Rotation balancing mechanism for orbiting scrolls of scroll-type compressors

Information

  • Patent Grant
  • 6190147
  • Patent Number
    6,190,147
  • Date Filed
    Tuesday, November 2, 1999
    25 years ago
  • Date Issued
    Tuesday, February 20, 2001
    24 years ago
Abstract
A rotation balancing mechanism of an orbiting scroll of a scroll-type compressor that reduces the outer diameter of the compressor housing. A compression mechanism includes a fixed scroll and an orbiting scroll. The compression mechanism is coupled to a support frame at the front of a drive motor. A drive crankshaft is located between the drive shaft of the motor and a base plate of the orbiting scroll. The drive crankshaft causes the orbiting scroll to orbit. Follower crankshafts are located between the support frame and the base plate. The follower crankshafts permit the orbiting scroll to orbit and prevent the orbiting scroll from rotating about its own axis. A central balance weight is located on the drive crankshaft. The central balance weight opposes part of the centrifugal force that is applied to the drive crankshaft when the orbiting scroll orbits. Outer balance weights are attached to the follower crankshafts to oppose the remainder of the centrifugal force.
Description




BACKGROUND OF THE INVENTION




The present invention relates to a rotation balancing mechanism for balancing orbiting scrolls of scroll-type compressors.





FIGS. 9 and 10

show a prior art scroll-type compressor. The scroll type compressor includes a motor housing


15


for a motor


12


and a compressor housing


31


for a compression mechanism


13


. A support frame


16


is attached to the front of the motor housing


15


. The compressor housing


31


is fixed to the support frame


16


. The motor


12


includes a drive shaft


18


. The compression mechanism


13


includes a fixed scroll


32


and an orbiting scroll


33


, which includes a base plate


36


. A crankshaft


51


is located between the drive shaft


18


and the orbiting scroll


33


to cause the orbiting scroll


33


to orbit. Bearing sleeves


63


are formed on the support frame


16


. Bearing sleeves


66


are formed on the rear and peripheral surface of the base plate


36


of the orbiting scroll


33


. Follower crankshafts


61


arc located between the bearing sleeves


63


and the outer bearing sleeves


66


. The follower crankshafts


61


permit orbital movement of the orbiting scroll


33


and prevent rotation about its own axis of the orbiting scroll


33


.




The orbiting scroll


33


orbits with the crank shaft


51


while rotation about its own axis of the orbiting scroll


33


is prevented by the follower crankshafts


61


. This movement draws refrigerant gas from a suction chamber


39


, compresses the gas in a compression chamber


38


, and discharges the gas to an external refrigerant circuit through a discharge port


41


. The compression chamber


38


is defined by the fixed scroll


32


and the orbiting scroll


33


.




The center of gravity of the orbiting scroll


33


is located at an axis O


2


of an eccentric pin


53


. When the orbiting scroll


33


orbits during the operation of the compressor, a centrifugal force is applied to the eccentric pin


53


. The centrifugal force is based on the moment of inertia about the axis O


1


of the crankshaft


51


(drive shaft


18


). That is, centrifugal force FT (WT*R


1





2


) is applied to the eccentric pin


53


. R


1


represents the distance between the axis O


1


of the drive shaft


18


and the axis O


2


of the eccentric pin


53


, which is the orbiting radius of the orbiting scroll


33


. The mass of the orbiting scroll


33


that orbits the axis O


2


is represented by WT. The orbiting speed (angular velocity) of the orbiting scroll


33


is represented by ω. Therefore, a central balance weight


57


, which has a mass W, is integrally attached to the crankshaft


51


. The balance weight is located on the opposite side of crankshaft


51


from the eccentric pin


53


with respect to the axis O


1


. The central balance weight


57


achieves dynamic balancing, that is, the net centrifugal force applied to the crankshaft


51


is null.




In the prior art scroll-type compressor shown in

FIGS. 9 and 10

, since the central balance weight


57


is attached only to the crankshaft


51


, the following problem occurs. As shown in

FIG. 10

, to offset the centrifugal force FT of the orbiting scroll


33


with the single central balance weight


57


, the center of gravity G


1


of the central balance weight


57


must be radially spaced from the axis O


1


of the drive shaft


18


and the central balance weight


57


cannot be compact. Therefore, the central path C


1


, which is the path of the periphery of the central balance weight


57


, is relatively large.




