The present disclosure relates to a compressor and more particularly to a compressor having a counterweight cover.
This section provides background information related to the present disclosure which is not necessarily prior art.
Cooling systems, refrigeration systems, heat-pump systems, and other climate-control systems typically include a condenser, an evaporator, an expansion device disposed between the condenser and evaporator, and a compressor circulating fluid between the condenser and the evaporator. The compressor may be one of any number of different compressors. For example, the compressor may be a reciprocating compressor or a scroll compressor that selectively circulates fluid among the various components of a cooling, refrigeration, or heat-pump system. Regardless of the particular type of compressor employed, consistent and reliable operation of the compressor is required to ensure that the cooling, refrigeration, or heat-pump system in which the compressor is installed is capable of consistently and reliably providing a cooling and/or heating effect on demand.
Compressors of the type described above often include a compression mechanism that compresses the fluid, thereby circulating the fluid within the refrigeration, cooling, or heat-pump system. Depending on the particular type of compressor, a drive shaft may be used to impart a force on and drive the compression mechanism. In order to reduce vibration of the compressor, such a drive shaft may include one or more counterweights that are sized and positioned relative to the drive shaft to rotationally balance the drive shaft. While the counterweight improves operation of the drive shaft and, thus, the compression mechanism, rotation of the counterweight may cause undesirable windage and/or oil circulation due to rotation within a shell of the compressor. Excessive oil circulation reduces the overall efficiency of the cooling, refrigeration, or heat-pump system, as oil within each system prevents optimal heat transfer within the condenser unit and evaporator unit of each system.
This section provides a general summary of the disclosure, and is not a comprehensive disclosure of its full scope or all of its features.
A counterweight cover for a compressor is provided and may include an annular body having a recess at least partially defined by an outer circumferential portion, an inner circumferential portion, and an upper portion connecting the outer circumferential portion and the inner circumferential portion. A suction baffle may be disposed on the annular body and may direct a flow of suction gas within the compressor.
A compressor is provided and may include a motor assembly at least partially supported by a main-bearing housing, a counterweight associated with the motor assembly, and a counterweight cover fixed to the main-bearing housing and at least partially covering the counterweight. At least one anti-rotation feature may prevent relative rotation between the counterweight cover and the main-bearing housing.
A compressor is provided and may include a motor assembly at least partially supported by a main-bearing housing, a counterweight associated with the motor assembly, and a counterweight cover fixed to the main-bearing housing and at least partially covering the counterweight. A suction baffle may be integrally formed with the counterweight cover and a wire guide may be integrally formed with the counterweight cover.
Further areas of applicability will become apparent from the description provided herein. The description and specific examples in this summary are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
The drawings described herein are for illustrative purposes only of selected embodiments and not all possible implementations, and are not intended to limit the scope of the present disclosure.
Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
Example embodiments will now be described more fully with reference to the accompanying drawings.
Example embodiments are provided so that this disclosure will be thorough, and will fully convey the scope to those who are skilled in the art. Numerous specific details are set forth, such as examples of specific components and devices, to provide a thorough understanding of embodiments of the present disclosure. It will be apparent to those skilled in the art that specific details need not be employed, that example embodiments may be embodied in many different forms and that neither should be construed to limit the scope of the disclosure. In some example embodiments, well-known processes, well-known device structures, and well-known technologies are not described in detail.
The terminology used herein is for the purpose of describing particular example embodiments only and is not intended to be limiting. As used herein, the singular forms “a,” “an” and “the” may be intended to include the plural forms as well, unless the context clearly indicates otherwise. The terms “comprises,” “comprising,” “including,” and “having,” are inclusive and therefore specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof.
When an element or layer is referred to as being “on,” “engaged to,” “connected to” or “coupled to” another element or layer, it may be directly on, engaged, connected or coupled to the other element or layer, or intervening elements or layers may be present. In contrast, when an element is referred to as being “directly on,” “directly engaged to,” “directly connected to” or “directly coupled to” another element or layer, there may be no intervening elements or layers present. Other words used to describe the relationship between elements should be interpreted in a like fashion (e.g., “between” versus “directly between,” “adjacent” versus “directly adjacent,” etc.). As used herein, the term “and/or” includes any and all combinations of one or more of the associated listed items.
