The present invention relates to a swash plate type variable displacement compressor.
Japanese Laid-Open Patent Publications No. 5-172052 and No. 52-131204 disclose conventional swash plate type variable displacement type compressors (hereinafter, referred to as compressors). The compressors include a suction chamber, a discharge chamber, a swash plate chamber, and a plurality of cylinder bores, which are formed in a housing. A drive shaft is rotationally supported in the housing. The swash plate chamber accommodates a swash plate, which is rotatable through rotation of the drive shaft. A link mechanism, which allows change of the inclination angle of the swash plate, is arranged between the drive shaft and the swash plate. The inclination angle is defined with respect to a line perpendicular to the rotation axis of the drive shaft. Each of the cylinder bores accommodates a piston in a reciprocal manner and thus forms a compression chamber. A conversion mechanism reciprocates each of the pistons in the associated one of the cylinder bores by the stroke corresponding to the inclination angle of the swash plate through rotation of the swash plate. An actuator is capable of changing the inclination angle of the swash plate and controlled by a control mechanism.
The actuator is arranged in the swash plate chamber, while being rotational integrally with the drive shaft. Specifically, the actuator has a rotation body rotating integrally with the drive shaft. The interior of the rotation body accommodates a movable body, which moves in the direction of the rotation axis of the drive shaft and is movable relative to the rotation body. A control pressure chamber, which moves the movable body using the pressure in the control pressure chamber, is formed between the rotation body and the movable body. A communication passage, which communicates with the control pressure chamber, is formed in the drive shaft. A pressure control valve is arranged between the communication passage and a discharge chamber. The pressure control valve changes the pressure in the control pressure chamber to allow the movable body to move in the direction of the rotation axis relative to the rotation body. The rear end of the movable body is held in contact with a hinge ball. The hinge ball is arranged in a center of the swash plate and couples the swash plate to the drive shaft to allow the swash plate to pivot. A pressing spring, which urges the hinge ball in such a direction as to increase the inclination angle of the swash plate, is arranged at the rear end of the hinge ball.
The link mechanism includes a hinge ball and an arm, which is arranged between the rotation body and the swash plate. The hinge ball is urged by a pressing spring arranged rearward to the hinge ball and maintained in contact with the rotation body. A first pin, which extends in a direction perpendicular to the rotation axis, is passed through the front end of the arm. A second pin, which also extends in a direction perpendicular to the rotation axis, is inserted through the rear end of the arm. The arm and the first and second pins support the swash plate with respect to the rotation body in a pivotal manner.
When a pressure regulation valve of the compressor is controlled to open, communication between a discharge chamber and a pressure regulation chamber is allowed. This raises the pressure in the control pressure chamber compared to the pressure in a swash plate chamber. The movable body thus retreats and presses the hinge ball rearward against the urging force of the pressing spring. This pivots the swash plate to decrease the inclination angle of the swash plate. The piston stroke is thus decreased. As a result, the compressor displacement per rotation cycle is reduced.
In contrast, by controlling the pressure regulation valve to close, the communication between the discharge chamber and the pressure regulation chamber is blocked. This lowers the pressure in the control pressure chamber to a level equal to the pressure level in the swash plate chamber. The movable body is thus moved forward and the hinge ball is operated correspondingly by the urging force of the pressing spring. This pivots the swash plate in the opposite direction to the corresponding direction of the case where the inclination angle of the swash plate decreases. The inclination angle of the swash plate is thus increased to increase the piston stroke.
However, the above-described conventional compressor operates the actuator such that the inclination angle of the swash plate is increased by lowering the pressure in the control pressure chamber. This makes it difficult to raise the compressor displacement rapidly.
Accordingly, it is an objective of the present invention to provide a compressor that increases its displacement rapidly.
A swash plate type variable displacement compressor according to the present invention includes a housing in which a suction chamber, a discharge chamber, a swash plate chamber, and a cylinder bore are formed, a drive shaft rotationally supported by the housing, a swash plate rotatable in the swash plate chamber by rotation of the drive shaft, a link mechanism, a piston, a conversion mechanism, an actuator, and a control mechanism. The link mechanism is arranged between the drive shaft and the swash plate, and allows change of an inclination angle of the swash plate with respect to a line perpendicular to the rotation axis of the drive shaft. The piston is reciprocally received in the cylinder bore. The conversion mechanism causes the piston to reciprocate in the cylinder bore by a stroke corresponding to the inclination angle of the swash plate through rotation of the swash plate. The actuator is capable of changing the inclination angle of the swash plate. The control mechanism controls the actuator. The actuator is arranged in the swash plate chamber and rotates integrally with the drive shaft. The actuator includes a rotation body fixed to the drive shaft, a movable body that is connected to the swash plate and movable relative to the rotation body in the direction of the rotation axis of the drive shaft, and a control pressure chamber that is defined by the rotation body and the movable body and moves the movable body using pressure in the control pressure chamber. One of the suction chamber and the swash plate chamber is a low pressure chamber. The control mechanism has a control passage through which the control pressure chamber communicates with the low pressure chamber and the discharge chamber and a control valve capable of adjusting the opening degree of the control passage. At least a section of the control passage is formed in the drive shaft. The movable body is arranged such that the inclination angle of the swash plate is increased through a rise of the pressure in the control pressure chamber.
