Fitting structure for controlling valve in variable capacity compressor

Information

  • Patent Grant
  • 6254356
  • Patent Number
    6,254,356
  • Date Filed
    Monday, February 28, 2000
    24 years ago
  • Date Issued
    Tuesday, July 3, 2001
    23 years ago
Abstract
In a fitting structure of a control valve in a variable capacity compressor according to the present invention, a step portion 92 is formed by connecting two taper surfaces 93a and 93b, the diameter of each of which decreases progressively towards the depth of a fitting hole 32 (in an inserting direction of a control valve 33) between each step surface portion 57, 67, 74, 91 of a fitting hole 32. A first taper surface 93a at a deep part of each step portion 92 has a smaller inclination in the inserting direction than a second taper surface 93b on the inlet side. The first taper surface 93a is formed so that its inner diameter on the inlet side is a little greater than the outer diameter of each O-ring 61, 70, 77 disposed on each step surface portion 57, 67, 74 in a free condition.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




This invention relates to a fitting structure for a control valve for controlling a discharge capacity in a variable capacity compressor used for a car air conditioner, for example.




2. Description of the Related Art




The following construction is known for a variable capacity compressor (hereinafter called merely the “compressor”) of the kind described above. A crank chamber is defined and partitioned inside a housing, and a drive shaft is rotatably supported by the housing in such a fashion as to cross, transversely, the crank chamber. A swash plate is supported by the drive shaft through a rotary support member inside the crank chamber in such a fashion as to be capable of integrally rotating and rocking. A plurality of pistons are engaged with to the outer peripheral portion of the swash plate. Cylinder bores are formed in a cylinder block, that constitutes a part of the housing, equiangularly arranged around the drive shaft. The head of each piston is fitted into each cylinder bore and is allowed to reciprocate.




When the drive shaft is driven for rotation by driving force transmitted thereto from an external driving source such as a car engine through a belt, or the like, the swash plate is rotated through the rotary support. The rotary motion of this swash plate is converted to the reciprocating motion of each piston. In consequence, a series of compression cycles such as suction of a refrigerant gas into the cylinder bores, compression of the refrigerant gas so sucked and discharge of the compressed refrigerant gas from the cylinder bores are repeated.




In the compressor described above, a discharge pressure region, in which the compressed refrigerant gas stays temporarily, and the crank chamber are connected through an supply passage having a control valve. The control valve is fitted into a fitting hole formed in a rear housing that constitutes a part of the housing of the compressor. This control valve plays the roles of changing an open area in the supply passage and regulating the feeding amount of the high-pressure discharge refrigerant gas into the crank chamber. When the feeding amount of the discharge refrigerant gas is adjusted, the internal pressure of the crank chamber is varied, and the pressure difference between the pressure of the crank chamber piston and the pressure of the cylinder bores through the piston is varied, too. As the pressure difference is varied, the tilt angle of the swash plate is varied, and the stroke of each piston, that is, the discharge capacity, is regulated.




The control valve shown in

FIG. 7

is known as a control valve


200


of this kind. The control valve


200


includes a valve body


202


for opening and closing the supply passage


201


described above, an electromagnetic driving portion


203


for changing the load applied to the valve body


202


in accordance with an input current value, and a pressure-sensitive mechanism


205


for changing the load applied to the valve body


202


in accordance with the pressure of the suction pressure region of the compressor. In this control valve, the overall force of the impressed load from the pressure-sensitive mechanism


205


and the impressed load from the electromagnetic driving portion


203


operates the valve body


202


, and the open area of the supply passage


201


is decided.




Gas chambers such as a valve chest


207


for storing the valve body


202


and a pressure-sensitive chamber


208


for storing the pressure-sensitive mechanism


205


are defined and partitioned inside the valve housing


206


of the control valve


200


. A plurality of step portions


209




a


to


209




c


are defined in the valve housing


206


. A pressure-sensitive hole


210


that communicates with the pressure-sensitive chamber


208


is open to the first step portion


209




a


. A valve port


211


that can be connected and disconnected to the valve chest


207


by the valve body


202


is open to the second step portion


209




b


. An inlet port


212


that communicates with the valve chest


207


is open to the third step portion


209




c.






Each of these step portions


209




a


to


209




c


is partitioned hermetically by an O-ring


214


while the control valve


200


is fitted to the fitting hole


213


of the compressor. This is because different pressures are guided to the pressure-sensitive hole


210


, the valve port


211


and the inlet port


212


, respectively.




A taper surface


216


the diameter of which decreases progressively towards the bottom of the fitting hole


213


is formed in the fitting hole


213


in such a fashion as to correspond to a holding portion


215


of the O-ring


214


as shown in

FIGS. 5B and 7

. As the O-ring


214


passes over the taper surface


216


during the fitting operation of the control valve, it is compressed in a predetermined quantity.




Incidentally, the compressor is mounted in the proximity of the engine inside the car engine room. The mounting space of the compressor inside the engine room is limited, and there has been a strong requirement for reducing the size of the compressor, particularly the requirement for reducing its projecting distance from the outer periphery in the diametric direction of the housing


217


.




In the compressor having the conventional construction described above, its control valve


200


includes the electromagnetic driving portion


203


and the pressure-sensitive mechanism


205


. Therefore, it is elongated in the axial direction. As indicated by two-dot-chain line in

FIG. 3

, the control valve


200


is fitted while its proximal end portion protrudes from the outer periphery of the housing


217


of the compressor. When this protruding distance is great, the control valve


200


interferes with the car engine or other auxiliary machinery, and mountability of the compressor to the car is poor.