On the other hand, the peripheral surfaces of the outer bearing sleeves


66


, which support the eccentric pins


65


of the follower crankshafts


61


, must not interfere with the central path C


1


. As a result, journal shafts


62


of the follower crankshafts


61


and outer bearing sleeves


66


are obliged to be located to extend radially from peripheral rim of the base plate


36


of the orbiting scroll


33


as shown in FIG.


10


. Accordingly, to avoid interference between the outer paths C


2


, which are the paths of the peripheral surfaces of the outer bearing sleeves


66


, and the inner surface of the housing


31


, projections


31




a


must be formed on the housing


31


. This increases radial size of the compressor housing


31


.




Japanese Unexamined Utility Model Publication No. 1-61480 shows a compressor that is similar to the compressor of

FIGS. 9 and 10

. As shown in

FIG. 11

, the follower crankshafts


61


of the compressor shown in the publication include balance weights


81


, which compensate for the mass imbalance of the crankshafts


61


when orbiting. In this case, since each balance weight


81


is formed perpendicular to a corresponding eccentric pin


65


, trim weights


82


, which nullify the centrifugal force of the corresponding follower crankshaft


61


, are attached to the follower crankshafts


61


. Therefore, the journal shafts


62


are rearwardly extended by the trim weights


82


.




In the above scroll-type compressor of

FIG. 11

, only the balance weight that is attached to the drive crankshaft opposes the centrifugal force caused by the mass of the orbiting scroll. Therefore, the follower crankshafts


61


and the outer bearing sleeves


66


extend radially outward from the base plate


36


of the orbiting scroll


33


, which increases the size of the compressor housing


31


. In addition, the trim weights


82


complicate the structure and increase the mass of the compressor.




SUMMARY OF THE INVENTION




A first objective of the present invention is to provide a rotation balancing mechanism of an orbiting scroll for a scroll-type compressor that reduces the size of the compressor.




A second objective of the present invention is to provide a rotation balancing mechanism for an orbiting scroll that simplifies the structure and reduces the mass.




A third objective of the present invention is to provide a rotation balancing mechanism for an orbiting scroll that that enables smooth orbital movement of the orbiting scroll with a drive crankshaft.




To achieve the above objectives, the present invention provides a scroll type compressor structured as follows. The compressor includes a housing, a fixed scroll, and an orbiting scroll. The fixed scroll is fixed to the housing. The fixed scroll has a base and a spiral portion formed on the base. The orbiting scroll has a base and a spiral portion formed on the base to engage the fixed scroll. The orbiting scroll has a center axis offset from that of the fixed scroll. A driving crankshaft is connected to the base of the orbiting scroll to produce orbital motion. Follower crankshafts are connected to the housing and the base of the orbiting scroll to follow the motion of the orbiting scroll and to prevent the orbiting scroll from rotating about its own axis. Balance weights for balancing a moment of inertia of the orbiting scroll about the driving crankshaft. The balance weights are located on at least the follower crankshafts.




Other aspects and advantages of the present invention will become apparent from the following description, taken in conjunction with the accompanying drawings, illustrating by way of example the principles of the invention.











BRIEF DESCRIPTION OF THE DRAWINGS




The features of the present invention that are believed to be novel are set forth with particularity in the appended claims. The invention, together with objects and advantages thereof, may best be understood by reference to the following description of the presently preferred embodiments together with the accompanying drawings in which:





FIG. 1

is a cross-sectional view showing a scroll-type compressor according to one embodiment of the present invention;





FIG. 2

is a partial transverse cross-sectional view of the scroll-type compressor;





FIG. 3

is an exploded perspective view of the rotation balancing mechanism;





FIG. 4

is an enlarged cross-sectional view of the rotation balancing mechanism;





FIG. 5

is a partial cross-sectional view showing another embodiment of the present invention;





FIG. 6

is a cross-sectional view showing a scroll-type compressor according to another embodiment of the present invention;





FIG. 7

is a perspective view illustrating the moment of inertia of each member of

FIG. 6

;





FIG. 8

is a partial cross-sectional view showing another embodiment of the present invention;





FIG. 9

is a cross-sectional view showing a prior art scroll-type compressor;





FIG. 10

is a transverse cross-sectional view showing the prior compressor of

FIG. 9

; and





FIG. 11

is a partial cross-sectional view showing another prior art scroll-type compressor.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




A scroll-type compressor according to a first embodiment of the present invention will now be described with reference to

FIGS. 1-4

.




