Rotary compressor

Information

  • Patent Grant
  • 6336800
  • Patent Number
    6,336,800
  • Date Filed
    Thursday, July 27, 2000
    24 years ago
  • Date Issued
    Tuesday, January 8, 2002
    23 years ago
Abstract
A rotary compressor of the low operational noise type is disclosed. This compressor consists of a casing, a rotating shaft set within the casing, a roller eccentrically fixed to the rotating shaft and eccentrically, rotatably set within a cylinder so as to form a variable suction chamber and a variable compression chamber within the cylinder. The compressor also has a bypass passage, which is formed on the internal surface of the cylinder at a position around the refrigerant exhaust stroke initiating point, thus allowing the compression and exhaust chambers to communicate with each other through the bypass passage and allowing highly compressed refrigerant to be fed from the compression chamber back into the suction chamber at the initial stage of each exhaust stroke. Therefore, the compressor of this invention effectively reduces excessive pressure pulsation generated at the initial stage of each exhaust stroke, thereby effectively reducing impact exciting force caused by the pressure pulsation within the compression chamber of the cylinder and effectively reducing impact vibration and pulsation noise.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to rotary compressors and, more particularly, to a rotary compressor of the low operational noise type, having a bypass passage on the internal surface of its cylinder at a position around a fluid exhaust stroke initiating point to effectively reduce excessive pressure pulsation generated at the initial stage of an exhaust stroke, thus effectively reducing impact exciting force caused by the pressure pulsation within the compression chamber of the cylinder and effectively reducing pulsation noise having a wide frequency band.




2. Description of the Prior Art




As well known to those skilled in the art, compressors are machines used for compressing fluid, such as liquid or gas, to a desired pressure and have been preferably and widely used for a variety of applications. Such compressors are recognized as very important elements in a variety of refrigeration systems, such as air conditioners or refrigerators, since the compressors are used for compressing refrigerant of refrigeration cycles and determine the operational capacities and operational efficiencies of such refrigeration systems. Conventional compressors have been classified into two types: rotary compressors and scroll compressors. Of the two types, the scroll compressors are designed to compress refrigerant by a rotating action of a rotatable scroll, operated in conjunction with a drive unit, relative to a fixed scroll. On the other hand, the rotary compressors compress refrigerant by a roller, which is operated in conjunction with a drive unit and is eccentrically rotated within the bore of a cylinder.





FIGS. 1 and 2

show the construction of a conventional rotary compressor. As shown in the drawings, the conventional rotary compressor comprises a casing


10


provided with both a refrigerant inlet port


10




a


for introducing refrigerant into the casing


10


and a refrigerant outlet port


10




b


for discharging compressed refrigerant from the casing


10


. A stator


11


is fixed within the casing


10


, while a rotor


12


is positioned to be electromagnetically rotatable relative to the stator


11


when it is electrically activated. A rotating shaft


13


having an eccentric portion (


13


′) is integrated with the central axis of the rotor


12


and is rotatable along with the rotor


12


. A roller


17


is fixed to the eccentric portion (


13


′) of the rotating shaft


13


and set within the bore


16




a


of a cylinder


16


. The cylinder


16


has a suction port


21


and an exhaust port


22


and compresses working fluid, sucked into the bore


16




a


through the suction port


21


, in accordance with an eccentric rotating action of the roller


17


within the bore


16




a


and discharges the compressed fluid from the bore


16




a


through the exhaust port


22


.




A vane


18


is provided within the bore


16




a


of the cylinder


16


at a position around the exhaust port


22


and is normally biased by a spring


19


so as to elastically come into contact with the external surface of the roller


17


. The above vane


18


partitions the chamber, formed between the cylinder


16


and the roller


17


, into a variable suction chamber


16




b


and a variable compression chamber


16




c


. An exhaust control valve (not shown) is provided within the exhaust port


22


of the cylinder


16


and is used for controlling the port


22


so as to allow the port


22


to exhaust the compressed fluid from the cylinder


16


when the roller


17


completely rotates within the cylinder


16


at a predetermined angle. A main bearing


14


is installed at an upper position within the cylinder


16


, while a sub-bearing


15


is installed at a lower position within the cylinder


16


.




