1. Field of the Invention
The present invention relates to scroll compressors and, particularly, to a baffle member for a scroll compressor.
2. Description of the Related Art
Compressors generally have mating axially or radially loaded surfaces, such as the interfacing surfaces of thrust bearings and radial bearings. For example, in a scroll compressor, the orbiting scroll member orbits upon a thrust surface that is formed as a portion of the crankcase of the compressor. These surfaces tend to experience high wear and usually require a substantial amount of lubrication. The retention of lubricant on the interfacing bearing surface is often facilitated by the use of recesses, grooves, or clearances spaces on the interfacing surface. When the compressor is operating at high speeds, some of the lubricant on the bearing surface may be thrown outwardly from the bearing surface, and there is a need to contain such lubricant.
The present invention provides a baffle member for use in scroll compressors. In one exemplary embodiment, the baffle member is attached to a portion of the crankcase and, in use, deflects lubricant that may be thrown from the thrust surface of the crankcase during operation of the compressor away from the flow of working fluid, and also aids in directing the flow of working fluid away from the thrust surface of the crankcase and toward a suction inlet in the compression mechanism.
In one exemplary embodiment, the baffle member includes a body portion having an inclined surface. The body portion is positioned atop an upper surface of the crankcase, such that the body portion of the baffle member is positioned above the thrust surface of the crankcase. In one exemplary embodiment, the inclined surface of the baffle member terminates at a position that is spaced from an upper surface of the crankcase. The inclined surface of the baffle member acts to direct working fluid traveling from a suction port of the compressor over the inclined surface, away from the thrust surface of the crankcase, and toward the suction inlet of the compression mechanism, such that the working fluid substantially bypasses any lubricant that may be thrown from the thrust surface of the crankcase. As a result, lubricant that may be thrown radially outwardly from the thrust surface is prevented from being entrained in the working fluid and the efficiency of the compressor is increased.
In one exemplary embodiment, the body portion of the baffle member is positioned atop a rib of the crankcase that is adjacent to the thrust surface of the crankcase. In this embodiment, the body portion of the baffle member acts to deflect any lubricant that may be thrown from the thrust surface of the crankcase during operation of the compressor. Specifically, the body portion of the baffle member may extend to a height in an axial direction that is greater than the height of the thrust surface of the crankcase in an axial direction. As a result, the body portion of the baffle member acts as a barrier to the passage of lubricant thrown from the thrust surface of the crankcase and prevents the lubricant from entering the flow path of working fluid traveling into the compression mechanism. Stated another way, lubricant that is thrown from the thrust surface of the crankcase that would normally pass over the rib of the crankcase contacts the body portion of the baffle member instead, which deflects the lubricant.
The baffle member is also removably attached to the crankcase such that the baffle member may be selectively used with a crankcase depending on whether the added benefits of the baffle member are desirable. For example, in a variable speed compressor, the baffle member may be desirable when the compressor is operated at a relatively high speeds, in which lubricant is more likely to be thrown radially outwardly from the thrust surface. In contrast, if the compressor is a single speed compressor and is configured to operate at a relatively low speed, the baffle member may not be needed, allowing assembly of the compressor without the baffle member. This modularity reduces manufacturing costs by allowing a single crankcase design to be used with multiple compressor configurations and also decreases the overall manufacturing cost by eliminating the need to tool and manufacture crankcases of different designs.
In one form thereof, the present invention provides a vertical scroll compressor defining perpendicular axial and radial directions, including a housing having a suction port; a compression mechanism disposed within said housing and including a non-orbiting scroll having a first involute wrap and an orbiting scroll having a second involute wrap; a motor drivingly connected to said orbiting scroll; a crankcase including a thrust surface disposed at an axial thrust surface height, said thrust surface having a plurality of lubricant retaining recesses formed therein and said orbiting scroll bearingly supported on said thrust surface; and a baffle member removably positioned on said crankcase and disposed radially between said thrust surface and said suction port, said baffle member having a body portion with an upper surface disposed at an axial baffle member height, said baffle member height being greater than said thrust surface height, whereby said baffle member extends above said support surface of said crankcase.
