Rotary compressor with muffler discharging into oil sump

Information

  • Patent Grant
  • 6658885
  • Patent Number
    6,658,885
  • Date Filed
    Wednesday, October 2, 2002
    21 years ago
  • Date Issued
    Tuesday, December 9, 2003
    20 years ago
Abstract
The entire discharge flow in a high side, vertical, hermetic rotary compressor is directed into the oil sump which generates foam for sound attenuation and heats the oil to reduce its viscosity and to drive off refrigerant dissolved in the oil.
Description




BACKGROUND OF THE INVENTION




Commonly assigned U.S. Pat. Nos., 4.900,234; 4,907,414 and 5,077,981 each disclose a low side hermetic compressor in which a portion of the discharge of the compressor is bled into the oil sump. The high pressure gas being bled into the oil sump represents a loss but, because the interior of the compressor shell and the oil sump are at suction pressure, the foam generated by the high pressure gas expanding to suction pressure in the oil provides sound attenuation.




Discharge gas pulsation in the shell cavity beneath the motor in a high side vertical, hermetic rotary compressor has been found to be one of the major noise sources. In current compressor designs, the compressed gas discharges from the pump structure into the muffler cavity and then passes into the lower shell cavity. The discharge gas passes from the lower shell cavity to the discharge at the top of the compressor shell by passing through the gap between the rotor and stator and/or passing through passages between the stator and the compressor shell.




SUMMARY OF THE INVENTION




According to the teachings of the present invention the discharge gas in a high side rotary compressor passes from the pump structure into the muffler cavity and then passes via tubes into the oil sump located beneath the pump structure. Discharging the hot high pressure gas into the oil sump heats the oil and thereby reduces its viscosity. Additionally, the discharging of the high pressure gas into the oil sump, which is also at discharge pressure, generates foam roughly in the volume of the gas discharged from the pump structure. The foam will pass from the oil sump, through the pump structure to the upper part of the lower shell cavity, i.e. the part below the motor. Any foam entering the gap between the rotor and stator will tend to be collapsed and the oil will tend to be centrifugally separated such that it collects on the stator and drains due to gravity.




It is an object of this invention to reduce rotary compressor noise due to discharge gas pulsation.




It is another object of this invention to provide additional attenuation without reducing efficiency.




It is a further object of this invention to improve oil lubrication capability by increasing oil temperature in the sump. These objects, and others as will become apparent hereinafter, are accomplished by the present invention.




Basically, the entire discharge flow in a high side, vertical, hermetic rotary compressor is directed into the oil sump which generates foam for sound attenuation and heats the oil to reduce its viscosity and to drive off refrigerant dissolved in the oil.











BRIEF DESCRIPTION OF THE DRAWINGS




For a fuller understanding of the present invention, reference should now be made to the following detailed description thereof taken in conjunction with the accompanying drawings wherein:





FIG. 1

is a partially sectioned view of a compressor employing the present invention schematically located in a refrigeration circuit;





FIG. 2

is a sectional view taken along line


2





2


of

FIG. 1

;





FIG. 3

is a sectional view taken along line


3





3


of

FIG. 2

;





FIG. 4

is a partially cutaway view of the discharge muffler of the present invention;





FIG. 5

is an enlarged view of a portion of

FIG. 1

; and





FIG. 6

is a sectional view taken along line


6





6


of FIG.


5


.











DESCRIPTION OF THE PREFERRED EMBODIMENT




In

FIGS. 1-3

and


5


, the numeral


10


generally designates a vertical, high side, rolling piston compressor. Compressor


10


is in a refrigeration circuit serially including compressor


10


, discharge line


60


, condenser


70


, expansion valve


80


and evaporator


90


. The numeral


12


generally designates the shell or casing. Suction tube


16


is sealed to shell


12


and provides fluid communication between suction accumulator


14


, which is connected to evaporator


90


, and suction chamber S. Cylinder


20


, piston


22


, pump end bearing


24


, motor end bearing


28


and vane


30


collectively make up the pump structure. Suction chamber S and compression chamber C are defined by bore


20


-


1


in cylinder


20


, piston


22


, bearings


24


and


28


, and vane


30


which separates suction chamber S and compression chamber C.