As shown in

FIG. 1

, the scroll-type compressor


11


includes a drive motor


12


, a compression mechanism


13


, and a rotation balancing mechanism


14


. The compression mechanism


13


is located frontward of the motor


12


. The rotation balancing mechanism


14


is located between the motor


12


and the compression mechanism


13


.




A front support frame


16


is fixed by a bolt to the front end of a cylindrical motor housing


15


, which accommodates the motor


12


. A rear support frame


17


is fixed by a bolt to the rear end of the motor housing


15


. A drive shaft


18


is supported in the center of the front and rear support frames


16


,


17


through radial ball bearings


19


,


20


. A rotor


21


is fitted on the drive shaft


18


. Coiled wires


22


are fixed on the inner surface of the motor housing


15


. When the coiled wires


22


are excited, the rotor


21


rotates with the drive shaft


18


, which operates the compressor


11


.




The compression mechanism


13


will now be described. A compressor housing


31


is fixed by a bolt to the front surface of the support frame


16


. The support frame


16


forms part of the compressor housing


31


. A fixed scroll


32


is integrally formed in the compressor housing


31


. The fixed scroll


32


is engaged with an orbiting scroll


33


. That is, a fixed spiral portion


35


is integrally formed on a base plate


34


of the fixed scroll


32


and an orbiting spiral portion


37


is integrally formed on a base plate


36


of the orbiting scroll


33


. The spiral portions


35


,


37


engage one another and contact one another at plural points. Due to the orbital motion of the orbiting scroll


33


, the spiral portions


35


,


37


shift with a predetermined angular displacement with respect to one another. A plurality of compression chambers


38


are formed between the fixed and orbiting spiral portions


35


,


37


. The compression chambers


38


shift spirally from the outer region toward the center of the engaged spiral portions


35


,


37


while their volumes are reduced in response to the movement of the orbiting scroll


33


.




A suction chamber


39


is formed between the peripheral surface of the orbiting scroll


33


and the inner surface of the compressor housing


31


. Refrigerant gas is drawn to the suction chamber


39


from an external refrigerant circuit through an inlet


40


, which is formed in the housing


31


. When the orbiting scroll


33


is rotated by a rotation balancing mechanism


14


, refrigerant gas in the suction chamber


39


is drawn to the compression chambers, which are formed between the fixed scroll


32


and the orbiting scroll


33


. Since the radially inner compression chambers


38


have smaller volumes than the radially outer compression chambers


38


, refrigerant gas is compressed as it moves from the periphery to the center and is discharged to the external refrigerant circuit through the outlet


41


, which is formed in the housing


31


.




The rotation balancing mechanism


14


will now be described.




A drive crankshaft


51


is located between the drive shaft


18


of the motor


12


and the base plate


36


of the orbiting scroll


33


. The crankshaft


51


converts rotation of the drive shaft


18


into orbital motion of the orbiting scroll


33


. A splined shaft


18




a


is formed at the front end of the drive shaft


18


and projects into the suction chamber


39


. A connecting sleeve


52


forms part of the drive crankshaft


51


. The connecting sleeve


52


engages the splined shaft


18




a


. A web


53




a


couples an eccentric pin


53


to the connecting sleeve


52


. The web


53




a


is fastened to the splined shaft


18




a


by a bolt


54


. A central bearing sleeve


55


, which extend axially, is integrally formed on the rear surface of the base plate


36


of the orbiting scroll


33


. The eccentric pin


53


is supported by a radial ball bearing


56


, which is fitted in the central sleeve


55


. When the drive crankshaft


51


is rotated by the drive shaft


18


, the eccentric pin


53


orbits, which causes the orbiting scroll


33


to orbit about the axis O


1


of the drive shaft


18


(drive crankshaft


18


). As shown in

FIG. 4

, the orbital radius is a distance R


1


between the axis O


1


and the axis O


2


of the eccentric pin


53


.