In this compressor, the inclination angle of the swash plate is rapidly increased by applying the pressure in the discharge chamber to the control pressure chamber through the control passage by means of the control valve. As a result, the compressor increases its displacement rapidly.
Additionally, in the compressor according to the present invention, at least a section of the control passage is formed in the drive shaft. This simplifies the configuration of the compressor and thus reduces the compressor in size.
First to fourth embodiments of the present invention will now be described with reference to the attached drawings. A compressor of each of the first to fourth embodiments forms a part of a refrigeration circuit in a vehicle air conditioner and is mounted in a vehicle.
As shown in
With reference to
The front housing member 17 has a boss 17a, which projects forward. A shaft sealing device 25 is arranged in the boss 17a and arranged between the inner periphery of the boss 17a and the drive shaft 3. A suction chamber 27a and a first discharge chamber 29a are formed in the front housing member 17. The first suction chamber 27a is arranged at a radially inner position and the first discharge chamber 29a is located at a radially outer position in the front housing member 17.
A control mechanism 15 is received in the rear housing member 19. A second suction chamber 27b, a second discharge chamber 29b, and a pressure regulation chamber 31 are formed in the rear housing member 19. The second suction chamber 27b is arranged at a radially inner position and the second discharge chamber 29b is located at a radially outer position in the rear housing member 19. The pressure regulation chamber 31 is formed in the middle of the rear housing member 19. The first discharge chamber 29a and the second discharge chamber 29b are connected to each other through a non-illustrated discharge passage. The discharge passage has an outlet communicating with the exterior of the compressor.
A swash plate chamber 33 is formed by the first cylinder block 21 and the second cylinder block 23. The swash plate chamber 33 is arranged substantially in the middle of the housing 1.
A plurality of first cylinder bores 21a are formed in the first cylinder block 21 to be spaced apart concentrically at equal angular intervals, and extend parallel to one another. The first cylinder block 21 has a first shaft hole 21b, through which the drive shaft 3 is passed. A first recess 21c is formed in the first cylinder block 21 at a position rearward to the first shaft hole 21b. The first recess 21c communicates with the first shaft hole 21b and is coaxial with the first shaft hole 21b. The first recess 21c communicates with the swash plate chamber 33. A step is formed in an inner peripheral surface of the first recess 21c. A first thrust bearing 35a is arranged at a front position in the first recess 21c. The first cylinder block 21 also includes a first suction passage 37a, through which the swash plate chamber 33 and the first suction chamber 27a communicate with each other.
As in the first cylinder block 21, a plurality of second cylinder bores 23a are formed in the second cylinder block 23. A second shaft hole 23b, through which the drive shaft 3 is inserted, is formed in the second cylinder block 23. The second shaft hole 23b communicates with the pressure regulation chamber 31. The second cylinder block 23 has a second recess 23c, which is located forward to the second shaft hole 23b and communicates with the second shaft hole 23b. The second recess 23c and the second shaft hole 23b are coaxial with each other. The second recess 23c communicates with the swash plate chamber 33. A step is formed in an inner peripheral surface of the second recess 23c. A second thrust bearing 35b is arranged at a rear position in the second recess 23c. The second cylinder block 23 also has a second suction passage 37b, through which the swash plate chamber 33 communicates with the second suction chamber 27b.
The swash plate chamber 33 is connected to a non-illustrated evaporator through an inlet 330, which is formed in the second cylinder block 23.
A first valve plate 39 is arranged between the front housing member 17 and the first cylinder block 21. The first valve plate 39 has suction ports 39b and discharge ports 39a. The number of the suction ports 39b and the number of the discharge ports 39a are equal to the number of the first cylinder bores 21a. A non-illustrated suction valve mechanism is arranged in each of the suction ports 39b. Each one of the first cylinder bores 21a communicates with the first suction chamber 27a via the corresponding one of the suction ports 39b. A non-illustrated discharge valve mechanism is arranged in each of the discharge ports 39a. Each one of the first cylinder bores 21a communicates with the first discharge chamber 29a via the corresponding one of the discharge ports 39a. A communication hole 39c is formed in the first valve plate 39. The communication hole 39c allows communication between the first suction chamber 27a and the swash plate chamber 33 through the first suction passage 37a.
