The present invention relates to a multi-stage pump; and more particularly relates to a center bushing for a multi-stage pump.
In multi-stage pumps, e.g., like that shown in
To aid in balancing the axial forces, the higher pressures must be able to flow to an area of lower pressure, e.g., via balance holes, pump out vanes, or other similar thrust reducing designs which may allow this pressure to be reduced. The introduction of these passages increases the leakage between the stages which may negatively affect the efficiency. If these forces are not reduced, it may lead to increasing the size of the bearing system. A larger bearing/frame system may cost more and these larger bearings may use more power, therefore reducing the overall efficiency.
Currently, in the 8200 Series multi-stage pumps there are a total of eight (8) parts that need to be assembled to help reduce the axial forces; and the parts are as follows:
The assembly and serviceability are rather difficult because of the complexity of the components.
In view of this, there is a need for a better way to balance the uneven axial forces generated within a multi-stage pump, e.g., in order to allow the higher pressures to flow to a location of lower pressure.
In summary, the present invention provides a new and unique center bushing that still has a small controlled leakage between the stationary and rotating elements. The present invention will increase the axial forces in the higher pressure section of the pump, by introducing pockets to the center bushing. The velocity that is on the backside of the high pressure stage is reduced, which will increase the pressure locally on the backside of the respective stage. Since the pressure in this section is now being increased, a new way of balancing is introduced. As the pressure on the high pressure side is increased due to a decreased velocity, this helps to create an axial force balance between the different stages. When the multi-stage pump designer is calculating the axial forces, the results are a force with a magnitude and a direction. The present invention will be directionally interchangeable depending on the direction of the axial force. Depending on the direction of the thrust, the present invention will allow for a placement so it can always be located on the desired side to help increase the local pressure which will help to balance the axial forces. The center bushing or device will only need to be pinned in one locating to prevent rotation, and with running tight tolerances between the center bushing or device and the pump's casing these tight clearances allow for the removal of O-ring features or devices that aid in the prevention of leakage. By making the diameter of the center bushing or device the same diameter as the wear rings, no diameter difference is introduced that may create another location for axial forces to act upon. Also by removing the extra balance holes drilled through the center bushing, which helps offset the axial forces, there is less of a leakage path. By reducing the leakage path, efficiency may be increased. By balancing axial forces, the thrust absorbing bearing system may be reduced. If the bearing system is retained without reduction, it will improve reliability. If the bearing system is reduced, both cost of the bearing and power loss within the bearing will be reduced. Reduction of power can lead to gains in efficiency.
The original and alternate center bushing configurations disclosed herein are designed to reduce velocity behind the stage of higher pressure which will proportionally increase the pressure behind the respective stage. This pressure increase may help to offset the larger axial forces generated from the pressure rise across the stage which will help to balance resultant axial forces.
According to some embodiments, the present invention may take the form of a multi-stage pump, featuring:
the different stages of the multistage pump.
The multi-stage pump according to the present invention may include one or more of the following features:
The pockets may include, or take the form of, radially-formed rib pockets.
By way of example, the center bushing side may include a center bushing surface having an inner wall, an outer wall and a plurality of radial walls all extending from the center bushing surface, each radially-formed rib pocket having by a combination of an inner wall portion, a corresponding outer wall portion and adjacent radial walls connecting the inner wall portion and the corresponding outer wall portion.
The inner wall may include, or form part of, an inner circular wall extending around the inner edge of the center bushing.
The outer wall may include, or form part of, an outer circular wall extending around the outer edge of the center bushing.
The pockets may include, or take the form of, curved rib pockets.
By way of example, the center bushing surface may include an inner wall, an outer wall and a plurality of curved rib walls all extending from the center bushing surface, each radially-formed rib pocket having by a combination of an inner wall portion, a corresponding outer wall portion and adjacent curved rib walls connecting the inner wall portion and the corresponding outer wall portion.
The pockets may include, or take the form of, extruded circle or circular pockets, e.g., which are formed as raised cylindrical protrusions having an outer cylindrical wall and a top surface.
The pockets may include, or take the form of, full length rib pockets.
By way of example, the center bushing surface may include an inner wall, an outer wall and a plurality of full length rib walls all extending from the center bushing surface, each radially-formed rib pocket having by a combination of an inner wall portion, a corresponding outer wall portion and adjacent full length rib walls connecting the inner wall portion and the corresponding outer wall portion.
The different stages may have an area/location of higher pressure and a corresponding area/location of lower pressure; and the pockets may be configured to increase the axial forces in the area/location of higher pressure.