The above conventional rotary compressor is operated as follows: That is, when the compressor is electrically activated, the rotor


12


is electromagnetically rotated along with the rotating shaft


13


relative to the stator


11


. Therefore, the roller


17


is eccentrically rotated within the cylinder bore


16




a


while coming into tangential contact with the internal surface of the cylinder


16


. When the roller


17


is eccentrically rotated within the cylinder bore


16




a


, refrigerant is introduced into the bore


16




a


through the suction port


21


. The refrigerant is thus gradually compressed as the compression chamber


16




c


, formed by the roller


17


, the internal surface of the cylinder


16


and the vane


18


, is gradually reduced in its volume due to the eccentric rotating action of the roller


17


within the cylinder bore


16




a


. When the pressure of the refrigerant reaches a predetermined reference level as it is compressed, the exhaust control valve is opened, thus allowing the compressed refrigerant to be exhausted from the cylinder


16


through the exhaust port


22


. The exhausted compressed air is, thereafter, discharged from the compressor through the refrigerant outlet port


10




b


formed on the casing


10


of the compressor.




In the drawings, the reference numeral


20


denotes an accumulator.





FIG. 3

is a sectional view corresponding to

FIG. 2

, showing a resonator installed within the cylinder of the conventional rotary compressor. As shown in the drawing, a resonator


40


, designed to reduce operational noise of a predetermined frequency band, is formed in the cylinder


16


to communicate with the exhaust port


22


. Due to the resonator


40


, the compressor reduces pulsation noise, caused by refrigerant gas within the cylinder


16


during a refrigerant compression stroke of the cylinder


16


. The resonator


40


also prevents an undesirable quick discharging of the pressure pulsation from the cylinder


16


during a refrigerant exhaust stroke of the cylinder


16


, thus reducing operational noise and vibration during the refrigerant exhaust stroke. The resonator


40


is determined in its resonating frequency band in accordance with both the shape of a resonating cavity determined by the acoustic resonance and the shape of a pressure leading passage.




Since both the shape of the resonating cavity and the shape of the pressure leading passage are fixed, the resonating frequency band of the resonator


40


for the cylinder


16


is fixed. However, since the compression chamber


16




c


is gradually reduced in its volume in a refrigerant compression stroke, the internal pressure of the compression chamber


16




c


continuously varies, with the pressure pulsation being exhausted from the cylinder


16


through the exhaust port


22


. Therefore, the compressor inevitably generates operational noises having a variety of frequency bands, and so the resonator


40


, having a fixed resonating frequency band, does not desirably reduce the pressure pulsation in the compressor.




In addition, lubrication oil may be undesirably introduced from the cylinder bore


16




a


into the resonating cavity of the resonator


40


at the initial stage of the operation of the compressor. In such a case, it is almost impossible to effectively remove the lubrication oil from the resonator


40


during the operation of the compressor since the pressure leading passage of the resonator


40


is positioned above the resonating cavity. The amount of lubrication oil, remaining in the resonating cavity, varies during the operation of the compressor, and changes the noise reduction characteristics of the resonator


40


. Therefore, the resonator


40


does not maintain its designed noise reductirefrigeranton characteristics and fails to accomplish its desired noise reducing operational effect.




In addition, since the resonator


40


is formed on the middle portion of the exhaust line while communicating with the exhaust port


22


, the quantity of refrigerant, which is undesirably remained in the compression chamber


16




c


at the final stage of a compressed refrigerant exhaust stroke and is free from exhausting compressed refrigerant from the cylinder


16


, is undesirably increased. Therefore, the highly compressed refrigerant gas, remaining in the dead cavity, is undesirably fed back to the suction chamber


16




b


of the cylinder bore


16




a


after the exhaust stroke, thus causing a re-expansion of completely compressed refrigerant and deteriorating the compression efficiency of the compressor.




