TECHNICAL FIELD
[0001] The present invention relates to a variable displacement compressor having a linkage
mechanism.
BACKGROUND ART
[0002] A variable displacement compressor includes a drive shaft, a rotor that is fixed
to the drive shaft and rotates integrally with the drive shaft, a swash plate (cam
plate) that is attached to the drive shaft and changeable its tilt with respect to
the axis of the drive shaft, a linkage mechanism that links the rotor and the swash
plate, and pistons that are engaged to the swash plate. When the drive shaft rotates,
the swash plate rotates with the rotor and the piston reciprocates corresponding to
the inclination angle of the swash plate. The linkage mechanism links the rotor and
the swash plate so that the inclination angle of the swash plate can be changed as
transferring the rotation of the rotor to the swash plate. With this, the piston strokes
are changed by changing the inclination angle of the swash plate so as to change the
discharging amount (see
Japanese Patent Laid-Open No. 2004-068756, for example).
[0003] The conventional linkage mechanism includes a projection extending from the rotor
toward the swash plate and a projection extending from the swash plate toward the
rotor. The projection of the rotor and the projection of the swash plate overlap each
other in the rotating direction and, with this structure, rotary torque from the rotor
is transferred to the swash plate. The projection of the swash plate slidably contacts
with a base of the projection of the rotor. The base of the projection of the rotor
functions an axial direction load receiving face for receiving an axial direction
load applied to the swash plate. The inclination angle of the swash plate changes
with the slide of the projection of the swash plate on the pressure receiving face.
DISCLOSURE OF THE INVENTION
[0004] With such a conventional structure, the inclination angle of the swash plate is changed
while a large compression reaction force (the axial direction load) from the pistons
is applied to the contact between the axial direction load receiving face and the
projection of the swash plate so that the contact are easily worn. Accordingly, the
contact are required to be quenched or the like in order to enhance their hardness
and to prevent such damages. If the contact are worn down compared to the initial
condition, the upper dead center of the each piston is lowered so that the compressive
performance of the compressor may be decrease.
[0005] The contact between the axial direction load receiving face and the projection of
the swash plate are formed in a complicated shape so that the inclination angle of
the swash plate varies as the projection of the swash plate slides on the axial direction
load receiving face. Since the contacting face is formed on the projection of the
rotor or the swash plate, difficult processing is required and manufacturing cost
increases.
[0006] The present invention is made based on such a conventional technique. An object of
the present invention is to provide a variable displacement compressor capable of
preventing an abrasion of a portion where a large axial direction load is applied
and reducing manufacturing cost of the variable displacement compressor.
[0007] An aspect of the present invention is a variable displacement compressor, including:
a drive shaft; a rotating member fixed to the drive shaft and rotating integrally
with the drive shaft; a tilting member attached to the drive shaft and being changeable
a tilt thereof with respect to an axis of the drive shaft; a linkage mechanism configured
to rotate the rotating member and the tilting member integrally as allowing the tilt
of the tilting member; and a piston configured to reciprocate in a cylinder bore corresponding
to rotary movement of the tilting member. The linkage mechanism includes an arm extending
from the rotating member; an arm extending from the tilting member and overlapping
with the arm of the rotating member in a rotating direction; a pin fixed to one of
the arm of the rotating member and the arm of the tilting member; and an axial direction
load receiving face formed on the other of the arm of the rotating member and the
arm of the tilting member and configured to contact with the pin to receive an axial
direction load applied between the rotating member and the tilting member.