Eccentric shaft


40


includes a portion


40


-


1


supportingly received in bore


24


-


1


of pump end bearing


24


, eccentric


40


-


2


which is received in bore


22


-


1


of piston


22


, and portion


40


-


3


supportingly received in bore


28


-


1


of motor end bearing


28


. Oil pick up tube


34


extends into sump


36


from a bore in portion


40


-


1


. Stator


42


is secured to shell


12


by a shrink fit, welding or any other suitable means. Commonly there will be passages in the form of slots or grooves


42


-


2


in the outer surface of the stator


42


running its entire length to provide flow paths for refrigerant gas across the motor defined by stator


42


and rotor


44


and for the return flow of oil to oil sump


36


. Rotor


44


is suitably secured to shaft


40


, as by shrink fit, and is located within bore


42


-


1


of stator


42


in a spaced relationship and coacts therewith to define a variable speed motor. Vane


30


is biased into contact with piston


22


by spring


31


.




Discharge port


28


-


2


in motor end bearing


28


is overlain by normally closed valve


29


. Valve


29


is within and opens into muffler


32


. As described so far, compressor


10


is generally conventional. The present invention differs in the details of muffler


32


and the resultant differences in operation of compressor


10


. Referring specifically to

FIGS. 3 and 4

it will be evident that muffler


32


differs from conventional mufflers in that it has two downwardly directed discharge tubes


32


-


1


and


32


-


2


which are blocked at their ends and which have a plurality of ports


32


-


1




a


and


32


-


2




a


, respectively, which are each located within the portion of the 180° perimeter of tubes


32


-


1


and


32


-


2


which is not directed towards the other one of discharge tubes


32


-


1


and


32


-


2


or pick up tube


34


. The reason for these locations of ports


32


-


1




a


and


32


-


2




a


is to avoid discharging gas towards oil pick up tube


34


. Referring specifically to

FIG. 3

, it will be noted that discharge tubes


32


-


1


and


32


-


2


extend into oil sump


36


and that all of ports


32


-


1




a


and


32


-


2




a


are located above the intake of oil pick up tube


34


. This is to prevent the generation of foam from uncovering oil pick up tube


34


and thereby interfering with compressor lubrication.




Although two discharge tubes


32


-


1


and


32


-


2


are illustrated with each having a plurality of ports


32


-


1




a


and


32


-


2




a


, respectively, one discharge tube and any convenient number of ports may be employed. The critical consideration is to avoid unnecessary restrictions. Accordingly, the discharge tubes should have a combined cross section at least equal to that of discharge port


28


-


2


and the ports


32


-


1




a


and


32


-


2




a


should be at least 0.25 inches in diameter and have a total cross sectional area on the order of 1.2 to 1.5 times the area of discharge port


28


-


2


.




As best shown in

FIGS. 1

,


5


and


6


, an oil separator


50


is suitably secured to the top of the interior of shell


12


in a surrounding relationship to discharge line


60


. Referring specifically to

FIGS. 5 and 6

, oil separator


50


includes: (1) a flat portion


50


-


1


facing rotor


44


and having a plurality of ports


50


-


1


a for oil drainage; (2) an inner annular wall member


50


-


2


having a plurality of ports


50


-


2




a


and being welded or otherwise suitably secured to the interior of shell


12


; and, (3) outer annular wall member


50


-


3


having a plurality of ports


50


-


3




a


and being spaced from the interior of shell


12


.




