The present disclosure relates, generally, to the field of reciprocating compressors. More particularly, the present disclosure relates to an oil separation assembly and high pressure reciprocating compressors including the same.
Reciprocating compressors generally have a housing with a partition member, such as a wall, which divides the space within the housing into a suction chamber and a crankcase chamber, the lowest portion of which serves as an oil sump. The partition member is provided with relatively large openings in which cylinder sleeves are mounted and pistons are slidably mounted for reciprocating motion in the cylinder sleeves to compress gas passing through the suction chamber. The pistons are connected by connecting rods, which are provided with connecting rod bearings, to a crankshaft which is rotatably mounted on crankshaft bearings in the lower crankcase chamber. The partition member also supports capacity reduction mechanisms which are located in the upper suction chamber and which operate gas inlet valves which are located at the upper ends of the cylinder sleeves. The partition also includes one or more small pressure equalizers or vent holes which serve to provide for gas pressure equalization between the suction chamber and the crankcase chamber. The pressure equalizers or vent holes also serve to drain oil collected in the suction chamber to the crankcase chamber. The pressure equalizers or vent holes may include pressure relief valves.
During compressor operation, lubricating oil is supplied under pressure through passages in the housing, crankshaft and piston rods to the connecting rod bearings and crankshaft bearings in the crankcase. As oil drains out of the bearings during crankshaft rotation, oil droplets are sprayed about the crankcase chamber and eventually drain into the oil sump from whence the oil is recovered and recirculated. Because of the “blow-by” phenomena which occurs as the pistons compress the gas, some gas leaks past the pistons and rings and tends to pressurize the crankcase. As this gas is vented back to the suction chamber, it carries oil mist through the vent hole into the suction chamber where they mix with the gas being drawn into the cylinders compressed and expelled into the system. This is undesirable for two reasons. Frist, most of such oil is lost into the refrigeration system and is no longer available in the sump for lubrication purposes. Over time, the amount of oil lost is substantial and is costly to replace. Second, such oil contaminates both the refrigerant gas and the refrigeration system and reduces system efficiency.
As a practical matter, some of the oil mist coalesces in the suction chamber and collects on the partition member but is able to drain back into the crankcase chamber through the pressure equalizer hole and into the oil sump therein. However, oil dripping or draining through the pressure equalizer hole falls onto the rotating crankshaft and is sprayed about the crankcase chamber in the form of mist causing some mist to be expelled up through the pressure equalizer hole back into the suction chamber.
For at least these reasons, therefore, it would be advantageous if a new or improved oil separation assembly could be developed that addressed one or more of the above-described concerns, and/or other concerns.
The present disclosure provides an oil separation assembly for use in a high pressure reciprocating compressor. According to embodiments of the present disclosure, the compressor comprising a suction chamber, a crankcase chamber, and at least one partition member at least partially separating the suction chamber and the crankcase chamber, the at least one partition member including at least one opening, and the oil separation assembly comprises at least one demisting structure positioned within the crankcase chamber adjacent the at least one partition member at the at least one opening; and at least one securing structure secured in operable relation with the at least one demisting structure so as to secure the at least one demisting structure relative to the opening.
In another embodiment, the present disclosure provides a high pressure reciprocating compressor. According to embodiments of the present disclosure, the high pressure reciprocating compressor comprises a suction chamber; a crankcase chamber; a partition member at least partially separating the suction chamber and the crankcase chamber and comprising at least one opening; and at least one oil separation assembly comprising a first demisting structure positioned in the crankcase chamber adjacent the partition member at the at least one opening, and at least one securing structure secured in operable relation with the first demisting structure so as to secure the first demisting structure relative to the opening.
Embodiments of the crankcase oil separation assembly and related methods are disclosed with reference to the accompanying drawings and are for illustrative purposes only. The crankcase oil separation assembly and related methods are not limited in application to the details of construction or the arrangement of the components illustrated in the drawings. The crankcase oil separation assembly and related methods are capable of other embodiments or of being practiced or carried out in other various ways. Like reference numerals are used to indicate like components. In the drawings:
In the embodiment shown, the oil separation assembly 100 includes a suction chamber-side demisting structure 40 and a crankcase chamber-side demisting structure 42. The demisting structures 40, 42 are materials or assemblies, or combinations thereof, used to enhance the removal of liquid droplets of oil from the gaseous refrigerant stream. The demisting structures 40, 42 may be the same structures or different structures.
Nonlimiting examples of suitable demisting structures include materials such as mesh-type coalescers, including wire mesh-type coalescers (e.g., steel wool), mesh-type materials made of natural or synthetic fibers, other similar mesh-like materials, serpentine channels, and steel or stainless mesh. In still further embodiments, one of the demisting structures 40, 42 may be a combination of one or more demisting materials used in combination with one or more demisting structures, such as, for example, serpentine channels packed with a demisting material such as steel wool.
In one embodiment, at least one of the demisting structures 40, 42 is a material having a thickness T40, T42. In some embodiment, the thickness of the demisting structures 40, 42, particularly when one or both of the demisting structures is a mesh-type coalescer or other material, may be specifically selected based on the size of the opening 12 and/or the capacity, performance, or other metric of the compressor.
As liquid droplets of oil pass through the demisting structures 40, 42, the liquid droplets coalesce until they are too large and/or heavy to be sustained within the demisting structures 40, 42. The coalesced oil droplets then drop into the crankcase chamber 30 and are collected in the oil sump (not shown).
