AU2008200755A1 - Parabolic radial flow impeller - Google Patents
Parabolic radial flow impeller Download PDFInfo
- Publication number
- AU2008200755A1 AU2008200755A1 AU2008200755A AU2008200755A AU2008200755A1 AU 2008200755 A1 AU2008200755 A1 AU 2008200755A1 AU 2008200755 A AU2008200755 A AU 2008200755A AU 2008200755 A AU2008200755 A AU 2008200755A AU 2008200755 A1 AU2008200755 A1 AU 2008200755A1
- Authority
- AU
- Australia
- Prior art keywords
- center line
- segment
- blade
- disc
- parabola
- 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
- 238000000034 method Methods 0.000 claims description 12
- 239000000463 material Substances 0.000 description 5
- 238000010276 construction Methods 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000005587 bubbling Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 235000014366 other mixer Nutrition 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F27/00—Mixers with rotary stirring devices in fixed receptacles; Kneaders
- B01F27/05—Stirrers
- B01F27/11—Stirrers characterised by the configuration of the stirrers
- B01F27/115—Stirrers characterised by the configuration of the stirrers comprising discs or disc-like elements essentially perpendicular to the stirrer shaft axis
- B01F27/1152—Stirrers characterised by the configuration of the stirrers comprising discs or disc-like elements essentially perpendicular to the stirrer shaft axis with separate elements other than discs fixed on the discs, e.g. vanes fixed on the discs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F23/00—Mixing according to the phases to be mixed, e.g. dispersing or emulsifying
- B01F23/20—Mixing gases with liquids
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F27/00—Mixers with rotary stirring devices in fixed receptacles; Kneaders
- B01F27/05—Stirrers
- B01F27/11—Stirrers characterised by the configuration of the stirrers
- B01F27/112—Stirrers characterised by the configuration of the stirrers with arms, paddles, vanes or blades
- B01F27/1123—Stirrers characterised by the configuration of the stirrers with arms, paddles, vanes or blades sickle-shaped, i.e. curved in at least one direction
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F27/00—Mixers with rotary stirring devices in fixed receptacles; Kneaders
- B01F27/05—Stirrers
- B01F27/11—Stirrers characterised by the configuration of the stirrers
- B01F27/115—Stirrers characterised by the configuration of the stirrers comprising discs or disc-like elements essentially perpendicular to the stirrer shaft axis
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/281—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/30—Vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/38—Blades
- F04D29/384—Blades characterised by form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Mixers Of The Rotary Stirring Type (AREA)
- Optical Elements Other Than Lenses (AREA)
Description
AUSTRALIA
Patents Act COMPLETE SPECIFICATION
(ORIGINAL)
Class Int. Class Application Number: Lodged: Complete Specification Lodged: Accepted: Published: Priority Related Art: Name of Applicant: SPX Corporation Actual Inventor(s): Bernd Gigas, Kevin Logsdon Address for Service and Correspondence: PHILLIPS ORMONDE FITZPATRICK Patent and Trade Mark Attorneys 367 Collins Street Melbourne 3000 AUSTRALIA Invention Title: PARABOLIC RADIAL FLOW IMPELLER Our Ref: 822075 POF Code: 458455/172291 The following statement is a full description of this invention, including the best method of performing it known to applicant(s): -1- 00 PARABOLIC RADIAL FLOW IMPELLER This application claims priority from US Application No. 11/707,089 filed on 16 February 2007, the contents of which are to be taken as incorporated herein by this reference.
FIELD OF '[HE INVENTION [0001] The present invention pertains generally to thc field of mixers and mixing devices and methods. In particular, thc invention relates to radial flow impellers used in such mixing systems and methods.
00 BACKGROUND OF THE INVENTION [0002] Mixing devices and mixing methods are in wide use in industry. For example, in some mixing systems, a vessel is provided which has a rotating shaft extending therein that is driven by a drive system typically external to the vessel. The vessel forms a containment chamber for material that is to be mixed, agitated or otherwise to have energy imparted into it.