SUMMARY OF THE INVENTION




Accordingly, the present invention has been made keeping in mind the above problems occurring in the prior art, and an object of the present invention is to provide a rotary compressor of the low operational noise type, which has a bypass passage on the internal surface of its cylinder at a position around a fluid exhaust stroke initiating point to effectively reduce excessive pressure pulsation generated at the initial stage of each exhaust stroke, thus effectively reducing impact exciting force caused by the pressure pulsation within the compression chamber of the cylinder and effectively reducing pulsation noise having a wide frequency band.




In order to accomplish the above object, the present invention provides a rotary compressor comprising a casing, a rotating shaft set within the casing, a roller eccentrically fixed to the rotating shaft and eccentrically, rotatably set within a cylinder so as to form a variable suction chamber and a variable compression chamber within the cylinder, further comprising a bypass passage formed on the internal surface of the cylinder at a position around the refrigerant exhaust stroke initiating point, thus allowing the compression and exhaust chambers to communicate with each other through the bypass passage at the initial stage of each exhaust stroke.











BRIEF DESCRIPTION OF THE DRAWINGS




The above and other objects, features and other advantages of the present invention will be more clearly understood from the following detailed description taken in conjunction with the accompanying drawings, in which:





FIG. 1

is a sectional view, showing the construction of a conventional rotary compressor;





FIG. 2

is a sectional view, showing the cylinder and the eccentric roller of the conventional rotary compressor;





FIG. 3

is a sectional view corresponding to

FIG. 2

, showing a resonator installed within the cylinder of the conventional rotary compressor;





FIG. 4

is a sectional view, showing the cylinder and the eccentric roller of a rotary compressor in accordance with the preferred embodiment of the present invention;





FIG. 5

is a sectional view of the rotary compressor of this invention, showing a flow of refrigerant within the cylinder provided with a bypass passage;





FIG. 6

is a graph, showing pressure as a function of rotating angle of the eccentric roller within the cylinder of the rotary compressor according to this invention in comparison with a conventional rotary compressor; and





FIG. 7

is a waveform diagram, showing operational noise as a function of frequency of the rotary compressor according to the present invention in comparison with a conventional rotary compressor.











DETAILED DESCRIPTION OF THE INVENTION.





FIG. 4

is a sectional view, showing the cylinder and the eccentric roller of a rotary compressor in accordance with the preferred embodiment of the present invention.

FIG. 5

is a sectional view of the rotary compressor of this invention, showing a flow of refrigerant within the cylinder provided with a bypass passage.




As shown in the drawings, the general shape of the rotary compressor according to the preferred embodiment of this invention remains the same as that of the conventional rotary compressor of

FIG. 1

, but a bypass passage


60


is formed on the internal surface of the cylinder


16


at a position around a refrigerant exhaust stroke initiating point spaced apart from the vane


18


at a counterclockwise angle θ.




That is, the rotary compressor according to the preferred embodiment of this invention comprises a casing


10


provided with the cylinder


16


therein. The cylinder


16


defines a bore


16




a


therein, with both a refrigerant suction port


21


and a refrigerant exhaust port


22


being formed on the cylinder


16


. An eccentric roller


17


, eccentrically fixed to the rotating shaft


13


of a rotor


12


, is set within the cylinder bore


16




a


. This roller


17


is eccentrically rotated within the bore


16




a


and compresses refrigerant. A vane


18


is provided within the cylinder bore


16




a


while being normally biased by a spring


1


p to elastically come into contact with the external surface of the roller


17


. This vane


18


thus partitions the chamber, formed between the cylinder


16


and the roller


17


, into a low pressure variable suction chamber


16




b


and a high pressure variable compression chamber


16




c


. The bypass passage


60


is formed by a groove, which is formed on the internal surface of the cylinder


16


at a position around the refrigerant exhaust stroke initiating point spaced apart from the spring-biased vane