As shown in

FIG. 4

, a central balance weight


57


, which has a mass W


1


, is integrally formed on the web


53




a


. The central balance weight


57


is located on the opposite side of the axis O


1


from the eccentric pin


53


. When the orbiting scroll


33


, which has a mass WT, orbits, a centrifugal force, which is based on a moment of inertia MT (WT*R


1




2


) about the axis O


1


of the drive crankshaft


51


, is generated. The central balance weight


57


, which has a mass W


1


, opposes part of the centrifugal force of the orbiting scroll


33


. In other words, the central balance weight


57


balances part of the moment of inertia of the orbiting scroll


33


.




Follower crankshafts


61


(three in this embodiment) are located between the support frame


16


and the base plate


36


of the orbiting scroll


33


. The follower crankshafts


61


permit orbiting motion of the orbiting scroll


33


and prevent the orbiting scroll


33


from rotating about its own axis. Journal shafts


62


of the follower crankshafts


61


are supported by radial ball bearings


64


, which are fitted in annular bearing supports


63


. The bearing supports


63


are formed on the support frame


16


. The bearing supports


63


are closed at the rear ends and extend axially. Eccentric pins


65


are integrally formed at the front ends of the follower crankshafts


61


on webs


65




a


. The eccentric pins


65


are supported by the radial ball bearings


61


, which are fitted in outer bearing sleeves


66


. The outer bearing sleeves


66


are formed on the rear surface of the base plate


36


and extend axially.




As shown in

FIG. 4

, the axes O


3


of the journal shafts


62


are arranged at equal angular intervals on a circle C


62


centered on the axis O


1


of the drive shaft


18


. The orbital radius R


2


of the eccentric pins


65


, which is the distance between the axes O


3


of the journal shafts


62


and the axes O


4


of the eccentric pins


65


, is the same as the orbital radius Rl of the eccentric pin


53


of the drive crankshaft


51


.




Accordingly, when the drive crankshaft


51


orbits, the follower crankshafts


61


permit orbital movement of the orbiting scroll


33


and prevent the orbiting scroll


33


from rotating about the axis O


2


of the eccentric pin


53


.




As shown in

FIG. 2

, predetermined clearances


68


are provided between the peripheral surface


55




a


of the central bearing sleeve


55


of the drive crankshaft


51


and the peripheral surfaces


66




a


of the outer bearing sleeves


66


of the follower crankshafts


61


. Outer balance weights


69


are integrally formed on the webs


65




a


of the follower crankshafts


61


. The outer balance weights


69


can pass through the clearances


68


when rotating. The total mass W


4


of each of the outer balance weights


69


is not determined simply to balance the moment of inertia of the eccentric pins


65


about the axes O


3


of the journal shafts


62


of the respective follower crankshafts


61


. Since the moment of inertia MW


1


(W


1


*R


1




2


) which is based on the mass W


1


of the central balance weight


57


of the crankshaft


51


, is not sufficient to balance the moment of inertia of the orbiting scroll


33


, the masses W


4


of the balance weights


69


are determined to compensate for the insufficiency. In other words, the outer balance weights


69


are not simply for dynamically balancing the respective follower crankshafts


61


but are also for opposing, or balancing, the moment of inertia of the orbiting scroll


33


in cooperation with tho central balance weight


57


. One example of the method for determining the mass of the balance weights


57


,


69


will be described as follows.