[00031 Impellers or impeller assemblies are mounted to rotate with the rotating driven shaft. The impellers typically extend radially outwardly from the shaft for some distance towards the outside walls of the vessel. The impellers in some cases may be paddle type elements or blade elements that may extend directly outwardly from a hub on the shaft, or may extend outwardly from a disc mounted to the shaft or may be a single disc having features disposed around the circumference of the disc.
[00041 In somne mixers, the material to be mixed or otherwise treated is simply loaded into the vessel and then the impellers are activated. In some other mixers, it is known to aerate the material to be mixed by adding bubbles to the mixture via a gas sparger disposed s omewhere in the vessel located near rear the bottom of the vessel or at least below a set of'
I
00 the impellers. In some of these mixers, the gas sparger is generally central so that the bubbles rise up and interact with the moving impellers.
[0005] Two general types of impellers are known for many mixer systems. One type Sof impeller is a so-called axial flow impeller. These axial flow impellers, which often take the shape of simply angled plates, or in other cases take the shape of a propeller, or winged C shaped blade, move the material in a generally axial direction either upwards or downwards 00 Sin the vessel parallel to the direction of the shaft elongation.
[0006] Another type of impeller is a so-called radial flow impeller. Radial flow impellers often take the shape of a flat plate or some other geometric shape, and typically push the material outwardly away from the impeller region using centrifugal force, thus creating a radial flow vector, generally outward, in the region outside of the impeller location.
[0007] One type of radial flow impeller utilizes a central disc having a number of circumferentially spaced blades or paddle portions extending out from the disc so that they partially overlap the disc and partially extend outward from the disc. When looked at from a side cross section, one commonly used type of blade has a generally parabolic cross section with two leading edges spanning back towards a single trailing vortex. In the past, these blades have generally been mounted with the center line of the parabola being located coplanar with the plane in which the disc lives. In such an arrangement, the combination of the disc and the blades is symmetrical with respect to the plane in which the disc lies. That is, the location of the blades from the disc is a mirror image of the portion of the blades below the disc.
[0008] In a variation of the above described arrangement, it has been known to provide one leg of the parabola (either the upper leg or the lower leg) to be longer than the other. However, such arrangements have still been symmetrical insofar as the shorter leg and 00 0 the longer leg are symmetrical, with the only difference being that the longer N leg extends further forward.
The above described arrangements are generally suitable in many applications. However, it is always desirable to improve the performance of parabolic radial flow impellers. Accordingly, there is a need in the art for an In improved parabolic radial flow impeller, impeller blade, and mixing methods.
SSUMMARY OF THE INVENTION oo 00 0 c In one aspect, an impeller assembly has a hub for mounting the assembly for rotation of the assembly on an axis of rotation; and a plurality of blades mounted in relation to the hub, radially outwardly from the axis of rotation, with each blade in cross-section having a shape that is substantially symmetrical along a center line of the blade and having a first segment and a second segment disposed on opposite sides of the center line, with one segment being symmetrical with at least a portion of the other segment, and with the blades mounted so that the respective center line of each blade is at an angle relative to a common plane which is perpendicular to said axis of rotation.
In another aspect, an impeller assembly for use with a shaft has a generally planar central mounting means for mounting to the shaft; and a plurality of blades mounted to the mounting means and extending radially outward beyond the mounting means with the blades in cross-section having a shape that is substantially symmetrical about a center line and having a first segment and a second segment disposed on opposite sides of the center line, with one segment being symmetrical with at least a portion of the other segment, and with the blades mounted so that the respective center line of each blade is at an angle relative to a plane in which the mounting means lies.
WSa~dr2OO&Ko Deiste 200CW22075 tped IS Feb 08.doc 00 In another aspect, a mounting method includes rotating a shaft to drive an Simpeller assembly that comprises a generally planar disc; and a plurality of blades mounted to the disc and extending beyond the disc, with the blades in cross-section having a shape that has a first segment and a second segment disposed on opposite sides of the center line, with one segment being symmetrical with at least a portion of the other segment, and with the blades n mounted so that the respective center line of each blade is at an angle relative to a plane in which the disc lies.
