CA2325752A1 - Oiless rotary scroll air compressor tipseal assembly - Google Patents
Oiless rotary scroll air compressor tipseal assembly Download PDFInfo
- Publication number
- CA2325752A1 CA2325752A1 CA002325752A CA2325752A CA2325752A1 CA 2325752 A1 CA2325752 A1 CA 2325752A1 CA 002325752 A CA002325752 A CA 002325752A CA 2325752 A CA2325752 A CA 2325752A CA 2325752 A1 CA2325752 A1 CA 2325752A1
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- Canada
- Prior art keywords
- stationary
- orbiting
- tipseal
- scroll
- compressible
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C27/00—Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
- F04C27/005—Axial sealings for working fluid
Abstract
A tipseal assembly for a rotary scroll compressor is disclosed. The rotary scroll compressor has a stationary scroll element with a stationary spiral flange and an orbiting scroll element with an orbiting spiral flange. An orbital drive mechanism drives the orbiting scroll element in an orbit about the stationary scroll element, and a non-rotation bearing device maintains the orbiting scroll element substantially non-rotational with respect to the stationary scroll element.
The stationary and orbiting spiral flanges are intermeshed and nested with one another to form at least one spiraling compression pocket therebetween. The tipseal assembly forms a substantially airtight seal between at least one of the stationary and orbiting spiral flanges and the base of the other scroll element. The tipseal assembly includes an inwardly extending groove formed in an end surface of at least one of the stationary and orbiting spiral flanges, a compressible element disposed within and along the groove and a tipseal overlaying the compressible element. Preferably, the tipseal element extends beyond the end surface when the compressible element is in an uncompressed state, the tipseal element includes at least one of a non-metallic substance, a fluorosint material and a PTFE based product and the compressible element includes at least one of an elastomeric material, a silicone rubber material and a high temperature resistant O-ring material.
The stationary and orbiting spiral flanges are intermeshed and nested with one another to form at least one spiraling compression pocket therebetween. The tipseal assembly forms a substantially airtight seal between at least one of the stationary and orbiting spiral flanges and the base of the other scroll element. The tipseal assembly includes an inwardly extending groove formed in an end surface of at least one of the stationary and orbiting spiral flanges, a compressible element disposed within and along the groove and a tipseal overlaying the compressible element. Preferably, the tipseal element extends beyond the end surface when the compressible element is in an uncompressed state, the tipseal element includes at least one of a non-metallic substance, a fluorosint material and a PTFE based product and the compressible element includes at least one of an elastomeric material, a silicone rubber material and a high temperature resistant O-ring material.
Description
OILESS ROTARY SCROLL AIR COMPRESSOR TIPSEAL ASSEMBLY
CROSS-REFERENCES TO RELATED AI?PLICATIONS
The present application is directed to similar subject matter as is disclosed in the following U.S Patent Applications:
"Oiless Rotary Scroll Air Compressor Crankshaft Assembly", U.S. Patent Application Serial No. , filed on by Michael V. Kazakis and Charlie E. Jones;
"Oiless Rotary Scroll Air Compressor Antirotation Assembly", U.S. Patent Application Serial. No. , filed on by Michael V. Kazakis and Charlie E. Jones;
"Oiless Rotary Scroll Air Compressor Antirotation Lubrication Mechanism", U.S. Patent Application Serial No.
filed on by Michael V. Kazakis and Charlie E. Jone s "Oiless Rotary Scroll Air Compressor Axial Loading Support for Orbiting Member", U.S. Patent Application Serial No.
filed on by Michael V. Kazakis and Charlie E. Jones; and "Oiless Rotary Scroll Air Compressor Air Inlet Valve", U.S. Patent Application Serial No. , filed on by Michael V. Kazakis and Charlie E. Jones.
The subject matter disclosed in each of the above cross-referenced copending U.S. patent applications is hereby expressly incorporated by reference with the same effect as if fully set forth herein.
FIELD OF THE INVENTION
The present invention relates, in general, to scroll compressors which are used to compress a fluid, for example, a gas such as a refrigerant for cooling purposes or ambient air in order to furnish a compressed air supply.
More particularly, the present invention relates to a tipseal assembly for use in such a rotary scroll compressor.
BACKGROUND OF THE INVENTION
So-called ~~scroll" compressors have achieved wider application recently, particularly in the fields of refrigeration and air conditioning, due to a number of advantages which they possess over reciprocating type compressors. Among these advantages are: low operating sound levels; reduction in "wear parts" such as compression valves, pistons, piston rings and cylinders (resulting in reduced maintenance); increased efficiency as versus reciprocating compressor designs; and cooler operating temperatures.
DESCRIPTION OF THE RELATED ART
While the number of wear parts in a scroll compressor may be reduced in comparison to a reciprocating type compressor, there are still a number surfaces which move relative to one another and lubrication between these surfaces cannot be ignored. One design for a refrigerant scroll compressor utilizes an oil sump located in the lowermost portion of the compressor housing and an oil pump which draws oil from the sump upward to lubricate the moving parts of the compressor.
The oil used as a lubricant in such a design is relatively free to mix with the air which is being compressed. Lubricating oil which becomes suspended in the refrigerant is, for the most part, separated therefrom by changing the direction of flow of the refrigerant and by impinging the refrigerant on surfaces located within the compressor. After it is separated, the oil is then drained back to the oil sump.
However, due to the gas having been relatively free to mix with the oil lubricant, the compressed gas exiting the scroll compressor may still have a relatively high degree of oil content. Such oil content may carry over to the compressed gas supply system and have deleterious effects such as reduced life of air driven mechanisms (e. g., air driven tools, brakes, etc.) which utilize the compressed gas supply as a power source.
OBJECTS OF THE INVENTION
One object of the present invention is the provision of a rotary scroll compressor which is "oilers" in the sense that the lubricant used to lubricate the various moving parts of the compressor is not intermingled with the gas being compressed.
CROSS-REFERENCES TO RELATED AI?PLICATIONS
The present application is directed to similar subject matter as is disclosed in the following U.S Patent Applications:
"Oiless Rotary Scroll Air Compressor Crankshaft Assembly", U.S. Patent Application Serial No. , filed on by Michael V. Kazakis and Charlie E. Jones;
"Oiless Rotary Scroll Air Compressor Antirotation Assembly", U.S. Patent Application Serial. No. , filed on by Michael V. Kazakis and Charlie E. Jones;
"Oiless Rotary Scroll Air Compressor Antirotation Lubrication Mechanism", U.S. Patent Application Serial No.
filed on by Michael V. Kazakis and Charlie E. Jone s "Oiless Rotary Scroll Air Compressor Axial Loading Support for Orbiting Member", U.S. Patent Application Serial No.
filed on by Michael V. Kazakis and Charlie E. Jones; and "Oiless Rotary Scroll Air Compressor Air Inlet Valve", U.S. Patent Application Serial No. , filed on by Michael V. Kazakis and Charlie E. Jones.
The subject matter disclosed in each of the above cross-referenced copending U.S. patent applications is hereby expressly incorporated by reference with the same effect as if fully set forth herein.
FIELD OF THE INVENTION
The present invention relates, in general, to scroll compressors which are used to compress a fluid, for example, a gas such as a refrigerant for cooling purposes or ambient air in order to furnish a compressed air supply.
More particularly, the present invention relates to a tipseal assembly for use in such a rotary scroll compressor.
BACKGROUND OF THE INVENTION
So-called ~~scroll" compressors have achieved wider application recently, particularly in the fields of refrigeration and air conditioning, due to a number of advantages which they possess over reciprocating type compressors. Among these advantages are: low operating sound levels; reduction in "wear parts" such as compression valves, pistons, piston rings and cylinders (resulting in reduced maintenance); increased efficiency as versus reciprocating compressor designs; and cooler operating temperatures.
DESCRIPTION OF THE RELATED ART
While the number of wear parts in a scroll compressor may be reduced in comparison to a reciprocating type compressor, there are still a number surfaces which move relative to one another and lubrication between these surfaces cannot be ignored. One design for a refrigerant scroll compressor utilizes an oil sump located in the lowermost portion of the compressor housing and an oil pump which draws oil from the sump upward to lubricate the moving parts of the compressor.
The oil used as a lubricant in such a design is relatively free to mix with the air which is being compressed. Lubricating oil which becomes suspended in the refrigerant is, for the most part, separated therefrom by changing the direction of flow of the refrigerant and by impinging the refrigerant on surfaces located within the compressor. After it is separated, the oil is then drained back to the oil sump.
However, due to the gas having been relatively free to mix with the oil lubricant, the compressed gas exiting the scroll compressor may still have a relatively high degree of oil content. Such oil content may carry over to the compressed gas supply system and have deleterious effects such as reduced life of air driven mechanisms (e. g., air driven tools, brakes, etc.) which utilize the compressed gas supply as a power source.
OBJECTS OF THE INVENTION
One object of the present invention is the provision of a rotary scroll compressor which is "oilers" in the sense that the lubricant used to lubricate the various moving parts of the compressor is not intermingled with the gas being compressed.
Thus, there is no contamination to the compressed gas due to the lubricant, and additional special provisions or designs need not be utilized for separating the lubricant from the compressed gas prior to using the compressed gas.
Another object of the present invention is the provision of a novel and inventive tipseal assembly for a rotary scroll compressor which forms a substantially airtight seal between at least one, preferably both, of the spiral flanges therein and the base member of the opposing scroll element.
A further object of the present invention is the provision of such a tipseal assembly for a rotary scroll compressor which is inexpensive to manufacture and reliable in operation.
In addition to the objects and advantages of the present invention described above, various other objects and advantages of the invention will become more readily apparent to those persons skilled in the relevant art from the following more detailed description of the invention, particularly when such description is taken in conjunction with the attached drawing Figures and with the appended claims.