Although the terms first, second, third, etc. may be used herein to describe various elements, components, regions, layers and/or sections, these elements, components, regions, layers and/or sections should not be limited by these terms. These terms may be only used to distinguish one element, component, region, layer or section from another region, layer or section. Terms such as “first,” “second,” and other numerical terms when used herein do not imply a sequence or order unless clearly indicated by the context. Thus, a first element, component, region, layer or section discussed below could be termed a second element, component, region, layer or section without departing from the teachings of the example embodiments.
Spatially relative terms, such as “inner,” “outer,” “beneath,” “below,” “lower,” “above,” “upper” and the like, may be used herein for ease of description to describe one element or feature's relationship to another element(s) or feature(s) as illustrated in the figures. Spatially relative terms may be intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as “below” or “beneath” other elements or features would then be oriented “above” the other elements or features. Thus, the example term “below” can encompass both an orientation of above and below. The device may be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.
With reference to
The shell assembly 12 may house the main-bearing housing assembly 14, the motor assembly 16, and the compression mechanism 18. The shell assembly 12 may generally form a compressor housing and may include a cylindrical shell 28, an end cap 30 at the upper end thereof, a transversely extending partition 32, and a base 34 at a lower end thereof. An oil sump 35 may be disposed at a lower end of the shell 28 and may provide lubricating oil to moving components of the compressor 10 such as, for example, compression mechanism 18. The end cap 30 and partition 32 may cooperate to form a discharge chamber 36 that functions as a discharge muffler for the compressor 10.
The refrigerant discharge fitting 22 may be attached to the shell assembly 12 at an opening 38 in the end cap 30. A discharge valve assembly (not shown) may be located within the discharge fitting 22 and may prevent a reverse-flow condition to prevent fluid from entering the compressor 10 via the discharge fitting 22. The suction gas inlet fitting 26 may be attached to the shell assembly 12 at an opening 40 of the shell 28 and is in fluid communication with an interior of the shell assembly 12. The partition 32 may include a discharge passage 46 therethrough providing communication between the compression mechanism 18 and the discharge chamber 36. The discharge-valve assembly could alternatively be located at or near the discharge passage 46.
Referring now to
Referring now to
The compression mechanism 18 may generally include an orbiting scroll 104 and a non-orbiting scroll 106. The orbiting scroll 104 may include an end plate 108 having a spiral vane or wrap 110 extending therefrom and an annular flat thrust surface 112. The thrust surface 112 may interface with the thrust bearing surface 66 of the main-bearing housing 52. The orbiting scroll 104 may also include a cylindrical hub 114 that projects downwardly from the thrust surface 112 and engages a drive bushing 116. The drive bushing 116 may include an inner bore in which the crank pin 84 is drivingly disposed. In one configuration, the crank pin flat 86 drivingly engages a flat surface in a portion of the inner bore of the drive bushing 116 to provide a radially compliant driving arrangement.
The non-orbiting scroll 106 may include an end plate 118 having a spiral wrap 120 extending therefrom and a discharge passage 119 extending through the end plate 118. The spiral wrap 120 may cooperate with the wrap 110 of the orbiting scroll 104 to create a series of moving fluid pockets when the orbiting scroll 104 is moved relative to the non-orbiting scroll 106. The pockets created by the spiral wraps 110, 120 decrease in volume as they move from a radially outer position to a radially inner position, thereby compressing the fluid throughout a compression cycle of the compression mechanism 18.
An Oldham coupling 117 may be positioned between orbiting scroll 104 and the main-bearing housing 52 and may be keyed to orbiting scroll 104 and non-orbiting scroll 106. The Oldham coupling 117 transmits rotational forces from the drive shaft 80 to the orbiting scroll 104 to compress a fluid disposed between the orbiting scroll 104 and non-orbiting scroll 106. Oldham coupling 117 and its interaction with orbiting scroll 104 and non-orbiting scroll 106 may be of the type disclosed in assignee's commonly-owned U.S. Pat. No. 5,320,506, the disclosure of which is incorporated herein by reference.
