two curves, 190 and 192. Each of
these curves were obtained through the use of a prototype configuration including
the arcuate vanes 144 as described in greater detail above with an entry angle of
26°, an exit angle of 30° and a 45° chamfer on the trailing edge of the base portion
of the vane, with an 85 mm diameter impeller, no filter and powered by 13.5 volt power
source.
[0037] According to the present invention, the airflow of the pump is increased while not
detrimentally effecting the overall efficiency of the pump by tapering the cross-sectional
area of the pump chamber 28 from a maximum area at the inlet end 70A to a lesser area
at the outlet end 72A, as seen in Figures 20-21. The impeller cover 22 shown in Figure
20 is similar to that previously described. The flat surface 56 formed on the rear
side of impeller cover 22 is seated in face to face engagement with the machined surface
50 of the impeller housing 20. The annular recess or side channel portion 28C in the
flat rear surface 56 of the impeller cover 22 forms a portion of the pump chamber
28 which is coextensive with and matched to the portion of the pump chamber 28 in
the impeller housing 20. The impeller cover 22 provides the peripheral flange 76 for
fitting over the front end of the impeller housing 20 as well as providing bores 80
in impeller cover 22 for receiving bolts to connect the impeller cover 22 to the impeller
housing 20. The impeller cover 22 also provides a fluid inlet 200 having the inlet
end 70A opening into the side channel portion 28C which in turn communicates with
the outlet end 72A opening into a fluid outlet 202 of the impeller cover 22.
[0038] A flow path defining means is preferably formed in at least one side wall 52, 56
of the casing defining the pump chamber 28 for defining a flow path 204 between the
fluid inlet 200 and the fluid outlet 202. As previously described, the flow path defining
means may include at least one of the first and second side walls 52, 56, respectively,
having a generally ring-shaped, side channel portion 28C formed in the casing around
the axis of rotation for directing fluid back in contact with the impeller 26 as the
impeller 26 rotates. The side channel portion 28C is generally perpendicular to the
axis of rotation and extends along an arc of constant radius centered on the axis
of rotation.
[0039] The flow path defining means provides a cross-sectional area of said pump chamber
28 wherein the cross-sectional area of the pump chamber 28 at the fluid inlet 200
is greater than the cross-sectional area of the pump chamber 28 at the fluid outlet
202. The reduction in the cross-sectional area of the pump chamber 28 is provided
by tapering the side channel portions 28C of the side walls 52, 56 which define the
flow path 204 between the fluid inlet 200 and the fluid outlet 202. Preferably, the
side channel portions 28C are tapered axially inward toward the impeller 26 while
maintaining a constant radial width or radial spacing of the side channel portions
28C. Preferably, the taper occurs on a constant slope, as shown in Figure 21. In addition,
the reduction in the cross-sectional area provided by the taper may be reduced ten
to fifty percent between the cross-sectional area at the fluid inlet 200 and the cross-sectional
area at the fluid outlet 202. Preferably, the taper may reduce the cross-sectional
area of the flow path 204 by twenty-five percent when extended from the fluid inlet
200 to the fluid outlet 202. It should be noted that the flow path defining means
need not be symmetrical between the first and second side walls 52, 56 but rather
may be asymmetrical such that the previously described spacers 170 or the larger incorporated
side channel portions 28C may be utilized with this embodiment.
[0040] Figure 22 is a graph of an electrical air pump according to the present invention
showing air flow in kilograms per hour of the pump versus discharge pressure in millibars
wherein the data compiled was generated from a prototype pump having an 85 millimeter
diameter impeller, no filter and a 13.5 volt power source. The various curves show
operating characteristics for tapers applied to the impeller housing 20, the impeller
cover 22 and to neither the impeller housing 20 nor the impeller cover 22. The first
curve 206 illustrates the device with no taper applied to either the impeller housing
20 or the impeller cover 22. The impeller housing 20 has a constant depth of 6.0 millimeters,
and the impeller cover 22 has a constant depth of 6.9 millimeters throughout the side
channel portion 28C. The second curve 208 illustrates the performance characteristics
of the modified pump with a taper applied to the impeller housing 20 and no taper
applied to the impeller cover 22. The taper applied to the impeller housing 20 extends
from a depth of 8.4 millimeters at the inlet end 70A to a depth of 6.0 millimeters
at the outlet end 72A. The depth of the side channel portion 28C is maintained at
a constant depth of 6.9 millimeters in the impeller cover 22. The third curve 210
illustrates the performance characteristics of the pump with the impeller cover 22
tapered from 8.4 millimeters at the inlet end 70A to a depth of 6.0 millimeters at
the outlet end 72A. The impeller housing 20 has its side channel portion 28C maintained
at a constant depth of 7.6 millimeters.