Initially, compressor


10


will be charged with oil up to, or a little above, the top surface of motor end bearing


28


. During operation of compressor


10


, some oil will be carried off to the refrigeration circuit due to the affinity between oil and refrigerant. The generation of foam by the discharge gas will temporarily remove oil from the sump as the foam moves into the space above motor end bearing


28


. Foam will be continuously generated, collapsed and drained back into sump


36


but the oil level will drop due to the removal of oil as foam. To prevent the excess loss of oil due to foam generation, ports


32


-


1




a


and


32


-


2




a


must be located above the inlet of oil pick up tube


34


by a minimum of a quarter of an inch. If the level of oil in sump


36


drops below ports


32


-


1




a


and


32


-


2




a


, no foam is generated and compressor


10


will be noisier but will operate without problems as long as the oil is able to circulate for compressor lubrication.




In operation, rotor


44


and eccentric shaft


40


rotate as a unit and eccentric


40


-


2


causes movement of piston


22


. Oil from sump


36


is drawn through oil pick up tube


34


into bore


40


-


4


which acts as a centrifugal pump. The pumping action will be dependent upon the rotational speed of shaft


40


. As best shown in

FIG. 2

, oil delivered to bore


40


-


4


is able to flow into a series of radially extending passages, in portion


40


-


1


, eccentric


40


-


2


, and portion


40


-


3


exemplified by passage


40


-


5


in eccentric


40


-


2


, to lubricate bearing


24


, piston


22


, and bearing


28


, respectively. The excess oil flows from bore


40


-


4


and either passes downwardly over the rotor


44


and stator


42


to the sump


36


or is carried by the gas flowing from the annular gap between rotor


44


and stator bore


42


-


1


and impinges and collects on the inside of cover


12


-


1


or oil separator


50


before draining to sump


36


.




Piston


22


coacts with vane


30


in a conventional manner such that refrigerant gas is drawn through suction tube


16


and passageway


20


-


2


to suction chamber S. The gas in suction chamber S is compressed after suction chamber S has been cut off from suction tube


16


and has been transformed into a compression chamber C while a new suction chamber is being formed. The hot compressed gas in compression chamber C passes through discharge port


28


-


2


unseating discharge valve


29


and enters into the interior of muffler


32


. The compressed gas divides in muffler


32


with part flowing into tube


32


-


1


and out ports


32


-


1




a


and part flowing into tube


32


-


2


and out ports


32


-


2




a


. The gas, at discharge pressure, passing from muffler


32


via ports


32


-


1




a


and


32


-


2




a


enters oil sump


36


which is also at discharge pressure. Depending upon the oil level in sump


36


and the location of ports


32


-


1




a


and


32


-


2




a


relative to the oil in sump


36


, foam may or may not be generated. The passing of the hot discharge gas into oil sump


36


increases the temperature of the oil in sump


36


and tends to generate foam. Under certain operating conditions, such as those encountered in heat pump operation, the solubility of the refrigerant in the oil could be very high due to low ambient temperature. In such a case, the oil lubrication capability may be compromised but refrigerant solubility will be significantly reduced due to the heating of the oil thereby improving its lubricating effectiveness. Additionally, the discharge of the gas into the oil sump


36


produces a foam which has a greater volume than the oil forming the foam and so tends to flow through the passages defined by recessed portions


20


-


3


and


20


-


4


and the interior of shell


12


, as best shown in FIG.


2


. There will be a tendency for the lower shell, i.e. the portion of shell


12


below rotor


44


and stator


42


to fill with foam. Because the gas/liquid impedance is ineffective for sound transmission and because there is no direct path for sound to travel, the compressor


10


is quieter than conventional compressors. If ports


32


-


1




a


and


32


-


2




a


are located above the surface of the oil in sump


36


, no foam will be generated but the oil will be heated by the hot discharge gas thereby improving the lubricating effectiveness of the oil.