To cope with this problem, the full length of the control valve


200


in the axial direction may be reduced. In this case, the reduction of the length in the axial direction is limited because the electromagnetic driving portion


203


and the pressure-sensitive mechanism


205


have to apply predetermined impressed loads to the valve body


202


inside the control valve


200


. In other words, if the length of electromagnetic driving portion


203


and the pressure-sensitive mechanism


205


are greatly decreased in the axial direction, the predetermined impressed loads are likely to be insufficient, and the regulation capability of the valve body


202


of adjusting the open area to the supply passage


201


may drop. In consequence, stability of discharge capacity control in the compressor may drop.




Therefore, the length in the axial direction must be reduced at the intermediate portion between the electromagnetic driving portion


203


and the pressure-sensitive mechanism


205


in the valve housings


206


. In this case, the width of the second and third step portions


209




b


and


209




c


becomes small. Consequently, the distances between the O-rings


214


that separate them and the distances between the pressure-sensitive hole


210


, the valve port


211


and the inlet port


212


opening to the step portions


209




a


to


209




c


become short, too. The distances between the taper surfaces


216


inside the fitting hole


213


become short, as well. The requirement for machining accuracy of the pressure detecting passage


218


and the supply passage


201


that open to oppose the pressure-sensitive hole


210


, the valve port


211


and the inlet port


212


on the inner peripheral surface of the fitting hole


213


, becomes higher with the result that the production cost of the compressor becomes higher.




A predetermined open area must be secured, in some cases, in each of the supply passage


201


and the pressure detecting passage


218


in order to restrict an excessive pressure loss. In such a case, a part of each passage extends over the taper surface


216


. When a part of the pressure detecting passage


218


or the supply passage


201


is open over the taper surface


216


, the O-ring


214


is damaged when it passes over the taper surface


216


while being compressed, and a pressure leak is more likely to occur. In consequence, capacity control in the compressor becomes unstable.




If the inclination of the taper surface


216


is increased in order to avoid the possible damage of the O-ring


214


, the problem that a part of the pressure detecting passage


218


and the supply passage


201


is open over the taper surface


216


can be avoided. However, because the O-ring


214


is drastically compressed, the resistance increases remarkably when the control valve


200


is inserted, and the assembling property of the control valve


200


to the compressor drops. In this case, too, the production cost of the compressor becomes higher.




SUMMARY OF THE INVENTION




In view of the problems of the fitting structures of the prior art described above, the present invention is directed to provide a fitting structure of a control valve in a variable capacity compressor which fitting structure makes it easy to fit the control valve without inviting the increase of the production cost and the drop of capacity controllability in the compressor.




To accomplish this object, the fitting structure of the control valve according to a preferred embodiment of the present invention has the following structure. In a fitting structure of a control valve in a variable capacity compressor of the type which includes a plurality of step portions in appearance and in which a hole communicating with a gas chamber defined inside the control valve is open to at least one of the step portions and each of the step portions is partitioned by a seal member under the condition where the control valve is fitted into a fitting hole of the variable capacity compressor, the fitting structure according to the present invention is characterized in that the fitting hole has a plurality of step portions so formed as to correspond to seal member holding portions of the control valve, each of the step portions is shaped into an inclined surface the diameter of which progressively decreases from the inlet side towards the bottom in an inserting direction of the control valve, and a diameter reduction amount per unit moving distance of the control valve on the inclined surface is greater on the inlet side of the inclined surface than on the depth side.




According to this embodiment, the inclination of the inclined surface on the inlet side can be increased while the other side has a small inclination in the inserting direction of the control valve. Because the seal member is compressed by the bottom portion of the inclined surface, the increase in the resistance at the time of fitting of the control valve can be avoided. On the other hand, because the inclination on the inlet side of the inclined surface is increased, the width of the slope can be made smaller than when the slope comprises a single small inclination. In consequence, the open area of the pressure detecting passage and the supply passage in the fitting hole of the compressor can be secured sufficiently while the length in the axial direction of the control valve is reduced.




In a fitting structure of a control valve in a variable capacity compressor of the type which includes a plurality of step portions in appearance and in which a hole communicating with a gas chamber defined inside the control valve is open to at least one of the step portions and each of the step portions is partitioned by a seal member under the condition where the control valve is fitted into a fitting hole of the variable capacity compressor, the fitting structure of a control valve according to the present invention is characterized in that the fitting hole has a plurality of step portions so formed as to correspond to seal member holding portions of the control valve, and each of the step portions forms a curve surface having a different radius of curvature from the inlet side towards the other side in the inserting direction of the control valve.




According to this embodiment, the curve surfaces are formed so that their radii of curvature become gradually greater from the inlet side towards the other side. Therefore, the inclination of the control valve at the step portion in the inserting direction can be made greater towards the inlet side while the increase of the resistance at the time of fitting of the control valve is avoided.











The present invention may be more fully understood from the description of preferred embodiments of the invention set forth below, together with the accompanying drawings.




BRIEF DESCRIPTION OF THE DRAWINGS




In the drawings:





FIG. 1

is a sectional view showing a fitting structure of a control valve according to one embodiment of the present invention;





FIG. 2

is a sectional view showing a variable capacity compressor equipped with the fitting structure of the control valve shown in

FIG. 1

;





FIG. 3

is a side view of the variable capacity compressor shown in

FIG. 2

when it is viewed from a rear housing side;





FIG. 4

is a partial sectional view showing in enlargement the step portions shown in FIG.