A lower counterweight 130 and/or an upper counterweight 132 may be associated with the motor assembly 16. In one configuration, the counterweight 132 may be fixed to the rotor 78 to facilitate balanced rotation of the drive shaft 80. In another configuration, the lower counterweight 130 and/or the upper counterweight 132 may be fixed to the drive shaft 80 instead of the rotor 78 to facilitate balanced rotation of the drive shaft 80. A lower counterweight shield or cover 134 may at least partially cover the lower counterweight 130 and an upper counterweight shield or cover 136 may at least partially cover the upper counterweight 132. The lower counterweight cover 134 may be mounted to the drive shaft 80 between the lower counterweight 130 and the oil sump 35 and may restrict oil from the oil sump 35 from splashing, splattering or otherwise flowing onto the lower counterweight 130. Preventing oil from flowing onto the lower counterweight 130 reduces viscous drag on the lower counterweight 130 and the motor assembly 16 and reduces oil circulation by shielding the oil from the windage of the lower counterweight 130. The lower counterweight cover 134 may be of the type disclosed in Assignee's commonly owned U.S. Pat. No. 5,064,356, the disclosure of which is hereby incorporated by reference.
Referring now to
The annular body 138 may include a recess 146 defined by an outer circumferential portion 148, an inner radial portion 150 and a generally flat upper portion 149. The upper portion 149 may extend between the outer circumferential portion 148 and the inner radial portion 150 and generally perpendicular thereto. The upper portion 149 may include an upper surface 153 and a lower surface 152. The inner radial portion 150 may include a plurality of resiliently flexible fingers 154 extending away from the upper portion 149. Each of the flexible fingers 154 may include an inwardly extending lip 156 that engages a groove 158 formed in the second hub portion 62 of the main-bearing housing 52 via a snap fit, for example.
As described above, the second hub portion 62 may house the first bearing 54, which rotatably supports the drive shaft 80. The upper counterweight 132 may be fixed to the drive shaft 80 and may rotate therewith at least partially within the recess 146 of the upper counterweight cover 136. In this manner, the outer circumferential portion 148 at least partially shrouds the upper counterweight 132 to reduce or prevent the upper counterweight 132 from spreading oil radially outward during rotation of the drive shaft 80. Further, the upper counterweight cover 136 shields the motor assembly 16 from fluids disposed within the compressor 10, such as oil and refrigerant, for example.
The anti-rotation features 140 may extend from the outer circumferential portion 148 and/or the upper surface 153 to the plurality of arms 58 of the main-bearing housing 52. In the particular embodiment illustrated, the upper counterweight cover 136 includes four anti-rotation features 140, each one corresponding to one of the four radially extending arms 58 of the main-bearing housing 52. Each of the anti-rotation features 140 may include a cutout 160 having a generally rectangular shape that is sized and shaped to receive a portion of the corresponding arm 58 (as shown in
While the cutouts 160 are described above as being rectangular, the cutouts 160 could alternatively be formed in any other shape, such as triangular, trapezoidal, or arcuate, for example. In other embodiments, the anti-rotation features 140 may include pegs, pins or other features that engage the arms 58 of the main-bearing housing 52 and prevent relative rotation between the upper counterweight cover 136 and the main-bearing housing 52. While the anti-rotation features 140 are described above as being integrally formed with the upper counterweight cover 136, the anti-rotation features 140 could alternatively be separate members mounted to the annular body 138, the suction baffle 142, and/or the wire guide 144.
The suction baffle 142 may include a first face 162, a second face 164, and a third face 166. The first, second and third faces 162, 164, 166 may be generally flat or curved members with the third face 166 connecting the first and second faces 162, 164. The first and second faces 162, 164 may be obtusely angled relative to the third face 166 while the third face 166 may be generally tangent to the outer circumferential portion 148 of the annular body 138. The third face 166 may be positioned at an angle relative to the opening 40 of the suction gas inlet fitting 26, such that the suction baffle 142, as a whole, may be positioned at an angle relative to the suction gas inlet fitting 26 (
The suction baffle 142 directs the flow of suction gas entering the shell 28 through the suction gas inlet fitting 26 towards a suction window 169 (
Oil mixed in with the suction gas may contact the suction baffle 142 and subsequently drip down into the oil sump 35. In another configuration, the lip 168 may extend outwardly and downwardly (relative to the view shown in
The wire guide 144 may be integrally formed with the second face 164 of the suction baffle 142 and may include a generally tubular portion 170 and a tab 172 extending therefrom. The tubular portion 170 may include a first portion 171 and a second portion 173 having a smaller diameter than the first portion 171. A distal end of the second face 164 may curl inward to form the tubular portion 170 of the wire guide 144 such that the tubular portion 170 is integrally formed with the second face 164.
