ROTARY COMPRESSOR GAS ROUTING FOR MUFFLER SYSTEM

Abstract: A hermetically sealed rotary compressor is disclosed wherein gas compressed within a compression chamber (85) defined by a cylinder block (84) is discharged through respective discharge ports (130, 140) in the main and outboard bearings (64, 74) defining the ends of the cylinder. Mufflers (90, 92) are provided on the outside ends of the bearings into which the compressed gas is expanded. A constricting gas passageway (160) extending through the bearings (64, 74) and the cylinder block (84) provides a path for constricted flow of gas from one muffler (90) to the other (92). The constricted gas expands upon entry into the other muffler (92), thereby providing a cooler recombined discharge gas for use in cooling oil in the oil sump (114) and cooling the motor stator windings (26).

Description: The invention pertains to a rotary compressor as per the preamble of claim 1 and claim 9. A compressor of this kind is disclosed by JP-A- 62-214292. In general, prior art hermetic rotary compressors comprise a housing which is hermetically sealed. Located in the housing are an electric motor and a compressor mechanism. The electric motor is connected to a crankshaft which has an eccentric portion thereon. The eccentric portion of the crankshaft is located within a compression chamber bore of the compressor cylinder block. A roller located within the compression chamber is mounted on the eccentric portion of the crankshaft and is driven thereby. The roller cooperates with a sliding vane to compress refrigerant within the bore of the cylinder block. Rotary hermetic compressors of the type herein disclosed generally have a pressurized or high side sealed housing. Compressed gas from within the compression chamber is discharged through a gas routing system into the compressor housing. This discharge gas exhibits undesirable properties with respect to achieving quiet and efficient operation of the compressor. Specifically, noise pulsations are ordinarily caused by the discharge gas due to opening and closing of valving in response to the cyclical compression and suction created in the compression chamber within the cylinder block. Under certain operating conditions, and particularly for higher capacity compressors, these noise pulsations become objectionable to the consumer. Another problem associated with rotary hermetic compressors, wherein pressurized gas is discharged into the sealed housing, is a hot operating environment which tends to decrease the efficiency of the electric motor. High operating temperatures also result in undesirable high temperatures for the lubricating oil, the housing, and the discharge gas. Prior art gas routing systems for rotary compressors have generally addressed the problem of excessive noise pulsations by providing a single discharge port in either of the main or outboard bearings through which compressed gas is removed from the compression chamber into a muffler or a series of mufflers. In several prior art gas routing systems, after the compressed gas is discharged through a bearing into a muffler cavity, it is rerouted through passageways extending through both bearings and the cylinder block and then through an auxiliary muffler system or directly into the housing. Another prior art gas routing system provides for multiple discharge ports in the sidewall of the cylindrical compression chamber providing communication between the compression chamber and a discharge chamber defined within the cylinder block. From the discharge chamber, discharge gas passes through a single port extending through a bearing into a muffler before being discharged into the interior of the compressor housing. By providing a plurality of discharge ports in the sidewall of the compression chamber, cooler gas is discharged into the discharge chamber defined within the cylinder block. The gas is then discharged through a single smaller opening in one of the bearings. A disadvantage of the prior art solutions wherein compressed gas is discharged through a single opening in one of the main or outboard bearings is that a single opening in a rotary compressor cannot be made large enough to sufficiently reduce the level of noise pulsations. Furthermore, the temperature of gas discharged through a limited size opening is hotter than can otherwise be achieved though larger openings, thus increasing operating temperatures of the compressor and reducing compressor efficiency. The prior art rotary compressor design utilizing a plurality of discharge ports in the sidewall of the cylinder provides a baffling chamber in the cylinder block. However, the discharge gas is ultimately discharged through one port in one of the bearings into a single muffler, thereby maintaining objectionable sound pulsations. A further problem with a rotary compressor having a discharge chamber defined within the cylinder block is that compressor size may be increased by the need for space surrounding the compression chamber. Also, heat generated in the compression chamber and dissipated into the cylinder block maintains the discharge gas within the discharge chamber at higher temperatures, thereby decreasing its ability to cool compressor components when discharged within the housing. It is also known in the art to provide a discharge muffler mounted on the outboard bearing in fluid communication with oil in the oil sump for the purpose