1


and portions around the former;





FIG. 5A

is a partial sectional view showing in enlargement the principal portions of

FIG. 1

;





FIG. 5B

is a partial enlarged view showing the principal portions of a fitting structure of a control valve according to the prior art;





FIG. 6

is a partial sectional view showing in enlargement the principal portions of the fitting structure of the control valve according to a modified embodiment of the present invention; and





FIG. 7

is a sectional view showing the fitting structure of the control valve according to the prior art.











DESCRIPTION OF THE PREFERRED EMBODIMENTS




Hereinafter, an embodiment wherein the present invention is applied to the fitting structure of a control valve of a single-head piston, swash type variable capacity compressor, will be explained with reference to

FIGS. 1

to


5


.




To begin with, the general construction of the variable capacity compressor (hereinafter called merely the “compressor”) will be explained.




A front housing


11


is joined and fixed to the front end of a cylinder block


12


as shown in

FIG. 2. A

rear housing


13


is joined and fixed to the rear end of the cylinder block


12


through a valve plate


14


. The front housing


11


, the cylinder block


12


and the rear housing


13


together constitute the housing of the compressor.




A crank chamber


15


as a pressure chamber is defined and encompassed by the front housing


11


and the cylinder block


12


. A drive shaft


16


is supported by, and extends between, the front housing


11


and the cylinder block


12


in such a manner as to cross the crank chamber


15


and to be capable of rotating. The front end side of this drive shaft


16


is connected to an external driving source such as a car engine through pulleys, belts, and the like, that are not shown, and is caused to rotate by the driving force from the car engine.




A lug plate


17


is fixed to the drive shaft


16


inside the crank chamber


15


, and the drive shaft


16


is inserted through a swash plate


18


as a cam plate. This swash plate


18


is interconnected to the lug plate in such a manner as to be capable rotating with the lug plate


17


through a hinge mechanism


19


. The hinge mechanism


19


, the swash plate


18


and the drive shaft


16


are fitted to one another in such a fashion that the swash plate


18


can slide while inclining with respect to the drive shaft


16


in the axial direction of the driving shaft


16


.




When the radial center portion of the swash plate


18


slides and moves towards the cylinder block


12


as indicated by two-dot-chain lines in

FIG. 2

, the tilt angle of the swash plate


18


decreases. On the other hand, when the radial center portion of the swash plate


18


slides and moves towards the lug plate


17


as indicated by solid lines in

FIG. 2

, the tilt angle of the swash plate


18


increases.




A plurality (six, for example) of cylinder bores


12




a


are formed in the cylinder block


12


equiangularly round the axis of the drive shaft


16


with predetermined distances between them. Each cylinder bore


12




a


accommodates therein the head portion


20




a


of a singlehead type piston


20


in such a manner as to allow its reciprocation. The neck (


20




b


) side of each piston


20


is engaged with to the outer peripheral portion of the swash plate


18


through a pair of shoes


21


. In consequence, the rotary motion of the drive shaft


16


is converted to the longitudinal reciprocating motion of the head portion


20




a


of the piston


20


inside the cylinder bore


12




a


through the lug plate


17


, the hinge mechanism


19


, the swash plate


18


and the shoe


21


.




A suction chamber


24


as a pressure chamber that constitutes a suction pressure region and a discharge chamber


25


as a pressure chamber that constitutes a discharge pressure region are partitioned and defined inside the rear housing


13


. Suction ports


26


, suction valves


27


, discharge ports


28


and discharge valves


29


are formed in the valve plate


14


in such a manner as to correspond to the cylinder bores


12




a


, respectively. The suction port


26


communicates the suction chamber


24


with each cylinder bore


12




a


, and the suction valve


27


opens and closes the suction port


26


. The discharge port


28


communicates the discharge chamber


25


with each cylinder bore


12




a


, and the discharge valve


29


opens and closes this discharge port


28


.




When the drive shaft


16


is driven and rotated by an external driving source, not shown, and the piston


20


is moved from the upper dead point towards the lower dead point, the refrigerant gas inside the suction chamber


24


is sucked into the cylinder bores


12




a


through the suction port


26


while pushing away the suction valve


27


. The refrigerant gas sucked into the cylinder bores


12




a


in this way is compressed to a predetermined pressure due to the movement of the piston from the lower dead point side towards the upper dead point side. The refrigerant gas so compressed is discharged into the discharge chamber


25


while pushing away the discharge valve


29


.




The crank chamber


15


and the suction chamber


24


are communicated with each other by a bleeding passage


30


. The discharge chamber


25


and the crank chamber


15


are communicated with each other as an supply passage


31


, that is, a communication passage. A control valve


33


is fitted to an intermediate part of this supply passage


31


inside a fitting hole


32


that is formed at the rear end portion of the rear housing


13


.




An external refrigerant circuit


34


communicates the suction chamber


24


and the discharge chamber


25


. This external refrigerant circuit


34


includes a condenser


35


, an expansion valve


36


and an evaporator


37


. The external refrigerant circuit


34


and the compressor, that has the construction described above, together constitute a refrigerating circuit. An evaporator temperature sensor


38


is disposed in the proximity of the evaporator


37


, detects the temperature of the evaporator


37


and outputs this detection temperature information to a controlling computer


39


. A cabin temperature setter


40


for setting the temperature inside the cabin of the car and a cabin temperature sensor


41


, for example, are connected to the controlling computer


39


.