00 oo In another aspect, an impeller assembly has a hub for mounting the assembly c for rotation on an axis of rotation; and a plurality of blades mounted in relation to the hub, radially outwardly from the axis of rotation, with each blade in cross-section having a shape that is substantially symmetrical along a center line of the blade and having a first segment and a second segment disposed on opposite sides of the center line, with one segment being symmetrical with at least a portion of the other segment, and with the blades mounted so that the respective center line of each blade is parallel to a common plane which is perpendicular to said axis of rotation, and the center line of each blade is offset from the common plane.
In another aspect, an impeller assembly for use with a shaft has a generally planar central mounting means for mounting to the shaft; and a plurality of blades mounted to the mounting means and extending radially outward beyond the mounting means with the blades in cross-section having a shape that is substantially symmetrical about a center line and having a first segment and a second segment disposed on opposite sides of the center line, with one segment being symmetrical with at least a portion of the other segment, and with the blades mounted so that the respective center line of each blade is parallel to a plane in which the mounting means lies, and the center line is offset from the first plane in which the disc lies.
WASanlamQ2( Delete 200B822075 sped 15 Feb 08.oc 00 _Q[0015] In another aspect, a mounting method includes rotating a shaft to drive an Simpeller assembly that comprises: a generally planar disc; and a plurality of blades mounted to the disc and extending beyond the disc, with the blades in cross-section having a shape that has a first segment and a second segment disposed on opposite sides of the center line, with one segment being symmetrical with at least a portion of the other segment, and with the N" blades mounted so that the respective center line of each blade is at an angle relative to a 00 O plane in which the disc lies.
[0016] There has thus been outlined, rather broadly, certain embodiments of the invention in order that the detailed description thereof herein may be better understood, and in order that the present contribution to the art may be better appreciated. There are, of course, additional embodiments of the invention that will be described below and which will form the subject matter of the claims appended hereto.
[0017] In this respect, before explaining at least one embodiment of the invention in detail, it is to be understood that the invention is not limited in its application to the details of construction and to the arrangements of the components set forth in the following description or illustrated in the drawings. The invention is capable of embodiments in addition to those described and of being practiced and carried out in various ways. Also, it is to be understood that the phraseology and terminology employed herein, as well as the abstract, are for the purpose of description and should not be regarded as limiting.
[0018] As such, those skilled in the art will appreciate that the conception upon which this disclosure is based may readily be utilized as a basis for the designing of other structures, methods and systems for carrying out the several purposes of the present invention. It is important, therefore, that the claims be regarded as including such equivalent constructions insofar as they do not depart from the spirit and scope of the present invention.
00
O
BRIEF DESCRIPTION OF THE DRAWINGS [0019] FIG. I is a perspective view of an impeller assembly according to a first embodiment.
[0020] FIG. 2 is an end cutaway view of a portion of the impeller assembly of FIG. 1.
O
0 [0021] FIG. 3 is a perspective view of an impeller assembly according to a second 00 0embodiment.
C [0022] FIG. 4 is an end cutaway view of a portion of the impeller of FIG. 3.
DETAILED DESCRIPTION [0023] A first preferred embodiment of a radial flow impeller assembly mounted or a shaft is shown in FIGS. 1 and 2. In particular, the impeller assembly 10 includes a radially extending disc 12 having an outer peripheral region 14. A plurality of individual blades 16 are provided which each have an upper segment 18 and a lower segment 20. The upper segment 18 has a leading edge 22 and the lower segment 20 has a leading edge 23. The segments converge at a rear vertex 24. A hub 26 mounts the impeller assembly 10 to a shaft 28.
[0024] Turning to FIG. 2, it will be appreciated that in this embodiment the upper segment 18 and lower segment 20 are symmetrical with respect to each other about an imaginary center line CL1, which is indicated by dotted lines. The blade 16 is mounted to overlap with the outer portion of the disc 12 so that its imaginary center line CL1 is at an angle (alpha) a with respect to the plane in which the disc 12 lies.