W


1


represents a hypothetical mass that is located at the center of gravity G


1


of the central balance weight


57


of the drive crankshaft


51


. W


2


represents a hypothetical mass that is located at the center of gravity G


2


of each of the outer balance weights


69


to balance the moments of inertia about the axes O


3


of the follower crankshafts


61


, respectively. W


3


represents a mass that compensates for the shortage in the mass W


1


to balance the moment of inertia (WT*Rl


2


) about the axis O


1


caused by the mass WT of the orbiting scroll


33


, and the centers of gravity G


1


, G


2


are located on the circles Cr


1


, Cr


2


, which have radiuses R


1


, R


2


, respectively. Further, the journal shafts


62


of the follower crankshafts


61


are located on the circle C


62


about the axis O


1


of the drive shaft


18


at equal angular intervals. The center of gravity GI of the central balance weight


57


is located on the circle Crl of the axis O


2


(center of gravity G


3


) of the eccentric pin


53


of the drive crankshaft


51


and is equidistant with the center of gravity G


3


from the axis O


1


of the drive shaft


18


. The centers of gravity G


2


of the outer balance weights


69


of the follower crankshafts


61


are located on the circles Cr


2


of the axes O


4


(center of gravity G


4


) of the eccentric pins


65


and are equidistant with the centers of gravity G


4


from the axes O


3


of the journal shafts


62


. The centers of the circles Cr


2


are the axes O


3


of the journal shafts


62


of the follower crankshafts


61


.




The total mass W


4


of each balance weight


69


is represented by the following expression.






W


4


=W


2


+W


3


/3






The moment of inertia MT (WT*R


1




2


) about the axis O


1


caused by the mass WT of the orbiting scroll


33


is opposed by the moment of inertia MW


1


(W


1


*R


1




2


) about the axis O


1


caused by the mass W


1


of the central balance weight


57


of the drive crankshaft


51


and by the moments of inertia MW


3


/3(W


3


/3*R


2




2


) about the axes O


3


caused by the masses W


3


/


3


of the outer balance weights


69


of the follower crankshafts


61


.




The ratio of the mass W


3


, which represents the shortage of mass W


1


required to counter the moment of inertia caused by the mass WT of the orbiting scroll


33


to the whole mass (W


1


+W


3


) is in the range of 20 to 100 percent.




Operation of the illustrated scroll-type compressor will now be described.




As shown in

FIGS. 1

,


2


, and


4


, when the drive shaft


18


of the motor


12


rotates, the eccentric pin


53


of the drive crankshaft


51


orbits with the radius R


1


about the axis O


1


of the drive shaft


18


, which causes the orbiting scroll


33


to orbit about the axis O


1


through the bearing


56


. During this movement, the eccentric pins


65


of the follower crankshafts


61


orbit with the radius R


2


(which is equal to radius R


1


) about the axis O


3


of the journal shafts


62


. This permits the orbiting scroll


33


to orbit without rotating about the eccentric pin


53


.




Therefore, refrigerant gas is drawn to the suction chamber


39


through the suction port


40


and then to the compression chambers


38


. As the orbiting scroll


33


orbits, the compression chambers move from the periphery to the center of the spiral portions


35


,


37


, and this gradually reduces their volumes. Accordingly, refrigerant gas in the compression chambers


38


is gradually compressed and is discharged to the external refrigerant circuit through the discharge port


41


.




The scroll-type compressor has the following advantages.




(1) In the illustrated embodiment of

FIGS. 1-4

, the mass W


3


/3 is added to each outer balance weight


69


of the follower crankshafts


61


to generate a moment of inertia that balances part of the moment of inertia MT of the orbiting scroll


33


. Therefore, it is possible to reduce the mass W


1


of the central balance weight


57


of the drive crankshaft


51


and to reduce the radius of the path C


1


of the central balance weight


57


as shown in

FIG. 4

compared to the prior art examples. As a result, the outer bearing sleeves


66


, which support the eccentric pins


65


of the follower crankshafts


61


, are formed radially near the central bearing sleeve


55


of the drive crankshaft


51


on the base plate


36


of the orbiting scroll


33


. Therefore, the outer bearing sleeves


66


do not extend outward from the periphery of the base plate


36


, which reduces the size of the compressor housing


31


.




As shown in

FIG. 4

, the peripheral surfaces of the outer balance weights


69


of the follower crankshafts


61


define the circles C


3


about the axes O


3


of the fixed journal shafts


62


. Therefore, when the orbiting scroll


33


orbits, the outer balance weights


69


do not interfere with the housing


31


shown in FIG.


2


.