The controlling computer


39


gives an input current value to a driving circuit


42


on the basis of external signals such as the room temperature set in advance by the cabin temperature setter


40


, the detection temperature acquired from the evaporator temperature sensor


38


and the detection temperature acquired from the cabin temperature sensor


41


, for example. The driving circuit


42


outputs and applies the instructed input current value to a coil


86


of the control valve


33


described later.




Next, the control valve


33


will be explained.




The control valve


33


has a construction in which an electromagnetic driving portion


51


and a valve housing


52


are joined at the center as shown in

FIG. 1. A

pressure-sensitive chamber


53


as a gas chamber is partitioned and defined on the distal end side inside the valve housing


52


. Bellows


54


are accommodated in this pressure-sensitive chamber


53


. A first step portion


55


is formed on the outer peripheral surface of the portion of the valve housing


52


that corresponds to the pressure-sensitive chamber


53


. A pressure-sensitive hole


56


communicating with the pressure-sensitive chamber


53


is open to the first step portion


55


. The inner peripheral surface


32




a


of the fitting hole


32


in the rear housing


13


opposing the first step portion


55


functions as a first step surface portion


57


. A pressure detecting passage


58


, that serves as a communication passage communicating with the suction chamber


24


, is open at the position on the first step surface portion


57


that opposes the pressure-sensitive hole


56


.




A second step portion


59


is formed on the outer peripheral surface of the valve housing


52


in such a manner as to continue the first step portion


55


. A first O-ring holding portion


60


which is in the shape of an annular groove is formed on the distal end side of the second step portion


59


, and holds a first O-ring


61


as a seal member. The first O-ring


61


hermetically partitions to seal the space between the first step portion


55


and the first step surface portion


57


opposing the former. The suction pressure Ps inside the suction chamber


24


is guided into the pressure-sensitive chamber


53


through the pressure detecting passage


58


and the pressure-sensitive hole


56


.




A valve chest


64


as a gas chamber is partitioned and defined inside the valve housing


52


on the side of the electromagnetic driving portion


51


, and a valve body


65


for regulating the open area of the supply passage


31


is accommodated in the valve chest


64


. A valve port


66


that communicates with the valve chest


64


is open to the position opposing the valve body


65


of the valve chest


64


on one hand, and is open onto the second step portion


59


, on the other.




The inner peripheral surface


32




a


of the fitting hole


32


in the rear housing


13


, opposing the second step portion


59


, functions as a second step surface portion


67


. An upstream side supply passage


31




a


communicating with the discharge chamber


25


is open at a position opposing the valve port


66


on this second step surface portion


67


.




A third step portion


68


is formed on the outer peripheral surface of the valve housing


52


in such a manner as to continue the second step portion


59


. A second O-ring holding portion


69


which is in the shape of an annular groove is formed on the distal end side of the third step portion


68


, and a second O-ring


70


as a seal member is held by this second O-ring holding portion


69


.




The second O-ring


70


and the first O-ring


61


described above hermetically partition to seal the space between the second step portion


59


and the second step surface portion


67


opposing the second step portion


59


. The discharge pressure Pd inside the discharge chamber


25


is guided into the valve port


66


through the upstream side supply passage


31




a.






The third step portion


68


is the portion that corresponds the valve chest


64


of the outer peripheral surface of the valve housing


52


. An supply hole


73


that communicates with the valve chest


64


is open to the third step portion


68


. The inner peripheral surface


32




a


of the fitting hole


32


in the rear housing


13


opposing the third step portion


68


, serves as the third step surface portion


74


. A downstream side supply passage


31




b


communicating with the crank chamber


15


is open at the position on the third step surface portion


74


that opposes the supply hole


73


.




A fourth step portion


75


, as still another step portion, is formed on the outer peripheral surface of the valve housing


52


in such a manner as to continue the third step portion


68


. A third O-ring holding portion


76


which is in the shape of an annular groove is formed on the distal end side of this fourth step portion


75


, and a third O-ring


77


as a seal member is held by this third O-ring holding portion


76


. The third O-ring


77


and the second O-ring


70


hermetically partition to seal the space between the third step portion


68


and the third step surface portion


74


opposing the former. The crank chamber pressure Pc inside the crank chamber


15


is guided into the valve chest


64


through the downstream side supply passage


31




b


and the supply hole


73


. In this way, the valve chest


64


and the valve port


66


constitute a part of the supply passage


31


.




A pressure-sensitive rod


80


is formed integrally with the valve body


65


, and the bellows


54


and the valve body


65


are operatively connected through this pressure-sensitive rod


80


. In other words, the bellows


54


extend and contract in accordance with the change of the suction pressure Ps, and the biasing force corresponding to the change of the suction pressure Ps is transmitted to the valve body


65


through the pressure-sensitive rod


80


.




A compulsive opening spring


81


is disposed between the valve body


65


and the inner wall surface of the valve chest


64


opposing the valve body


65


. The valve body


65


opens the valve port


66


by the operation of this compulsive opening spring


81


under the non-operative condition of the bellows


54


and the electromagnetic driving portion


51


.