In another form thereof, the present invention provides a vertical scroll compressor defining perpendicular axial and radial directions, including a housing having a suction port; a compression mechanism disposed within said housing and including a non-orbiting scroll having a first involute wrap and a suction inlet, and an orbiting scroll having a second involute wrap; a motor drivingly connected to said orbiting scroll; a crankcase including a thrust surface disposed at an axial thrust surface height, said orbiting scroll bearingly supported on said thrust surface; and a baffle member removably positioned on said crankcase and disposed radially between said thrust surface and said suction port, said baffle member having a body portion including an inclined surface disposed at least partially axially above said crankcase, said inclined surface positioned within a flow path of working fluid from said suction port to said suction inlet.
The above-mentioned and other features and advantages of this invention, and the manner of attaining them, will become more apparent and the invention itself will be better understood by reference to the following description of an embodiment of the invention taken in conjunction with the accompanying drawings, wherein:
Corresponding reference characters indicate corresponding parts throughout the several views. The exemplification set out herein illustrates one preferred embodiment of the invention, in one form, and such exemplification is not to be construed as limiting the scope of the invention in any manner.
Referring to
Motor 22 and compression mechanism 23 generally include first, non-orbiting scroll 24, second, orbiting scroll 26, crankcase 28, crankshaft 30, stator 32, rotor 34, and outboard bearing assembly 36. Separator plate 18 is secured around its perimeter to the interior of housing 12, such as by welding, and divides the interior of the housing 12 into a relatively low pressure suction chamber 38 that is in fluid communication with suction port 40 in housing 12, and a relatively high pressure discharge chamber 42 in fluid communication with discharge port 44 in top cap 20.
Non-orbiting scroll 24 is secured to separator plate 18, such as by a plurality of bolts, and includes outer wall 46 extending from base plate 48, and involute wrap 50 extending from base plate 48 and disposed inwardly of outer wall 46. Non-orbiting scroll 24 further includes a plurality of mount flanges 52 spaced radially about the end of outer wall 46 opposite base plate 48, and a plurality of bolts (not shown) secure mount flanges 52 to crankcase 28. Crankcase 28 includes main bearing 54 in which the upper portion of crankshaft 30 is rotatably supported. Stator 32 is fixed within housing 12 by a plurality of bolts (not shown) which pass through outboard bearing assembly 36, stator 32, and into crankcase 28. Crankshaft 30 is secured to rotor 34 in a suitable manner, and outboard bearing assembly 36 includes outboard bearing 56 which supports a lower end of crankshaft 30. The upper portion of crankshaft 30 includes an eccentric end mounted within annular hub 58 extending downwardly from base plate 60 of orbiting scroll 26. Orbiting scroll 26 additionally includes involute wrap 62 extending upwardly from base plate 60 thereof, which is in meshing relationship with wrap 50 of non-orbiting scroll 24. Oldham coupling 64 is operatively coupled between orbiting scroll 26 and crankcase 28 to prevent rotation of orbiting scroll 24, as is known.
In operation, electrical energization of stator 32 of motor 22 rotatably drives rotor 34 of motor 22 and crankshaft 30 to move orbiting scroll 26 in an orbiting manner with respect to non-orbiting scroll 24. A working fluid, such as a refrigerant, at suction pressure is drawn from suction chamber 38 into suction inlet 66 of non-orbiting scroll 24, and is compressed within the plurality of variable volume, working pockets which are defined between wraps 50 and 62 of fixed and orbiting scrolls 24 and 26, respectively, in a known manner, as orbiting scroll 26. The compressed working fluid is then discharged through discharge outlet 68 in base plate 48 of non-orbiting scroll 24, through discharge check valve assembly 70, and into discharge chamber 42 at a discharge pressure.