BRIEF DESCRIPTION OF THE DRAWINGS
[0008]
Fig. 1 is a cross-sectional view showing a variable displacement compressor in a full
stroke condition according to an embodiment of the present invention;
Fig. 2 is a cross-sectional view showing the variable displacement compressor in a
no-stroke condition;
Fig. 3 is a perspective view showing an assembly of a drive shaft, a rotor, and a
swash plate of the variable displacement compressor in a full stroke condition;
Fig. 4 is a perspective view showing the assembly of the drive shaft, the rotor, and
the swash plate of the variable displacement compressor in a no-stroke condition;
Fig. 5 is a side view showing the assembly taken along the arrow V-V in Fig. 3;
Fig. 6 is a side view showing the assembly taken along the arrow VI-VI in Fig. 4;
Fig. 7 is a cross-sectional view showing a pin of a linkage mechanism in the variable
displacement compressor;
Fig. 8 is a perspective view showing the first modification of the first embodiment
corresponding to Fig. 3;
Fig. 9 is a perspective view showing the second modification of the first embodiment
corresponding to Fig. 3; and
Fig. 10 is a perspective view showing the third modification of the first embodiment
corresponding to Fig. 3.
DETAILED DESCRIPTION OF THE INVENTION
[0009] A variable displacement compressor according to an embodiment of the present invention
and a linkage mechanism used therein will be explained with reference to the drawings.
[0010] Firstly, an over all structure of the variable displacement compressor will be explained
with reference to Figs. 1 and 2. Fig. 1 shows a full stroke condition and Fig. 2 shows
a destroke condition.
[0011] As shown in Figs. 1 and 2, a variable displacement compressor 1 includes a cylinder
block 2, a front head 4 attached to a front end of the cylinder block 2, a rear head
6 attached to a rear end of the cylinder block 2 via a valve plate 9. The cylinder
block 2, the front head 4, and the rear head 6 are fixed to each other by a plurality
of penetrating bolts B and compose a housing of the compressor.
[0012] The cylinder block 2 is formed in a substantially cylindrical shape and has a plurality
of cylinder bores 3 placed evenly spaced apart in a circumferential direction. The
front head 2 is attached to the front end of the cylinder block 2 and has a crank
chamber 5 therein. The rear head 6 is attached to the rear end of the cylinder block
2 via the valve plate 9 and has a suction chamber 7 and a discharge chamber 8 therein.
[0013] The valve plate 9 is formed with suction ports 11 that communicates the cylinder
bores 3 with the suction chamber 7 and is formed with discharge ports 12 that communicates
the cylinder bores 3 with the discharge chamber 8.
[0014] A valve system (not shown) adapted to open and close the suction ports 11 is provided
on the valve plate 9 at the cylinder block side. On the other hand, a valve system
(not shown) adapted to open and close the discharge ports 12 is provided on the valve
plate 9 at the rear head side. A gasket is interposed between the valve plate 9 and
the rear head 6 for providing an airtight sealing property between the suction chamber
7 and the discharge chamber 8.
[0015] A drive shaft 10 is supported by bearings 17, 18 in support holes 19, 20 that are
formed at centers of the cylinder block 2 and the front head 4so that the drive shaft
10 is rotatable in the crank chamber 5.
[0016] the crank chamber 5 accommodates a rotor 21 as a "rotating member" fixed to the drive
shaft 10, a swash plate 24 as a "tilting member" attached to the drive shaft slidably
in the axial direction and tiltably with respect to the axis of the drive shaft, and
a linkage mechanism 40 for linking the rotor 21 and the swash plate 24. The linkage
mechanism 40 links the rotor 21 and the swash plate 24 so that the rotor 21 and the
swash plate 24 rotate integrally as allowing changes of the inclination angle of the
swash plate 24. The swash plate 24 includes a hub 25 attached to the drive shaft 10
and a swash plate body 26 fixed to a boss segment 25a of the hub 25. To the swash
plate body 26 of the swash plate 24, a piston 29 is linked via a pair of hemispherical-shaped
shoes 30, 30. The pistons 29 are slidably fit in each cylinder bore 3.
[0017] When the drive shaft 10 rotates, the rotor 21 rotates integrally with the drive shaft
10, and the swash plate 24 rotates corresponding to the rotor 21 via the linkage mechanism
40. The rotation of the swash plate 24 is converted into a reciprocating movement
of the pistons 29 by the pairs of piston shoes 30, 30 so that the pistons 29 reciprocate
in the cylinder bores 3. By the reciprocation of the pistons 29, refrigerant in the
suction chamber 7 is sucked into the cylinder bores 3 through the suction ports 11
of the valve plate 9 to be compressed, and then discharged to the discharge chamber
8 through the discharge ports 12 of the valve plate 9.