The electromagnetic driving portion


51


is joined in such a manner as to continue the fourth step portion


75


of the valve housing


52


. A plunger chamber


82


is partitioned and defined inside the electromagnetic driving portion


51


on the opposite side to the pressure-sensitive chamber


53


relative to the valve chest


64


. A fixed iron core


83


is fitted to an upper opening of the plunger chamber


82


. A movable iron core


83


is so accommodated in the plunger chamber


82


as to oppose the fixed iron core


83


. A follower spring


85


is interposed between the movable iron core


84


and the bottom surface of the plunger chamber


82


and biases the movable iron core


84


towards the valve chest


64


. A coil


86


is disposed outside the fixed iron core


83


and the movable iron core


84


in such a manner as to bridge over both iron cores


83


and


84


. The driving circuit


42


described above is connected to this coil


86


so that the electromagnetic force corresponding to the input current value from the driving circuit


42


can be generated.




An electromagnetic driving rod


87


is formed integrally with the valve body


65


on the opposite side to the pressure-sensitive rod


80


. The end portion of this electromagnetic driving rod


87


on the side of the movable iron core


84


is brought into contact with the movable iron core


84


by the biasing force of the follower spring


85


and the compulsive opening spring


81


. In consequence, the movable iron core


84


and the valve body


65


are operatively connected through the electromagnetic driving rod


87


, and the biasing force corresponding to the electromagnetic force generated in the coil


86


is transmitted to the valve body


65


.




Next, the changing operation of the discharge capacity by the compressor having the construction described above will be explained.




When the detection temperature acquired from the cabin temperature sensor


41


is higher than the set temperature of the cabin temperature setter


40


, the controlling computer


39


gives the instruction to the driving circuit


42


to supply a predetermined current to the coil


86


of the control valve


33


. As the supply of the current to the coil


86


is started, the attraction force (electromagnetic force) is generated in accordance with the input current value between both iron cores


83


and


84


. This attraction force is transmitted to the valve body


65


as the load in the approaching direction to the valve port


66


against the biasing force of the compulsive opening spring


81


, that is, in the direction in which the open area of the supply passage


31


decreases.




On the other hand, the bellows


54


extend and contract in accordance with the change of the suction pressure Ps introduced into the pressure-sensitive chamber


53


through the pressure detecting passage


58


.




The load transmitted to the valve body


65


through the pressure-sensitive rod


80


changes in accordance with the extension and contraction of the bellows


54


.




In other words, when the suction pressure Ps becomes high, the bellows


54


undergo contraction, and the load in the approaching direction to the valve port


66


, that is, the direction in which the open area of the supply passage


31


decreases, is transmitted to the valve body


65


. When the suction pressure Ps becomes low, on the other hand, the bellows


54


undergo extension, and the load in the departing direction from the valve port


66


, that is, in the direction in which the open area of the supply passage


31


increases, is transmitted to the valve body


65


. The control valve


33


operates the valve body


65


by the overall force based on the force of the compulsive opening spring


81


and the follower spring


85


in addition to the impressed load based on the attraction force between both cores


83


and


84


and the impressed load based on the extension and contraction of the bellows


54


. In this way, the control valve


33


determines the open area of the supply passage


31


.




When the open area of the supply passage


31


inside the control valve


33


becomes small, the amount of the refrigerant gas supplied from the discharge chamber


25


to the crank chamber


15


through the supply passage


31


becomes small. Since a predetermined amount of the refrigerant gas in the crank chamber


15


always flows out into the suction chamber


24


through the bleeding passage


30


, the crank chamber pressure Pc inside the crank chamber


15


drops. Therefore, the pressure difference, through the piston


20


, between the crank chamber pressure Pc and the pressure inside the cylinder bores


12




a


becomes small, and the tilt angle of the swash plate


18


becomes great. As a result, the stroke of the piston


20


becomes great and the discharge capacity increases.




When the open area of the supply passage


31


inside the control valve


33


becomes great, on the other hand, the amount of the refrigerant gas supplied from the discharge chamber


25


to the crank chamber


15


becomes great. In consequence, the crank chamber pressure Pc of the crank chamber


15


rises. The difference, through the piston


20


, between the crank chamber pressure Pc and the pressure of the cylinder bore


12




a


becomes therefore great, and the tilt angle of the swash plate


18


becomes small. As a result, the stroke of the piston


20


becomes small and the discharge amount decreases.




When the cooling requirement inside the cabin is great, the difference between the detection temperature detected by the cabin temperature sensor


41


and the set temperature by the cabin temperature setter


40


becomes great, for example. The greater the difference between the detection temperature and the set temperature, the higher input current value to the coil


86


of the control valve


33


the controlling computer


39


instructs the driving circuit


42


. In consequence, the attraction force between the fixed iron core


83


and the movable iron core


84


becomes great and the impressed load to the valve body


65


in the direction for decreasing the open area of the supply passage inside the control valve


33


increases.




Therefore, the control valve


33


lets the bellows


54


operate the valve body


65


with a lower suction pressure Ps as the target (set suction pressure) to open and close the valve hole


66


. In other words, the control valve


33


controls the discharge capacity of the compressor in such a manner as to keep a lower suction pressure Ps since the input current value to the coil


86


is increased.