[0025] This angled orientation of the center line CLI of the parabolic blades 16 with respect to the plane of the disc 12 as described in FIG. 2, provides several advantages in some applications. For example, where gas is being sparged from beneath the impeller assembly 00 because of the increased volumetric area inside the parabola lower segment 20 (compared to if the angle a was zero), greater gas handling can be achieved by the angled orientation.
That is, greater gas handling is achieved prior to reaching the impeller gas handling flood condition in some situations. This is due at least in part to the larger enclosed region between the lower impeller segment 20 and the bottom of the disc 12, so that more gas can be ri entrained.
00 [0026] Further, for the portion of the blade 16 that extends radially outward past the disc 12, it will be appreciated that the tilting of the blade 16 causes the upper region 22 to reach forward (that is the entire blade faces downward to some extent), and so gas also tends to be entrained under the lower surface of the upper segment 1,8, which may increase one or both of the residence time or the total volume of gas that is temporarily contained by the impeller 16.
[00271 Turning to FIGS. 3 and 4, a second embodiment is depicted. In this embodiment the blade 16 is mounted to the disc 12 so that its center line CL2 is at least substantially parallel, or completely parallel, with the plane in which disc 12 lies, but the center line CL2 is also located offset a distance from the plane of the disc 12. In this example, the center line CL2 is offset below the plane of the disc 12 by an offset distance D.
[0028] It will be appreciated that this offset also provides a greater volumetric region in the area bounded by the underside of the disc 12 and the upper inside of the lower segment as well as a portion 22' which is a region of the upper segment of the parabola that is disposed below the plane of the disc 12. This arrangement also has a portion 22" of the upper segment of the parabola that is disposed above the disc 12. In this way, this embodiment also can provide benefits in terms of larger gas handling compared to a prior 00
(N
system where the parabolic blade is mounted with its center line co-linear with the plane of the disc 12.
[0029] Two exemplary embodiments are described and illustrated in FIGS. 2 and 4, tI respectively. In the embodiment of FIG. 2, the vertex of the parabola is located on a center line and the vertex of the parabola in the center line intersect with the plane of the disc. In NS FIG. 4, the center line of the parabola is parallel with the plane of the disc, but is offset by a 00 Sdistance D. Other embodiments are also possible. For example, the embodiment of FIG. 4 could also have the parabola tilted downwardly somewhat similar to FIG. 2, so that the center line intersects with the plane of the disc but not at the point of the vertex.
[0030] Other variations are also possible. For example, instead of being tilted downwardly in FIG. 2, the parabola could be tilted upwardly. Also, in the embodiment of FIG. 4, rather than being spaced downwardly the center line could be spaced upwardly relative to the disc. Further, references in this application to upward and downward are examples. In the case of gas spargers, the gas will generally be bubbling upwards and the orientations described above will generally be the most advantageous. However, impellers having blades according to various embodiments can also be oriented at other angles and in other directions.
[0031] Further, while a solid disc 12 is illustrated, the impellers could be mounted to the shaft via a different type of hub, for example a disc having spokes rather than being solid, or a plurality of individual arms extending from a hub or the shaft itself. In other embodiments, the blades themselves may be mounted directly to a hub or to the shaft and extend radially therefrom.
[0032] Further, while the illustrated embodiment utilizes a parabolic cross section, a circular or a v-shaped cross section may also be possible. For example, in the case of a v- 00
O
O
Sshaped cross section, each blade could be made of two flat pieces meeting at a corer vertex.
T In the case of a v-shaped cross section, an embodiment similar to FIG. 2 being tilled downwardly, or an embodiment similar to FIG. 4 offset downwardly, can also be realized.
S[0033] Also, in other embodiments, the cross section of the blades does not have to be symmetrical with respect to the center line. For example, either the upper or lower legs of the
O
N, parabola may be longer or shorter than each other. Alternatively, one of the upper or lower 00 Slegs could have a cross sectional shape that is different than the opposite upper or lower leg.
Further, although the blades are shown as being solid items, the blades may be slotted or have ports extending therethrough at similar locations.