of providing sound muffling. To this end, discharge gas may be discharged into the oil to cause cavitation and adherance of air bubbles to the discharge muffler for further sound muffling. The present invention overcomes the disadvantages of the above-described prior art hermetic rotary compressors by providing an improved discharge gas routing system for discharging gas from within the compression chamber of the cylinder block to the interior of the sealed compressor housing. Generally, the State of the Art upon which the invention is based provides a rotary compressor comprising a cylinder block defining a cylinder, and a main bearing and an outboard bearing located on respective ends of the cylinder block enclosing the cylinder at each of its opposite ends. In accord with the present invention, compressed gas from within the cylinder is discharged through first and second discharge ports extending through the main and outboard bearings, respectively. Accordingly, flow of the compressed gas discharged from within the cylinder is divided between the first and second discharge ports. More specifically, said State of the Art provides, in one form thereof, a gas routing system for a rotary compressor wherein compressed gas from within the compression chamber in the cylinder block is discharged through respective ports in the main and outboard bearings into mufflers mounted on the outside of the main and outboard bearings. The discharge gas is expanded upon entering each of the mufflers, whereby cooling of the gas occurs. The expanded gas of one of the mufflers flows through a passageway extending through the main and outboard bearings and the cylinder block and is combined with the expanded discharge gas in the other muffler prior to being discharged into the interior of a hermetically sealed housing. An advantage of said prior art structure was that compressed gas from within the compression chamber can be discharged axially outwardly through both the main and outboard bearings, thereby increasing the effective size of the discharge port previously provided in only one of the main or outboard bearings. This results in noise pulsations of a lesser magnitude and discharge gas at lower temperatures. Another advantage of said gas routing system was that flow of the combined discharge gas exhibiting a cooler temperature may be directed at the stator windings of the electric motor in order to provide better cooling and more efficient operation thereof. Also, the cooler discharge gas directed for cooling the stator windings contributes to an overall cooler temperature within the sealed compressor housing. The paramount advantages of the gas routing system in accordance with the present invention are reduced sound levels achieved through the axial discharge of compressed gas through both of the bearings, and improved efficiency due to lower operating temperatures within the compressor housing, including lower oil temperatures, lower stator winding temperatures, etc. Yet another advantage of the structure of the present invention, in one form thereof, is that the passageways provided between the compression chamber and the mufflers, between the two mufflers, and between one of the mufflers and the interior of the compressor housing are comprised of substantially aligned holes through the main and outboard bearings and the cylinder block, whereby the mufflers do not require tubing connections, thus contributing to ease and lower costs of manufacturing. Furthermore, the plurality of holes extending through the main and outboard bearings and the cylinder block reduce the mass of the cylinder and bearings and require no additional tubing. The rotary compressor of the present invention, in one form thereof, provides a cylinder block defining a cylinder, and a main bearing and an outboard bearing located on respective ends of the cylinder block to close the cylinder at each of its opposite ends. An eccentric roller is rotationally mounted in the cylinder, whereby rotation of the roller in the cylinder results in compressed gas within the cylinder. A rotatable crankshaft is operably supported by the main and outboard bearings and is drivingly connected to the roller for rotation thereof. Means for discharging the compressed gas from within the cylinder is provided, comprising a first discharge port in communication with and extending from the cylinder through the main bearing and a second discharge port in communication with and extending from the cylinder through the outboard bearing. Accordingly, flow of the compressed gas discharge from within the cylinder is divided between the first and second discharge ports. There are furthermore a first and second discharge muffler mounted respectively on the main and outboard bearings, being in fluid communication with the first and second discharge posts respectively, whereby compressed gas is discharged through the main bearing is expanded upon entry into the first muffler and compressed gas discharged through the outboard bearing is expanded upon entry into the second muffler. Furthermore these provided gas passage means communicating between the first and second mufflers for allowing expanded gas in one of the first and second mufflers to flow from the one muffler to the other muffler and gas discharge outlet means providing fluid communication between the other muffler and the inside of the housing. The discharge outlet