Compressor

Information

  • Patent Grant
  • 6402485
  • Patent Number
    6,402,485
  • Date Filed
    Monday, December 11, 2000
    23 years ago
  • Date Issued
    Tuesday, June 11, 2002
    22 years ago
Abstract
Scroll compressor including a shell having an inlet tube for drawing a refrigerant, and an outlet tube for discharging the compressed refrigerant, a compressor part arranged in an upper portion of the shell having an inlet hole for drawing refrigerant flowed through the inlet tube for compressing the refrigerant flowed through the inlet hole, a motor part arranged in a lower portion of the shell for transmission of a driving force for operating the compressor part, and a main frame having an edge arranged adjoined to a baffle, which baffle is provided for splitting the refrigerant flowed into the shell through the inlet tube into a flow for the compressor part and a flow for the motor part, and which edge has a curved guide surface extended to the inlet hole of the compressor part for forming a refrigerant flow passage together with the baffle, thereby improving performance of the compressor by preventing additional pressure loss and temperature rise.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to a scroll compressor, and more particularly, to a refrigerant inlet of the scroll compressor.




2. Background of the Related Art




In general, the scroll compressor is used for compressing a gas by means of one pair of opposite scrolls, and employed mostly in a room air conditioner or a car for compressing a refrigerant gas owing to a high efficiency, low noise, small size and light weight.




Referring to

FIG. 1

, a related art scroll compressor is provided with a compressor part


10


for compressing a refrigerant gas drawn into a shell


1


from an evaporator(not shown) in a cooling cycle through an inlet tube


1




a


, and a motor part


20


for transmission of a driving force to the compressor part


10


to compress the refrigerant. The shell


1


encloses the compressor part


10


and the motor part


20


for preventing leakage of the refrigerant during the compression. There is a main frame


30


supports the compressor part


10


for stable power transmission from the motor part


20


to the compressor part


10


. The compressor part


10


has a stationary scroll


11


fixed to an upper portion of inside of the shell


1


, and a rotating scroll


12


engaged with the stationary scroll


11


for being rotated by a driving force received from the motor part


20


. The rotating scroll


12


is rotatably mounted on the main frame


30


, and the stationary scroll


11


is fixed to the main frame


30


on the rotating scroll


12


. The stationary scroll


11


and the rotating scroll


12


have laps


11




a


and


12




a


of involute curve projected in a vertical direction, and for forming a compression chamber


13


in the compressor part


10


. And, there is an inlet


40


for communication between an inner space of the shell


1


and the compression chamber


13


in the scrolls


11


and


12


for compression of the refrigerant. The motor part


20


has rotor


21


/stator


22


for generating a driving power from an external power source, i.e., a motor and a rotating shaft


50


. The rotating shaft


50


is fitted to an inside of the rotor


21


and the rotating scroll


12


on a top end thereof, for transmission of the driving force generated at the rotor


21


/stator


22


to the rotating scroll


12


through the shaft


50


. In the meantime, there is a discharge chamber


14


at a central portion of atop of the compressor part


10


in communication with the compression chamber


13


, and the discharge chamber


14


is in turn in communication with an outlet tube


1




b


for discharging compressed refrigerant to a condenser(not shown). And, the inlet tube


1




a


is positioned at one side of the shell


1


for receiving the refrigerant from the evaporator(not shown), and there is a baffle


60


on a discharge side of the inlet tube


1




a


for deflecting flow of the refrigerant. In the operation of the compressor, the refrigerant enters into the shell


1


through the inlet tube


1




a


and split in upper and lower directions at the baffle


60


. The refrigerant in the lower direction cools down the motor part


20


as the refrigerant flows through an inner portion of the shell


1


, and flows upward to enter into the compression chamber


13


through the inlet


40


, finally. On the other hand, the split refrigerant in the upper direction flows upward to an upper portion of the shell


1


, and turns back to enter into the compression chamber


13


through the inlet


40


opened substantially at a right angle to a direction of the upward refrigerant flow. Though there is a temperature rise caused by a heat from the motor part


20


and a pressure loss caused by the split flow, the system and operation of the related art compressor is essential for an effective prevention of overheating of the motor part


20


by using the refrigerant without provision of any additional cooling device. In fact, however, there is additional pressure loss and temperature rise in the operation of the compressor other than what is just explained, which will be explained, in detail.




Referring to

FIG. 2

, a related art refrigerant flow structure up to the compression chamber has a flow passage formed continuously inclusive of the baffle


60


and an edge of the main frame


30


adjoining to the baffle


60


, and an inlet hole


40


formed adjacent to the main frame


30


. An axis of the inlet hole


40


is perpendicular to the flow passage, and the inlet hole


40


is positioned on an inner side of an edge of the main frame


30


. Therefore, the refrigerant in the upper direction is involved in a flow separation during the refrigerant passes through the flow passage, to pass by the inlet hole


40


and flow to the upper portion of the shell


1


.