18


at a counterclockwise angle θ. In the present invention, it is preferable to design the groove of the bypass passage


60


to have a depth of not larger than 20% of the height of the cylinder


16


. At the refrigerant exhaust stroke initiating point, the roller


17


completely compresses the refrigerant within the compression chamber


16




c


and initially exhausts the compressed refrigerant from the cylinder


16


through the exhaust port


22


that is opened by an exhaust control valve (not shown).




In the present invention, the bypass passage


60


may be provided in the upper portion of the cylinder


16


around the main bearing


14


or in the lower portion of the cylinder


16


around the sub-bearing


15


. Alternatively, two bypass passages


60


may be formed in the upper and lower portions of the cylinder


16


.




In addition, the bypass passage


60


may be preferably formed on the internal surface of the cylinder


16


at a position within an area having a range of θ ± 10°.




In the rotary compressor of this invention, the refrigerant suction and exhaust strokes are alternately and periodically performed under the control of the exhaust control valve, which periodically opens and closes the exhaust port


22


of the compression chamber


16




c


. That is, the exhaust control valve opens the exhaust port


22


at a time the internal pressure of the compression chamber


16




c


becomes higher than the exhaust pressure, thus quickly discharging pressure pulsation from the compression chamber


16




c


into the interior of the compressor casing


10


. In such a case, the compressor typically generates impact vibration and pulsation noise. However, the compressor of this invention has the bypass passage


60


on the internal surface of the cylinder


16


at a position around the refrigerant exhaust stroke initiating point spaced apart from the spring-biased vane


18


at the angle θ. Therefore, at the exhaust stroke initiating point, the remaining highly compressed refrigerant gas is fed back from the compression chamber


16




c


into the suction chamber


16




b


through the bypass passage


60


, thus reducing the pressure pulsation. That is, at a time the roller


17


passes by the exhaust stroke initiating point of the angle θ with the exhaust control valve being opened, the high pressure compression chamber


16




c


communicates with the low pressure suction chamber


16




b


through the bypass passage


60


. Therefore, the pressure pulsation of the highly compressed refrigerant gas is discharged from the compression chamber


16




c


into the low pressure suction chamber


16




b


, thus preventing a rapid pressure variation at a time the exhaust control valve is opened. Therefore, it is possible to prevent an undesired excessive compression of refrigerant gas at the initial stage of each exhaust stroke. This finally reduces both impact vibration and pulsation noise caused by such an excessive pressure variation.




In such a case, the refrigerant compression efficiency of the compressor may be undesirably reduced since the highly compressed refrigerant gas is fed from the compression chamber


16




c


back into the suction chamber


16




b


through the bypass passage


60


. However, such a communication of the compression chamber


16




c


with the suction chamber


16




b


through the bypass passage


60


only continues for a very short time of the initial stage of each exhaust stroke. Therefore, the deterioration in compression efficiency of the compressor caused by the communication of the chambers


16




b


and


16




c


may be negligible particularly in comparison with that of the conventional compressor caused by undesirable excessive compression of refrigerant due to the resonator


40


. In addition, different from the conventional compressor having the resonator


40


, the compressor of this invention is free from any dead cavity, which is undesirably remained in the compression chamber


16




c


at the final stage of a compressed refrigerant exhaust stroke and is free from exhausting compressed refrigerant from the cylinder


16


. Therefore, the compressor of this invention is free from any deterioration in its refrigerant compression efficiency caused by a re-expansion of completely compressed refrigerant.





FIG. 6

is a graph, showing pressure as a function of rotating angle of the eccentric roller within the cylinder of the rotary compressor according to this invention in comparison with a conventional rotary compressor.