means extends through the main and outboard bearings and the cylinder block. The rotary hermetic compressor of the instant invention further provides, in one form thereof, a vertically disposed hermetically sealed cylindrical casing. An electric motor unit is mounted within the casing and includes a rotatable rotor and a stator. The hermetic compressor also includes an oil sump located in a lower portion of the housing and a cylinder block having a compression chamber defined therein. An upper bearing is mounted to the upper end of the cylinder and defines an upper end wall of the chamber. The upper bearing has an upper discharge port extending therethrough. A lower bearing is mounted to the lower end of the cylinder block and defines a lower end wall of the compression chamber. The lower bearing has a lower discharge port extending therethrough. A crankshaft is drivingly connected to the rotor and operably supported by the upper and lower bearings. Piston means for compressing gas within the chamber is drivingly connected to the crankshaft. An upper muffler is mounted to the top of the upper bearing, whereby the upper discharge port provides gaseous communication between the chamber and the upper muffler. A lower muffler is mounted to the bottom of the lower bearing and is in fluid contact with oil in the oil sump. The lower discharge port provides gaseous communication between the chamber and the lower muffler, whereby compressed gas from within the chamber is discharged and expanded into the upper and lower mufflers. Additionally, the compressor of this form provides gas passage means communicating between the upper and lower mufflers for discharging gas from the upper muffler and delivering it to the lower muffler. The lower muffler then communicates with the inside of the housing by means of discharge gas outlet means for directly delivering discharge gas from the lower muffler through the bearings and the cylinder block to the inside of the the housing in an upward direction toward the motor for cooling thereof. Fig. 1 is a side sectional view of a rotary compressor of the type to which the present invention pertains; Fig. 2 is a sectional view of the compressor of Fig. 1 taken along line 2-2 of Fig. 1 and viewed in the direction of the arrows; Fig. 3 is an exploded perspective view of the compressor mechanism of the rotary compressor assembly of Fig. 1, particularly showing the axial assembly of the various compressor mechanism components; and Fig. 4 is an exploded perspective view of the compressor mechanism of the rotary compressor assembly of Fig. 1, particularly showing the routing of gas compressed within the cylinder and eventually delivered to the interior of the compressor housing. In an exemplary embodiment of the invention as shown in the drawings, and in particular by referring to Fig. 1, a compressor is shown having a housing generally designated at 10. The housing has a top portion 12, a lower portion 14 and a central portion 16. The three housing portions are hermetically secured together as by welding or brazing. A flange 18 is welded to the bottom of housing 10 for mounting the compressor. Located inside the hermetically sealed housing is a motor generally designated at 20 having a stator 22 and a rotor 24. The stator is provided with windings 26. The stator is secured to the housing 10 by an interference fit such as by shrink fitting. The rotor 24 has a central aperture 28 provided therein into which is secured a crankshaft 30 by an interference fit. A terminal cluster 32 is provided on the top portion 12 of the compressor for connecting the compressor to a source of electric power. A post 34 is welded to top portion 12 for mounting a protective cover (not shown) for terminal cluster 32. A refrigerant discharge tube 36 extends through top portion 12 of the housing and has an end 38 thereof extending into the interior of the compressor as shown. The tube is sealingly connected to housing 10 at 40 as by soldering. Similarly, a suction tube 42 extends into the interior of compressor housing 10 and is sealed thereto as by soldering, brazing, or welding. The outer end 44 of suction tube 42 is connected to accumulator 46 which has support plates 48 disposed therein for supporting a filtering mesh 50. A bracket 52 secures accumulator 46 to the outside wall of housing 10. By referring specifically to Figs. 1 and 3, it can be seen that crankshaft 30 is provided with an eccentric portion 54 which revolves around the crankshaft axis as crankshaft 30 is rotatably driven by rotor 24. Counterweights 56 and 58 are provided to balance eccentric 54 and are secured to respective end rings 60 and 62 of rotor 24 by riveting. Crankshaft 30 is journalled in a main bearing 64 having a cylindrical journal portion 66 and a generally flat planar mounting portion 68. Planar portion 68 is secured to housing 10 at three points 70 such as by welding of flanges 72 to the housing, as best illustrated in Fig. 2. A second bearing or journal 74, sometimes referred to as the outboard bearing, is also shown disposed in the lower part of housing 10. Outboard bearing 74 is provided with a journal portion 76 having aperture 78 therein and a generally planar portion 80. Crankshaft 30 has a lower portion 82 journalled in journal portion 76 of outboard bearing 74 as illustrated in Fig. 1. Located intermediate main bearing 64 and outboard bearing 74 is a compressor cylinder