Embodiments disclosed herein relate generally to lubricant separators, such as for example an oil separator. In particular, apparatuses, systems and methods are directed to lubricant separators, such as for example cyclonic type lubricant separators, which may be implemented in fluid systems. Such fluid systems include for example refrigeration or cooling systems and/or heating, ventilation, and air conditioning (HVAC) systems, which employ refrigerant as a working fluid.
Cyclonic lubricant separators receive a fluid mixture, including a lubricant such as for example oil and other vapor(s) (e.g. refrigerant gas) and/or liquid(s). The fluid mixture is received by the separator through an inlet, flows into the shell of the separator, swirls within the shell, where the oil adheres around the inner surfaces (e.g. sides) of the shell inside the separator. The refrigerant gas can continue to swirl and be separated from the oil, be released into a suction or discharge tube that is placed within the shell, and then exit the separator. The separated oil has a different momentum than the vapor and flows to a bottom sump and drains out of the shell.
Improvements may be made to lubricant (e.g. oil) separators, such as for example cyclonic type oil separators. Lubricant separators herein include various features that provide one or more of the advantages of reducing pressure losses, addressing local gas velocities which may contribute to entrainment of liquid(s) (e.g. oil), maintaining and/or improving oil separation (e.g. achieving lower oil circulation rates), reducing the size of the lubricant separator, and/or reducing or minimizing costs of production.
In one embodiment, lubricant separators herein include a shell, a fluid inlet, a vapor outlet, a liquid outlet, and a discharge tube within the shell. Various embodiments herein of the lubricant separator features, including for example, the fluid inlet and/or the discharge tube can provide the one or more above advantages.
In some embodiments, the fluid inlet comprises multiple inlets.
In some embodiments, the inlet(s) each have an opening such that the majority of the discharge tube is out of sight relative to the opening(s) of the inlet(s). In some embodiments, the opening(s) are configured so that the discharge tube is out of sight relative to the opening(s) of the inlet(s).
In one embodiment, the discharge tube includes one or more openings along the length of the tube, or for example along the height of the discharge tube in the assembled state. In one embodiment, the one or more openings can be disposed at locations about the circumference of the discharge tube.
In one embodiment, the lubricant separator includes a flow director on the discharge tube. The flow director includes one or more surfaces that extend away from the outer dimension of the discharge tube. In one embodiment, the flow director is a flare like structure including a drip edge.
In one embodiment, the discharge tube is structurally secured at both ends.
In one embodiment, the inlets are on the same horizontal plane. In some embodiments, the inlets are on different horizontal planes. In some embodiments, the inlets are oriented at or about 90 to at or about 180 degrees relative to each other about the circumference of the shell. In some embodiments, the inlets have openings that are angled relative to a horizontal plane.
In one embodiment, and end of the discharge tube includes a plug. In one embodiment, the plug closes the end of the discharge tube.
These and other features, aspects, and advantages of lubricant separators herein will become better understood when the following detailed description is read with reference to the accompanying drawings, wherein:
While the above-identified figures set forth particular embodiments of lubricant separators, other embodiments are also contemplated, as noted in the descriptions herein. In all cases, this disclosure presents illustrated embodiments of lubricant separators by way of representation but not limitation. Numerous other modifications and embodiments can be devised by those skilled in the art which fall within the scope and spirit of the principles of the lubricant separators described and illustrated herein.
Embodiments disclosed herein relate generally to lubricant (e.g. oil) separators. In particular, apparatuses, systems and methods are directed to oil separators, such as for example cyclonic type oil separators, which may be implemented in fluid systems, such as for example in refrigeration or cooling systems and/or HVAC systems, which employ refrigerant as a working fluid. The lubricant separators herein may be employed for example in a fluid chiller (e.g. water chiller) with a screw or scroll compressor design, and such as may be used in a HVAC system. It will be appreciated that the lubricant separators herein may be implemented in fluid systems other than an HVAC, refrigeration, or cooling system, implemented in units other than a fluid chiller, implemented with fluids other than a lubricant (e.g. oil), and/or implemented with compressors other than a screw or scroll compressor.