(2) In the illustrated embodiment, the clearances


68


are formed between the peripheral surface


55




a


of the central bearing sleeve


55


and the peripheral surfaces


66




a


of the outer bearing sleeves


66


. The outer balance weights


69


pass through the clearances


68


. Also, the center of gravity G


4


is equidistant with and 180 degrees from the corresponding center of gravity G


2


with respect to the axis O


3


of the corresponding journal shaft


62


to generate rotational imbalance from the moment of inertia in the follower crankshaft


61


. Therefore, the prior art trim weights as shown in

FIG. 11

are not required, which reduces the number of parts and simplifies the structure of the compressor.




The masses W


2


of the outer balance weights


69


, which balance the moments of inertia about the axes O


3


of the respective follower crank shafts


61


, are minimized, that is, the mass W


2


can be the same as the mass of one of the eccentric pins


65


. This reduces the mass of the follower crankshafts


61


.




(3) The moment of inertia MT (WT*R


2




2


) due to the mass WT of the orbiting scroll


33


is countered by the combination of the moment of inertia MW


1


(WT*R


1




2


) caused by the mass W


1


of the central balance weight


57


and the equal moments of inertia caused by the masses W


3


/3 of the three outer balance weights


69


. This reduces the mass of each balance weight


57


,


69


and also reduces the maximum radii, which relatively stabilizes the orbital movement of the orbiting scroll


33


compared to the prior art structure. In the prior art structure, a relatively great balance weight is located only on the drive crankshaft


51


, and the drive crankshaft


51


orbits with a relatively large maximum path radius.




(4) In the illustrated embodiment, the journal shafts


62


of the follower crankshafts


61


are arranged on the circle C


62


about the axis O


1


of the drive shaft


18


at equal intervals. Also, the center of gravity G


1


of the central balance weight


57


is located on the circular path Cr


1


of the center of gravity G


3


(axis O


2


) of the eccentric pin


53


, which orbits about the axis O


1


of the drive shaft


18


and is equidistant with the center of gravity G


3


from the axis O


3


. Further, the centers of gravity G


2


of the outer balance weights


69


of the follower crankshafts


61


are located on the circular path Cr


2


of the centers of gravity G


4


(axes O


4


) of the eccentric pins


65


about the axes O


3


of the journal shafts


62


, and are equidistant with the centers of gravity G


4


from the axes O


3


, respectively.




Accordingly, this minimizes the masses W


1


, W


4


of the central balance weight


57


and the outer balance weights


69


.




(5) Under the conditions described in part (4) above, the masses W


4


of the outer balance weights


69


are determined based on the expression W


4


=W


2


+W


3


/n. This facilitates determining the masses W


4


.




The present invention can further be embodied as follows.




As shown in

FIG. 5

, the central balance weight


57


of the drive crankshaft


51


may be omitted, and outer balance weights


69


having the equal masses W


4


=W


2


+W


3


/4 may be attached to four follower crankshafts, which are provided at four locations. The structure of the compressor of

FIG. 5

is otherwise the same as that of the first embodiment.




The embodiment of

FIG. 5

has the advantages (1), (2), (3), (4), and (5).




In a third embodiment shown in

FIG. 6

, a trim weight


84


is secured to the rear end of the drive shaft


18


(on the opposite end of the drive shaft


18


from the drive crankshaft


51


) by a bolt


85


. The trim weight


84


mitigates a force that tends to bend the drive crankshaft


51


(and the drive shaft


18


).

FIG. 7

is a diagrammatic view for illustrating the moments of inertia of each member of FIG.


6


. The method of determining the mass and location of the trim weight


84


will now be described with reference to FIG.


7


.




MW


1


represents a moment of inertia about the axis O


1


of the orbiting scroll


33


, which is countered by the central balance weight


57


. M


65


and M


65




a


represent moments of inertia about the axes O


3


of the eccentric pins


65


and the webs


65




a


of the follower crankshafts


61


. MW


4


represents moments of inertia about the axes O


3


of the outer balance weights


69


. M


53


and M


53




a


represent moments of inertia about the axis O


1


of the eccentric shaft


53


and a web


53




a


of the drive crankshaft


51


. M


84


represents a moment of inertia about the axis O


1


of the trim weight


84


. A principal axis of inertia that nullifies the product of inertia, which is the sum of these moments of inertia, is determined to coincide with the axis O


1


of the drive crankshaft


51


.