When the cooling requirement inside the cabin is small, on the contrary, the difference between the detection temperature detected by the cabin temperature sensor


41


and the set temperature by the cabin temperature setter


40


, for example, becomes small. The smaller the difference between the detection temperature and the set temperature, the lower input current value to the coil


86


of the control valve


33


the controlling computer instructs the driving circuit


42


. In consequence, the attraction force between the fixed iron core


83


and the movable iron core


84


becomes small, and the impressed load to the valve body


65


in the direction for decreasing the open area of the supply passage


31


inside the control valve


33


decreases.




Therefore, the control valve


33


lets the bellows


54


operate the valve body


65


with the higher suction pressure Ps as the set suction pressure to open and close the valve hole


66


. In other words, the control valve


33


regulates the discharge capacity of the compressor so as to keep the higher suction pressure Ps by decreasing the input current value to the coil


86


.




As described above, the opening/closing operation of the supply passage


31


by the bellows


54


in the control valve


33


changes in accordance with the input current value given to the coil


86


. When equipped with such a control valve


33


, the compressor plays the role of changing the refrigerating capacity in the refrigeration circuit.




Next, the features of this embodiment will be explained.




Step portions


92


are formed on the inner peripheral surface


32




a


of the fitting hole


32


between the step surface portions


57


and


67


, between


67


and


74


, and between the third step surface portion


74


and the fourth step surface portion


91


that is the step surface portion opposing the outer peripheral surface of the electromagnetic driving portion


51


of the control valve


33


, as shown in

FIGS. 1

,


4


and


5


A. Each step portion


92


is formed by two adjoining taper surfaces


93




a


and


93




b


, the diameter of which decreases progressively towards the depth of the fitting hole


32


.




The first taper surface


93




a


positioned on a deeper side of each step portion


92


has an angle θ of about 15 to 35 degrees, preferably 20 to 30 degrees, with the extension surface of each step surface portion


57


,


67


,


74


, to which it is connected through a continuous curve surface


94


having a predetermined radius of curvature. The inner diameter of the open section of the first taper surface


93




a


on its inlet side is somewhat greater than the outer diameter of each O-ring


61


,


70


,


77


disposed on each step surface portion


57


,


67


,


74


continuing the first taper surface


93




a


, under the free condition of each O-ring.




The second taper surface


93




b


positioned on the inlet side of each step portion


92


is connected to the first surface


93




a


through a connecting curve surface


95


having a predetermined radius of curvature. This second taper surface


93




b


is formed so that its angle α with an extension surface of the first taper surface


93




a


is from about 10 to about 25 degrees, preferably 15 to 20 degrees.




In other words, this second taper surface


93




b


is formed so that its inclination to the extension surface of each of the step surface portions


57


,


67


and


74


is greater than the inclination of the first taper surface


93




a


. This second taper surface


93




b


continues to each step surface portion


67


,


74


,


91


on the inlet side through a continuous curve surface


96


having a predetermined radius of curvature.




Because the fitting hole


32


of the compressor is constituted as described above, each O-ring


61


,


70


,


77


is guided and accommodated reliably into each O-ring holding portion


60


,


69


,


76


when it passes over the second taper surface


93




b


. Each O-ring


61


,


70


,


77


is compressed by a predetermined quantity when it passes over the first taper surface


93




a


. Each O-ring is held reliably between each O-ring holding portion


60


,


69


,


76


of the control valve


33


and each step surface portion


67


,


74


,


91


of the fitting hole


32


opposing the former. Consequently, each space between each step portion


55


,


59


,


68


of the control valve and each step surface portion


57


,


67


,


74


is partitioned in the hermetic condition.




A part of each of the pressure detecting passage


58


and the supply passage


31


is open to only each step surface portion


57


,


67


,


74


without opening to each taper surface


93




a


,


93




b


. Therefore, each O-ring


61


,


70


,


77


under the compressed condition does not pass over each passage


31


,


58


and is almost free from possible damage.




This embodiment provides the following effects.




In this embodiment, each step portion


92


is formed in the fitting hole


32


of the compressor in such a fashion as to correspond to each O-ring holding portion


60


,


69


,


76


of the control valve


33


. This step portion


92


comprises the two taper surfaces


93




a


and


93




b


the diameters of which decrease progressively from the inlet side to the depth in the inserting direction when the control valve


33


is fitted. The inclination on the second taper surface


93




b


on the inlet side in the inserting direction is greater than that of the first taper surface


93




a


on the depth side.




In other words, the first taper surface


93




a


on the depth side keeps small inclination in the inserting direction of the control valve


33


, but the second taper surface


93




b


on the inlet side has a large inclination. Therefore, as the O-rings


61


,


70


and


77


are compressed by the first taper surface which has small inclination, the increase of the resistance can be avoided when the control valve


33


is inserted. In other words, the control valve


33


can be fitted easily, and an increase in the production cost of the compressor can be avoided.




On the other hand, the inclination of the second taper surface


93




b


on the inlet side is great as shown in FIG.


5


A. Therefore, in comparison with the prior art construction in which the taper surface


216


of the fitting hole


213


comprises a single small inclination as shown in

FIG. 5B

, the width of each step portion


92


can be made smaller. In consequence, as shown in

FIG. 3

, the length of the control valve


33


in the axial direction can be decreased by the decrease of the width of each step portion


92


, and the protruding length of the control valve


33


from the outer periphery of the rear housing


13


can be prevented. Therefore, the requirement for reducing the size of the compressor can be satisfied.