A second valve plate 41 is arranged between the rear housing member 19 and the second cylinder block 23. Like the first valve plate 39, the second valve plate 41 has suction ports 41b and discharge ports 41a. The number of the suction ports 41b and the number of the discharge ports 41a are equal to the number of the second cylinder bores 23a. A non-illustrated suction valve mechanism is arranged in each of the suction ports 41b. Each one of the second cylinder bores 23a communicates with the second suction chamber 27b via the corresponding one of the suction ports 41b. A non-illustrated discharge valve mechanism is arranged in each of the discharge ports 41a. Each one of the second cylinder bores 23a communicates with the second discharge chamber 29b via the corresponding one of the discharge ports 41a. A communication hole 41c is formed in the second valve plate 41. The communication hole 41c allows communication between the second suction chamber 27b and the swash plate chamber 33 through the second suction passage 37b.
The first suction chamber 27a and the second suction chamber 27b communicate with the swash plate chamber 33 via the first suction passage 37a and the second suction passage 37b, respectively. This substantially equalizes the pressure in the first and second suction chambers 27a, 27b and the pressure in the swash plate chamber 33. More specifically, the pressure in the swash plate chamber 33 is influenced by blow-by gas and thus slightly higher than the pressure in each of the first and second suction chambers 27a, 27b. The refrigerant gas sent from the evaporator flows into the swash plate chamber 33 via the inlet 330. As a result, the pressure in the swash plate chamber 33 and the pressure in the first and second suction chambers 27a, 27b are lower than the pressure in the first and second discharge chambers 29a, 29b. The swash plate chamber 33 is thus a low pressure chamber.
A swash plate 5, an actuator 13, and a flange 3a are attached to the drive shaft 3. The drive shaft 3 is passed rearward through the boss 17a and received in the first and second shaft holes 21b, 23b in the first and second cylinder blocks 21, 23. The front end of the drive shaft 3 is thus located inside the boss 17a and the rear end of the drive shaft 3 is arranged inside the pressure regulation chamber 31. The drive shaft 3 is supported by the walls of the first and second shaft holes 21b, 23b in the housing 1 in a manner rotatable about the rotation axis O. The swash plate 5, the actuator 13, and the flange 3a are accommodated in the swash plate chamber 33. A flange 3a is arranged between the first thrust bearing 35a and the actuator 13, or, more specifically, the first thrust bearing 35a and a movable body 13b, which will be described below. The flange 3a prevents contact between the first thrust bearing 35a and the movable body 13b. A radial bearing may be employed between the walls of the first and second shaft holes 21b, 23b and the drive shaft 3.
A support member 43 is mounted around a rear portion of the drive shaft 3 in a pressed manner. The support member 43 is a second member. The support member 43 has a flange 43a, which contacts the second thrust bearing 35b, and an attachment portion 43b, through which a second pin 47b is passed as will be described below. An axial passage 3b is formed in the drive shaft 3 and extends from the rear end toward the front end of the drive shaft 3 in the direction of the rotation axis O. A radial passage 3c extends radially from the front end of the axial passage 3b and has an opening in the outer peripheral surface of the drive shaft 3. The axial passage 3b and the radial passage 3c correspond to a communication passage. The rear end of the axial passage 3b has an opening in the pressure regulation chamber 31, which is the low pressure chamber. The radial passage 3c has an opening in a control pressure chamber 13c, which will be described below.
The swash plate 5 is shaped as a flat annular plate and has a front surface 5a and a rear surface 5b. The front surface 5a of the swash plate 5 in the swash plate chamber 33 faces forward in the compressor. The rear surface 5b of the swash plate 5 in the swash plate chamber 33 faces rearward in the compressor. The swash plate 5 is fixed to a ring plate 45. The ring plate 45 is a first member. The ring plate 45 is shaped as a flat annular plate and has a through hole 45a at the center. As illustrated in
The link mechanism 7 has a lug arm 49. The lug arm 49 is arranged rearward to the swash plate 5 in the swash plate chamber 33 and located between the swash plate 5 and the support member 43. The lug arm 49 substantially has an L shape. As illustrated in
The distal end of the lug arm 49 is connected to the ring plate 45 through a first pin 47a. This configuration supports the distal end of the lug arm 49 to allow the distal end of the lug arm 49 to pivot about the axis of the first pin 47a, which is a first pivot axis M1, relative to the ring plate 45, or, in other words, relative to the swash plate 5.