SUMMARY OF THE INVENTION
In one aspect, the invention generally features a tipseal assembly for a scroll compressor, the scroll compressor including a housing, a stationary scroll element mounted within the housing substantially stationary with respect to the housing, the stationary scroll element ;-ncluding a stationary spiral flange, an orbiting scroll element disposed within the housing, the orbiting scroll element _including an orbiting spiral flange, each of the stationary and orbiting scroll elements having a central axis, the stationary and orbiting spiral flanges being intermeshed and nested with one another to define a spiraling compression pocket therebetween, an orbital drive mechanism for driving the central axis of the orbiting scroll element in an orbit about the central axis of the stationary scroll element while maintaining the orbiting scroll element substantially non-rotational with respect to the stationary scroll element, the tipseal assembly including an inwardly extending groove formed in an end surface of at least one of the stationary and orbiting spiral flanges, a compressible element disposed substantially within and along at least a portion of a length of the inwardly extending groove formed in the end surface of the at least one of the stationary and orbiting spiral flanges and a tipseal element overlaying the compressible element and disposed at least partially within the inwardly extending groove formed in the end surface of the at least one of the stationary and orbiting spiral flanges.
In another aspect, the invention generally features an improvement in a rotary scroll compressor of the type described, the improvement including a t:ipseal assembly which includes an inwardly extending groove formed in an end surface of one of the spiral flanges, a compressible element disposed within the inwardly extending groove and a tipseal element overlaying the compressible element and being disposed at least partially within the groove.
In yet another aspect, the invention generally features a scroll compressor having a tipseal assembly and including a housing, a stationary scroll element mounted within the housing substantially stationary with respect to the housing, the stationary scroll element including a stationary spiral flange, an orbiting scroll element disposed within the housing, the orbiting scroll element including an orbiting spiral flange, each of the stationary and orbiting scroll elements having a central axis, the stationary and orbiting spiral flanges being intermeshed and nested with one another to define a spiraling compression pocket therebetween, an orbital drive mechanism for driving the central axis of the orbiting scroll element in an orbit about the central axis of the stationary scroll element while maintaining the orbiting scroll element substantially non-rotational with respect to the stationary scroll element and a tipseal assembly for forming a substantially airtight seal, the tipseal assembly including an inwardly extending groove formed in an end surface of at least one of the stationary and orbiting spiral flanges, a compressible element disposed substantially within and along at least a portion of a length of the inwardly extending groove formed in the end surface of the at least one of the stationary and orbiting spiral flanges and a tipseal element overlaying the compressible element and disposed at least partially within the inwardly extending groove.
The present invention will now be described by way of a particularly preferred embodiment, reference being made to the various Figures of the accompanying drawings, wherein:
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is perspective view of an oiless rotary scroll compressor, constructed according to the present invention.
Fig. 2 is an exploded isometric view of the inventive oiless rotary scroll compressor.
Fig. 3 is a cross sectional elevational view of the inventive oiless rotary scroll compressor.
Fig. 4 is another cross sectional elevational view of the inventive oiless rotary scroll compressor, taken along a section rotated approximately 90° from the section of Fig. 3.
Fig. 5 is a cross sectional plan view of the inventive oiless rotary scroll compressor.
Fig. 6 is an exploded isometric view of a crankshaft used in the inventive oiless rotary scroll compressor.
Another object of the present invention is the provision of a novel and inventive tipseal assembly for a rotary scroll compressor which forms a substantially airtight seal between at least one, preferably both, of the spiral flanges therein and the base member of the opposing scroll element.
A further object of the present invention is the provision of such a tipseal assembly for a rotary scroll compressor which is inexpensive to manufacture and reliable in operation.
In addition to the objects and advantages of the present invention described above, various other objects and advantages of the invention will become more readily apparent to those persons skilled in the relevant art from the following more detailed description of the invention, particularly when such description is taken in conjunction with the attached drawing Figures and with the appended claims.
SUMMARY OF THE INVENTION
In one aspect, the invention generally features a tipseal assembly for a scroll compressor, the scroll compressor including a housing, a stationary scroll element mounted within the housing substantially stationary with respect to the housing, the stationary scroll element ;-ncluding a stationary spiral flange, an orbiting scroll element disposed within the housing, the orbiting scroll element _including an orbiting spiral flange, each of the stationary and orbiting scroll elements having a central axis, the stationary and orbiting spiral flanges being intermeshed and nested with one another to define a spiraling compression pocket therebetween, an orbital drive mechanism for driving the central axis of the orbiting scroll element in an orbit about the central axis of the stationary scroll element while maintaining the orbiting scroll element substantially non-rotational with respect to the stationary scroll element, the tipseal assembly including an inwardly extending groove formed in an end surface of at least one of the stationary and orbiting spiral flanges, a compressible element disposed substantially within and along at least a portion of a length of the inwardly extending groove formed in the end surface of the at least one of the stationary and orbiting spiral flanges and a tipseal element overlaying the compressible element and disposed at least partially within the inwardly extending groove formed in the end surface of the at least one of the stationary and orbiting spiral flanges.
In another aspect, the invention generally features an improvement in a rotary scroll compressor of the type described, the improvement including a t:ipseal assembly which includes an inwardly extending groove formed in an end surface of one of the spiral flanges, a compressible element disposed within the inwardly extending groove and a tipseal element overlaying the compressible element and being disposed at least partially within the groove.
In yet another aspect, the invention generally features a scroll compressor having a tipseal assembly and including a housing, a stationary scroll element mounted within the housing substantially stationary with respect to the housing, the stationary scroll element including a stationary spiral flange, an orbiting scroll element disposed within the housing, the orbiting scroll element including an orbiting spiral flange, each of the stationary and orbiting scroll elements having a central axis, the stationary and orbiting spiral flanges being intermeshed and nested with one another to define a spiraling compression pocket therebetween, an orbital drive mechanism for driving the central axis of the orbiting scroll element in an orbit about the central axis of the stationary scroll element while maintaining the orbiting scroll element substantially non-rotational with respect to the stationary scroll element and a tipseal assembly for forming a substantially airtight seal, the tipseal assembly including an inwardly extending groove formed in an end surface of at least one of the stationary and orbiting spiral flanges, a compressible element disposed substantially within and along at least a portion of a length of the inwardly extending groove formed in the end surface of the at least one of the stationary and orbiting spiral flanges and a tipseal element overlaying the compressible element and disposed at least partially within the inwardly extending groove.
The present invention will now be described by way of a particularly preferred embodiment, reference being made to the various Figures of the accompanying drawings, wherein:
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is perspective view of an oiless rotary scroll compressor, constructed according to the present invention.
Fig. 2 is an exploded isometric view of the inventive oiless rotary scroll compressor.
Fig. 3 is a cross sectional elevational view of the inventive oiless rotary scroll compressor.
Fig. 4 is another cross sectional elevational view of the inventive oiless rotary scroll compressor, taken along a section rotated approximately 90° from the section of Fig. 3.
Fig. 5 is a cross sectional plan view of the inventive oiless rotary scroll compressor.
Fig. 6 is an exploded isometric view of a crankshaft used in the inventive oiless rotary scroll compressor.
Fig. 7 is a cross sectional elevational view of the crankshaft of Fig 6.
Fig. 8 is an exploded isometric view of an anti-rotation bearing employed in the inventive oiless rotary scroll compressor.
Fig. 9 is a cross sectional view of the anti-rotation bearing of Fig. 8.
Fig. 10 is a cross sectional elevational view of an angular contact bearing assembly which is preferably utilized in the anti-rotation bearing of Figs. 8 and 9.
Fig. 11 is a cross sectional view through an orbiting spiral flange and a stationary spiral flange of the inventive oiless rotary scroll compressor, showing a novel tipseal assembly for providing a substantially airtight seal therebetween.
Fig. 12 is an isometric view of a tipseal element utilized in the tipseal assembly of Fig. 11.
Fig. 13 is an enlarged view of a portion of the elevational cross section of Fig. 4, most particularly showing an air inlet valve assembly used to provide ambient air to be compressed to the inventive oiless rotary scroll compressor;
Fig. 14 is a cross sectional elevational view of an alternative embodiment of the air inlet valve assembly.
Fig. 8 is an exploded isometric view of an anti-rotation bearing employed in the inventive oiless rotary scroll compressor.
Fig. 9 is a cross sectional view of the anti-rotation bearing of Fig. 8.
Fig. 10 is a cross sectional elevational view of an angular contact bearing assembly which is preferably utilized in the anti-rotation bearing of Figs. 8 and 9.
Fig. 11 is a cross sectional view through an orbiting spiral flange and a stationary spiral flange of the inventive oiless rotary scroll compressor, showing a novel tipseal assembly for providing a substantially airtight seal therebetween.
Fig. 12 is an isometric view of a tipseal element utilized in the tipseal assembly of Fig. 11.
Fig. 13 is an enlarged view of a portion of the elevational cross section of Fig. 4, most particularly showing an air inlet valve assembly used to provide ambient air to be compressed to the inventive oiless rotary scroll compressor;
Fig. 14 is a cross sectional elevational view of an alternative embodiment of the air inlet valve assembly.
Fig 15 is an exploded isometric view of the alternative air inlet assembly of Fig. 14.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
Prior to proceeding to a much more detailed description of the present invention, it should be noted that identical components which have identical functions have been identified with identical reference numerals throughout the several views illustrated in the drawing Figures for the sake of clarity and understanding of the invention.
Referring initially to Figs. 1 and '~, a scroll compressor constructed according to the present invention and generally designated by reference numeral 10 generally includes a bearing cap 12, a crankshaft 14 positioned within the bearing cap 12 and a stationary scroll 16. The stationary scroll 16 is bolted to the bearing cap 12 through a circular arrangement of bolts 18 with associated washers, lockwashers, etc. The stationary scroll 16 itself is provided with a series of radially extending fins 20 to improve the dissipation of heat therefrom. In the presently preferred embodiment, the radially extending fins 20 are preferably provided in the form of a separate bolt-on heat sink. The radially extending fins 20 could, however, be furnished integral with the stationary scroll 16. A hood 22 substantially covers the fins 20 and is provided with a forced air intake 24 through which ambient air is preferably forced toward the stationary scroll 16 and fins 20 to aid in heat dissipation. This forced air escapes through a central aperture 26 and through openings 28 and 30 provided about the periphery of the hood 22. The central aperture 26 also provides clearance for a compressed air discharge port 32 located in the center of the stationary scroll 16, while the peripheral opening 30 additionally provides clearance for an air inlet valve assembly 34 disposed on a peripheral portion of the stationary scroll 16.