Lubricant separators herein include various features that provide one or more of the advantages of reducing pressure losses, addressing local gas velocities which may contribute to entrainment of liquids, maintaining and/or improving oil separation (e.g. oil circulation rates), reducing the size of the lubricant separator, and/or reducing or minimizing costs of production.
For example, lubricant separators herein can provide a cost reduction of currently produced oil separators that are used, such as for example in systems that employ a screw compressor design. Lubricant separators herein can also provide cost containment on future systems, such as for example that may employ scroll compressor designs, incorporating an oil separator with a relatively high pressure (e.g. “high side”) oil sump, and which may also be used in certain screw compressor designs. Such lubricant separators herein can be implemented for example in a fluid chiller that has a compressor capacity, such as for example greater than 50 tons, where a high side oil sump may be employed. Lubricant separators herein can be implemented with various working fluids, including for example various refrigerants and blends thereof, including for example R134a and/or R410a or other refrigerants including for example relatively medium to high pressure refrigerants.
For example, current screw compressor designs employed in chillers such as for an HVAC system, have the oil separator between the compressor and condenser to separate oil from refrigerant gas. Such oil separators are designed with well over 6.00 inches of inside diameter for the shell (e.g. 12 inches, 10 inches, 8 inches and the like), which classifies them as pressure vessels requiring them to be code complying under standards set for example by the American Society of Mechanical Engineers (ASME). Lubricant separators herein can have an inner shell diameter that is less than 6.00 inches and can be shorter than 24-28 inches which is a typical height range of certain oil separators.
In one embodiment, the lubricant separator herein includes a shell with an inside diameter of less than 6.00 inches. In one embodiment, the lubricant separator is not an ASME rated pressure vessel due to for example the size of the inside diameter being within a certain dimension, e.g. less than 6.00 inches. In some cases, such a designed lubricant separator provides a significant cost advantage over ASME rated pressure vessels.
It will be appreciated that the lubricant separators herein may have shells with inside diameters at or greater than 6.00 inches. Generally, the lubricant separators herein can provide an advantage of a size reduction (e.g. shells with smaller inside diameters) relative to various application in which the lubricant separators herein may be implemented, including for example relatively smaller and relatively larger capacity applications.
In the embodiment shown, the lubricant separator 100 has a shell 8 and a cap 6, which may be domed shaped. In the embodiment shown, the separator 100 has a twin inlet configuration, illustrated by inlets 1 and 2. Refrigerant gas and liquid oil enter through the inlets 1, 2. The separator 100 has a vapor outlet 7 and a liquid (e.g. lubricant) exit 11
In the embodiment shown, the inlets 1, 2 are located, positioned, or otherwise arranged tangentially on the perimeter of the shell 8. In some embodiments, the inlets 1, 2 may be sized, e.g. the inner diameter size, to allow for example a maximum inlet velocity. In some embodiments, the inlet size (e.g. inlet inner diameter) may be limited to a size so that the opening through the inlet(s) does not have a line of sight relative to a discharge tube 5 within the shell 8. For example, when looking through the inlets 1, 2, the discharge tube 5 is not in the line of sight, such as for example not visible through the inlets or is only partially or is minimally visible. In an embodiment, in looking through the opening of the inlet(s) there is no line of sight to the discharge tube. In an embodiment, in looking through the opening of the inlet(s) there is only a partial or minimal view of the discharge tube, where the majority of the discharge, such as for example substantially all of the discharge tube is out of sight.
The opening of the inlets, e.g. inlets 1, 2, being within the line of sight of the discharge tube 5 may in some cases degrade the oil separation efficiency, by potentially allowing oil to impinge on the discharge tube 5, rather than the shell 8 thereby risking oil entrainment with the vapor and into the discharge tube 5. It will be appreciated that the inlet size can be partially within the line of sight of the discharge tube without degrading the oil separation efficiency, for example in certain operating conditions such as when the local gas velocities are relatively low and/or in conditions where impingement of oil on the discharge tube is relatively less of a risk.