Accordingly, orbiting movement of the orbiting scroll


33


is smoothly performed by the drive shaft


18


and the drive crankshaft


51


in the present embodiment.




As shown in

FIG. 8

, in the prior art scroll-type compressor of

FIG. 11

, balance weights


83


, each having a mass W


3


/n (n represents the number of the balance weights


83


) may be attached to the balance weights


81


of the follower crankshafts


61


. Accordingly, the sum of the moments of inertia about the axes O


3


of the journal shafts


62


of the entire follower crankshafts


61


may not be null.




The present embodiment also prevents the outer bearing sleeves


66


from projecting from the circumferential surface of the base plate


36


.




The number of the follower crankshafts


61


may be varied to be one, two, or five or more. As the number of the follower crankshafts


61


is increased, the mass W


1


of the central balance weight


57


is reduced, and the mass W


3


/n of each outer balance weight


69


is reduced. This achieves smooth orbiting of the orbiting scroll


33


. However, there is an upper limit to the number of the follower crankshafts due to interference.




It should be apparent to those skilled in the art that the present invention may be embodied in many other specific forms without departing from the spirit or scope of the invention. Therefore, the present examples and embodiments are to be considered as illustrative and not restrictive and the invention is not to be limited to the details given herein, but may be modified within the scope and equivalence of the appended claims.