Moreover, the open space of the pressure detecting passage


58


and the supply passage


31


can be secured sufficiently on each step portion


57


,


67


,


74


of the fitting hole


32


although the distances between the O-rings


61


,


70


and


77


become small. In other words, the requirement for machining accuracy of the supply passage


31


does not increase, and the production cost of the compressor does not increase, either.




Furthermore, it is easy to prevent a part of the supply passage


31


from opening to each step portion


92


. Therefore, the damage of each O-ring


61


,


70


,


77


can be avoided, and the occurrence of the pressure leak from the supply passage


31


or the pressure detecting passage


58


can be restricted. Consequently, capacity controllability can be secured, in a stable way, in the compressor.




In the fitting hole


32


of the compressor according to this embodiment, each step portion


92


comprises the two taper surfaces


93




a


and


93




b.






Even though the construction is extremely simple as described above, the effect described above can be accomplished. Moreover, this fitting hole


32


can be bored easily using one cutting or boring tool corresponding to the shape of its inner peripheral surface


32




a


, for example.




In the fitting hole


32


of the compressor according to this embodiment, each taper surface


93




a


,


93




b


is connected through the predetermined connecting curve surface


95


.




Therefore, each taper surface


93




a


,


93




b


can be connected smoothly, and it becomes possible to avoid more effectively the increase of the resistance at the time of fitting of the control valve


33


and to avoid the possible damage of each O-ring


61


,


70


,


77


.




Consequently, the production cost can be further reduced in the compressor and stability of its capacity control can be further improved.




In the fitting hole


32


of the compressor according to this embodiment, the inner diameter on the inlet side is somewhat greater than the outer diameter of each O-ring


61


,


70


,


77


, in the free condition, on each first taper surface


93




a


on the depth side of each step portion


92


. The inner diameter on the depth side of the first taper surface


93




a


is smaller than the outer diameter of each O-ring in a free condition.




Therefore, the second taper surface


93




b


on the inlet side does not compress each O-ring


61


,


70


,


77


but only guides them. The first taper surface


93




a


on the depth side plays the role of reliably compressing each O-ring


61


,


70


,


77


. In consequence, each O-ring


61


,


70


,


77


can be reliably accommodated in each O-ring holding portion


60


,


69


,


76


of the control valve


33


.




Therefore, air-tightness at each step portion


55


,


59


,


68


of the control valve


33


, to which the pressure-sensitive hole


56


communicating with the pressure-sensitive chamber


53


and the supply hole


73


communicating with the valve port


66


and with the valve chest


64


are open, can be secured. In consequence, the occurrence of the pressure leak in the pressure detecting passage


58


and in the supply passage


31


can be prevented, and stable capacity controllability of the compressor can be secured.




In the fitting hole


32


of the compressor according to this embodiment, the pressure detecting passage


58


communicating with the suction chamber


24


, the downstream side supply passage


31




b


communicating with the crank chamber


15


and the upstream side supply passage


31




a


communicating with the discharge chamber


25


, are open only to the step surface portions


57


,


67


and


74


, respectively.




Therefore, a part of each passage


58


,


31




b


,


31




a


is not open to each step portion


92


, and the damage of each O-ring


61


,


70


,


77


can be avoided more reliably.




In the fitting hole


32


of the compressor according to this embodiment, each taper surface


93




a


,


93




b


continues each step surface portion


57


,


67


,


74


,


91


through each predetermined continuous curve surface


94


,


96


.




Therefore, the resistance at the time of fitting of the control valve


33


can be further reduced, and the improvement in assembling the control valve


33


can be accomplished.




Incidentally, the embodiment of the present invention described above may be modified in the following ways.




In the embodiment described above, the step portion


92


of the fitting hole


32


comprises the two taper surfaces


93




a


and


93




b


. In contrast, the step portion


101


may comprise an elliptical surface


102


having, as a guide line, an ellipse the radius of curvature of which increases gradually from the inlet side to the depth side of the fitting hole


32


, for example, as shown in FIG.


6


. The step portion


101


may also comprise a curvature having, as a guide line, a curve the radius of which becomes gradually greater, such as a parabola, an involute curve, a spiral line, one of the hyperbola, and so forth.




In such a case, the inclination of the step portion


101


with respect to the inserting direction of the control valve


33


can be increased at the inlet side while avoiding the increase of the resistance to the insertion of the control valve


33


at the depth of the step portion


101


is avoided. Therefore, the width of the step portion


101


can be further decreased, and the length of the control valve


33


in the axial direction can be further decreased.




Therefore, the protruding distance of the control valve


33


on the outer peripheral portion of the rear housing


13


can be further limited.




In the embodiment described above, the step portion


92


of the fitting hole


32


comprises the two taper surfaces


93




a


and


93




b


. However, the step portion


92


may comprise three or more taper surfaces that are serially connected to one another in such a fashion that the inclination in the inserting direction of the control valve


33


becomes small.




This construction provides substantially the same effects as the effects of the modified embodiments given above.




The embodiment given above embodies concretely the fitting structure of the control valve


33


for controlling the discharge capacity of the compressor on the basis of both the change of the suction pressure Ps and the signals from outside the compressor. However, the present invention may be embodied into the fitting structure of the control valve for controlling the discharge capacity of the compressor that is based on either one of the change of the suction pressure Ps and the signals from outside the compressor.




The embodiment given above embodies the present invention into the fitting structure of the control valve for changing the feed quantity of the refrigerant gas from the discharge chamber


25


into the crank chamber


15


. However, the present invention may be embodied into the fitting structure of the control valve for changing the release quantity of the refrigerant gas from the crank chamber


15


into the suction chamber


24


.