FIG. 7

is a drawing showing operational noise as a function of frequency of the rotary compressor according to the present invention in comparison with a conventional rotary compressor. As shown in

FIG. 6

, the pressure of the rotary compressor of this invention at a position around the exhaust stroke initiating point of the angle θ is lower than that of the conventional rotary compressor, and so the compressor of this invention is free from excessive compression of refrigerant and is effectively reduced in its operational noise at the initial stage of each exhaust stroke. In addition, the graph of

FIG. 7

shows that the compressor of this invention is remarkably reduced in its operational noise over a variety of frequency bands in comparison with the conventional rotary compressor.




As described above, the rotary compressor according to the invention has a bypass passage on the internal surface of the cylinder at a position around a refrigerant exhaust stroke initiating point spaced apart from the spring-biased vane at a counterclockwise angle θ, with the bypass passage allowing the compression and exhaust chambers to communicate with each other at the initial stage of each exhaust stroke. Due to such a bypass passage, pressure pulsation of highly compressed refrigerant gas is effectively discharged from the compression chamber into the suction chamber at the initial stage of each exhaust stroke, thus remarkably reducing a rapid pressure variation at a time the exhaust port of the cylinder is opened different from a conventional rotary compressor having a resonator at its cylinder. The bypass passage also prevents an undesired excessive compression of refrigerant at the initial stage of each exhaust stroke, thus finally reducing both impact vibration and pulsation noise caused by such an excessive pressure variation.




The rotary compressor of this invention is effectively reduced in its operational noise over a variety of frequency bands from a low frequency band to a high frequency band. Therefore, the operational noise of the compressor according to this invention is preferably reduced by 3 dB or more.




In the rotary compressor of this invention, the compression efficiency is almost free from excessive compression of refrigerant, thus being less likely to be reduced in its compression efficiency due to such excessive compression of refrigerant. Another advantage of the rotary compressor of this invention resides in that it is free from any dead cavity, which is undesirably remained in the compression chamber of its cylinder at the final stage of each exhaust stroke and is free from exhausting compressed refrigerant from the cylinder. The compressor of this invention is thus free from any deterioration in its refrigerant compression efficiency caused by a re-expansion of completely compressed refrigerant.




Although a preferred embodiment of the present invention has been described for illustrative purposes, those skilled in the art will appreciate that various modifications, additions and substitutions are possible, without departing from the scope and spirit of the invention as disclosed in the accompanying claims.



Claims
  • 1. A rotary compressor comprising a casing, a rotating shaft set within the casing, a roller eccentrically fixed to the rotating shaft and rotatably, eccentrically set within a cylinder so as to form a variable suction chamber and a variable compression chamber within said cylinder, further comprising:a bypass passage formed on an internal surface of the cylinder at a position within an area having a range of an angle of ±10° from a refrigerant exhaust stroke initiating point, thus allowing said compression and exhaust chambers to communicate with each other through the bypass passage at an initial stage of each exhaust stroke.
  • 2. The rotary compressor according to claim 1, wherein said bypass passage is a groove formed on said internal surface of the cylinder.
  • 3. The rotary compressor according to claim 2, wherein said groove has a depth of not larger than 20% of a height of said cylinder.
Priority Claims (1)
Number Date Country Kind
99-30800 Jul 1999 KR
US Referenced Citations (5)
Number Name Date Kind
2612311 Warrick et al. Sep 1952 A
4537567 Kawaguchi et al. Aug 1985 A
4881879 Ortiz Nov 1989 A
4884956 Fujitani et al. Dec 1989 A
4960372 Scheldorf et al. Oct 1990 A
Foreign Referenced Citations (5)
Number Date Country
936214 Mar 1954 DE
184281 Jun 1986 EP
57-070989 Jan 1982 JP
2-308997 Dec 1990 JP
5-079482 Mar 1993 JP