[0034] The many features and advantages of the invention are apparent from the detailed specification, and thus, it is intended by the appended claims to cover all such features and advantages of the invention which fall within the true spirit and scope of the invention. Further, since numerous modifications and variations will readily occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation illustrated and described, and accordingly, all suitable modifications and equivalents may be resorted to, falling within the scope of the invention.
Claims (20)
1. An impeller assembly, including: a hub for mounting the assembly for rotation on an axis of rotation; and a plurality of blades mounted in relation to the hub, radially outwardly from the axis of rotation, with each blade in cross-section having a shape that I is substantially symmetrical along a center line of the blade and having a first segment and a second segment disposed on opposite sides of the center line, C with one segment being symmetrical with at least a portion of the other 00 oo segment, and with the blades mounted so that the respective center line of c each blade is at an angle relative to a common plane which is perpendicular to said axis of rotation.
2. The assembly according to claim 1, wherein the cross-section of each blade is at least partially in the shape of a parabola.
3. The assembly according to claim 2, wherein the parabola has a central vertex at which the first and second segments meet with the vertex located on the center line of the parabola, and wherein each blade is mounted so that the vertex extends through the first plane in which the disc lies.
4. The assembly according to claim 1, wherein the blades are equally circumferentially spaced around the disc edge.
5. An impeller assembly for use with a shaft, comprising: a generally planar central mounting means for mounting to the shaft; and a plurality of blades mounted to the mounting means and extending radially outward beyond the mounting means with the blades in cross-section having a shape that is substantially symmetrical about a center line and having a first segment and a second segment disposed on opposite sides of the center line, with one segment being symmetrical with at least a portion of the other segment, and with the blades mounted so that the respective center line WAanraOOMO Deiewe 2Mfl$8D75 Sped 15 Fab MOWdc 00 of each blade is at an angle relative to a plane in which the mounting means Slies.
S6. The assembly according to claim 5, wherein the cross-section of each blade is in the shape of a parabola.
7. The assembly according to claim 6, wherein the parabola has a central 0vertex located on the center line of the parabola, and wherein the blade is C mounted so that the vertex extends through the plane of the disc. 00 oo c
8. The assembly according to claim 5, wherein the blades are equally circumferentially spaced around the disc edge.
9. A mounting method comprising: rotating a shaft to drive an impeller assembly that comprises: a generally planar disc; and a plurality of blades mounted to the disc and extending beyond the disc, with the blades in cross-section having a shape that has a first segment and a second segment disposed on opposite sides of the center line, with one segment being symmetrical with at least a portion of the other segment, and with the blades mounted so that the respective center line of each blade is at an angle relative to a plane in which the disc lies.
The mounting method according to claim 9, wherein the parabola has a central vertex located on the center line of the parabola, and wherein the blade is mounted so that the vertex extends at the plane of the disc.
11. An impeller assembly, including: a hub for mounting the assembly for rotation on an axis of rotation; and a plurality of blades mounted in relation to the hub, radially outwardly from the axis of rotation, with each blade in cross-section having a shape that is substantially symmetrical along a center line of the blade and having a first segment and a second segment disposed on opposite sides of the center line, with one segment being symmetrical with at least a portion of the other W SaraUVO8XlXo DeIlee 2008B22O15 SpW 15 Feb 08dC 00 segment, and with the blades mounted so that the respective center line of 0 each blade is parallel to a common plane which is perpendicular to said axis of (N Srotation, and the center line of each blade is offset from the common plane. aT,
12. The assembly according to claim 11, wherein the cross-section of each blade is at least partially in the shape of a parabola.
13. The assembly according to claim 12, wherein the parabola has a central Svertex at which the first and second segments meet, with the vertex located on 00 the center line of the parabola, and wherein the blade is mounted so that the Svertex is offset from the first plane in which the disc lies.
14. The assembly according to claim 11, wherein the blades are equally circumferentially spaced around the disc edge.
An impeller assembly for use with a shaft, comprising: a generally planar central mounting means for mounting to the shaft; and a plurality of blades mounted to the mounting means and extending radially outward beyond the mounting means with the blades in cross-section having a shape that is substantially symmetrical about a center line and having a first segment and a second segment disposed on opposite sides of the center line, with one segment being symmetrical with at least a portion of the other segment, and with the blades mounted so that the respective center line of each blade is parallel to a plane in which the mounting means lies, and the center line is offset from the first plane in which the disc lies.