If excessive oil passes from compressor


10


with the discharge gas it can interfere with heat transfer in the refrigeration system and can leave an inadequate amount of oil in oil sump


36


for proper lubrication. The presence of foam greatly increases the amount of oil present with the discharge gas. The discharge gas must however go past the motor and this can only be done by passing through the clearance between rotor


44


and stator bore


42


-


1


or by passing through the slots or grooves


42


-


2


in the outer surface of stator


42


. Because the clearance between rotor


44


and stator bore


42


-


1


is small and because the relative movement of rotor


44


with respect to stator


42


results in a shearing force on any foam bubbles entering the clearance, the foam tends to collapse in passing between the rotor


44


and stator


42


. Additionally, the relative rotation of rotor


44


with respect to stator


42


tends to cause the discharge gas to move in a spiral path that tends to centrifugally remove oil from the gas. The swirling flow tends to persist into the space between rotor


44


and discharge line


60


. Oil separator


50


tends to collect oil and prevents its being entrained with the gas passing from compressor


10


through discharge line


60


to the condenser


70


of the refrigeration circuit. Specifically, refrigerant, oil and any remaining foam passing between rotor


44


and stator


42


tends to be moving in a spiral path which tend to move any oil outward. The refrigerant and any entrained oil will flow either through ports


50


-


3




a


or between wall member


50


-


3


and the interior of shell


12


before passing through ports


50


-


2




a


and the changes in flow direction will tend to separate out entrained oil which will drain through drainage ports


50


-


1




a


. The refrigerant and any entrained oil passing through ports


50


-


2




a


will undergo a change in flow direction prior to flowing into discharge line


60


which will tend to separate out entrained oil which will drain through drainage ports


50


-


1




a


. The oil draining through drainage ports


50


-


1




a


will tend to fall into the swirling flow passing between rotor


44


and stator


42


and will thereby be directed towards the interior of casing


12


. While discharge gas may flow past stator


42


via grooves


42


-


2


, it is more likely to be the location of return oil flow to sump


36


given the fact that there is no pressure gradient so that gravity flow of the oil will take place and because of the centrifugal effect on oil in the gap between rotor


44


and stator bore


42


-


1


.




Although the present invention has been illustrated and described in terms of a vertical, high side, variable speed compressor, other modifications will occur to those skilled in the art. For example, the invention is applicable to both horizontal and vertical compressors. The only significant difference would be the location of the oil sump relative to the muffler and the discharge from the muffler could be straight down into the portion of the oil sump between the pump structure and the stator which would be well removed from the appropriate oil pick up tube. It is therefore intended that the present invention is to be limited only by the scope of the appended claims.



Claims
  • 1. In a refrigeration system containing refrigerant and serially including a high side rotary compressor, a condenser, expansion means and an evaporator, said compressor comprising:shell means having a first end and a second end; cylinder means containing pump means including a vane and a piston coacting with said cylinder means to define suction and compression chambers; said cylinder means being fixedly located in said shell means near said first end; first bearing means secured to said cylinder means and extending towards said first end; second bearing means secured to said cylinder means and extending towards said second end; a discharge port in said second bearing means; a normally closed discharge valve controlling flow through said discharge port, an oil sump located at the lowest portion of said shell means and containing oil therein; and muffler means for directing at least a major portion of the discharge flow passing through said discharge port into said oil in said oil sump whereby said oil is heated and foam is generated.
  • 2. The compressor of claim 1 wherein:said compressor is a vertical compressor; and said oil sump is located beneath said pump means.
  • 3. The compressor of claim 1 wherein said muffler means includes at least one discharge tube having a blocked end and at least one port along its length.
  • 4. The compressor of claim 1 further including means for oil separation secured to and located within said shell means at said second end and forming a portion of a discharge flow path leading to said condenser.
US Referenced Citations (7)
Number Name Date Kind
1897199 Kenney Feb 1933 A
2084341 Hornaday Jun 1937 A
3031861 McCormack May 1962 A
3066857 MoCloy Dec 1962 A
4061444 Dirk et al. Dec 1977 A
4907414 Fraser et al. Mar 1990 A
5605447 Kim et al. Feb 1997 A