block 84. Cylinder block 84 defines a cylinder therein, referred to herein as compression chamber 85. Compressor cylinder block 84, outboard bearing 74, and main bearing 64 are secured together by means of twelve bolts 86, two of which are indicated in Fig. 1. By referring to Fig. 2, it can be seen that six threaded holes 88 are provided in cylinder block 84 for securing bearings 64, 74 and cylinder block 84 together. Of the twelve bolts 86, six of them secure outboard bearing 74 to cylinder block 84 and are threaded into holes 88. The remaining six bolts secure main bearing 64 to cylinder block 84 and are also threaded into holes 88. An upper discharge muffler plate 90 is secured to main bearing 64 and a lower discharge muffler plate 92 is secured to outboard bearing 74 by bolts 86, as indicated in Fig. 1. By referring to Figs. 1 and 2 it can be seen that cylinder block 84 has a vane slot 94 provided in the cylindrical side wall 96 thereof into which is received a sliding vane 98. Roller 100 is provided which surrounds eccentric portion 54 of crankshaft 30 and revolves around the axis of crankshaft 30 and is driven by eccentric 54. Tip 102 of sliding vane 98 is in continuous engagement with roller 100 as vane 98 is urged against the roller by spring 104 received in spring pocket 106. Referring to Fig. 2, during operation, as roller 100 rolls around compression chamber 85, refrigerant will enter chamber 85 through suction tube 42. Next, the compression volume enclosed by roller 100, cylinder wall 96, and sliding vane 98 will decrease in size as roller 100 revolves clockwise around compression chamber 85. Refrigerant contained in that volume will therefore be compressed and after compression will exit through a relief 110 in sidewall 96. The aforementioned compressor mechanism is presented by way of illustration only, it being contemplated that other piston means for compressing gas within chamber 85 may be used without departing from the spirit and scope of the present invention. The rotary compressor disclosed herein provides a lubrication system for lubricating components of the compressor, including eccentric 54 and roller 100. Such a system is disclosed in U. S. Patent No. 4,640,669, assigned to the same assignee as the present invention, the disclosure of which is hereby incorporated by reference. Referring to Figures 1 and 3, components of an exemplary lubrication system are shown, including aperture 112 in crankshaft 30 into which oil is drawn from oil in oil sump 114. Aperture 112 delivers oil to opening 116 in crankshaft 30 to lubricate roller 100. Oil also flows into annular chamber 118 and radially outwardly therefrom through passageway 120, as described more fully in U. S. Patent No. 4,640,669. A conventional oil paddle 122 is axially mounted to end portion 82 of crankshaft 30 for contact with oil in oil sump 114. As best shown in Figures 3 and 4, the discharge gas routing system of the present invention provides means for discharging compressed gas from within chamber 85 and comprises a first discharge port 130 in communication with chamber 85 and extending through main bearing 64. A first discharge valve 132 and valve retainer 134 are mounted on outer surface 136 by means of a rivet 138. Likewise, a second discharge port 140 extends through outboard bearing 74. A second discharge valve 142 and valve retainer 144 are mounted on outer surface 146 by means of a rivet 148. Compressed refrigerant gas which is discharged through relief 110 flows axially outwardly through discharge port 130 in the main bearing and discharge port 140 in the outboard bearing. Discharge of the compressed gas through discharge ports 130 and 140 occurs simultaneously when the two ports are axially aligned, as disclosed in the preferred embodiment. The gas is then discharged into first and second discharge mufflers comprising muffler chambers 150 and 152 defined by discharge muffler plates 90 and 92 and the outer surfaces 136 and 146 of bearings 64 and 74, respectively. In the preferred embodiment, a collar 154 is provided in muffler plate 90 to sealingly engage over journal portion 66 as by a slip-fit. Likewise, a collar 156 is provided in muffler plate 92 to sealingly engage over journal portion 76. Figure 4 illustrates the routing of discharge gas during operation of the compressor. More specifically, compressor refrigerant gas is discharged through relief 110 in cylinder block 84 and flows axially outwardly in opposite directions as illustrated by directional lines A and B. With respect to the vertical orientation of the compression mechanism in Figure 4, the discharge gas indicated by line A flows through discharge port 130 in upper main bearing 64. Upon passing by discharge valve 132 and valve retainer 134, the discharge gas is expanded into upper muffler chamber 150 defined by muffler plate 90 and the top surface 136 of main bearing 64. The expansion of the discharge gas upon entry into muffler chamber 150 provides cooling of the discharge gas. Discharge gas discharged axially downwardly as indicated by directional arrow B flows through discharge port 140 in lower outboard bearing 74 and passes through discharge valve 142 and valve retainer 144 before entering lower muffler chamber 152 defined by muffler plate 92 and outer surface 146 of outboard bearing 74. As the discharge gas is expanded into discharge space 152, a certain amount of cooling of the gas is