The first pivot axis M1 extends perpendicular to the rotation axis O of the drive shaft 3.
The basal end of the lug arm 49 is connected to the support member 43 through a second pin 47b. This configuration supports the basal end of the lug arm 49 to allow the basal end of the lug arm 49 to pivot about the axis of the second pin 47b, which is a second pivot axis M2, relative to the support member 43, or, in other words, relative to the drive shaft 3. The second pivot axis M2 extends parallel to the first pivot axis M1. The lug arm 49 and the first and second pins 47a, 47b correspond to the link mechanism 7 according to the present invention.
In the compressor, the swash plate 5 is allowed to rotate together with the drive shaft 3 by connection between the swash plate 5 and the drive shaft 3 through the link mechanism 7. The inclination angle of the swash plate 5 is changed through pivoting of the opposite ends of the lug arm 49 about the first pivot axis M1 and the second pivot axis M2.
The weight portion 49a is provided at the opposite side to the second pivot axis M2 with respect to the distal end of the lug arm 49, or, in other words, with respect to the first pivot axis M1. As a result, when the lug arm 49 is supported by the ring plate 45 through the first pin 47a, the weight portion 49a passes through a groove 45b in the ring plate 45 and reaches a position corresponding to the front surface of the ring plate 45, that is, the front surface 5a of the swash plate 5. As a result, the centrifugal force produced by rotation of the drive shaft 3 about the rotation axis O is applied to the weight portion 49a at the side corresponding to the front surface 5a of the swash plate 5.
Pistons 9 each include a first piston head 9a at the front end and a second piston head 9b at the rear end. The first piston head 9a is reciprocally received in the corresponding first cylinder bore 21a and forms a first compression chamber 21d. The second piston head 9b is reciprocally accommodated in the corresponding second cylinder bore 23a and forms a second compression chamber 23d. Each of the pistons 9 has a recess 9c. Each of the recesses 9c accommodates semispherical shoes 11a, 11b. The shoes 11a, 11b convert rotation of the swash plate 5 into reciprocation of the pistons 9. The shoes 11a, 11b correspond to a conversion mechanism according to the present invention. The first and second piston heads 9a, 9b thus reciprocate in the corresponding first and second cylinder bores 21a, 23a by the stroke corresponding to the inclination angle of the swash plate 5.
The actuator 13 is accommodated in the swash plate chamber 33 at a position forward to the swash plate 5 and allowed to proceed into the first recess 21c. The actuator 13 has a rotation body 13a and a movable body 13b. The rotation body 13a is formed in a disk-like shape. The front surface of the rotation body 13a includes an inclined surface 131, which is shaped with an inner diameter increasing from the middle of the rotation body 13a toward the outer peripheral surface of the rotation body 13a. The diameter of the front surface of the rotation body 13a thus increases toward the sliding surface between the rotation body 13a and the movable body 13b. The rotation body 13a is fixed to the drive shaft 3. This allows the rotation body 13a only to rotate with the drive shaft 3. An O ring is attached to the outer periphery of the movable body 13b.
The movable body 13b includes a through hole 130a, a flange 130d, a body portion 130b, and an attachment portion 130c. The drive shaft 3 is passed through the through hole 130a. The flange 130d extends radially from the rotation axis O and is arranged around the drive shaft 3. The body portion 130b is formed continuously from the flange 130d and extends from a front position to a rear position in the movable body 13b. The attachment portion 130c is formed at the rear end of the body portion 130b. The through hole 130a, the flange 130d, and the body portion 130b form the movable body 13b in a lidded cylindrical shape. The body portion 130b corresponds to the outer peripheral wall of the present invention.
The thickness of the movable body 13b is small compared to the thickness of the rotation body 13a. The outer diameter of the movable body 13b is set not to contact the wall surface of the first recess 21c and substantially equal to the diameter of the first recess 21c. The movable body 13b is arranged between the first thrust bearing 35a and the swash plate 5.
The drive shaft 3 extends into the body portion 130b of the movable body 13b through the through hole 130a. The rotation body 13a is received in the body portion 130b in a manner that permits the body portion 130b to slide with respect to the rotation body 13a. In other words, the rotation body 13a is surrounded by the body portion 130b. The movable body 13b is rotatable together with the drive shaft 3 and movable in the swash plate chamber 33 in the direction of the rotation axis O of the drive shaft 3. Since the drive shaft 3 is passed through the movable body 13b, the movable body 13b opposes the link mechanism 7 with the swash plate 5 arranged between the movable body 13b and the link mechanism 7. An O ring is mounted in the through hole 130a. The drive shaft 3 thus extends through the actuator 13 and allows the actuator 13 to rotate integrally with the drive shaft 3 about the rotation axis O.