[0041] Figure 23 is a graph depicting overall efficiency in percent versus discharge pressure
in millibars wherein the data was compiled from a prototype pump having an 85 millimeter
diameter impeller, no filter and a 13.5 volt power source. The various curves again
illustrate the operating characteristics for the pump wherein the taper is applied
to the impeller housing 20, the impeller cover 22 and neither the impeller housing
20 nor the impeller cover 22. The first curve 212 illustrates the device with neither
the side channel portion 28C of the impeller housing 20 nor the side channel portion
28C of the impeller cover 22 tapered. The side channel portion 28C of the impeller
housing 20 is maintained at a constant depth of 6.0 millimeters, and the side channel
portion 28C of the impeller cover 22 is maintained at a constant depth of 6.9 millimeters.
The second curve 214 illustrates the performance characteristics of the modified pump
wherein the depth of the side channel portion 28C of the impeller housing 20 is 8.4.millimeters
at the inlet end 70A and 6.0 millimeters at the outlet end 72A. The side channel portion
28C of the impeller cover 22 is maintained at a constant depth of 6.9 millimeters.
The third curve 216 illustrates the performance characteristics of the pump with a
taper applied to the side channel portion 28C of the impeller cover 22 wherein the
inlet end 70A of the impeller cover 22 has a depth of 8.4 millimeters, and the outlet
end 72A has a depth of 6.0 millimeters. The depth of the side channel portion 28C
of the impeller housing 20 provides a constant depth of 7.6 millimeters.
1. Regenerativpumpe, um einem Fluid Energie hinzuzufügen, die folgendes umfaßt:
ein Gehäuse (20, 22) mit einem Fluideinlaß (70) und einem einzelnen Fluidauslaß (72),
die durch einen Abscheider (74) getrennt sind, wobei das Gehäuse (20, 22) ein Laufradgehäuse
(20) und eine Laufradabdeckung (22) beinhaltet und eine erste (56) und eine zweite
(52) axial beabstandete, sich radial erstreckende Seitenwand besitzt;
ein Laufrad (26) mit einer Reihe von Laufradschaufeln (140), die vom Gehäuse (20,
22) umgeben sind, wobei das Laufrad (26) eine Drehachse sowie eine erste (26A) und
eine zweite (26B) axial beabstandete, sich radial erstreckende Oberfläche besitzt,
die der ersten (56) bzw. der zweiten (52) Seitenwand des Gehäuses (20, 22) zugewandt
sind; und
ein Paar Strömungskammern (28A, 28C), wobei eine Strömungskammer (28A, 28C) jeweils
in der Laufradabdeckung (22) und dem Laufradgehäuse (20) ausgebildet und axial auf
jeder Seite des Laufrads (26) angeordnet ist, um einen Strömungsweg (166) zwischen
dem Fluideinlaß (70) und dem einzelnen Fluidauslaß (72) zu definieren, wobei das Gehäuse
(20, 22) eine Umfangsfläche definiert, die das Laufrad (26) eng umgibt, jedoch ausreichenden
Zwischenraum zuläßt, so daß das Fluid radial aus dem Laufrad (26) austreten und sich
dann vorwärts oder rückwärts in die Strömungskammern (28A, 28C) hineindrehen kann,
dadurch gekennzeichnet, daß der Strömungsweg (166), der mindestens eine der Kammern (28A, 28C) definiert, im
wesentlichen entlang seiner gesamten Länge zwischen dem Fluideinlaß (70) und dem Fluidauslaß
(72) in Axialrichtung konisch so ausgeführt ist, daß eine erste Querschnittsfläche
(70A) am Fluideinlaß (70) größer als eine zweite Querschnittsfläche (72A) am einzelnen
Fluidauslaß (72) ist.
2. Regenerativpumpe nach Anspruch 1, die weiterhin folgendes umfaßt:
das strömungswegdefinierende Mittel, das axial nach innen zum Laufrad (26) hin in
einer konstanten Neigung vom Fluideinlaß (70) zum Fluidauslaß (72) hin konisch ausgeführt
ist.
3. Regenerativpumpe nach Anspruch 1, die weiterhin folgendes umfaßt:
das strömungswegdefinierende Mittel, das in der ersten (50) und der zweiten (52) Seitenwand
des Gehäuses (20) um die Drehachse herum asymmetrisch ausgebildet ist, um Fluid, während
sich das Laufrad (26) dreht, zurück zum Laufrad (26) zu leiten.
4. Regenerativpumpe nach Anspruch 1, bei der das strömungswegdefinierende Mittel (166)
weiterhin folgendes umfaßt:
mindestens die erste (50) oder die zweite (52) Seitenwand, die einen allgemein ringförmigen
Seitenkanalabschnitt (28A oder 28C) aufweist, der im Gehäuse um die Drehachse herum
ausgebildet ist, um Fluid, während sich das Laufrad (26) dreht, hin zum Laufrad (26)
zu leiten.
5. Regenerativpumpe nach Anspruch 4, die weiterhin folgendes umfaßt:
den Seitenkanalabschnitt (28A oder 28B), der allgemein senkrecht zu und entlang einem
Bogen mit konstantem Radius, auf der Drehachse zentriert, angeordnet ist.
6. Regenerativpumpe nach Anspruch 1, die weiterhin folgendes umfaßt:
die zweite Querschnittsfläche (72A) am Fluidauslaß (72), die 10% bis 50% kleiner als
die erste Querschnittsfläche (70A) am Fluideinlaß (70) ist.