It will be appreciated that the discharge tube 5, or any discharge tube herein, may not be entirely out of the line of sight relative to the opening(s) of the inlet(s). For example, the discharge tube in some embodiments may be partially within the line of sight of the opening(s), such as for example where the majority of the discharge tube is out of the line of sight, or it is nearly out of sight from the opening(s) of the inlet(s).
Generally, it may be desired in certain circumstances to physically limit the size of the inlets 1, 2 to be suitably compact relative to a line of sight orientation with respect to the discharge tube 5. In some cases, the discharge tube may have a portion that is observable through the inlet(s), e.g. partially within the line of sight.
It will be appreciated that one inlet may be implemented, or more than two inlets may be implemented. The inlets can be positioned or located, such as for example at the same height or at different heights along the discharge tube 5, and can be oriented at the same angle or at different angles relative to horizontal. Generally, additional inlets can allow for additional fluid flow area while also reducing the risk of being in the line of sight relative to the discharge tube 5, and depending on their sizing.
In some embodiments where multiple inlets are employed, the inlets can be angled or otherwise oriented in different directions so that flow from one inlet does not disrupt the flow from another inlet. For example, the inlets may be angled somewhat downward in different directions. As one example, the inlets could be constructed, configured, and/or arranged to provide a flow resembling a double helix type flow, with angled inlets (e.g. not horizontal) facing different directions, and/or different flows.
It will also be appreciated that the inlets of the lubricant separators herein can be configured to support more than one compressor (e.g. two compressors for a twin inlet design, one inlet for each compressor), where the inlets can be sized and oriented to design a certain flow as desired and/or needed.
In some embodiments, the inlet(s) can have various geometries including geometries that vary through any given inlet.
In the embodiment shown in
With further reference to
In the embodiment shown, the discharge tube 5 is positioned relatively centered within the inner diameter of the shell 8 and receives the refrigerant gas.
The discharge tube 5 is shown as a cylindrical component. However, it will be appreciated that the discharge tube 5 is not limited to a cylindrical shape, and can be suitably constructed as an outlet component, such as an outlet pipe which may be any shape or design. It will also be appreciated that the discharge tube 5 height (e.g. length) can vary.
In the embodiment shown, the discharge tube 5 includes openings 4 to receive the refrigerant gas.
In some embodiments, the openings 4 are on the side of the discharge tube 5, and can be in various numbers, shapes, sizes, arrangements, patterns, locations and the like. For example, the openings can 4 be round-like or circular, square or rectangular-like, triangular, trapezoidal, other polygonal shape, or other suitable shapes. The openings 4 can be sized and shaped depending on a flow rate/internal pressure of the type of system in which the separator 100 is employed. It will also be appreciated that the openings 4 can be constructed, configured, and/or arranged to meter the flow of vapor through the discharge tube 5 and exiting the outlet 7. It will also be appreciated that the number, placement, and/or geometry of the openings 4 can be pre-determined to achieve a uniform flow rate entering the discharge tube 5 along the dimensions of the openings.
In some examples, such as shown in
The openings 4 are constructed, configured, and/or arranged to in certain circumstances reduce local gas velocities and/or minimize local gas velocities within the main separator shell, such as for example that may be observed along and/or proximate the discharge tube. High local gas velocities can have a tendency to re-entrain liquid, e.g. oil, thereby decreasing the efficiency of the separator and/or have undesired pressure drop.
In some examples such as the embodiment shown in
The slots help to distribute the flow of gas over a wider area, e.g. spread it out along the length of the discharge tube 5. The slots help to provide a more gradual gas flow, rather than requiring all of the flow to move down the discharge tube 5, and turn sharply to move vertically upward into the discharge tube (e.g. at opening or port 3).
The slots help to reduce pressure losses, while reducing or avoiding liquid (e.g. oil) entrainment into the discharge tube, or other local effects and potential sudden tendency carryover phenomena. Such local effects may be conditions of relatively high velocity in a low pressure region, which can cause stripping, e.g. leading to carryover over liquids into the discharge tube 5.