The ring plate 45 is connected to the attachment portion 130c of the movable body 13b through a third pin 47c. In this manner, the ring plate 45, or, in other words, the swash plate 5, is supported by the movable body 13b such that the ring plate 45, or the swash plate 5, is allowed to pivot about the third pin 47c, which is an operation axis M3. The third pin 47c through which the attachment portion 130c is connected to the ring plate 45, or, in other words, the operation axis M3, is the point of application M3 with which the inclination angle of the swash plate 5 is changed with respect to the rotation axis O of the drive shaft 3. For illustrative purposes, the operation axis and the point of application are referred to with the common reference numeral M3. The operation axis M3 extend parallel to the first and second pivot axes M1, M2. The movable body 13b is thus held in a state connected to the swash plate 5. The movable body 13b comes into contact with the flange 3a when the inclination angle of the swash plate 5 is maximized. As a result, in the compressor, the movable body 13b is capable of maintaining the swash plate 5 at the maximum inclination angle.
The control pressure chamber 13c is formed between the rotation body 13a and the movable body 13b. The control pressure chamber 13c is surrounded by the body portion 130b. The radial passage 3c has an opening in the control pressure chamber 13c. The control pressure chamber 13c communicates with the pressure regulation chamber 31 via the radial passage 3c and the axial passage 3b.
With reference to
The bleed passage 15a is connected to the pressure regulation chamber 31 and the second suction chamber 27b. The pressure regulation chamber 31 communicates with the control pressure chamber 13c through the axial passage 3b and the radial passage 3c. The bleed passage 15a thus allows communication between the control pressure chamber 13c and the second suction chamber 27b. The orifice 15d is formed in the bleed passage 15a to restrict the amount of the refrigerant gas flowing in the bleed passage 15a.
The supply passage 15b is connected to the pressure regulation chamber 31 and the second discharge chamber 29b. As a result, as in the case of the bleed passage 15a, the control pressure chamber 13c and the second discharge chamber 29b communicate with each other through the supply passage 15b, the axial passage 3b, and the radial passage 3c. In other words, the axial passage 3b and the radial passage 3c each configure a section in the bleed passage 15a and a section in the supply passage 15b, each of which serves as the control passage.
The control valve 15c is arranged in the supply passage 15b. The control valve 15c is capable of adjusting the opening degree of the supply passage 15b in correspondence with the pressure in the second suction chamber 27b. The control valve 15c thus adjusts the amount of the refrigerant gas flowing in the supply passage 15b. More specifically, when the thermal load in the evaporator drops and thus the pressure in the second suction chamber 27b decreases, the control valve 15c adjusts its opening degree to reduce the amount of the refrigerant gas flowing in the supply passage 15b. A publicly available valve may be employed as the control valve 15c.
A threaded portion 3d is formed at the distal end of the drive shaft 3. The drive shaft 3 is connected to one of a non-illustrated pulley and the pulley of a non-illustrated electromagnetic clutch through the threaded portion 3d. A non-illustrated belt, which is driven by the engine of the vehicle, is wound around one of the pulley and the pulley of the electromagnetic clutch.
A pipe (not shown) extending to the evaporator is connected to the inlet 330. A pipe extending to a condenser (neither is shown) is connected to the outlet. The compressor, the evaporator, an expansion valve, and the condenser configure the refrigeration circuit in the air conditioner for a vehicle.
In the compressor having the above-described configuration, the drive shaft 3 rotates to rotate the swash plate 5, thus reciprocating the pistons 9 in the corresponding first and second cylinder bores 21a, 23a. This varies the volume of each first compression chamber 21d and the volume of each second compression chamber 23d in correspondence with the piston stroke. The refrigerant gas is thus drawn from the evaporator into the swash plate chamber 33 via the inlet 330 and sent into the first and second suction chambers 27a, 27b. The refrigerant gas is then compressed in the first and second compression chambers 21d, 23d before being sent into the first and second discharge chambers 29a, 29b. The refrigerant gas is then sent from the first and second discharge chambers 29a, 29b into the condenser through the outlet.
In the meantime, rotation members including the swash plate 5, the ring plate 45, the lug arm 49, and the first pin 47a receive the centrifugal force acting in such a direction as to decrease the inclination angle of the swash plate 5. Through such change of the inclination angle of the swash plate 5, displacement control is carried out by selectively increasing and decreasing the stroke of each piston 9.