This refrigerant flow can be explained clearly with reference to FIG.


3


. The refrigerant entered into the shell


1


through the inlet tube


1




a


passes by the inlet hole


40


owing to a geometry of the flow structure explained before in a process the refrigerant flows in a vertical direction guided by the baffle


60


and the main frame


30


. Accordingly, the refrigerant flow to the inlet hole


40


is not smooth, but enters into the compression chamber


13


formed by respective scrolls


11


and


12


through the inlet hole


40


after the refrigerant flows to the upper portion of the shell


1


. Consequently, there is collision of the refrigerant flow passing by the inlet


40


and rising upward and the refrigerant flow heated in the process flowing around the motor, to cause a turbulent flow, that causes an additional pressure loss. And, the refrigerant absorbs heat from the main frame


30


in an extended flow path, to cause an additional temperature rise. At the end, since the additional pressure loss and the additional temperature rise interfere a smooth entrance of the refrigerant into the inlet hole


40


, resulting in overheating of the refrigerant, an overall compression efficiency of the compressor is deteriorated.




SUMMARY OF THE INVENTION




Accordingly, the present invention is directed to a compressor that substantially obviates one or more of the problems due to limitations and disadvantages of the related art.




An object of the present invention is to provide a compressor which can minimize a pressure loss and a temperature rise of a refrigerant while various components of the compressor are cooled down smoothly.




Additional features and advantages of the invention will be set forth in the description which follows, and in part will be apparent from the description, or may be learned by practice of the invention. The objectives and other advantages of the invention will be realized and attained by the structure particularly pointed out in the written description and claims hereof as well as the appended drawings.




To achieve these and other advantages and in accordance with the purpose of the present invention, as embodied and broadly described, the Scroll compressor including a shell having an inlet tube for drawing a refrigerant, and an outlet tube for discharging the compressed refrigerant, a compressor part arranged in an upper portion of the shell having an inlet hole for drawing refrigerant flowed through the inlet tube for compressing the refrigerant flowed through the inlet hole, a motor part arranged in a lower portion of the shell for transmission of a driving force for operating the compressor part, and a main frame having an edge arranged adjoined to a baffle, which baffle is provided for splitting the refrigerant flowed into the shell through the inlet tube into a flow for the compressor part and a flow for the motor part, and which edge has a curved guide surface extended to the inlet hole of the compressor part for forming a refrigerant flow passage together with the baffle, thereby improving performance of the compressor by preventing additional pressure loss and temperature rise.




The guide surface preferably has a radius of curvature set to be equal to a distance from the edge of the main frame to the inlet hole.




It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory and are intended to provide further explanation of the invention as claimed.











BRIEF DESCRIPTION OF THE DRAWINGS




The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention:




In the drawings:





FIG. 1

illustrates a longitudinal section of a related art scroll compressor;





FIG. 2

illustrates an enlarged view of “A” part in

FIG. 1

;





FIG. 3

illustrates a refrigerant flow around an inlet of a related art scroll compressor, schematically;





FIG. 4

illustrates a longitudinal section of a scroll compressor in accordance with a preferred embodiment of the present invention;





FIG. 5

illustrates an enlarged view of “B” part in

FIG. 4

; and,





FIG. 6

illustrates a refrigerant flow around an inlet of the scroll compressor of the present invention, schematically.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT




Reference will now be made in detail to the preferred embodiments of the present invention, examples of which are illustrated in the accompanying drawings. In explanations of the present invention, identical components will be given the same names and reference symbols, and explanations of which will be omitted.

FIG. 4

illustrates a longitudinal section of a scroll compressor in accordance with a preferred embodiment of the present invention, and

FIG. 5

illustrates an enlarged view of “B” part in FIG.


4


.




Referring to

FIG. 4

, the scroll compressor in accordance with a preferred embodiment of the present invention includes a compressor part


10


for compressing a refrigerant gas, a motor part


20


for transmission of a driving force to the compressor part


10


, a shell


1


for accommodating the compressor part


10


and the motor part


20


, and a main frame


130


for supporting the compressor part


10


. Since systems other than above are the same with the related art compressor, detailed explanation of which will be omitted.




In the meantime, referring to

FIG. 5

, there is a flow passage structure of the compressor of the present invention including a flow passage formed continuously inclusive of a baffle


160


and an edge of the main frame


130


adjoining to the baffle


160


, and an inlet hole


40




a


formed adjacent to the edge of the main frame


130


. In the flow passage structure of the present invention, the edge of the main frame


130


is provided with a curved guide surface


131


. That is, the edge of the main frame


130


is curved surface continuous to the inlet hole


40




a


, so that the upward refrigerant deflected at the baffle


160


flows guided by the guide surface


131


until the refrigerant enters into the inlet hole


40


, directly. In this instance, it is preferable that a radius of curvature ‘r’ of the curved surface, i.e., the guided surface


131


, of the main frame


103


is set to be a distance ‘h’ from the edge of the main frame


130


to the inlet hole


40




a


substantially, for minimizing the separation of the refrigerant flow.