Control of Variable Capacity
[0018] In the variable displacement compressor, a pressure control mechanism is provided.
The pressure control mechanism is configured to adjust a difference in pressure (pressure
balance) between the crank chamber pressure Pc in back of the pistons 29 and the suction
chamber pressure Ps in front of the pistons 29 is provided in order to change the
inclination angle of the swash plate 24. The pressure control mechanism includes a
gas extraction passage (not shown) that allows the crank chamber 5 to communicate
with the suction chamber 7, an gas supply passage (not shown) that allows the crank
chamber 5 to communicate with the discharge chamber 8, and a control valve 33 that
is provided in the midstream of the gas supply passage to open and close the gas supply
passage.
[0019] When the control valve 33 opens the gas supply passage, the refrigerant flows from
the discharge chamber 8 into the crank chamber 5 through the gas supply passage, so
that the crank chamber pressure Pc increases. With this, the pressure balance between
the crank chamber pressure Pc and the suction chamber pressure Ps decreases the inclination
angle of the swash plate 24. As a result, piston strokes become smaller so as to decrease
the discharging amount. On the other hand, when the control valve 33 closes the gas
supply passage, the refrigerant is gradually extracted from the crank chamber 5 to
the suction chamber 7 through the gas extraction passage, so that the crank chamber
pressure Pc reduces. With this, the pressure balance between the crank chamber pressure
Pc and the suction chamber pressure Ps increases the inclination angle of the swash
plate 24. As a result, the piston strokes become longer so as to increase the discharging
mount. In other words, the inclination angle of the swash plate 24 reduces when the
hub 25 moves toward the cylinder block 2 and the inclination angle of the swash plate
24 increases when the hub 25 moves away from the cylinder block 2.
Linkage Mechanism
[0020] A linkage mechanism 40 will be explained with reference to Figs. 3 to 7.
[0021] As shown in Figs. 3 to 6, the linkage mechanism 40 includes an arm 41 extending from
the rotor 21 toward the hub 25 and an arm 43 extending from the hub 25 toward the
rotor 21. The arm 41 of the rotor and the arm 43 of the hub are overlapped in the
rotary torque transfer direction Ft (that is, the rotating direction of the drive
shaft 10). With this structure, the rotary torque of the rotor 21 is transferred to
the swash plate 24. In this example, as shown in Figs. 3 and 4, the arm 43 is formed
in a bifurcated shape having a slit S extending in the axial direction XY (orthogonally
to the rotary torque transfer direction Ft) and the arm 41 is slidably fit in the
slit S in a sandwiched manner.
[0022] When the swash plate 24 rotates, the pistons 29 reciprocate so that compression reaction
force (axial direction load Fp) from the pistons is applied to the swash plate 24.
The arm 43 of the swash plate 24 is formed with press-insertion holes 43s (see Fig.
7) that a pin 151 is pressed into and fixed in. An axial direction load receiving
face 53 is formed on an end of the arm 41 of the rotor 21. The compression reaction
force Fp is received at a contact between the pin 151 and the an axial direction load
receiving face 53.
[0023] The pin 151 extends in a tangential direction of rotary orbits of the rotating member
21 and the swash plate 24, in other words, extends toward the rotary torque transfer
direction Ft. Since a large compression reaction force (axial direction load Fp) is
applied to the contact between the pin 151 and the axial direction pressure receiving
face 53 of the rotor 21, the hardness of the pin 151 and the axial direction pressure
receiving face 53 of the rotor 21 is enhanced by a quenching process or the like.
Effects
[0024] With the above described structure, the present embodiment brings about the following
effects.