The crankshaft 14 is rotationally driven within the bearing cap 12 by a rotational power source of choice. For example, when the scroll compressor 10 is to be employed to supply compressed air for a pneumatic braking system of a diesel or electric rail transportation vehicle (e. g., a train or light rail vehicle), the crankshaft 14 will typically be rotationally driven by an electric motor. The crankshaft 19 in turn drives an orbiting scroll element 3Fi in an orbital motion within the bearing cap 12. The orbiting scroll element 36 meshes with a stationary scroll element 37 (shown in Figs. 3 and 4) which is preferably formed integrally with the stationary scroll 16 and is described more fully below. The mechanism by which the orbiting scroll e7_ement 36 is driven in such orbital fashion is more clearly shown in Figs. 3, 6 and 7, to which we now turn.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
Prior to proceeding to a much more detailed description of the present invention, it should be noted that identical components which have identical functions have been identified with identical reference numerals throughout the several views illustrated in the drawing Figures for the sake of clarity and understanding of the invention.
Referring initially to Figs. 1 and '~, a scroll compressor constructed according to the present invention and generally designated by reference numeral 10 generally includes a bearing cap 12, a crankshaft 14 positioned within the bearing cap 12 and a stationary scroll 16. The stationary scroll 16 is bolted to the bearing cap 12 through a circular arrangement of bolts 18 with associated washers, lockwashers, etc. The stationary scroll 16 itself is provided with a series of radially extending fins 20 to improve the dissipation of heat therefrom. In the presently preferred embodiment, the radially extending fins 20 are preferably provided in the form of a separate bolt-on heat sink. The radially extending fins 20 could, however, be furnished integral with the stationary scroll 16. A hood 22 substantially covers the fins 20 and is provided with a forced air intake 24 through which ambient air is preferably forced toward the stationary scroll 16 and fins 20 to aid in heat dissipation. This forced air escapes through a central aperture 26 and through openings 28 and 30 provided about the periphery of the hood 22. The central aperture 26 also provides clearance for a compressed air discharge port 32 located in the center of the stationary scroll 16, while the peripheral opening 30 additionally provides clearance for an air inlet valve assembly 34 disposed on a peripheral portion of the stationary scroll 16.
The crankshaft 14 is rotationally driven within the bearing cap 12 by a rotational power source of choice. For example, when the scroll compressor 10 is to be employed to supply compressed air for a pneumatic braking system of a diesel or electric rail transportation vehicle (e. g., a train or light rail vehicle), the crankshaft 14 will typically be rotationally driven by an electric motor. The crankshaft 19 in turn drives an orbiting scroll element 3Fi in an orbital motion within the bearing cap 12. The orbiting scroll element 36 meshes with a stationary scroll element 37 (shown in Figs. 3 and 4) which is preferably formed integrally with the stationary scroll 16 and is described more fully below. The mechanism by which the orbiting scroll e7_ement 36 is driven in such orbital fashion is more clearly shown in Figs. 3, 6 and 7, to which we now turn.
The crankshaft 14 includes an elongated shaft portion 38 having a central axis of rotation 40 about which the crankshaft 14 is rotationally driven by the power source of choice. An orbiting cylindrical bearing 42 is affixed to a first distal end of the crankshaft 14 adjacent the orbiting scroll element 36. Preferably, this first distal end of the crankshaft adjacent the orbiting scroll element 36 is provided with a recessed cup portion 44 formed integrally thereon, and the orbiting cylindrical bearing 42 is disposed within the recessed cup portion 44. The orbiting scroll element 36 also has a central axis 46 and is provided caith a hub portion 48 which projects along this central axis 46 into the orbiting cylindrical bearing 42 to thereby rotationally engage the orbiting cylindrical bearing 42. The orbiting cylindrical bearing 42 is positioned such that it is radially offset from the central axis of rotation of the crankshaft by a distance r, with the result that the orbiting cylindrical bearing 42, the hub portion 48 and the orbiting scroll element 36 itself are all driven by the crankshaft 14 in an orbital motion having a radius of orbit equal to r about the central axis 40 of the crankshaft 14.
In order to provide lubrication access to the orbiting cylindrical bearing 42, the crankshaft 14 is provided with a lubricating channel 50 which extends from its second and opposite distal end to a point adjacent the orbiting cylindrical bearing 92. Preferably, as shown, the lubricating channel 50 extends along the central axis 40 of the crankshaft member 14 to the recessed cup portion 44. Provision of the lubricating channel 50 allows the orbiting cylindrical bearing 42 to be lubricated from a readily accessible single vantage point, namely, the second distal end of the crankshaft 14, during maintenance.
The lubricating channel 50 also serves another function during assembly of the scroll compressor 10. More particularly, during assembly, the hub portion 48 of the of the orbiting scroll element 36 enters the orbiting bearing 42.
During this step, the lubricating channel 50 serves as a vent, allowing any air that would be otherwise trapped to be vented.
The crankshaft 14 is additionally preferably furnished with a counterweight portion 52 that extends radially from the shaft portion 38 in a direction opposite to the radial offset r of the orbiting cylindrical bearing 42 from the central axis 40 of the crankshaft 14. The crankshaft. 14 is rotationally mounted within the bearing cap 12 through the provision of a main crankshaft bearing 54 and a rear crankshaft bearing 56.
The main crankshaft bearing 54 rotationally engages the shaft portion 38 at a point that is between the first distal end near the orbiting cylindrical bearing 92 and the second distal end of the crankshaft 19, while the rear crankshaft bearing 56 rotationally engages the shaft portion 38 at a point that is between the main crankshaft bearing 54 and the second distal end of the crankshaft 14. Both of the main and rear crankshaft bearings 54 and 56 may be, for example, of a caged roller bearing design or a caged ball bearing design. The orbiting cylindrical bearing 42 may be only of a caged roller bearing design.
The main crankshaft bearing 54 is preferably positioned within the bearing cap 12 by a main bearing sleeve 58 having a radially inwardly extending lip 60. A z-ear bearing sleeve 62 similarly serves to position the rear crankshaft bearing 56 within the bearing cap 12. As seen most clearly in Figs. 6 and 7, a crankshaft locknut member 6:3 urges a crankshaft lockwasher member 64 into contact with a rear surface of the crankshaft rear bearing 56. The rear bearing sleeve 62 is provided with an inwardly extending ledge 65. A snap ring 67 (shown most clearly in Figs. 9 and 7) snaps into an groove encircling the exterior face of the rear crankshaft bearing 56.
The snap ring 67 limits axial movement of the crankshaft 19 in an upward direction (as seen in Fig. 4), thereby locking the crankshaft axially within the bearing cap 12.
As shown in Figs. 3 and 7, the recessed cup portion 44 is provided with an annular ledge 66 spaced away from the bottom of the recessed cup portion 99. The orbiting cylindrical bearing 42 rests on this annular ledge 66 to thus create a lubrication reservoir 68 beneath the orbiting cylindrical bearing 42, the lubrication reservoir 68 being connected to the lubrication channel 50. An orbiting seal 93 overlays the orbiting cylindrical bearing 42 within the recessed cup portion 44.
The orbiting scroll element 36 includes an orbiting base member 70 and an orbiting spiral flange 72 projecting outward therefrom. In order to provide the stationary scroll element 37 referred to above, the stationary scroll 16 is in turn provided with a preferably integrally formed stationary spiral flange 79 which projects outward from the stationary scroll 16 and has a common central axis 40 with the crankshaft 14. As seen most clearly in Figs. 3 and 5, the stationary and orbiting spiral flanges 74 and 72, respectively, are intermeshed and nested with one another. For those not familiar with the manner in which compression is achieved in a scroll-type compressor, the compression mechanics may be difficult to visualize. However, for those of ordinary skill in the scroll-type compressor arts, the compression mechanics are well understood. In brief, the stationary scroll flange 74, being affixed to or an integrally formed portion of the stationary scroll 16, is maintained stationary. The orbiting scroll flange 72 executes an orbit of radius r with respect to the stationary scroll flange 74 and, during such orbiting motion, is maintained substantially non-rotational with respect to the stationary scroll flange 74. In other words, one may picture the stationary scroll flange 74 as having a stationary central axis z(stationary) 40, as well as remaining orthogonal coordinates x(stationary) and y(stationary) lying within the plane of the stationary spiral flange 74. One may also picture the orbiting spiral flange 72 as having an orbiting central axis z(orbiting) 46, as well as remaining orthogonal coordinates x(orbiting) and y(orbiting) lying within the plane of the orbiting spiral flange 72. In such case the orbiting motion which causes compression can be best described as an orbiting of the z(orbiting) central axis 46 about the z(stationary) central axis 90, while the remaining x and y axes of the stationary and orbiting spiral flanges remain in a parallel relationship to one another. In other words, the orbiting motion is accomplished with substantially no relative rotational motion occurring between the orbiting spiral flange 72 and the stationary spiral flange 74.
During such described motion, a compression pocket will be formed during each revolution of the orbiting spiral flange 72.
The compression pocket so formed will spiral toward the central area of the intermeshed stationary and orbiting spiral flanges 74 and 72, respectively, advancing and undergoing a compression step during each orbit. The number of revolutions required for a compression pocket so formed to reach a compressed air output 76 (which is located generally in the vicinity of the stationary central axis 90) depends on how many revolutions each of the stationary and orbiting spiral flanges 74 and 72, respectively, are provided with. In the present embodiment, each of the stationary and orbiting spiral flanges 74 and 72, respectively, is provided with somewhat over three revolutions. Preferably, each of the stationary and orbiting spiral flanges 74 and 72, respectively, extends over an arc of about 1350°, i.e., about 33~ evolutions.