Claims
  • 1. A scroll type compressor comprising:a housing; a fixed scroll fixed to the housing, the fixed scroll having a spiral portion formed on a base thereof; an orbiting scroll having a spiral portion formed on a base thereof to engage the fixed scroll, the orbiting scroll having a center axis offset from that of the fixed scroll; a driving crankshaft connected to the base of the orbiting scroll to produce orbital motion; follower crankshafts connected to the housing and the base of the orbiting scroll to follow the motion of the orbiting scroll and prevent the orbiting scroll from rotating about its own axis; and balance weights for balancing a moment of inertia of the orbiting scroll about the driving crankshaft, wherein the balance weights are located on at least the follower crankshafts.
  • 2. A scroll type compressor as recited in claim 1, wherein the balance weights are located on both the driving crankshaft and the follower crankshafts.
  • 3. A scroll type compressor as recited in claim 2, wherein the driving crankshaft has a connecting portion connected to a drive shaft, the driving crankshaft including an eccentric pin connected to the connecting portion by a web portion, wherein the eccentric pin is supported by a central bearing sleeve formed on the base of the orbiting scroll and wherein the balance weight of the driving crankshaft is connected to the web portion at a location that is on an opposite side of the axis of the connecting portion from the eccentric pin.
  • 4. A scroll type compressor as recited in claim 3, wherein each of the follower crankshafts has a journal shaft, which is supported by a bearing support formed on a portion of the housing, and an eccentric pin connected to the journal shaft by the web portion, wherein each eccentric pin is supported by a respective outer bearing sleeve formed on the base of the orbiting scroll, wherein the balance weight of each of the follower crankshafts is connected to the web portion at a location that is on an opposite side of the axis of the journal shaft from the eccentric pin, wherein radial clearances exist between an outer surface of the central bearing sleeve and outer surfaces of the outer bearing sleeves, and wherein each balance weight passes through at least one of the clearances.
  • 5. A scroll type compressor as recited in claim 4, wherein the journal shafts of the follower crankshafts are located at regular angular intervals on the same circle centered on the axis of the drive shaft, wherein the center of gravity of the balance weight of the driving crankshaft and the center of gravity of the eccentric pin are equidistant from the axis of the drive shaft, and wherein the center of gravity of the balance weight of each of the follower crankshafts and the center of gravity of the corresponding eccentric pin are equidistant from the axis of the corresponding journal shaft.
  • 6. A scroll type compressor as recited in claim 5, wherein a mass W4 of the balance weight of each of the follower crankshafts is represented by the expressionW4=W2+W3/n wherein the moment of inertia about the axis of the driving crankshaft of the orbiting scroll is balanced by the moment of inertia about the axis of the driving crankshaft of the balance weight of the driving crankshaft and the moments of inertia about the axes of the respective follower crankshafts of the balance weights of the follower crankshafts, wherein W2 is a mass at the center of gravity of each balance weight of each of the follower crankshafts necessary to balance the centrifugal force of the associated follower crankshaft, W3 is the difference between the mass of the balance weight of the driving crankshaft and the mass required to balance the moment of inertia of the orbiting scroll, and n is the number of balance weights of the follower crankshafts.
  • 7. A scroll type compressor as recited in claim 3, wherein the moment of inertia of the balance weight of the driving crankshaft is set to balance the moment of inertia occurring about the axis of the driving crankshaft of the eccentric pin of the driving crankshaft and a portion of the moment of inertia of the orbiting scroll, and wherein the moments of inertia of the balance weights of the follower crankshafts balance the respective moments of inertia occurring about the axes of the follower crankshafts by the eccentric pins of the follower crankshafts and a respective share of the remainder of the moment of inertia of the orbiting scroll.
  • 8. A scroll type compressor as recited in claim 7, wherein a ratio of W3 to W1+W3 is in the range of 20% to 100%, where W1 is the mass of the balance weight of the driving crankshaft and W3 represents the difference between W1 and the mass required to balance the moment of inertia of the orbiting scroll.
  • 9. A scroll type compressor as recited in claim 1, wherein the number of the follower crankshafts is three or more.
  • 10. A scroll type compressor as recited in claim 1, wherein the balance weights balance the moment of inertia of the orbiting scroll, the moment of inertia of the driving crankshaft and the total moments of inertia of each of the follower crankshafts.
  • 11. A scroll type compressor as recited in claim 10, further comprising a drive shaft for rotating the driving crankshaft and a trim weight provided on the drive shaft at a position axially spaced from the driving crankshaft, the trim weight balancing a first moment of inertia operating in a direction that tends to bend the driving crankshaft, wherein the mass and position of the trim weight are set so that a main axis of inertia coincides with the axis of the driving crankshaft where in the main axis of inertia, product of inertia becomes zero and product of inertia is the sum total of the first moment of inertia and the moment of inertia of the trim weight.
  • 12. A scroll type compressor as recited in claim 11, wherein the product of inertia includes the sum total of the moment of inertia of the orbiting scroll, the moment of inertia of a pin and a web portion of each of the follower crankshafts, the moment of inertia of each of the balance weights of the follower crankshafts, the moment of inertia of a pin and a web portion of the driving crankshaft, the moment of inertia of the balance weight of the driving crankshaft and the moment of inertia of the trim weight.
  • 13. A scroll type compressor as recited in claim 11, further comprising a trim weight provided on each follower crankshaft at a position axially spaced from the orbiting scroll, the trim weight balancing a moment of inertia created by the balance weight of the corresponding follower crankshafts in a direction that tends to bend the corresponding follower crankshaft.
  • 14. A scroll type compressor as recited in claim 1, wherein a central bearing sleeve is provided on the base of the orbiting scroll to receive part of the driving crankshaft to cause the orbiting scroll to orbit, and outer bearing sleeves are provided on the base of the orbiting scroll to receive parts of the follower crankshafts, wherein there are radial clearances between each outer bearing sleeve and the central bearing sleeve, and wherein each of the balance weights passes through at least one of the clearances.
Priority Claims (1)
Number Date Country Kind
10-315070 Nov 1998 JP
US Referenced Citations (5)
Number Name Date Kind
5033945 Kolb Jul 1991
5556269 Suzuki et al. Sep 1996
5690480 Suzuki et al. Nov 1997
5842842 Callens et al. Dec 1998
5951271 DuMoulin et al. Sep 1999
Foreign Referenced Citations (7)
Number Date Country
2025530 Jan 1980 GB
61-261689 Nov 1986 JP
64-063679 Mar 1989 JP
1-061480 Apr 1989 JP
4-308381 Oct 1992 JP
10-252668 Sep 1998 JP
10-299675 Nov 1998 JP