Specifically, since the thermal load in the evaporator drops and the pressure in the second suction chamber 27b decreases, the control mechanism 15 operates the control valve 15c, which is illustrated in
That is, with reference to
Such pivot of the swash plate 5 decreases the inclination angle of the swash plate 5 with respect to the rotation axis O of the drive shaft 3 and thus reduces the stroke of each piston 9. As a result, the suction amount and displacement of the compressor per rotation cycle decreases. The inclination angle of the swash plate 5 shown in
The swash plate 5 of the compressor receives the centrifugal force acting on the weight portion 49a and thus easily moves in such a direction as to decrease the inclination angle. The movable body 13b moves rearward in the axial direction of the drive shaft 3 and the rear end of the movable body 13b is arranged inward to the weight portion 49a. As a result, when the inclination angle of the swash plate 5 of the compressor is decreased, the weight portion 49a overlaps with approximately a half the rear end of the movable body 13b.
In contrast, when the thermal load in the evaporator increases and thus the pressure in the second suction chamber 27b rises, the control mechanism 15 operates the control valve 15c, which is illustrated in
That is, with reference to
As has been described, by applying the pressure in the second discharge chamber 29b to the control pressure chamber 13c through the supply passage 15b, the pressure regulation chamber 31, the axial passage 3b, and the radial passage 3c, the compressor increases the pressure in the control pressure chamber 13c compared to the pressure in the swash plate chamber 33. This allows the movable body 13b of the compressor to increase the inclination angle of the swash plate 5 rapidly.
The movable body 13b of the compressor has the flange 130d and the body portion 130b, which is formed continuously from the flange 130d. The body portion 130b is movable back and forth in the direction of the rotation axis O relative to the outer circumference of the rotation body 13a. This allows the movable body 13b to increase the inclination angle of the swash plate 5 using the pulling force by which the movable body 13b pulls the swash plate 5 and decrease the inclination angle of the swash plate 5 using the pressing force by which the movable body 13b presses the swash plate 5.
The attachment portion 130c of the body portion 130b has the point of application M3 connected to the swash plate 5. The pulling force or the pressing force applied by the movable body 13b is thus transmitted directly to the swash plate 5 to change the inclination angle of the swash plate 5. This facilitates desirable change of the inclination angle of the swash plate 5 through the actuator 13.
The rotation body 13a has the inclined surface 131. The inner diameter of the front surface of the rotation body 13a increases from the middle toward the outer peripheral surface of the rotation body 13a.
As a result, in the compressor, the lubricant contained in the refrigerant gas flowing into the control pressure chamber 13c is dispersed onto the inner peripheral surface of the rotation body 13a and the inner peripheral surface of the movable body 13b by the centrifugal force produced through rotation of the rotation body 13a and the movable body 13b together with the drive shaft 3. Also, the inclined surface 131, the diameter of which increases toward the sliding surface between the rotation body 13a and the movable body 13b, readily guides the lubricant onto the sliding surface. As a result, insufficient lubrication is not likely to occur on the sliding surface between the rotation body 13a and the movable body 13b. Further, since blockage of the radial passage 3c by the lubricant does not happen easily, desirable communication of the refrigerant gas between the pressure regulation chamber 31 and the control pressure chamber 13c is allowed.
As a result, the compressor is capable of rapidly controlling its displacement including not only increase but also decrease of the displacement.
The compressor also includes the axial passage 3b and the radial passage 3c in the drive shaft 3. In this configuration, the lubricant contained in the refrigerant gas flowing into the control pressure chamber 13c is dispersed in the control pressure chamber 13c in radially outward directions of the drive shaft 3 through the radial passage 3c by the centrifugal force generated through the rotation of the rotation body 13a and the movable body 13b together with the drive shaft 3. This makes it difficult for the lubricant to stagnate in the proximity of the radial passage 3c and the axial passage 3b and the radial passage 3c are not easily blocked by the lubricant. Desirable communication of the refrigerant gas between the pressure regulation chamber 31 and the control pressure chamber 13c is thus allowed. Further, the axial passage 3b and the radial passage 3c configure a communication passage in the compressor, thus simplifying the configuration of the communication passage. The compressor is thus reduced in size.
By controlling the control valve 15c to open, the control mechanism 15 applies the pressure in the second discharge chamber 29b into the pressure regulation chamber 31. As a result, the compressor is capable of switching particularly from a state in which the compressor displacement is decreased to a state in which the displacement is increased in a desirable manner.
The control valve 15c lowers the pressure in the pressure regulation chamber 31 through decrease of the pressure in the second suction chamber 27b. As a result, a vehicle having a refrigerating circuit configured using the compressor ensures air conditioning in the passenger compartment corresponding to a cooling request.
The compressor brings about a muffler effect by using the swash plate chamber 33 as a refrigerant gas passage to the first and second suction chambers 27a, 27b. This decreases suction pulsation in the refrigerant gas and thus decreases the noise produced by the compressor.