Referring now primarily to Fig. 5, the orbiting spiral flange 72 has a radially outward terminus portion 78. As the radially outward terminus 78 portion of the orbiting spiral flange 72 separates from the corresponding portion of the stationary spiral flange 74 during each non-rotational orbit, a progressively wider gap is formed into which low pressure air is introduced from a generally peripherally located suction region 80. As the orbiting spiral flange non-rotationally orbits further, this gap is eventually closed by the contact of the terminus portion 78 with the corresponding portion of the stationary spiral flange 74. The described action forms a compression pocket which spirals inward toward the centrally located compressed air output 76 during successive orbits of the orbiting spiral flange 72. Two successive compression pockets are generally designated as 82 and 84 in Fig. 5, with the more radially inward compression pocket 84 being more highly compressed than the more radially outward compression pocket 82.
In order to prevent any relative rotational movement between the stationary and orbiting spiral flanges 74 and 72 while simultaneously permitting the orbiting of the scroll element 72 through the orbit of radius r under the influence of the orbital drive mechanism described above, the scroll compressor 10 is additionally provided with an anti-rotation device 90 most clearly seen in Figs. 3, 8 and 9, to which we now turn.
The bearing cap 12 is provided with a bearing face portion 86 (seen in Figs. 2,3,4 and 9) which is formed as an semi-annular ledge projecting radially inward from the interior surface of the bearing cap 12. The bear__ng face portion 86 is provided with a cutout 88 (seen in Fig. 2) in order to provide clearance for the counterweight portion 52 of the crankshaft 14 during assembly/disassembly. Three anti-rotation assembly assemblies 90 are arranged equidistant from and preferably equally angularly spaced around the common central axis 40 of the stationary scroll element 37 and the crankshaft 19. Thus, the three anti-rotation assembly assemblies 90 are preferably spaced at angular intervals of 120°. In the presently preferred embodiment, each of the anti-rotation assembly assemblies 90 is radially spaced outward from the common central axis 40 of the crankshaft 14 and the stationary scroll element 37 at a distance R which is preferably substantially equal to about 5 inches.
Each anti-rotation assembly 90 includes a first rotational bearing 92 which is mounted fixedly and stationary with respect to the stationary scroll element 37, preferably in a the bearing face portion 86 (as shown in figs. 3 and 9) and a second rotational bearing 94 which is mounted fixedly on the orbiting scroll element 36. Preferably, each first rotational bearing 92 is disposed in a first cavity 96 provided in the bearing face portion 86, while each second rotational bearing 94 resides in a corresponding second cavity 98 provided in the orbiting scroll element 36. Each anti-rotation assembly 90 further includes an offset crank member 100 having a first shaft portion 102 which engages the first rotational bearing 92 and a second conically tapered shaft portion 109 which engages a similarly conically tapered cavity 110 provided in a bushing member 106 which rotationally engages the second rotational bearing 94. The first and second shaft portions 102 and 104, respectively, are aligned substantially in parallel to one another and are separated by a radially offset distance r which is substantially equal to the radial offset r between the central axis 46 of the orbiting scroll element 36 and the common central axis 90 of the stationary scroll element 36 and the crankshaft 14, the distance r also being the radius of orbit of the orbiting scroll element 36.
The present inventors have discovered that a particularly effective method for providing the engagement between the second shaft portion 104 of the offset crank member 100 and the second rotational bearing 94 is through the provision of the bushing member 106 which is itself non-rotationally engaged with the second shaft portion 104 but is rotationally engaged with the second rotational bearing 99. To this end, the second shaft portion 104 is provided with a conically tapered portion 108 which non-rotationally connects via a friction push fit with the similarly tapered cavity 110 provided in the bushing member 106. The non-tapered exterior periphery of the bushing 106 then rotationally mates with the second rotational bearing 94.
During operation of the scroll compressor 10, the pressure that is built up (e.g., in the spiraling compression pockets 82 and 84) exerts an axial force, that is a force acting parallel to the central axes 40 and 46 which tends to separate the stationary and orbiting spiral elements 37 and 36, respectively, from one another. From the viewpoint of merely providing for a rotational motion between the first shaft portion 102 and the first rotational bearing 92 and also between the bushing member 106 and the second rotational bearing 94, it is sufficient to furnish the first and second rotational bearings 92 and 94, respectively, in the form of conventional ball bearing assemblies o~ conventional roller bearing assemblies. Back pressure could then, for example, be utilized to balance or compensate for the above-noted axial forces which tend to separate the stationary and orbiting spiral elements 37 and 36, respectively. However, the present inventors have discovered that by utilizing a particular type of bearing for the first and second rotational bearings 92 and 94, respectively, the above-noted separating axial forces may be neutralized directly, thus eliminating the requirement of utilizing back pressure. In this regard, the rotational bearing components 92 and 94, respectively, are each preferably furnished in the form of angular contact bearing assemblies 112, an example of which is shown most particularly in Fig. 10. Fig. 10 shows the second rotational bearing 94 being provided as an angular contact bearing assembly 112 and the positioning of t:he second rotational bearing 94 relative to the central axis 40 and 96 during one extreme of the rotational orbit. It will be understood that the first rotational bearing 92 may be likewise provided in the form of a similar angular contact bearing assembly 112.
Preferably, both of the first and second rotational bearing components 92 and 94, respectively, are provided in the form of an angular contact bearing assembly 112 As seen in Fig. 10, the angular contact bearing assemblies 112 which are preferably employed for the first and second rotational bearing components 92 and 94, respectively, include at least one bearing surface 114 and/or 116 which projects a non-zero component parallel to the direction of t:he central axis 40 of the stationary scroll element 37 and parallel to the direction of the central axis 46 of the orbiting scroll element 36, both central axes 40 and 46 being parallel to one another. Due to the fact that the bearing surfaces 114 and/or 116 have a non-zero component projecting in a direction parallel to the central axes 90 and 46, the angular contact bearing assemblies 112 are able to resist the above-noted axial forces generated during compression which tend to exert a separating force between the stationary and orbiting scroll elements 37 and 36, respectively. Preferably, the angular contact bearing assemblies 112 employed are angular contact ball bearing assemblies and are of a single row configuration. Such angular contact ball bearing assemblies are available commercially and are well known to those of ordinary skill in the mechanical arts. Such angular contact ball bearing assemblies typically include two such bearing surfaces 114 and 116 which are angled so as to resist angular forces (i.e., having non-zero components in two orthogonal directions) applied thereto.
While it is possible to provide the rotational bearing components 92 and 94 in the form of sealed pre-lubricated bearing assemblies, in its presently preferred embodiment, the scroll compressor 10 includes a lubrication apparatus 118 for allowing the rotational bearing components 92 and 94 to be periodically lubricated. Provision of the lubrication apparatus 118 allows for a longer life of the first and second rotational bearing components 92 and 94, respectively.
Utilizing sealed pre-lubricated bearings could necessitate a costly disassembly procedure for replacement of the bearings near the end of their rated life. The provision of the lubrication apparatus 118 is made possible by a further unique construction of the anti-rotation assembly assemblies 90, wherein each of the first rotational bearing components 92 is fixedly mounted within the bearing cap 12 and wherein a lubrication channel portion is provided which interconnects the respective first and second rotational bearing components 92 and 94, respectively. Referring most particularly to Fig. 3, a lubrication port 120 is disposed on the exterior surface of the bearing cap 12 adjacent each of the anti-rotation assembly assemblies 90. A lubrication channel 122 extends from each of the lubrication ports 120 to at least a point adjacent the first rotational bearing 92 of the associated anti-rotation assembly 90. As is shown most particularly in Fig. 9, a channel portion 129 passing through the offset crank member 100 extends the lubrication channel 122 so that it ultimately extends to another point adjacent the second rotational bearing 94. A lubricating agent (e. g., grease) introduced into the lubrication channel 122 through the lubrication port 120 lubricates the first rotational bearing 92 via the first cavity 96 provided in the bearing face portion 86 in which the first rotational bearing 92 is mounted. Additionally, the lubricating agent is conducted through the channel portion 124 in the offset crank member 100 to the second cavity second cavity 98 provided in the orbiting scroll element 36, thereby lubricating the second rotational bearing 94.
As noted above, the orbiting spiral flange 72 and the stationary spiral flange 74 are nested and intermeshed with one another to form the spiraling compression pockets illustrated by the compression pockets 82 and 84 shown in Fig. 5. In order to provide a substantially airtight seal for these spiraling compression pockets (e. g., 82 and 84) the present scroll compressor 10 employs a unique '~tipseal" assembly 126, generally illustrated in Fig. 3 and most particularly shown in Figs. 11 and 12, to which we now turn.
The orbiting spiral flange 72 projecting outward from the orbiting base member 70 of the orbiting scroll element 36 terminates in an end surface 128 which is positioned immediately adjacent to and opposes the stationary scroll 16.
Similarly, the stationary spiral flange 74 projecting outward from the stationary scroll 16 terminates in an end surface 130 which is positioned immediately adjacent to and opposes the orbiting base member 70. Each of the encl surfaces 128 and 130 are provided with an inwardly extending groove 132 and 139, respectively. Preferably, each of the grooves 132 and 134 preferably extends substantially over the entire extent of the associated end surface 128 and 130, respectively. A
compressible element 136 is disposed within the groove 132, and another compressible element 138 is similarly disposed within groove 134. A first tipseal element 190 overlays compressible element 136, while a second tipseal element 142 overlays compressible element 138.