[0025] Firstly, according to the present embodiment, the linkage mechanism 40 includes an
arm 41 extending from a rotor 21, an arm 43 extending from a swash plate 24 and receiving
rotary torque from the arm 41 of the rotor, a pin 151 fixed to one of the arm 41 of
the rotor and the arm 43 of the swash plate (the arm 43 of the swash plate, in this
embodiment), and an axial direction load receiving face 53 formed on the other of
the arm 41 of the rotor and the arm 43 of the swash plate (the arm 41 of the rotor,
in this embodiment) and configured to contact with the pin 151 to receive compression
reaction force Fp (axial direction load) from the pistons 29.
[0026] Accordingly, the inclination angle of the swash plate 24 is changed in the condition
that great axial direction load Fp (compression reaction force from the pistons) is
applied between the pin 151 and the axial direction load receiving face 53. However,
since the pin 151 is a member formed separately from the arm (the arm 43 of the swash
plate, in this embodiment), only the pin 151 can be quenched, etc. in a hardness enhancement
process so that the arm (the arm 43 of the swash plate, in this embodiment) is not
needed to be quenched. As a result, manufacturing cost can be reduced.
[0027] Further, since the pin 151 is separated form the arm (the arm 43 of the swash plate,
in this embodiment), it is relatively easy to form the outer surface of the pin 151
to be complicated. With such a case, the manufacturing cost can be reduced comparing
to the case forming the arm (the arm 43 of the swash plate, in this embodiment) to
be a complicated shape.
[0028] Further, only the pin 151 can be exchanged.
[0029] Secondly, the linkage mechanism has a structure in which one of the arms 41, 43 (the
arm 43 of the swash plate, in this embodiment) is formed in a bifurcated shape having
a slit S and the other of the arms (the arm 41 of the rotor, in this embodiment) is
slidably fit in the slit S in a sandwiched manner. This structure is preferable since
backlash is hardly provided between the both arms 41, 43.
[0030] As described above, according to the present invention, the linkage mechanism includes
the arm extending form the rotating member, the arm extending from the tilting member
and overlapped with the arm of the rotating member, the pin fixed to one of the arm
of the rotating member and the arm of the tilting member, the axial direction load
receiving face formed on the other of the arm of the rotating member and the arm of
the tilting member arm and configured to contact with the pin to receive axial direction
load between the rotating member and the tilting member. In this structure, the inclination
angle of the tilting member is changed in a state that great axial direction load
(compression reaction force from the pistons) is applied between the pin and the axial
direction load receiving face. However, since the pin and the arm are individual members,
only the pin can be quenched, etc. in a hardness enhancement process and the arm is
not required to be quenched. As a result, the manufacturing cost can be reduced.
[0031] It is noted that the present invention should not be limited to the above described
embodiment.
[0032] For example, according to the above embodiment, the pin 51 is fixed to the arm 43
of the swash plate and the axial direction load receiving face 53 is formed on the
arm 41 of the rotor. However, in the present invention, as shown in the first modification
in Fig. 8 and the second modification in Fig. 9, the axial direction load receiving
face 53 may be formed on the arm 43 of the swash plate and the pin 151 may be fixed
to the arm 41 of the rotor.
[0033] According to the above embodiment, a slit S is provided to the arm 43 of the swash
plate and the arm 41 of the rotor is slidably held in the slit S. However, in the
present invention, as shown in the second modification in Fig. 9 and the third modification
in Fig. 10, the slit S may be provided to the arm 41 of the rotor and the arm 43 of
the swash plate may be slidably fit in the slit S.
[0034] According to the above embodiment, the cross-section of the pin is a circular shape;
however, in the present invention, it may be formed in other shapes.
[0035] Further, according to the above embodiment, the swash plate 24 is made in combination
of the swash plate body 26 and the hub 25 which are separately formed; however, in
the present invention, the swash plate body and the hub may be formed integrally in
advance to constitute the swash plate. Further, the above embodiment employs a sleeveless
structure in which the swash plate 24 is directly attached to the drive shaft 10 without
any sleeve; however, in the present invention, the swash plate may be attached to
the drive shaft via a sleeve.
INDUSTRIAL APPLICABILITY
[0036] The present invention may be applied to not only a swash plate type variable displacement
compressor but also a wobble plate type variable displacement compressor and the present
invention may be implemented with various modifications.