A center bushing side may include a high pressure side configured with the pockets facing the area/location of higher pressure.
The multi-stage pump may include a stationary element configured with an aperture; and the center bushing may include an outer circumferential rim configured with a pin to couple into the aperture of the stationary element to prevent rotation of the center bushing.
The stationary element may be configured with a circumferential surface having an inner diameter; and the outer circumferential rim may include an outer diameter that substantially corresponds in dimension to the inner diameter of the circumferential surface of the stationary element in order to substantially reduce or prevent leakage between the different stages.
The different stages may include:
a center bushing side having a high pressure side configured with the pockets facing the corresponding area/location of higher pressure.
According to some embodiments, the present invention may take the form of a multi-stage device featuring a device having different stages configured to provide a fluid; and a center bushing configured between the different stages, having a center bushing side configured with pockets to balance axial forces between the different stages of the multistage device. The multi-stage device may include, or take the form of, a multi-stage pump, fan, blower or compressor. The pockets may include, or be configured as, radially-formed rib pockets, or curved rib pockets, or extruded circle or circular pockets, or full length rib pockets.
By way of example, advantages of the present invention may include the following:
The new and unique center bushing helps to balance the uneven axial forces generated within the multi-stage pump, by allowing the higher pressures to flow to a location of lower pressure. Therefore, the axial thrust may be reduced and brought down to a level that can be handled by the bearing system.
The drawing, which is not necessarily drawn to scale, includes the following Figures:
The Figures include reference numerals and lead lines, which are included to describe each Figure in detail below. In the drawing, similar elements in the various Figures are labeled with similar reference numerals and lead lines. Moreover, not every element is shown and/or labeled with a reference numeral and lead line in every Figure to reduce clutter in the drawing as a whole.
According to some embodiments, the present invention may take the form of a multi-stage pump generally indicated as 10, featuring:
The different stages may have an area/location of higher pressure as shown and indicated in
The center bushing side CBS1 may include a high pressure side configured with the pockets (e.g., such as PKT (
The different stages may include:
By way of example, the pockets (PKTs) may be configured as radially-formed rib pockets.
The inner wall IW may include, or form part of, an inner circular wall extending around the inner edge of the center bushing, e.g., consistent with that shown in
The outer wall OW may include, or form part of, an outer circular wall extending around the outer edge of the center bushing, e.g., consistent with that shown in
By way of example, in
By way of example, in
Moreover, the scope of the invention is not intended to be limited to any particular pattern of extruded circle or circular pockets. For example, the scope of the invention is intended to include, and embodiments are envisioned using, a center bushing having other types or kinds of patterns, e.g., like a pattern of eighteen (18) pairs of extruded circle or circular pockets, each arranged equi-distant about the center bushing surface, or like a pattern of twelve (12) triplets of extruded circle or circular pockets, each arranged equi-distant about the center bushing surface, etc.
By way of example, the extruded pockets ECPs are shown as cylindrical protrusions; however, the scope of the invention is not intended to be limited to any particular geometric shape of the extruded pockets. The scope of the invention is intended to include, and embodiments are envisioned in which, the extruded pockets take the form of other geometric shapes such as extruded 3-sided or triangular pockets, extruded 4-sided or rectangular pockets, extruded 5-sided or pentagonal pockets, etc., as well as other extruded 1-side pockets like oval pockets.
The multi-stage pump 10 may include a stationary element, e.g., some part of the pump's casing C, configured with an aperture; and the center bushing CB may include an outer circumferential rim or wall OW (
According to some embodiments, the stationary element or part of the pump's casing C may be configured with a circumferential surface having an inner diameter; and the outer circumferential rim may include an outer diameter that substantially corresponds in dimension to the inner diameter of the circumferential surface of the stationary element in order to substantially reduce or prevent leakage between the different stages.
The scope of the invention is not intended to be limited by any particular dimensions of the pockets PKT (
By way of example, in addition to multi-stage pumps other possible applications of the present invention may include, or take the form of, fans, blowers and compressors.
It should be understood that, unless stated otherwise herein, any of the features, characteristics, alternatives or modifications described regarding a particular embodiment herein may also be applied, used, or incorporated with any other embodiment described herein. Also, the drawing herein is not necessarily drawn to scale.
Although the invention has been described and illustrated with respect to exemplary embodiments thereof, the foregoing and various other additions and omissions may be made therein and thereto without departing from the spirit and scope of the present invention.
This application claims benefit to provisional application Ser. No. 62/305,305, filed 8 Mar. 2016, which is hereby incorporated by reference in its entirety.
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Number | Date | Country | |
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