The depths of the grooves 132 and 139, the heights of the compressible elements 136 and 138 and the heights of the tipseal elements 140 and 142 are all selectively chosen such that, with these components are in their assembled configuration and with the compressible elements 136 and 138 in a substantially uncompressed state, each respective tipseal element 140 and 142 extends beyond the respective end surface 128 and 130 by a measurement ranging between about 0.018 inch and 0.022 inch. Stated another way, the combined height of the compressible element 136 and the tipseal element 140 exceeds the depth of the groove 132 by about 0.018 inch to about 0.022 inch when the compressible element 136 is in a substantially compressed state. Similarly, the combined height of the compressible element 138 and the tipseal element 142 exceeds the depth of the groove 134 by about 0.018 inch to about 0.022 inch when the compressible element 138 is in a substantially compressed state.
When the scroll compressor is in its assembled state (for example, as shown in Fig. 3), the compressible elements 136 and 138 will become somewhat compressed such that they exert biasing forces on the respective tipseal. elements 140 and 142 urging them into contact with the respective opposing surfaces of stationary scroll 16 and orbiting base member 70 to thereby form substantially airtight seals for the spiraling compression pockets (e.g., 82 and 84) formed between the nested and intermeshed stationary scroll element 37 and orbiting scroll element 36.
The present inventors have achieved good performance by providing the compressible elements 136 and 138 in the form of an elongated O-ring made of an elastomeric material, most preferably a silicone rubber material, and even more preferably a high temperature resistant O-ring material. Similarly, good performance has been achieved by furnishing the tipseal elements 140 and 192 in the form of a nc>n-metallic substance, preferably a PTFE based product, and most preferably a fluorosint material.
The air inlet valve assembly 34 discussed briefly above in connection with Figs. 1 and 2 is more particularly illustrated in Figs. 9 and 13-15, to which we now turn.
The air inlet valve assembly 34 is provided in order to conduct ambient air to the suction region 80 (shown in Figs. 5 and 13) which is located generally peripherally around the orbiting and stationary spiral flanges 72 and 74, respectively, and to also prevent any backward rotation of the orbiting scroll element 36 upon shut down of the power source which drives the crankshaft 14. To this end, an air inlet channel 144 connects the ambient environment located outside of the bearing cap 12 to the suction region 80 located within the bearing cap 12. As shown in Fig. 4, the a,~r inlet channel 144 preferably passes through the stationary scroll 16. In the configuration of Fig. 4, a portion of the air inlet channel 194 is formed by a air inlet port 146 formed in the stationary scroll 16. The air inlet valve assembly 34 includes a valve piston 148 which is positioned within the air inlet channel 144. The valve piston 148 is moveable between a first position (shown in Figs. 4, 13 and 14) wherein the valve piston 148 substantially blocks any flow through the air inlet channel 144 and a second position wherein the valve piston 148 substantially unblocks flow through the air inlet channel 194.
The valve piston 148 is biased toward the first blocking position by a biasing member 150. More particularly, the air inlet valve assembly 39 further includes a valve seat 152 which is mounted stationary with respect to the stationary scroll 16, and the biasing member 150 urges the valve piston 148 into contact with the valve seat 152 thereby preventing flow past the valve piston 148 and substantially b:Locking the air intake channel 194. The valve seat 152 is disposed on the opposite side of the valve piston 148 from the suction region 80, and therefore, the force exerted by the biasing member 150 is in a direction substantially away from the suction region 80.
In the embodiment shown in Figs. 2, 4 and 13, a valve housing 159 is provided which connects to the stationary scroll 16 via bolts 156. The valve piston 148 is disposed within a valve cavity 158 that is formed within the valve housing 154, and the valve seat 152 is provided as a surface formed within the valve cavity 158 enclosed by the valve housing 159. A valve stem 160 is connected to and extends from the valve housing 154 in the direction of the suction region 80. The valve piston 148 surrounds the valve stem 160 and is able to reciprocate in a sliding fashion thereon. A
first stop surface 162 is formed on the valve piston 148. A second stop surface 169 is formed on the valve stem 160 and is disposed between the first stop surface 162 formed on the valve piston 148 and the suction region 80. The biasing member 150 is preferably provided in the form of a coil spring 166 which encircles the valve stem 160 between the first stop surface 162 and the second stop surface 169. The valve piston 148 is able to slide along the valve stem 160 in the direction of the suction region 80 to admit ambient air to be compressed against the biasing force exerted by the coil spring 166. Movement of the valve piston 148 in the direction of the suction region 80 is limited by contact of the first stop surface 162 provided on the valve piston 198 with the second stop surface 164 formed on the valve stem 160.
In the embodiment of the air inlet valve assembly 34 shown in Figs. 2, 4 and 13, it is possible that vibration characteristics could be introduced by the presence of the biasing element 150 (e. g., the coil spring 166). In such cases, the present inventors have discovered that the biasing element 150 (e. g., coil spring 166) and its associated supporting structures may be eliminated from the design without introducing any serious compromise in function.
Figs. 14 and 15 illustrate an alternative embodiment of the air inlet valve assembly 34 which functions in substantially the same manner as described above but which is provided with a somewhat differently configured air intake valve body 168 having an air intake conduit 170 extending therefrom.
While the present invention has been described by way of a detailed description of a particularly preferred embodiment or embodiments, it will be apparent to those of ordinary skill in the art that various substitutions of equivalents may be affected without departing from the spirit or scope of the invention as set forth in the appended claims.
In order to provide lubrication access to the orbiting cylindrical bearing 42, the crankshaft 14 is provided with a lubricating channel 50 which extends from its second and opposite distal end to a point adjacent the orbiting cylindrical bearing 92. Preferably, as shown, the lubricating channel 50 extends along the central axis 40 of the crankshaft member 14 to the recessed cup portion 44. Provision of the lubricating channel 50 allows the orbiting cylindrical bearing 42 to be lubricated from a readily accessible single vantage point, namely, the second distal end of the crankshaft 14, during maintenance.
The lubricating channel 50 also serves another function during assembly of the scroll compressor 10. More particularly, during assembly, the hub portion 48 of the of the orbiting scroll element 36 enters the orbiting bearing 42.
During this step, the lubricating channel 50 serves as a vent, allowing any air that would be otherwise trapped to be vented.
The crankshaft 14 is additionally preferably furnished with a counterweight portion 52 that extends radially from the shaft portion 38 in a direction opposite to the radial offset r of the orbiting cylindrical bearing 42 from the central axis 40 of the crankshaft 14. The crankshaft. 14 is rotationally mounted within the bearing cap 12 through the provision of a main crankshaft bearing 54 and a rear crankshaft bearing 56.
The main crankshaft bearing 54 rotationally engages the shaft portion 38 at a point that is between the first distal end near the orbiting cylindrical bearing 92 and the second distal end of the crankshaft 19, while the rear crankshaft bearing 56 rotationally engages the shaft portion 38 at a point that is between the main crankshaft bearing 54 and the second distal end of the crankshaft 14. Both of the main and rear crankshaft bearings 54 and 56 may be, for example, of a caged roller bearing design or a caged ball bearing design. The orbiting cylindrical bearing 42 may be only of a caged roller bearing design.
The main crankshaft bearing 54 is preferably positioned within the bearing cap 12 by a main bearing sleeve 58 having a radially inwardly extending lip 60. A z-ear bearing sleeve 62 similarly serves to position the rear crankshaft bearing 56 within the bearing cap 12. As seen most clearly in Figs. 6 and 7, a crankshaft locknut member 6:3 urges a crankshaft lockwasher member 64 into contact with a rear surface of the crankshaft rear bearing 56. The rear bearing sleeve 62 is provided with an inwardly extending ledge 65. A snap ring 67 (shown most clearly in Figs. 9 and 7) snaps into an groove encircling the exterior face of the rear crankshaft bearing 56.
The snap ring 67 limits axial movement of the crankshaft 19 in an upward direction (as seen in Fig. 4), thereby locking the crankshaft axially within the bearing cap 12.
As shown in Figs. 3 and 7, the recessed cup portion 44 is provided with an annular ledge 66 spaced away from the bottom of the recessed cup portion 99. The orbiting cylindrical bearing 42 rests on this annular ledge 66 to thus create a lubrication reservoir 68 beneath the orbiting cylindrical bearing 42, the lubrication reservoir 68 being connected to the lubrication channel 50. An orbiting seal 93 overlays the orbiting cylindrical bearing 42 within the recessed cup portion 44.
The orbiting scroll element 36 includes an orbiting base member 70 and an orbiting spiral flange 72 projecting outward therefrom. In order to provide the stationary scroll element 37 referred to above, the stationary scroll 16 is in turn provided with a preferably integrally formed stationary spiral flange 79 which projects outward from the stationary scroll 16 and has a common central axis 40 with the crankshaft 14. As seen most clearly in Figs. 3 and 5, the stationary and orbiting spiral flanges 74 and 72, respectively, are intermeshed and nested with one another. For those not familiar with the manner in which compression is achieved in a scroll-type compressor, the compression mechanics may be difficult to visualize. However, for those of ordinary skill in the scroll-type compressor arts, the compression mechanics are well understood. In brief, the stationary scroll flange 74, being affixed to or an integrally formed portion of the stationary scroll 16, is maintained stationary. The orbiting scroll flange 72 executes an orbit of radius r with respect to the stationary scroll flange 74 and, during such orbiting motion, is maintained substantially non-rotational with respect to the stationary scroll flange 74. In other words, one may picture the stationary scroll flange 74 as having a stationary central axis z(stationary) 40, as well as remaining orthogonal coordinates x(stationary) and y(stationary) lying within the plane of the stationary spiral flange 74. One may also picture the orbiting spiral flange 72 as having an orbiting central axis z(orbiting) 46, as well as remaining orthogonal coordinates x(orbiting) and y(orbiting) lying within the plane of the orbiting spiral flange 72. In such case the orbiting motion which causes compression can be best described as an orbiting of the z(orbiting) central axis 46 about the z(stationary) central axis 90, while the remaining x and y axes of the stationary and orbiting spiral flanges remain in a parallel relationship to one another. In other words, the orbiting motion is accomplished with substantially no relative rotational motion occurring between the orbiting spiral flange 72 and the stationary spiral flange 74.