More specifically, referring to
Referring to
During orbital movement of orbiting scroll 26, orbiting scroll 26 is supported by thrust surface 74 of crankcase 28. Due to the forces experienced at thrust surface 74 during orbital movement of orbiting scroll 26, particularly during relatively high operating speeds of the compressor, a relatively large amount of lubricant may be needed between base plate 60 of orbiting scroll 26 and thrust surface 74 of crankcase 28 to facilitate the orbital movement of orbiting scroll 26. To contain and accommodate a relative higher amount of lubricant, thrust surface 74 of crankcase 28 may include a plurality of recesses, such as recesses 76, shown more clearly in
However, when compressor 10 is operating, particularly at high speeds, a portion of the lubricant received within recesses 76 and atop thrust surface 74 may be thrown radially outwardly from thrust surface 74 toward the inner surface of main housing 12 of compressor 10. In this manner, because the working fluid flows upwardly past thrust surface 74 as shown by arrow A4 in
Referring to
As shown in
In order to reduce the potential for lubricant becoming entrained in the flow of suction pressure working fluid traveling to suction inlet 66 of non-orbiting scroll 24 and to help direct the flow of suction pressure working fluid into suction inlet 66 of non-orbiting scroll 24, a removeable baffle member 86, shown in
Referring to
Referring to
Additionally, when baffle member 86 is positioned on rib 78 of crankcase, body portion 88 of baffle member 86 extends above support surface 102 of rib 78. Specifically, baffle member 86 and, more specifically, upper surface 104 of body portion 88 thereof, is disposed at a baffle member height BH (
Specifically, as illustrated by arrow L in
In other exemplary embodiment, shown in
Referring to
In exemplary embodiments, inclined surface 90 extends from a point that is substantially coplanar with support surface 102 of rib 78 and terminates at a point that is spaced vertically from support surface 102 of rib 78 by added height AH. Additionally, inclined surface 90 may extend between inner surface 80 and outer surface 100 of rib 78. As shown in
Advantageously, by using baffle member 86, the potential for lubricant that is radially thrown from thrust surface 74 to become entrained in the flow of suction pressure working fluid is substantially reduced or eliminated. Additionally, the use of baffle member 86 also improves the efficiency of compressor 10 by aiding to direct the flow of suction pressure working fluid into suction inlet 66 of non-orbiting scroll 24.
Furthermore, by providing baffle member 60 as a removable component capable of independent assembly to crankcase 28, a single design of crankcase 28 may be used with multiple configurations of compressor 10 and baffle member 86 may be added only when the additional benefits provided by baffle member 86 are desired. For example, in a variable speed compressor that may operate at relatively high speeds, the velocity of the lubricant and/or amount of lubricant that is thrown from thrust surface 72 may be relatively great and the use of baffle member 86 may be desirable. In contrast, in a single speed compressor that is operated at a substantially low speed, the velocity of the lubricant and/or the amount of lubricant that is thrown from thrust surface 72 may be relatively less and baffle member 86 may not be needed. This modularity reduces manufacturing costs by allowing a single crankcase 28 to be used with multiple compressor configurations and decreases the overall manufacturing cost by eliminating the need to tool and manufacture crankcases 28 of different designs.
While the baffle member of the present invention is described in detail with specific reference to crankcase 28 and compressor 10, the baffle member of the present invention may be used in conjunction with other compressor and/or crankcase designs. Additionally, while this invention has been described as having a preferred design, the present invention can be further modified within the spirit and scope of this disclosure. This application is therefore intended to cover any variations, uses, or adaptations of the invention using its general principles. Further, this application is intended to cover such departures from the present disclosure as come within known or customary practice in the art to which this invention pertains and which fall within the limits of the appended claims.
This application claims the benefit under Title 35 U.S.C. § 119(e) of U.S. Provisional Patent Application Ser. No. 61/061,899, entitled LUBRICANT BAFFLE FOR SCROLL COMPRESSORS, filed on Jun. 16, 2008, the entire disclosure of which is expressly incorporated by reference herein.
Number | Date | Country | |
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61061899 | Jun 2008 | US |