achieved. The present invention, in one form thereof, provides for the discharge gas in upper muffler chamber 150 to be routed into a gas passageway 160, as indicated by directional arrow C. Gas passageway 160 comprises holes 160a in main bearing 64, 160b in cylinder block 84, and 160c in outboard bearing 74. Holes 160a, 160b, and 160c are axially aligned to provide passageway 160, through which laminar flow of discharge gas is achieved, as indicated by directional arrow D. Gas passageway 160 provides communication between muffler chambers 150 and 152 located at opposite ends of the compressor mechanism. As shown in Figure 4, the discharge gas in muffler chamber 150 indicated by directional arrow C enters hole 160a in main bearing 64, proceeds through hole 160b in cylinder block 84, and finally passes through 160c in outboard bearing 74 before entering discharge space 152. Also, the routing of gas through the upper muffler and then through passageway 60 prior to entering the lower muffler provides several additional stages of baffling to reduce sound. When muffler plate 92 is in contact with the oil in oil sump 114, as illustrated in Fig. 1, cooling of the oil occurs as well as muffling of the sound created by discharge impulses. It will be appreciated that the discharge gas in muffler chamber 150 is cooler than ordinarily possible due to the discharge gas routing system of the present invention. The combined discharge gas in muffler chamber 152, as indicated by line E in Figure 4, is discharged into the inside of compressor housing 10 through a gas discharge outlet such as discharge gas passageway 162 communicating between muffler 152 and the inside of housing 10. Discharge passageway 162, in accord with one form of the present invention, comprises holes 162a in outboard bearing 74, 162b in cylinder block 84, 162c in main bearing 64, and 162d in muffler plate 90. A second discharge passageway 164 may also be provided in similar fashion, comprising holes 164a, 164b, 164c, and 164d. The combined discharge gas in chamber 152 is discharged through passageways 162 and 164 as indicated by directional arrows F and G, respectively. As can be seen from Figures 1 and 4, the discharge gas exiting passageways 162 and 164 is directed upwardly toward electric motor unit 20. In this way, the cooler discharge gases achieved by the gas routing system of the present invention provide more effective cooling of the stator windings 26. It has been discovered that for the best operation of the gas routing system of the present invention, discharge port 130 in the main bearing is preferably sized smaller than discharge port 140 in the outboard bearing in order to provide the necessary flow rate for gas to travel the longer distance through constricting passageway 160 before entering muffler chamber 152. For example, in an exemplary embodiment of the present invention, discharge port 130 is .181 inches in diameter while discharge port 140 is .312 inches in diameter. In such an embodiment, passageways 160, 162, and 164 are all approximately .343 inches in diameter. It is appreciated that the advantages of the present invention over gas routing systems of the prior art, i.e., reduced noise levels and cooler operating conditions, are achieved by the unique structure of the present device wherein discharge gas is simultaneously discharged through both the main and outboard bearings, thereby initially reducing noise pulsations by dividing the mass flow. Noise levels are further reduced by additional stages of baffling provided by the muffling chambers and passageways of the present invention. The advantages described herein result in quieter, more efficient operation of a rotary compressor.

Claims: A rotary compressor, comprising a cylinder block (84) defining a cylinder; a main bearing (64) and an outboard bearing (74) located on respective ends of the cylinder block and closing the cylinder at each of its opposite ends; an eccentrically mounted piston means (100) rotationally mounted in the cylinder; a rotatable crankshaft (30) operably supported by the main and outboard bearings and drivingly connected to the piston means, the rotation of the piston means in the cylinder resulting in compressed gas within the cylinder; means for discharging the compressed gas from within the cylinder, comprising a first discharge port (130) in communication with and extending from the cylinder through the main bearing and a second discharge port (140) in communication with and extending from the cylinder through the outboard bearing; a first discharge muffler (150) and a second discharge muffler (152) mounted on the main and outboard bearings, respectively, the first and second discharge mufflers being in fluid communication with the first and second discharge ports, respectively, whereby compressed gas discharged through the main bearing is expanded upon entry into the first muffler and compressed gas discharged through the outboard bearing is expanded upon entry into the second muffler; gas passage means (160) communicating between the first and second mufflers for allowing expanded gas in one of the first and second mufflers (150, 152) to flow from the one muffler to the other muffler (152) and gas discharge outlet means (162, 164) providing fluid communication between the other muffler and the inside of the housing, characterized in that the discharge outlet means extends through the main