During such described motion, a compression pocket will be formed during each revolution of the orbiting spiral flange 72.
The compression pocket so formed will spiral toward the central area of the intermeshed stationary and orbiting spiral flanges 74 and 72, respectively, advancing and undergoing a compression step during each orbit. The number of revolutions required for a compression pocket so formed to reach a compressed air output 76 (which is located generally in the vicinity of the stationary central axis 90) depends on how many revolutions each of the stationary and orbiting spiral flanges 74 and 72, respectively, are provided with. In the present embodiment, each of the stationary and orbiting spiral flanges 74 and 72, respectively, is provided with somewhat over three revolutions. Preferably, each of the stationary and orbiting spiral flanges 74 and 72, respectively, extends over an arc of about 1350°, i.e., about 33~ evolutions.
Referring now primarily to Fig. 5, the orbiting spiral flange 72 has a radially outward terminus portion 78. As the radially outward terminus 78 portion of the orbiting spiral flange 72 separates from the corresponding portion of the stationary spiral flange 74 during each non-rotational orbit, a progressively wider gap is formed into which low pressure air is introduced from a generally peripherally located suction region 80. As the orbiting spiral flange non-rotationally orbits further, this gap is eventually closed by the contact of the terminus portion 78 with the corresponding portion of the stationary spiral flange 74. The described action forms a compression pocket which spirals inward toward the centrally located compressed air output 76 during successive orbits of the orbiting spiral flange 72. Two successive compression pockets are generally designated as 82 and 84 in Fig. 5, with the more radially inward compression pocket 84 being more highly compressed than the more radially outward compression pocket 82.
In order to prevent any relative rotational movement between the stationary and orbiting spiral flanges 74 and 72 while simultaneously permitting the orbiting of the scroll element 72 through the orbit of radius r under the influence of the orbital drive mechanism described above, the scroll compressor 10 is additionally provided with an anti-rotation device 90 most clearly seen in Figs. 3, 8 and 9, to which we now turn.
The bearing cap 12 is provided with a bearing face portion 86 (seen in Figs. 2,3,4 and 9) which is formed as an semi-annular ledge projecting radially inward from the interior surface of the bearing cap 12. The bear__ng face portion 86 is provided with a cutout 88 (seen in Fig. 2) in order to provide clearance for the counterweight portion 52 of the crankshaft 14 during assembly/disassembly. Three anti-rotation assembly assemblies 90 are arranged equidistant from and preferably equally angularly spaced around the common central axis 40 of the stationary scroll element 37 and the crankshaft 19. Thus, the three anti-rotation assembly assemblies 90 are preferably spaced at angular intervals of 120°. In the presently preferred embodiment, each of the anti-rotation assembly assemblies 90 is radially spaced outward from the common central axis 40 of the crankshaft 14 and the stationary scroll element 37 at a distance R which is preferably substantially equal to about 5 inches.
Each anti-rotation assembly 90 includes a first rotational bearing 92 which is mounted fixedly and stationary with respect to the stationary scroll element 37, preferably in a the bearing face portion 86 (as shown in figs. 3 and 9) and a second rotational bearing 94 which is mounted fixedly on the orbiting scroll element 36. Preferably, each first rotational bearing 92 is disposed in a first cavity 96 provided in the bearing face portion 86, while each second rotational bearing 94 resides in a corresponding second cavity 98 provided in the orbiting scroll element 36. Each anti-rotation assembly 90 further includes an offset crank member 100 having a first shaft portion 102 which engages the first rotational bearing 92 and a second conically tapered shaft portion 109 which engages a similarly conically tapered cavity 110 provided in a bushing member 106 which rotationally engages the second rotational bearing 94. The first and second shaft portions 102 and 104, respectively, are aligned substantially in parallel to one another and are separated by a radially offset distance r which is substantially equal to the radial offset r between the central axis 46 of the orbiting scroll element 36 and the common central axis 90 of the stationary scroll element 36 and the crankshaft 14, the distance r also being the radius of orbit of the orbiting scroll element 36.
The present inventors have discovered that a particularly effective method for providing the engagement between the second shaft portion 104 of the offset crank member 100 and the second rotational bearing 94 is through the provision of the bushing member 106 which is itself non-rotationally engaged with the second shaft portion 104 but is rotationally engaged with the second rotational bearing 99. To this end, the second shaft portion 104 is provided with a conically tapered portion 108 which non-rotationally connects via a friction push fit with the similarly tapered cavity 110 provided in the bushing member 106. The non-tapered exterior periphery of the bushing 106 then rotationally mates with the second rotational bearing 94.
During operation of the scroll compressor 10, the pressure that is built up (e.g., in the spiraling compression pockets 82 and 84) exerts an axial force, that is a force acting parallel to the central axes 40 and 46 which tends to separate the stationary and orbiting spiral elements 37 and 36, respectively, from one another. From the viewpoint of merely providing for a rotational motion between the first shaft portion 102 and the first rotational bearing 92 and also between the bushing member 106 and the second rotational bearing 94, it is sufficient to furnish the first and second rotational bearings 92 and 94, respectively, in the form of conventional ball bearing assemblies o~ conventional roller bearing assemblies. Back pressure could then, for example, be utilized to balance or compensate for the above-noted axial forces which tend to separate the stationary and orbiting spiral elements 37 and 36, respectively. However, the present inventors have discovered that by utilizing a particular type of bearing for the first and second rotational bearings 92 and 94, respectively, the above-noted separating axial forces may be neutralized directly, thus eliminating the requirement of utilizing back pressure. In this regard, the rotational bearing components 92 and 94, respectively, are each preferably furnished in the form of angular contact bearing assemblies 112, an example of which is shown most particularly in Fig. 10. Fig. 10 shows the second rotational bearing 94 being provided as an angular contact bearing assembly 112 and the positioning of t:he second rotational bearing 94 relative to the central axis 40 and 96 during one extreme of the rotational orbit. It will be understood that the first rotational bearing 92 may be likewise provided in the form of a similar angular contact bearing assembly 112.
Preferably, both of the first and second rotational bearing components 92 and 94, respectively, are provided in the form of an angular contact bearing assembly 112 As seen in Fig. 10, the angular contact bearing assemblies 112 which are preferably employed for the first and second rotational bearing components 92 and 94, respectively, include at least one bearing surface 114 and/or 116 which projects a non-zero component parallel to the direction of t:he central axis 40 of the stationary scroll element 37 and parallel to the direction of the central axis 46 of the orbiting scroll element 36, both central axes 40 and 46 being parallel to one another. Due to the fact that the bearing surfaces 114 and/or 116 have a non-zero component projecting in a direction parallel to the central axes 90 and 46, the angular contact bearing assemblies 112 are able to resist the above-noted axial forces generated during compression which tend to exert a separating force between the stationary and orbiting scroll elements 37 and 36, respectively. Preferably, the angular contact bearing assemblies 112 employed are angular contact ball bearing assemblies and are of a single row configuration. Such angular contact ball bearing assemblies are available commercially and are well known to those of ordinary skill in the mechanical arts. Such angular contact ball bearing assemblies typically include two such bearing surfaces 114 and 116 which are angled so as to resist angular forces (i.e., having non-zero components in two orthogonal directions) applied thereto.
While it is possible to provide the rotational bearing components 92 and 94 in the form of sealed pre-lubricated bearing assemblies, in its presently preferred embodiment, the scroll compressor 10 includes a lubrication apparatus 118 for allowing the rotational bearing components 92 and 94 to be periodically lubricated. Provision of the lubrication apparatus 118 allows for a longer life of the first and second rotational bearing components 92 and 94, respectively.
Utilizing sealed pre-lubricated bearings could necessitate a costly disassembly procedure for replacement of the bearings near the end of their rated life. The provision of the lubrication apparatus 118 is made possible by a further unique construction of the anti-rotation assembly assemblies 90, wherein each of the first rotational bearing components 92 is fixedly mounted within the bearing cap 12 and wherein a lubrication channel portion is provided which interconnects the respective first and second rotational bearing components 92 and 94, respectively. Referring most particularly to Fig. 3, a lubrication port 120 is disposed on the exterior surface of the bearing cap 12 adjacent each of the anti-rotation assembly assemblies 90. A lubrication channel 122 extends from each of the lubrication ports 120 to at least a point adjacent the first rotational bearing 92 of the associated anti-rotation assembly 90. As is shown most particularly in Fig. 9, a channel portion 129 passing through the offset crank member 100 extends the lubrication channel 122 so that it ultimately extends to another point adjacent the second rotational bearing 94. A lubricating agent (e. g., grease) introduced into the lubrication channel 122 through the lubrication port 120 lubricates the first rotational bearing 92 via the first cavity 96 provided in the bearing face portion 86 in which the first rotational bearing 92 is mounted. Additionally, the lubricating agent is conducted through the channel portion 124 in the offset crank member 100 to the second cavity second cavity 98 provided in the orbiting scroll element 36, thereby lubricating the second rotational bearing 94.
As noted above, the orbiting spiral flange 72 and the stationary spiral flange 74 are nested and intermeshed with one another to form the spiraling compression pockets illustrated by the compression pockets 82 and 84 shown in Fig. 5. In order to provide a substantially airtight seal for these spiraling compression pockets (e. g., 82 and 84) the present scroll compressor 10 employs a unique '~tipseal" assembly 126, generally illustrated in Fig. 3 and most particularly shown in Figs. 11 and 12, to which we now turn.
The orbiting spiral flange 72 projecting outward from the orbiting base member 70 of the orbiting scroll element 36 terminates in an end surface 128 which is positioned immediately adjacent to and opposes the stationary scroll 16.