16. The assembly according to claim 15, wherein the cross-section of each blade is in the shape of a parabola.
17. The assembly according to claim 16, wherein the parabola has a central vertex at which the first and second segments meet, with the vertex located on the center line of the parabola, and wherein the blade is mounted so that the vertex is offset from the first plane in which the disc lies. W Sandra%208Wo Deltet 20=6=82275 sped 15 Fab08 doC 13 o00
18. The assembly according to claim 15, wherein the blades are equally Scircumferentially spaced around the disc edge.
19. A mounting method comprising: rotating a shaft to drive an impeller assembly that comprises: a generally planar disc; and a plurality of blades mounted to the disc and extending beyond Sthe disc, with the blades in cross-section having a shape that has a first segment and a second segment disposed on opposite sides of the center line, Nwith one segment being symmetrical with at least a portion of the other segment, and with the blades mounted so that the respective center line of each blade is at an angle relative to a plane in which the disc lies.
20. The mounting method according to claim 19, wherein the parabola has a central vertex located on the center line of the parabola, and wherein the blade is mounted so that the vertex extends through the plane of the disc. W ASarkm2OO\No Oeete 2OO8822075 SW 5 Feb 08doo
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/707,089 | 2007-02-16 | ||
US11/707,089 US20080199321A1 (en) | 2007-02-16 | 2007-02-16 | Parabolic radial flow impeller with tilted or offset blades |
Publications (1)
Publication Number | Publication Date |
---|---|
AU2008200755A1 true AU2008200755A1 (en) | 2008-09-04 |
Family
ID=39204436
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU2008200755A Abandoned AU2008200755A1 (en) | 2007-02-16 | 2008-02-15 | Parabolic radial flow impeller |
Country Status (9)
Country | Link |
---|---|
US (1) | US20080199321A1 (en) |
CN (1) | CN101306333A (en) |
AU (1) | AU2008200755A1 (en) |
CA (1) | CA2620485A1 (en) |
DE (1) | DE102008008507A1 (en) |
FR (1) | FR2912669A1 (en) |
GB (1) | GB2446924A (en) |
IT (1) | ITMI20080215A1 (en) |
ZA (1) | ZA200801400B (en) |
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US10618018B2 (en) | 2016-05-25 | 2020-04-14 | Spx Flow, Inc. | Low wear radial flow impeller device and system |
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-
2007
- 2007-02-16 US US11/707,089 patent/US20080199321A1/en not_active Abandoned
-
2008
- 2008-02-07 CA CA002620485A patent/CA2620485A1/en not_active Abandoned
- 2008-02-07 GB GB0802308A patent/GB2446924A/en not_active Withdrawn
- 2008-02-11 ZA ZA200801400A patent/ZA200801400B/en unknown
- 2008-02-11 DE DE102008008507A patent/DE102008008507A1/en not_active Withdrawn
- 2008-02-12 IT IT000215A patent/ITMI20080215A1/en unknown
- 2008-02-15 AU AU2008200755A patent/AU2008200755A1/en not_active Abandoned
- 2008-02-15 FR FR0800838A patent/FR2912669A1/en not_active Withdrawn
- 2008-02-18 CN CNA2008100093265A patent/CN101306333A/en active Pending
Also Published As
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DE102008008507A1 (en) | 2008-08-21 |
GB0802308D0 (en) | 2008-03-12 |
ZA200801400B (en) | 2009-01-28 |
CN101306333A (en) | 2008-11-19 |
ITMI20080215A1 (en) | 2008-08-17 |
FR2912669A1 (en) | 2008-08-22 |
CA2620485A1 (en) | 2008-08-18 |
US20080199321A1 (en) | 2008-08-21 |
GB2446924A (en) | 2008-08-27 |
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Legal Events
Date | Code | Title | Description |
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MK4 | Application lapsed section 142(2)(d) - no continuation fee paid for the application |