and outboard bearings and the cylinder block. The rotary compressor of Claim 1 further characterized by a first discharge valve (132) mounted to the main bearing (64) and a second discharge valve (142) mounted to the outboard bearing (74), the first and second discharge valves being in communication with the first and second discharge ports, respectively. The rotary compressor of Claim 1 characterized in that the first and second discharge ports (130, 140) are axially aligned, whereby discharge of compressed gas through the first and second discharge ports occurs simultaneously. The rotary compressor of Claim 1 characterized in that the gas passage means comprises a passageway (160) defined by substantially aligned holes (160a-c) through the main and outboard bearings (64, 74) and the cylinder block (84). The rotary compressor of Claim 1 characterized in that the discharge port (130) operably associated with the one (150) of the first and second mufflers (150, 152) has a smaller cross-sectional area than that of the other discharge port (140). The rotary compressor of Claim 1 characterized in that the discharge outlet means (162, 164) comprises a plurality of discharge passages each which is defined by substantially aligned holes (162a-c, 164a-c) through the main and outboard bearings (64, 74) and the cylinder block (84). The rotary compressor of Claim 1 characterized in that the first discharge muffler (150) comprises a first muffler plate (90) mounted on the axially outer end of the main bearing (64) to define a first muffler chamber therebetween, and the second discharge muffler (152) comprises a second muffler plate (92) mounted on the axially outer end of the outboard bearing (74) to define a second muffler chamber therebetween; and the gas discharge outlet means (162, 164) extends through the muffler plate (90) associated with the one muffler (150). The rotary compressor of Claim 7 characterized in that the muffler plate (90) through which the gas discharge outlet (162, 164) extends includes a flange portion attached adjacent the axially outer surface of the bearing (64) associated therewith, the flange portion having an aperture (162d, 164d) formed therein through which the gas discharge outlet extends. A hermetically sealed rotary compressor, comprising a vertically disposed hermetically sealed cylindrical casing (10); an electric motor unit (20) mounted within said casing and including a rotatable rotor (24) and a stator (22); an oil sump (114) located in a lower portion of the housing; a cylinder block (84) having a compression chamber (85) defined therein; an upper bearing (64) mounted to the upper end of the cylinder block and defining an upper end wall of the chamber, the upper bearing having an upper discharge port (130) extending therethrough; a lower bearing (74) mounted to the lower end of the cylinder block and defining a lower end wall of the compression chamber, the lower bearing having a lower discharge port (140) extending therethrough; a crankshaft (30) drivingly connected to the rotor and operably supported by the upper and lower bearings; piston means (98, 100) drivingly connected to the crankshaft for compressing gas within the chamber; an upper muffler (150) mounted to the top of the upper bearing, the upper discharge port providing gaseous communication between the chamber and the upper muffler; a lower muffler (152) mounted to the bottom of the lower bearing and being in fluid contact with oil in the oil sump, the lower discharge port providing fluid communication between the chamber and the lower and discharge gas outlet means (162, 164), communicating between the lower muffler and the inside of the housing through the upper and lower bearings and the cylinder block muffler; passage means (160) communicating between the upper and lower mufflers characterized in that said outlet means carry discharge gas from the upper muffler and deliver it to the lower muffler; and that the discharge gas outlet means directly delivers discharge gas from the lower muffler through the bearings and the cylinder block to the inside of the housing in an upward direction toward the motor for cooling thereof. The rotary compressor of Claim 9 characterized in that piston means (98, 100) comprises an eccentric roller (100); and the upper and lower discharge ports (130, 140) are axially aligned to achieve simultaneous discharge of compressed gas through the first and second discharge ports. The rotary compressor of Claim 9 characterized in that the upper muffler (150) comprises a muffler plate (90) attached to the top surface of the upper bearing (64) to define an upper muffler chamber therebetween; and the discharge gas outlet means (162, 164) comprises a plurality of circumferentially spaced passageways defined by substantially aligned holes (162a-d, 164a-d) through the upper and lower bearings (64, 74) , the cylinder block (84), and the muffler plate. The rotary compressor of Claim 11 characterized in that the muffler plate (90) includes a flange portion attached adjacent the top surface of the upper bearing (64), the aperture (162d, 164d) being formed in the flange portion in substantial alignment with the holes (162a-c, 164a-c) through the upper and lower bearings and the cylinder block (84).

Inventors: ORTIZ, ARTURO L.
Applicants: TECUMSEH PRODUCTS COMPANY
Application year: 1988
Main classification: F04C29
IPC codes: F04C23, F04C18, F04C29