Similarly, the stationary spiral flange 74 projecting outward from the stationary scroll 16 terminates in an end surface 130 which is positioned immediately adjacent to and opposes the orbiting base member 70. Each of the encl surfaces 128 and 130 are provided with an inwardly extending groove 132 and 139, respectively. Preferably, each of the grooves 132 and 134 preferably extends substantially over the entire extent of the associated end surface 128 and 130, respectively. A
compressible element 136 is disposed within the groove 132, and another compressible element 138 is similarly disposed within groove 134. A first tipseal element 190 overlays compressible element 136, while a second tipseal element 142 overlays compressible element 138.
The depths of the grooves 132 and 139, the heights of the compressible elements 136 and 138 and the heights of the tipseal elements 140 and 142 are all selectively chosen such that, with these components are in their assembled configuration and with the compressible elements 136 and 138 in a substantially uncompressed state, each respective tipseal element 140 and 142 extends beyond the respective end surface 128 and 130 by a measurement ranging between about 0.018 inch and 0.022 inch. Stated another way, the combined height of the compressible element 136 and the tipseal element 140 exceeds the depth of the groove 132 by about 0.018 inch to about 0.022 inch when the compressible element 136 is in a substantially compressed state. Similarly, the combined height of the compressible element 138 and the tipseal element 142 exceeds the depth of the groove 134 by about 0.018 inch to about 0.022 inch when the compressible element 138 is in a substantially compressed state.
When the scroll compressor is in its assembled state (for example, as shown in Fig. 3), the compressible elements 136 and 138 will become somewhat compressed such that they exert biasing forces on the respective tipseal. elements 140 and 142 urging them into contact with the respective opposing surfaces of stationary scroll 16 and orbiting base member 70 to thereby form substantially airtight seals for the spiraling compression pockets (e.g., 82 and 84) formed between the nested and intermeshed stationary scroll element 37 and orbiting scroll element 36.
The present inventors have achieved good performance by providing the compressible elements 136 and 138 in the form of an elongated O-ring made of an elastomeric material, most preferably a silicone rubber material, and even more preferably a high temperature resistant O-ring material. Similarly, good performance has been achieved by furnishing the tipseal elements 140 and 192 in the form of a nc>n-metallic substance, preferably a PTFE based product, and most preferably a fluorosint material.
The air inlet valve assembly 34 discussed briefly above in connection with Figs. 1 and 2 is more particularly illustrated in Figs. 9 and 13-15, to which we now turn.
The air inlet valve assembly 34 is provided in order to conduct ambient air to the suction region 80 (shown in Figs. 5 and 13) which is located generally peripherally around the orbiting and stationary spiral flanges 72 and 74, respectively, and to also prevent any backward rotation of the orbiting scroll element 36 upon shut down of the power source which drives the crankshaft 14. To this end, an air inlet channel 144 connects the ambient environment located outside of the bearing cap 12 to the suction region 80 located within the bearing cap 12. As shown in Fig. 4, the a,~r inlet channel 144 preferably passes through the stationary scroll 16. In the configuration of Fig. 4, a portion of the air inlet channel 194 is formed by a air inlet port 146 formed in the stationary scroll 16. The air inlet valve assembly 34 includes a valve piston 148 which is positioned within the air inlet channel 144. The valve piston 148 is moveable between a first position (shown in Figs. 4, 13 and 14) wherein the valve piston 148 substantially blocks any flow through the air inlet channel 144 and a second position wherein the valve piston 148 substantially unblocks flow through the air inlet channel 194.
The valve piston 148 is biased toward the first blocking position by a biasing member 150. More particularly, the air inlet valve assembly 39 further includes a valve seat 152 which is mounted stationary with respect to the stationary scroll 16, and the biasing member 150 urges the valve piston 148 into contact with the valve seat 152 thereby preventing flow past the valve piston 148 and substantially b:Locking the air intake channel 194. The valve seat 152 is disposed on the opposite side of the valve piston 148 from the suction region 80, and therefore, the force exerted by the biasing member 150 is in a direction substantially away from the suction region 80.
In the embodiment shown in Figs. 2, 4 and 13, a valve housing 159 is provided which connects to the stationary scroll 16 via bolts 156. The valve piston 148 is disposed within a valve cavity 158 that is formed within the valve housing 154, and the valve seat 152 is provided as a surface formed within the valve cavity 158 enclosed by the valve housing 159. A valve stem 160 is connected to and extends from the valve housing 154 in the direction of the suction region 80. The valve piston 148 surrounds the valve stem 160 and is able to reciprocate in a sliding fashion thereon. A
first stop surface 162 is formed on the valve piston 148. A second stop surface 169 is formed on the valve stem 160 and is disposed between the first stop surface 162 formed on the valve piston 148 and the suction region 80. The biasing member 150 is preferably provided in the form of a coil spring 166 which encircles the valve stem 160 between the first stop surface 162 and the second stop surface 169. The valve piston 148 is able to slide along the valve stem 160 in the direction of the suction region 80 to admit ambient air to be compressed against the biasing force exerted by the coil spring 166. Movement of the valve piston 148 in the direction of the suction region 80 is limited by contact of the first stop surface 162 provided on the valve piston 198 with the second stop surface 164 formed on the valve stem 160.
In the embodiment of the air inlet valve assembly 34 shown in Figs. 2, 4 and 13, it is possible that vibration characteristics could be introduced by the presence of the biasing element 150 (e. g., the coil spring 166). In such cases, the present inventors have discovered that the biasing element 150 (e. g., coil spring 166) and its associated supporting structures may be eliminated from the design without introducing any serious compromise in function.
Figs. 14 and 15 illustrate an alternative embodiment of the air inlet valve assembly 34 which functions in substantially the same manner as described above but which is provided with a somewhat differently configured air intake valve body 168 having an air intake conduit 170 extending therefrom.
While the present invention has been described by way of a detailed description of a particularly preferred embodiment or embodiments, it will be apparent to those of ordinary skill in the art that various substitutions of equivalents may be affected without departing from the spirit or scope of the invention as set forth in the appended claims.
Claims (20)
1. A tipseal assembly for a scroll compressor, such scroll compressor including a housing, a stationary scroll element mounted within such housing substantially stationary with respect to such housing, such stationary scroll element including a stationary spiral flange, an orbiting scroll element disposed within such housing, such orbiting scroll element including an orbiting spiral flange, each of such stationary and orbiting scroll elements having a central axis, such stationary and orbiting spiral flanges being intermeshed and nested with one another to define a spiraling compression pocket therebetween, an orbital drive mechanism for driving such central axis of such orbiting scroll element in an orbit about such central axis of such stationary scroll element while maintaining such orbiting scroll element substantially non-rotational with respect to such stationary scroll element, said tipseal assembly comprising:
an inwardly extending groove formed in an end surface of at least one of such stationary and orbiting spiral flanges;
a compressible element disposed substantially within and along at least a portion of a length of said inwardly extending groove formed in such end surface of such at least one of such stationary and orbiting spiral flanges; and a tipseal element overlaying said compressible element and disposed at least partially within said inwardly extending groove formed in such end surface of such at least one of such stationary and orbiting spiral flanges.
an inwardly extending groove formed in an end surface of at least one of such stationary and orbiting spiral flanges;
a compressible element disposed substantially within and along at least a portion of a length of said inwardly extending groove formed in such end surface of such at least one of such stationary and orbiting spiral flanges; and a tipseal element overlaying said compressible element and disposed at least partially within said inwardly extending groove formed in such end surface of such at least one of such stationary and orbiting spiral flanges.
2. A tipseal assembly for a scroll compressor according to Claim 1, wherein said tipseal element extends substantially beyond such end surface of said at least one of such orbiting and stationary spiral flanges when said compressible element is in a substantially uncompressed state.
3. A tipseal assembly for a scroll compressor according to Claim 1, wherein a combined height of said compressible element and said tipseal element exceeds a depth of said inwardly extending groove when said compressible element is in a substantially uncompressed state.
4. A tipseal assembly for a scroll compressor according to Claim 1, wherein a combined height of said compressible element and said tipseal element exceeds a depth of said inwardly extending groove by from about 0.018 inch to about 0.022 inch when said compressible element is in a substantially uncompressed state.
5. A tipseal assembly for a scroll compressor according to Claim 1, wherein said tipseal element includes at least one of:
a non-metallic substance;
a fluorosint material; and a PTFE based product.
a non-metallic substance;
a fluorosint material; and a PTFE based product.
6. A tipseal assembly for a scroll compressor according to Claim 1, wherein said compressible element includes at least one of:
an elastomeric material;
a silicone rubber material; and a high temperature resistant O-ring material.
an elastomeric material;
a silicone rubber material; and a high temperature resistant O-ring material.
7. A tipseal assembly for a scroll compressor according to Claim 1, wherein said tipseal forms a substantially airtight seal when said compressible element is compressed by contact with one of such stationary and orbiting scroll elements.
8. A tipseal assembly for a scroll compressor according to Claim 1, wherein:
an inwardly extending groove is formed in an end surface of each of such stationary and orbiting flanges;
one each of said compressible element is disposed substantially within and along at least a portion of a length of each of said inwardly extending grooves formed in each of such stationary and orbiting spiral flanges; and one each of said tipseal element overlays each of said compressible elements and is disposed at least partially within said inwardly extending grooves formed in each of such stationary and orbiting spiral flanges.
an inwardly extending groove is formed in an end surface of each of such stationary and orbiting flanges;
one each of said compressible element is disposed substantially within and along at least a portion of a length of each of said inwardly extending grooves formed in each of such stationary and orbiting spiral flanges; and one each of said tipseal element overlays each of said compressible elements and is disposed at least partially within said inwardly extending grooves formed in each of such stationary and orbiting spiral flanges.