The tubular portion 170 includes a first end 176 extending from the distal end of the second face 164 and a second end 178 that may be spaced less than 360 degrees apart from the first end 176 (
While the wire guide 144 is described above as being integrally formed with the second face 164, the wire guide 144 could alternatively be integrally formed with the first face or third face 162, 166. In other embodiments, the wire guide 144 may be a separate component mounted to the annular body 138, one of the anti-rotation features 140, the suction baffle 142, the stator 76, the shell 28 or any other suitable location.
Thermistor wires 180, 182 may extend between an electrical connection terminal 184 and scroll thermistor lead wires 186, 189 (
The tab 172 may be gripped by an assembly or repair technician and pulled away from the suction baffle 142 to spread the tubular portion 170 open, thereby allowing easy insertion and removal of the thermistor wires 180, 182 into and out of the tubular portion 170. While the wire guide 144 is described as positioning thermistor wires 180, 182, the wire guide 144 may also be used to route other wires within the shell 28 instead of or in addition to the thermistor wires 180, 182 such as, for example, lines supplying power to the motor assembly 16, a valve (not shown), or any other electrical device within the compressor 10.
Referring now to
The body portion 190 may include a back wall 196, side walls 198, one or more retaining members 200, a panel mount opening 202, and a rib 204 protruding from the back wall 196. The panel mount opening 202 may be defined by the back wall 196, the side walls 198, and the one or more retaining members 200. The thermistor wires 180, 182 may be routed from the tubular portion 170 of the wire guide 144 up through the body portion 190 of the thermistor wire guard 188. The panel mount opening 202 may receive and securely retain the first connector 185 via a snap-fit engagement, for example. The collar 192 may locate and guide the second connector 187 into engagement with the first connector 185, and prevent improper engagement therebetween.
The rib 204 may engage an inner surface the shell 28 (
The mounting stud 194 may be integrally formed with the body portion 190 and may include a stud portion 206 and a head portion 208. The stud portion 206 may be slip-fit or otherwise received into the wire guard mounting aperture 71 in the main-bearing housing 52 to fix and position the thermistor wire guard 188 relative to the main-bearing housing 52. The head portion 208 may facilitate installation of the mounting stud 194 onto the main-bearing housing 52 and may provide a stop to engage the non-orbiting scroll 106, thereby preventing disengagement between the mounting stud 194 and the main-bearing housing 52.
The scroll thermistor lead wires 186, 189 may extend between the second connector 187 and a scroll thermistor 210, which may be connected to the non-orbiting scroll 106. The scroll thermistor 210 may communicate with the discharge passage 119 (
A lanyard 212 may be employed to prevent any slack in the scroll thermistor lead wires 186, 189 from contacting the shell 28, thereby preventing insulation on the scroll thermistor lead wires 186, 189 from being damaged while the end cap 30 is welded onto the shell 28. The lanyard 212 may be formed from nylon or other polymeric material and may include a body portion 214, a clip 216, and a flag 218. The body portion 214 may include a mounting aperture 215 engaging the scroll thermistor 210 generally between a head 220 of the thermistor 210 and the non-orbiting scroll 106. In the configuration shown in
The clip 216 may be a generally C-shaped member extending from the body portion 214. The clip 216 may include a slot 222 in communication with a clip aperture 224. The scroll thermistor lead wires 186, 189 may be received through the slot 222 and into the clip aperture 224, thereby retaining the scroll thermistor lead wires 186, 189 in place and preventing contact between the scroll thermistor lead wires 186, 189 and the shell 28.
The flag 218 may extend from the body portion 214 and may be disposed approximately 180 degrees apart from the clip 216. The flag 218 may be in an engaged position (shown in
The foregoing description of the embodiments has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the invention. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the invention, and all such modifications are intended to be included within the scope of the invention.
This application claims the benefit of U.S. Provisional Application No. 61/232,626 filed on Aug. 10, 2009. The entire disclosure of the above application is incorporated herein by reference.
Number | Date | Country | |
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61232626 | Aug 2009 | US |