The embodiment given above embodies the present invention into the fitting structure of the control valve of the single head piston- and swash plate-type variable capacity compressor, but the present invention may be embodied into the fitting structure of a double-head piston, swash plate-type variable capacity compressor, a wobble type variable capacity compressor, and so forth.




While the present invention has thus been described by reference to one specific embodiment chosen for purposes of illustration, it should be apparent that numerous modifications could be made thereto by those skilled in the art without departing from the basic concept and scope of the invention.



Claims
  • 1. A fitting structure of a control valve in a variable capacity compressor of the type which control valve includes a plurality of step portions in appearance and in which a hole communicating with a gas chamber defined inside said control valve is open to at least one of said step portions and each of said step portions is partitioned by a seal member under the condition where said control valve is fitted into a fitting hole of said variable capacity compressor, wherein:said fitting hole has a plurality of step portions so formed as to correspond to seal member holding portions of said control valve, each of said step portions is shaped into an inclined surface the diameter of which progressively decreases from the inlet side towards the bottom in an inserting direction of said control valve, and a diameter reduction amount on said inclined surface is greater on the inlet side of said inclined surface than the bottom side.
  • 2. A fitting structure of a control valve according to claim 1, wherein said inclined surface comprises a plurality of taper surfaces.
  • 3. A fitting structure of a control valve according to claim 2, wherein each of said taper surfaces is connected through a predetermined connecting curve surface.
  • 4. A fitting structure of a control valve according to claim 2, wherein said taper surface at the deepest part among said taper surfaces is shaped so that the inner diameter thereof on the inlet side is greater than the outer diameter of said seal member under the free condition, and the inner diameter at a bottom part thereof is smaller than the outer diameter of said seal member under the free condition.
  • 5. A fitting structure of a control valve according to claim 3, wherein said taper surface at the deepest part among said taper surfaces is shaped so that the inner diameter thereof on the inlet side is greater than the outer diameter of said seal member under the free condition, and the inner diameter at a bottom part thereof is smaller than the outer diameter of said seal member under the free condition.
  • 6. A fitting structure of a control valve according to claim 1, wherein each of communication passages communicating with a plurality of pressure chambers defined inside said variable capacity compressor is open to one of step surface portions continuing each of said step portions, respectively.
  • 7. A fitting structure of a control valve according to claim 2, wherein each of communication passages communicating with a plurality of said pressure chambers defined inside said variable capacity compressor is open to one of said step surface portions continuing each of said step portions, respectively.
  • 8. A fitting structure of a control valve according to claim 3, wherein each of communication passages communicating with a plurality of said pressure chambers defined inside said variable capacity compressor is open to one of said step surface portions continuing each of said step portions, respectively.
  • 9. A fitting structure of a control valve according to claim 4, wherein each of communication passages communicating with a plurality of pressure chambers defined inside said variable capacity compressor is open to one of said step surface portions continuing each of said step portions, respectively.
  • 10. A fitting structure of a control valve according to claim 1, wherein said inclined surfaces of said step portions and the inner peripheral surfaces of said step surface portions continuing said step portions are connected continuously to each other through a predetermined continuous curve surface.
  • 11. A fitting structure of a control valve according to claim 2, wherein said inclined surfaces of said step portions and the inner peripheral surfaces of said step surface portions continuing said step portions are connected continuously to each other through a predetermined continuous curve surface.
  • 12. A fitting structure of a control valve according to claim 3, wherein said inclined surfaces of said step portions and the inner peripheral surfaces of said step surface portions continuing said step portions are connected continuously to each other by a predetermined continuous curve surface.
  • 13. A fitting structure of a control valve according to claim 4, wherein said inclined surfaces of said step portions and the inner peripheral surfaces of said step surface portions continuing said step portions are connected continuously to each other by a predetermined continuous curve surface.
  • 14. A fitting structure of a control valve in a variable capacity compressor of the type which control valve includes a plurality of step portions in appearance and in which a hole communicating with a gas chamber defined inside the control valve is open to at least one of said step portions and each of said step portions is partitioned by a seal member under the condition where said control valve is fitted into a fitting hole of said variable capacity compressor, wherein:said fitting hole has a plurality of step portions so formed as to correspond to seal member holding portions of said control valve, and a curve surface having different radii of curvature from the inlet side towards the depth are formed in each of said step portions in an inserting direction of said control valve.
Priority Claims (1)
Number Date Country Kind
11-057237 Mar 1999 JP
US Referenced Citations (10)
Number Name Date Kind
4170365 Haaland Oct 1979
5513673 Slavin et al. May 1996
5571248 Seetharaman et al. Nov 1996
5651387 Thor Jul 1997
5651391 Connolly et al. Jul 1997
5687997 Beacom Nov 1997
5890876 Suito et al. Apr 1999
5894860 Baldauf et al. Apr 1999
6036477 Kawaguchi et al. Mar 2000
6059538 Kawaguchi et al. May 2000
Foreign Referenced Citations (4)
Number Date Country
EP 0 220 798 A May 1987 EP
EP 0 396 017 A Nov 1990 EP
62-87680 Apr 1987 JP
62-131981 Jun 1987 JP
Non-Patent Literature Citations (1)
Entry
EP 00 10 4353 Search Report dated 11/22/00.