The use of the openings (e.g. slots) help the flow to approach and enter the discharge tube 5 at relatively lower velocities, which can be helpful due to a relatively close distance from discharge tube 5 and the inner surfaces of the shell 8.
Generally, the summed area of the openings 4, e.g. slots, provides a strategic approach to increasing the cross-sectional flow area compared for example to the cross-sectional flow area of a discharge tube with only an open bottom end (e.g. at 3). The openings 4 can also provide advantages of relatively lower pressure drop, e.g. pressure losses through the lubricant separator 100.
It will be appreciated that the openings 4, e.g. slots as shown in
The use of the openings 4 for gas to enter the discharge tube along its side wall in addition to or instead of the opening 3 or port at the bottom of the discharge tube 5. Advantages of doing this include for example being able to make the oil separator 100 overall, significantly smaller, e.g. by reducing the inner diameter of the shell 8, such as for example to 6.00 inches or less. The vessel material cost is lower, and becomes a non-ASME component which also reduces production cost. For example, as high as 50% cost reduction may be observed relative to for example oil separators with an 8″ or 10″ or 12″ inner diameter.
In some embodiments, the discharge tube 5 can also have an opening 3 at the lower end of the discharge tube, such as for example through the end and not along the vertical direction of the discharge tube. In an embodiment, it will be appreciated that side openings, e.g. 4, along the length of the discharge tube 5 may not be implemented, as shown and described with respect to further embodiments below.
Refrigerant gas can leave the lubricant separator through the outlet or port 7 of the discharge tube 5.
Oil drains downward along the inside surfaces of the side wall of the shell 8. In some embodiments, the oil flows past a plate 9 and into a sump area below the plate 9. In some embodiments, such as shown in
In another embodiment, the opening or port at the bottom of the discharge tube may not be open. For example, the opening may be manufactured as closed or provided with a plug structure. In such an embodiment, the refrigerant gas would enter the discharge tube through other openings, e.g. on the side of the tube, such as for example the slots shown in
In another example,
It will be appreciated that any of the lubricant separators herein may be implemented with any of the systems 400, 410, and 420.
In some embodiments, the discharge tube 5, 205 may be shortened or may be extended further downward, such as for example to a plate (e.g. plate 9, 209) relative to a sump area. The plate in some embodiments may include an alignment feature, such as for example to locate and/or center the discharge tube within the shell 8. The alignment feature, for example can be a pin and/or suitable key structure to receive the end of the discharge tube. In such an embodiment of implementing an alignment feature, the end of the discharge tube may be closed.
In such a configuration, the extension of the discharge tube 5, 205 can address or avoid potential vibration or mechanical issues, as the discharge tube would be further supported by additional structure, e.g. plate 9, 209.
In the embodiment shown, the discharge tube 505 may be closed at the end where the plug 512 is located. However, it will be appreciated that the plug or connective structure on the discharge tube 505 may not be fully closed and could have or leave opening(s) for vapor to enter the discharge tube 5 from the end (e.g. the bottom when installed).
It will be appreciated that when using the flow director, the inlet(s) used in a lubricant separator may be constructed to have some (e.g. minimal) line of sight relative to the discharge tube. It will also be appreciated that flow directors herein may be implemented in separators with a single or multiple inlets in various configurations and geometries, and/or in separators with or without openings (e.g. slots) along the outer side of the discharge tube.
In the example shown in
Flow directors herein may be useful to help prevent entrainment of liquid (e.g. oil) and carryover into the discharge tube and from exiting the outlet. Flow directors herein provide surfaces that extend away from the outer dimension of the discharge tube. Flow directors herein at their distal end (i.e. away from the outer dimension of the discharge tube) have a drip edge for liquid (e.g. oil) to drip and flow downward to the sump area of the separator. The drip edge is generally spaced away from the discharge tube so as to direct liquid away from the discharge tube. The spacing of the drip edge may vary depending on the design. It will also be appreciated that the location of the flow director on the height of the discharge can vary.
Flow directors herein can be useful in conditions of relatively low capacity and/or low flow rate, so as to reduce and/or minimize the risk of liquid oil being entrained with the vapor through the discharge tube and outlet.