A compressor according to a second embodiment of the invention includes a control mechanism 16 illustrated in
The bleed passage 16a is connected to the pressure regulation chamber 31 and the second suction chamber 27b. This configuration allows the bleed passage 16a to ensure communication between the control pressure chamber 13c and the second suction chamber 27b. The supply passage 16b is connected to the pressure regulation chamber 31 and the second discharge chamber 29b. The control pressure chamber 13c and the pressure regulation chamber 31 thus communicate with the second discharge chamber 29b through the supply passage 16b. The orifice 16d is formed in the supply passage 16b to restrict the amount of the refrigerant gas flowing in the supply passage 16b.
The control valve 16c is arranged in the bleed passage 16a. The control valve 16c is capable of adjusting the opening degree of the bleed passage 16a in correspondence with the pressure in the second suction chamber 27b. The control valve 16c thus adjusts the amount of the refrigerant flowing in the bleed passage 16a. As in the case of the aforementioned control valve 15c, a publicly available product may be employed as the control valve 16c. The axial passage 3b and the radial passage 3c each configure a section of the bleed passage 16a and a section of the supply passage 16b. The other components of the compressor of the second embodiment are configured identically with the corresponding components of the compressor of the first embodiment. Accordingly, these components are referred to using common reference numerals and detailed description thereof is omitted herein.
In the control mechanism 16 of the compressor, if the control valve 16c decreases the amount of the refrigerant gas flowing in the bleed passage 16a, the flow of refrigerant gas from the second discharge chamber 29b into the pressure regulation chamber 31 via the supply passage 16b and the orifice 16d is promoted. This substantially equalizes the pressure in the control pressure chamber 13c to the pressure in the second discharge chamber 29b. The movable body 13b of the actuator 13 thus moves forward against the centrifugal force acting on the rotation member. This increases the volume of the control pressure chamber 13c, thus increasing the inclination angle of the swash plate 5.
In the compressor of the second embodiment, the inclination angle of the swash plate 5 is increased to increase the stroke of each piston 9, thus raising the suction amount and displacement of the compressor per rotation cycle, as in the case of the compressor according to the first embodiment (see
In contrast, if the control valve 16c illustrated in
As a result, by decreasing the inclination angle of the swash plate 5 and thus the stroke of each piston 9, the suction amount and displacement of the compressor per rotation cycle are lowered (see
As has been described, the control mechanism 16 of the compressor of the second embodiment adjusts the opening degree of the bleed passage 16a by means of the control valve 16c. The compressor thus slowly lowers the pressure in the control pressure chamber 13c using the low pressure in the second suction chamber 27a to maintain desirable driving comfort of the vehicle. The other operations of the compressor of the second embodiment are the same as the corresponding operations of the compressor of the first embodiment.
As illustrated in
The housing 10 has a front housing member 18, in addition to the rear housing member 19 and the second cylinder block 23, which are the same components as those of the first embodiment. The front housing member 18 has a boss 18a projecting forward and a recess 18b. The shaft sealing device 25 is mounted in the boss 18a. Unlike the front housing member 17 of the first embodiment, the front housing member 18 includes neither the first suction chamber 27a nor the first discharge chamber 29a.
In the compressor, the swash plate chamber 33 is formed by the front housing member 18 and the second cylinder block 23. The swash plate chamber 33 is arranged substantially in the middle of the housing 10 and communicates with the second suction chamber 27b via the second suction passage 37b. The first thrust bearing 35a is arranged in the recess 18b of the front housing member 18.
Unlike the pistons 9 of the first embodiment, each of the pistons 90 only has the piston head 9b at the rear end of the piston 90. The other components of each piston 90 and the other components of the compressor of the third embodiment are configured identically with the corresponding components of the first embodiment. For illustrative purposes, the second cylinder bore 23a, the second compression chamber 23d, the second suction chamber 27b, and the second discharge chamber 29b of the first embodiment will be referred to as the cylinder bore 23a, the compression chamber 23d, the suction chamber 27b, and the discharge chamber 29b in the following description about the third embodiment.
In the compressor of the third embodiment, the drive shaft 3 rotates to rotate the swash plate 5, thus reciprocating the pistons 90 in the corresponding cylinder bores 23a. The volume of each compression chamber 23d is thus varied in correspondence with the piston stroke. Correspondingly, refrigerant gas is drawn from the evaporator into the swash plate chamber 33 through the inlet 330, reaches each compression chamber 23d via the suction chamber 27b for compression, and sent into the discharge chamber 29b. The refrigerant gas is then supplied from the discharge chamber 29b to the condenser through a non-illustrated outlet.