The operation of the compressor of the present invention will be explained with reference to FIGS.


4


˜


6


.




The refrigerant entered into the shell


1


through the inlet tube


1




a


via the evaporator(not shown) flows into respective compression chambers


13


between respective scrolls


11


and


12


through the inlet hole


40




a


in communication with the scrolls


11


and


12


. In this state, the rotating scroll


12


is rotated according to rotation of the rotating shaft


50


coupled to the rotating scroll


12


, and the laps


11




a


and


12




a


on respective scrolls


11


and


12


, maintaining a close contact, compresses the refrigerant in an inside of the scrolls


11


and


12


. The compressed refrigerant is discharged to the discharge chamber


14


through an outlet hole


11




b


in the stationary scroll


11


, and therefrom to the condenser(not shown) through an outlet tube


1




b


. Then, the compressed refrigerant is supplied to the condenser as the foregoing suction, compression and discharge processes are repeated in a sequence.




In this instance, as shown in

FIG. 6

, the refrigerant entered into the shell


1


through the inlet tube


1




a


is split into an upward refrigerant flow and a downward refrigerant flow, wherein the upward refrigerant flow proceeds along the guide surface


131


and enters into the inlet hole


40




a


, directly. This is because liquid has a nature to flow along a wall, particularly, adhered to a curved surface, i.e., the coanda effect. The present invention utilizes the coanda effect for improving a refrigerant flow passage structure.




Thus, the upward refrigerant flow split at the baffle


160


flows along the guide surface


131


and enters into the inlet hole


40




a


directly, i.e., the upward refrigerant flow passing by the inlet hole


40


is reduced sharply, and the unnecessary upward refrigerant flow to the upper portion of the shell


1


is prevented. Moreover, the smooth upward refrigerant flow permits a smooth downward refrigerant flow back into the inlet hole


40


without interference after cooling the motor. And, the smooth and direct refrigerant flow into the inlet hole


40




a


permits to prevent the additional absorption of heat from the main frame


130


. The table shown below is a result of an analysis of the refrigerant flow obtained according to the present invention.



















The Related Art




The Present Invention




























ΔT(° C.)




13.8




10.8







ΔP


loss


(Pa)




288




69.8















Where, ΔT denotes a temperature difference of the refrigerant entered into the shell


1


, and ΔP


loss


denotes a pressure loss of the refrigerant flowing through the shell


1


. That is, as can be known from the table 1, in comparison to the related art main frame


30


, the main frame


130


of the present invention can reduce an overall pressure loss by approx. 75%, and the refrigerant temperature difference by approx. 3° C. Such reduction of pressure loss and temperature rise improves an overall volumetric efficiency of the compressor by approx. one %, resulting to provide an improved compression performance, actually.




As has been explained, the compressor of the present invention has the following advantages.




The formation of a curved guide surface at an edge of the main frame permits a smooth refrigerant flow into an inlet, and to reduce absorption of a heat from the main frame. Prevention of such additional pressure loss and temperature rise of the refrigerant permits to minimize the pressure loss and the temperature rise of the refrigerant even though components of the compressor are cooled adequately, thereby improving a performance of the compressor.




It will be apparent to those skilled in the art that various modifications and variations can be made in the compressor of the present invention without departing from the spirit or scope of the invention. Thus, it is intended that the present invention cover the modifications and variations of this invention provided they come within the scope of the appended claims and their equivalents.



Claims
  • 1. A compressor comprising:a shell having an inlet tube for drawing a refrigerant, and an outlet tube for discharging the compressed refrigerant; a compressor part arranged in an upper portion of the shell having an inlet hole for drawing refrigerant flowed through the inlet tube for compressing the refrigerant flowed through the inlet hole; a motor part arranged in a lower portion of the shell for transmission of a driving force for operating the compressor part; and, a main frame having an edge arranged adjoined to a baffle, the baffle provided for splitting the refrigerant flowed into the shell through the inlet tube into a flow for the compressor part and a flow for the motor part, and the edge having a curved guide surface extended to the inlet hole of the compressor part for forming a refrigerant flow passage together with the baffle, wherein the guide surface has a radius of curvature set ti be equal to a distance from the edge of the main frame to the inlet hole.
Priority Claims (1)
Number Date Country Kind
00-179 Jan 2000 KR
US Referenced Citations (8)
Number Name Date Kind
5055010 Logan Oct 1991 A
5064356 Horn Nov 1991 A
5240391 Ramshankar et al. Aug 1993 A
5286179 Forni et al. Feb 1994 A
5342183 Rafalovich et al. Aug 1994 A
5366352 Deblois et al. Nov 1994 A
5745992 Caillat et al. May 1998 A
6186753 Hugenroth et al. Feb 2001 B1