As shown, the lubricant separator 1400 includes a shell 1408, inlets 1401, 1402, which in this embodiment may be constructed to have no line of sight or a minimal line of sight to a discharge tube 1405, e.g. the large majority of the discharge tube 1405 is not within the line of sight of the inlets 1401, 1402. In the embodiment shown, the inlets 1401, 1402 are on the same horizontal plane and are oriented about 180 degrees relative to each other. The lubricant separator 1400 also has a cap 1406, which may be a domed cap, and an outlet 1407. The oil exit may be from the bottom 1411. The discharge tube 1405 has openings 1404 (e.g. one slot is shown). The dimensions of the separator 1400 may be different from those dimensions described above for example with respect to
As shown, the lubricant separator 1500 includes a shell 1508, inlets 1501, 1502, which in this embodiment may be constructed to have no line of sight or a minimal line of sight to a discharge tube 1505, e.g. the large majority of the discharge tube 1505 is not within the line of sight of the inlets 1501, 1502. In the embodiment shown, the inlets 1501, 1502 are on the same horizontal plane and are oriented about 90 degrees relative to each other as shown in this example. The lubricant separator 1500 also has a cap 1506, which may be a removable cover, and an outlet 1507. The oil exit may be from the bottom 1511, and which may include a removable cover. As shown in
In an embodiment, the lubricant separator 1530 may have one or more of a plate 1509 to separate from a sump area, and/or one or more anti-swirl plates 1510 in the sump area. Lubricant, e.g. oil, can exit through the outlet 1511.
Aspects—any of aspects 1 to 15 may be combined with any of aspects 16 to 18, aspect 16 may be combined with aspects 17 or 18, and aspect 17 may be combined with aspect 18.
1. A lubricant separator includes a shell, a fluid inlet, a vapor outlet, a liquid outlet, and a discharge tube within the shell.
2. The lubricant separator of aspect 1, wherein the fluid inlet comprises multiple inlets that have openings such that the discharge tube is out of sight relative to the openings of the inlet.
3. The lubricant separator of aspect 1, wherein the fluid inlet comprises multiple inlets that have openings such that a majority of the discharge tube is out of sight relative to the openings of the inlets.
4. The lubricant separator of aspect 1, wherein the discharge tube includes one or more openings along the length of the tube, or for example along the height of the discharge tube in the assembled state.
5. The lubricant separator of aspect 4, wherein the one or more openings can be disposed at locations about the circumference of the discharge tube.
6. The lubricant separator of any one of aspects 1 to 5, further comprising a flow director on the discharge tube.
7. The lubricant separator of aspect 6, wherein the flow director includes one or more surfaces that extend away from the outer dimension of the discharge tube.
8. The lubricant separator of aspect 6 or 7, wherein the flow director is a flare like structure including a drip edge.
9. The lubricant separator of any one of aspects 1 to 8, wherein the discharge tube is structurally secured at both ends.
10. The lubricant separator of any one of aspects 1 to 9, wherein the inlets are on the same horizontal plane.
11. The lubricant separator of any one of aspects 1 to 9, wherein the inlets are on different horizontal planes.
12. The lubricant separator of any one of aspects 1 to 11, wherein the inlets are oriented at or about 90 to at or about 180 degrees relative to each other about the circumference of the shell.
13. The lubricant separator of any one of aspects 1 to 12, wherein the inlets have openings that are angled relative to a horizontal plane.
14. The lubricant separator of any one of aspects 1 to 13, wherein an end of the discharge tube includes a plug.
15. The lubricant separator of any one of aspects 1 to 14, wherein the plug closes the end of the discharge tube.
16. A chiller including the lubricant separator of any one of aspects 1 to 15.
17. A cooling or refrigeration system including the lubricant separator of any one of aspects 1 to 16.
18. A method of directing fluid flow through a lubricant separator of any one of aspects 1 to 17.
Filing Document | Filing Date | Country | Kind |
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PCT/US2016/016794 | 2/5/2016 | WO | 00 |
Number | Date | Country | |
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62112849 | Feb 2015 | US |