The first and second demisting structures 40, 42 each have a thickness T40, T42. In the embodiment shown in
The oil separation assembly 100 further includes at least one securing structure 44 which secures the suction chamber-side demisting structure 40, crankcase chamber-side demisting structure 42 or both in position relative to the opening 12. In other words, the at least one securing structure may be a single component or assembly which is secured in operable relation with the suction chamber-side demisting structure and/or crankcase chamber-side demisting structure so as to secure the demisting structure relative to the opening 12.
For example, in the embodiment shown in
The locking stud 44c passes through the first support 44a, first demisting structure 40, the opening 12, the second demisting structure 42 and the second support 44b and, along with washers and lock nuts 44d, for example, tightens the first and second supports 44a, 44b toward one another. The first and second demisting structures 40, 42 are thereby compressed against the partition member 10 and secured in position on either side of the opening 12.
While in the embodiment shown, the first support 44a is discussed and described with respect to the suction chamber-side of the oil separation assembly and the second support 44b is discussed and described with respect to the crankcase chamber-side of the oil separation assembly, it will be understood that the first and second supports 44a, 44b may be used interchangeably as permitted.
In the embodiment shown in
To secure the demisting structure 42 in position, the oil separation assembly 100″ includes at least one securing structure 44″ which includes a first support 44a″, a second support 44b″ and a locking structure 44c″. More particularly, in the embodiment shown, the first support 44a″ is a channel-forming support which extends from the opening 12 into the crankcase chamber 30. The first support 44a″ is a tube-like structure which creates a channel into the crankcase chamber 30 around which the demisting structure may be positioned. The first support 44a″ also serves as a structure with which the locking structure 44c″ can engage. To facilitate adequate flow through the suction chamber 20 and crankcase chamber 30, and facilitate pressure equalization between the chambers 20, 30, the embodiment shown in
One advantage of the oil separation assembly described herein is that the assembly may be installed into existing reciprocating compressors. That is, existing reciprocating compressors may be retrofit with the oil separation assembly of the present disclosure. Existing reciprocating compressors may therefore exhibit the improvements in operation provided by the oil separation assembly.
To install the oil separation assembly in a reciprocating compressor, whether a new compressor or an existing compressor, a first demisting structure is provided at an opening at the partition member of the compressor on the crankcase chamber-side of the opening. If a suction chamber-side demisting structure is to be used, the second demisting is provided at the opening at the suction chamber-side of the opening. The at least one securing structure is then assembled in operable relation to the first (and, if utilized, second) demisting structure(s) to secure the demisting structure(s) in place.
In an embodiment, the at least one securing structure includes a first support, a second support and a locking structure. In such embodiment, the step of assembling the at least one securing structure in operable relation to the first (crankcase chamber-side) demisting structure includes positioning a first support in relation to the demisting structure, positioning a second support in relation to the demisting structure, and securing the first and second supports in position using a locking structure.
In an embodiment, only a crankcase chamber-side demisting material is provided. In such an embodiment, the step of assembling the at least one securing structure in operable relation to the demisting material may include, for example, positioning a first support in relation to the opening at the partition member to extend into the crankcase chamber and into the demisting material, positioning a second support in relation to the demisting material in the crankcase chamber, and securing the first and second supports together in relation to the demisting structure using a locking structure.
In an embodiment in which two demisting structures are used on opposite sides of an opening (i.e., a suction chamber-side demisting material and a crankcase chamber-side demisting material are both used), the step of assembling the at least one securing structure in operable relation to the demisting structures may include, for example, positioning a first support in relation to the suction chamber-side demisting material, positioning a second support in relation to the crankcase chamber-side demisting material, and securing the first and second supports together in relation to the demisting structure using a locking structure.
The oil separation assembly described herein addresses at least three issues. First, the oil separation assembly assists in returning oil collected in the suction chamber back to the crankcase chamber.
Second, the oil separation assembly helps to maintain a pressure equilibrium between the suction chamber and the crankcase chamber.
Third, the oil separation assembly limits the amount of oil passing through the vent holes 12 from the crankcase chamber to the suction chamber when the rotating crankshaft splashes or sprays oil that comes in contact with it.
By (1) assisting in returning oil collected in the suction chamber back to the crankcase chamber, (2) helping to maintain a pressure equilibrium between the suction chamber and crankcase chamber, and (3) limiting the amount of oil passing from the crankcase chamber to the suction chamber, the oil separation assembly decreases oil loss and therefore costs associated with operating and maintaining a reciprocating compressor.
The disclosed oil separation assembly is also easily installed in existing reciprocating compressors at existing vent holes.
Additional advantages of the oil separation assembly will be readily identified and understood by those of skill in the art.
One of skill in the art will understand that the specific measurements (e.g., height, width, diameter, etc.) of the oil separation assembly may vary based on compressor design and the dimensions of the oil separation assembly may be altered accordingly to correspond to the measurements of the compressor.
The terms “comprising,” “including,” “having,” and their derivatives, are not intended to exclude the presence of any additional component, step or procedure, whether or not the same is specifically disclosed.
Unless stated to the contrary, implicit from the context, or customary in the art, all parts and percentages are based on weight and all test methods are current as of the filing date of this disclosure.
It is specifically intended that the crankcase oil separation assembly and related methods not be limited to the embodiments and illustrations contained herein, but include modified forms of those embodiments including portion so the embodiments and combinations of elements of different embodiments as come with the scope of the following claims. In addition, the order of various steps of operation described herein can be varied. Further, numerical ranges provided herein are understood to be exemplary and shall include all possible numerical ranges situated therebetween.
Number | Date | Country | |
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62586656 | Nov 2017 | US |