9. In a scroll compressor including a housing, a stationary scroll element disposed within such housing substantially stationary with respect to such housing, such stationary scroll element including a stationary spiral flange, an orbiting scroll element disposed within such housing, each of such stationary and orbiting scroll elements having a central axis, such orbiting scroll element including an orbiting spiral flange, such stationary and orbiting spiral flanges being intermeshed and nested with one another to define a spiraling compression pocket therebetween, and an orbital drive mechanism for driving such central axis of such orbiting scroll element in an orbit about such central axis of such stationary scroll element while maintaining such orbiting scroll element substantially non-rotational with respect to such stationary scroll element, the improvement comprising a tipseal assembly for forming a substantially airtight seal, said tipseal assembly comprising:
an inwardly extending groove former in an end surface of at least one of such stationary and orbiting spiral flanges;
a compressible element disposed substantially within and along at least a portion of a length of said inwardly extending groove formed in such end surface of such at least one of such stationary and orbiting spiral flanges; and a tipseal element overlaying said compressible element and disposed at least partially within said inwardly extending groove formed in such end surface of such at least one of such stationary and orbiting spiral flanges.
an inwardly extending groove former in an end surface of at least one of such stationary and orbiting spiral flanges;
a compressible element disposed substantially within and along at least a portion of a length of said inwardly extending groove formed in such end surface of such at least one of such stationary and orbiting spiral flanges; and a tipseal element overlaying said compressible element and disposed at least partially within said inwardly extending groove formed in such end surface of such at least one of such stationary and orbiting spiral flanges.
10. A tipseal assembly for a scroll compressor according to Claim 9, wherein said tipseal element extends substantially beyond such end surface of said at least one of such orbiting and stationary spiral flanges when said compressible element is in a substantially uncompressed stated.
11. A tipseal assembly for a scroll compressor according to Claim 9, wherein a combined height of said compressible element and said tipseal element exceeds a depth of said inwardly extending groove by from about 0.018 inch to about 0.022 inch when said compressible element is in a substantially uncompressed state.
12. A tipseal assembly for a scroll compressor according to Claim 9, wherein said tipseal element includes at least one of:
a non-metallic substance;
a fluorosint material; and a PTFE based product.
a non-metallic substance;
a fluorosint material; and a PTFE based product.
13. A tipseal assembly for a scroll compressor according to Claim 9, wherein said compressible element includes at least one of:
an elastomeric material;
a silicone rubber material; and a high temperature resistant O-ring material.
an elastomeric material;
a silicone rubber material; and a high temperature resistant O-ring material.
14. A tipseal assembly for a scroll compressor according to Claim 9, wherein:
an inwardly extending groove is formed in an end surface of each of such stationary and orbiting flanges;
one each of said compressible element is disposed substantially within and along at least a portion of a length of each of said inwardly extending grooves formed in each of such stationary and orbiting spiral flanges; and one each of said tipseal element overlays each of said compressible elements and is disposed at least partially within said inwardly extending grooves formed in each of such stationary and orbiting spiral flanges.
an inwardly extending groove is formed in an end surface of each of such stationary and orbiting flanges;
one each of said compressible element is disposed substantially within and along at least a portion of a length of each of said inwardly extending grooves formed in each of such stationary and orbiting spiral flanges; and one each of said tipseal element overlays each of said compressible elements and is disposed at least partially within said inwardly extending grooves formed in each of such stationary and orbiting spiral flanges.
15. A scroll compressor including a tipseal assembly, comprising:
a housing;
a stationary scroll element mounted within said housing substantially stationary with respect to said housing, said stationary scroll element including a stationary spiral flange;
an orbiting scroll element disposed within said housing, said orbiting scroll element including an orbiting spiral flange;
each of said stationary and orbiting scroll elements having a central axis;
said stationary and orbiting spiral flanges being intermeshed and nested with one another to define a spiraling compression pocket therebetween;
orbital drive means for driving said central axis of said orbiting scroll element in an orbit about. said central axis of said stationary scroll element while maintaining said orbiting scroll element substantially non-rotational with respect to said stationary scroll element; and a tipseal assembly for forming a substantially airtight seal, said tipseal assembly comprising:
an inwardly extending groove formed in an end surface of at least one of such stationary and orbiting spiral flanges;
a compressible element disposed substantially within and along at least a portion of a length of said inwardly extending groove formed in such end surface of such at least one of such stationary and orbiting spiral flanges; and a tipseal element overlaying said compressible element and disposed at least partially within said inwardly extending groove formed in such end surface of such at least one of such stationary and orbiting spiral flanges.
a housing;
a stationary scroll element mounted within said housing substantially stationary with respect to said housing, said stationary scroll element including a stationary spiral flange;
an orbiting scroll element disposed within said housing, said orbiting scroll element including an orbiting spiral flange;
each of said stationary and orbiting scroll elements having a central axis;
said stationary and orbiting spiral flanges being intermeshed and nested with one another to define a spiraling compression pocket therebetween;
orbital drive means for driving said central axis of said orbiting scroll element in an orbit about. said central axis of said stationary scroll element while maintaining said orbiting scroll element substantially non-rotational with respect to said stationary scroll element; and a tipseal assembly for forming a substantially airtight seal, said tipseal assembly comprising:
an inwardly extending groove formed in an end surface of at least one of such stationary and orbiting spiral flanges;
a compressible element disposed substantially within and along at least a portion of a length of said inwardly extending groove formed in such end surface of such at least one of such stationary and orbiting spiral flanges; and a tipseal element overlaying said compressible element and disposed at least partially within said inwardly extending groove formed in such end surface of such at least one of such stationary and orbiting spiral flanges.
16. A scroll compressor including a tipseal assembly according to Claim 15, wherein said tipseal element extends substantially beyond such end surface of said at least one of such orbiting and stationary spiral flanges when said compressible element is in a substantially uncompressed stated.
17. A scroll compressor including a tipseal assembly according to Claim 15, wherein a combined height of said compressible element and said tipseal element exceeds a depth of said inwardly extending groove by from about 0.018 inch to about 0.022 inch when said compressible element is in a substantially uncompressed state.
18. A scroll compressor including a tipseal assembly according to Claim 15, wherein said tipseal element includes at least one of:
a non-metallic substance;
a fluorosint material; and a PTFE based product.
a non-metallic substance;
a fluorosint material; and a PTFE based product.
19. A scroll compressor including a tipseal assembly according to Claim 15, wherein said compressible element includes at least one of:
an elastomeric material;
a silicone rubber material; and a high temperature resistant O-ring material.
an elastomeric material;
a silicone rubber material; and a high temperature resistant O-ring material.
20. A scroll compressor including a tipseal assembly according to Claim 15, wherein:
an inwardly extending groove is formed in an end surface of each of such stationary and orbiting flanges;
one each of said compressible element is disposed substantially within and along at least a portion of a length of each of said inwardly extending grooves formed in each of such stationary and orbiting spiral flanges; and one each of said tipseal element overlays each of said compressible elements and is disposed at least partially within said inwardly extending grooves formed in each of such stationary and orbiting spiral flanges.
an inwardly extending groove is formed in an end surface of each of such stationary and orbiting flanges;
one each of said compressible element is disposed substantially within and along at least a portion of a length of each of said inwardly extending grooves formed in each of such stationary and orbiting spiral flanges; and one each of said tipseal element overlays each of said compressible elements and is disposed at least partially within said inwardly extending grooves formed in each of such stationary and orbiting spiral flanges.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US584,323 | 1975-06-06 | ||
| US58432300A | 2000-06-01 | 2000-06-01 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2325752A1 true CA2325752A1 (en) | 2001-12-01 |
Family
ID=24336852
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002325752A Abandoned CA2325752A1 (en) | 2000-06-01 | 2000-11-10 | Oiless rotary scroll air compressor tipseal assembly |
Country Status (7)
| Country | Link |
|---|---|
| EP (1) | EP1160456A3 (en) |
| JP (1) | JP2002005056A (en) |
| AU (1) | AU2814301A (en) |
| BR (1) | BR0101609A (en) |
| CA (1) | CA2325752A1 (en) |
| MX (1) | MXPA01005260A (en) |
| ZA (1) | ZA200102885B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112012925A (en) * | 2019-05-30 | 2020-12-01 | 艾默生环境优化技术(苏州)有限公司 | Scroll compressor having a plurality of scroll members |
| CN217538996U (en) * | 2022-04-20 | 2022-10-04 | 广东美的环境科技有限公司 | Static scroll plate applied to scroll compressor and scroll compressor |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3994636A (en) * | 1975-03-24 | 1976-11-30 | Arthur D. Little, Inc. | Axial compliance means with radial sealing for scroll-type apparatus |
| US4462771A (en) * | 1981-02-09 | 1984-07-31 | The Trane Company | Wrap element and tip seal for use in fluid apparatus of the scroll type and method for making same |
| US4395205A (en) * | 1981-02-12 | 1983-07-26 | Arthur D. Little, Inc. | Mechanically actuated tip seals for scroll apparatus and scroll apparatus embodying the same |
| JPS60243301A (en) * | 1984-05-18 | 1985-12-03 | Mitsubishi Electric Corp | Scroll fluid machine |
| CH673135A5 (en) * | 1987-07-10 | 1990-02-15 | Bbc Brown Boveri & Cie |
-
2000
- 2000-11-10 CA CA002325752A patent/CA2325752A1/en not_active Abandoned
-
2001
- 2001-03-20 AU AU28143/01A patent/AU2814301A/en not_active Abandoned
- 2001-04-06 ZA ZA200102885A patent/ZA200102885B/en unknown
- 2001-04-10 EP EP01107882A patent/EP1160456A3/en not_active Withdrawn
- 2001-04-26 BR BR0101609-1A patent/BR0101609A/en not_active IP Right Cessation
- 2001-05-25 MX MXPA01005260A patent/MXPA01005260A/en unknown
- 2001-05-30 JP JP2001161859A patent/JP2002005056A/en active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| EP1160456A3 (en) | 2003-04-02 |
| ZA200102885B (en) | 2002-07-23 |
| BR0101609A (en) | 2002-04-23 |
| JP2002005056A (en) | 2002-01-09 |
| EP1160456A2 (en) | 2001-12-05 |
| AU2814301A (en) | 2001-12-06 |
| MXPA01005260A (en) | 2005-06-17 |
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