Like the compressor of the first embodiment, the compressor of the third embodiment is capable of executing displacement control by changing the inclination angle of the swash plate 5 to selectively increase and decrease the stroke of each piston 90.
As illustrated in
With reference to
The compressor of the third embodiment is formed without the first cylinder block 21 and thus has a simple configuration compared to the compressor of the first embodiment. As a result, the compressor of the third embodiment is further reduced in size. The other operations of the third embodiment are the same as those of the first embodiment.
A compressor according to a fourth embodiment of the present invention is the compressor according to the third embodiment employing the control mechanism 16 illustrated in
Although the present invention has been described referring to the first to fourth embodiments, the invention is not limited to the illustrated embodiments, but may be modified as necessary without departing from the scope of the invention.
For example, in the first to fourth embodiments, the inclined surface 131 is formed on the front surface of the rotation body 13a such that the diameter of the rotation body 13a increases toward the sliding surface between the rotation body 13a and the movable body 13b. However, an inclined surface may be formed in the inner peripheral surface of the body portion 130b of the rotation body 13a to incline from a front position toward a rear position such that the diameter of the movable body 13b increases toward the sliding surface between the movable body 13b and the rotation body 13a.
In the compressors of the first to fourth embodiments, refrigerant gas is sent into the first and second suction chambers 27a, 27b via the swash plate chamber 33. However, the refrigerant gas may be drawn into the first and second suction chambers 27a, 27b directly from the corresponding pipe through the inlet. In this case, the compressor should be configured to allow communication between the first and second suction chambers 27a, 27b and the swash plate chamber 33 so that the swash plate chamber 33 corresponds to a low pressure chamber.
The compressors of the first to fourth embodiments may be configured without the pressure regulation chamber 31.
In the compressor according to the present invention, the movable body may include an outer peripheral wall that surrounds the rotation body and the control pressure chamber. It is preferable that the outer peripheral wall of the movable body have a point of application connected to the swash plate. In this case, the outer peripheral wall of the movable body and the swash plate are connected to each other at the point of application. The force applied by the movable body is thus transmitted directly to the swash plate to change the inclination angle. As a result, the actuator of the compressor easily changes the inclination angle of the swash plate in a desirable manner and the displacement control is performed further rapidly.
It is preferable that the control passage formed in the drive shaft include a communication passage configured by an axial passage extending in the drive shaft in the direction of the rotation axis and a radial passage communicating with the axial passage and extending radially in the drive shaft to communicate with the control pressure chamber.
In this case, the lubricant contained in the refrigerant gas flowing into the control pressure chamber is dispersed in the control pressure chamber in radially outward directions through the radial passage of the communication passage by the centrifugal force produced through rotation of the rotation body and the movable body together with the drive shaft. This makes it difficult for the refrigerant to stagnate in the proximity of the radial passage of the communication passage. The communication passage is thus not readily blocked by the lubricant. This allows desirable communication of the refrigerant gas with respect to the control passage in the compressor. Also, the communication passage, which is a section in the control passage, is configured simply. It is thus easy to form the communication passage in the drive shaft.
It is preferable that at least a portion of the inner peripheral surface of at least one of the rotation body and the movable body have a diameter becoming greater toward the sliding surface between the rotation body and the movable body.
In this case, the lubricant contained in the refrigerant gas flowing into the control pressure chamber is dispersed onto the inner peripheral surface of the rotation body and the inner peripheral surface of the movable body by the centrifugal force generated through rotation of the rotation body and the movable body together with the drive shaft. The lubricant is also guided easily to the sliding surface by the inner peripheral surface the diameter of which increases toward the sliding surface. Insufficient lubrication is thus unlikely to occur on the sliding surface between the rotation body and the movable body.
The movable body may include a flange extending radially from the periphery of the drive shaft in a direction separating from the rotation axis. The outer peripheral wall of the movable body may be formed integrally with the flange at the outer circumference of the flange and extend in the direction of the rotation axis of the drive shaft. It is preferable that the outer peripheral wall be movable in the direction of the rotation axis relative to the outer circumference of the rotation body.
In this case, when the outer peripheral wall moves in the direction of the rotation axis of the movable body, the movable body applies one of pulling force and pressing force onto the swash plate at the point of application. As a result, the inclination angle of the swash plate is changed by one of the pulling force and the pressing force.
It is preferable that the control valve lower the pressure in the pressure regulation chamber through a decrease of the thermal load. In this case, when the thermal load decreases, the inclination angle of the swash plate is reduced to decrease the compressor displacement per rotation cycle. In this manner, the compressor controls its displacement in correspondence with the thermal load.
Number | Date | Country | Kind |
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2012-243989 | Nov 2012 | JP | national |