Technical Field
[0001] The present invention relates to a vane compressor suitable for a refrigeration cycle
using, for example, a working fluid as a refrigerant, more particularly to the structure
of a lower end portion in the forward or backward travel direction of the vane of
a vane compressor.
Background Art
[0002] As described in, for example, PTL 1, PTL 2, and the like, a vane compressor includes
a cylinder having both ends closed by side blocks or the like, a rotor, rotatably
housed in the cylinder, that has a perfect circular cross section, a vane groove formed
radially inward from an outer peripheral surface of the rotor, and a vane housed in
the vane groove movably forward and backward. In addition, the vane compressor has
the structure in which the vane is brought into slidable contact with the inner peripheral
surface of the cylinder by a centrifugal force caused by the rotation of the rotor
or a back pressure from a back pressure chamber provided on the bottom of the vane
groove.
[0003] In the vane compressor proposed in PTL 1, the bottom of the vane groove of the rotor
has an arc-shaped cross section and the lower end portion of the vane is arc-shaped
so as to match the shape of the bottom of the vane groove. Accordingly, even when
the lower end portion of the vane collides with the bottom of the vane groove, impact
sound is reduced because arcs make contact with each other.
[0004] In addition, since the bottom of the vane groove and the lower end portion of the
vane are arc-shaped so as to become close to each other, the vane can reach the bottom
of the vane groove until the centers in the arcs coincide. In consideration of this,
the length of the vane along the vane groove is formed so as not to project from the
vane groove even when the vane enters the deepest part of the vane groove. Accordingly,
even when the vane moves in the vane groove so as to follow the shape of the inner
peripheral surface of the cylinder as the rotor rotates and passes through the radial
seal portion on the inner peripheral surface of the cylinder, the vane can enter the
cylinder groove without interfering with the bottom of the vane groove.
Citation List
Patent Literature
Summary of Invention
Technical Problem
[0006] The material of the vane compressor can be formed by, for example, forging as described
in PTL 2. In the material of the rotor formed by forging, the vane groove including
the back pressure chamber, a through hole into which a shaft is inserted, and the
like are formed in advance. When the completed product of the rotor is created from
such rotor materials formed as described above by forging or molding, the vane groove
in which the vane slides and which requires dimensional accuracy is polished, but
the back pressure chamber in which no member slides or to which no member is fitted
is not machined.
[0007] When the rotor of the vane compressor described in PTL 1 is made from materials formed
by forging or molding, the vane groove of the rotor is polished at high accuracy,
but the back pressure chamber provided on the bottom of the vane groove has the shape
formed by forging as is. Accordingly, when the vane groove is polished, the position
of the vane groove deviates from the position of the back pressure chamber and the
center of the vane groove in which the vane slides may deviate from the center of
the back pressure chamber.
[0008] When the center of the vane groove in which the vane slides deviates from the center
of the back pressure chamber, as illustrated in Fig. 8, even if the vane enters the
deepest part of the vane groove, the center of the arc surface of the lower end portion
of the vane does not coincide with the center of the arc surface of the vane groove,
and the shoulder portion of the lower end portion of the vane overrides the arc surface
on the side of the bottom of the vane groove. Accordingly, the lower end portion of
the vane cannot enter the deepest part of the vane groove, the upper end portion projects
from the outer peripheral surface of the rotor and the vane interferes with the inner
peripheral surface of the cylinder, possibly disabling the rotation of the rotor.
[0009] The invention addresses the above problems with an object of providing a vane compressor
in which the structure of the lower end side in the forward or backward travel direction
of a vane is changed so that the shoulder portion of the lower end portion of the
vane has difficulty in overriding the arc surface on the side of the concave arc surface
of the back pressure chamber and the rotation of the rotor is thereby prevented from
being restricted by the vane protruding from the outer peripheral surface of the rotor.
Solution to Problem
[0010] A vane compressor according to the invention includes a cylinder having both ends
closed by side block members, a rotor rotatably provided in the cylinder, a vane groove
formed radially inward from an outer peripheral surface of the rotor, and a vane housed
in the vane groove movably forward and backward, one end portion of the vane making
slidable contact with an inner peripheral surface of the cylinder as the rotor rotates,
in which a back pressure chamber having a concave arc surface is formed on a bottom
of the vane groove, the other end portion of the vane has a convex arc surface facing
the concave arc surface of the vane groove, and voids are generated between the vane
and the bottom of the vane groove on both sides in a thickness direction of the vane
when the other end portion of the vane makes contact with the bottom of the vane groove.
In a vane compressor according to the second aspect, the convex arc surface of the
other end portion of the vane has a curvature radius smaller than the concave arc
surface on the bottom of the vane groove and the voids are thereby generated on both
sides of a contact portion between the other end portion of the vane and the bottom
of the vane groove.
[0011] Accordingly, if the center of the vane groove in the thickness direction of the vane
deviates from the center of the back pressure chamber in the thickness direction of
the vane, voids are formed between the lower end portion of the vane and the bottom
of the vane groove on both sides in the thickness direction of the vane when the lower
end portion of the vane makes contact with the concave arc surface of the back pressure
chamber. Accordingly, when the vane enters the deepest part of the vane groove, the
shoulder portion of the lower end portion of the vane has difficulty in overriding
the arc surface on the side of the back pressure chamber of the concave arc surface
on the bottom of the vane groove. Accordingly, it is possible to prevent a defect
that causes the upper end portion of the vane to project from the outer peripheral
surface of the rotor, interfere with the inner peripheral surface of the cylinder,
and inhibit the rotation of the rotor.
[0012] In a vane compressor according to the third aspect, tangential flat surfaces continued
to the convex arc surface are formed on both sides in the thickness direction of the
other end portion of the vane.
[0013] Accordingly, when the entire surface of the other end of vane facing the concave
arc surface on the bottom of the vane groove is the convex arc surface, since the
position of the shoulder portion of the vane is raised toward the outer peripheral
surface of the rotor, the width of the sliding surface of the vane is narrowed. However,
since the tangential flat surfaces are present, the position of the shoulder portion
of the vane is prevented from being raised toward the outer peripheral surface of
the rotor more than necessary, thereby preventing the width of the sliding surface
of the vane from being narrowed.
[0014] In addition, since the radius of the convex arc surface of the other end portion
of the vane can be reduced as compared with the case in which the entire surface facing
the concave arc surface on the bottom of the vane groove is the convex arc surface,
contact can be concentrated on the position at which the other end portion of the
vane makes contact with the bottom of the vane groove. Accordingly, even when, for
example, fine foreign matter enters the back pressure chamber, the foreign matter
is sandwiched between the other end portion of the vane and the bottom of the vane
groove, thereby preventing the possibility that the vane cannot enter the deep part
of the bottom of the vane groove.
[0015] In a vane compressor according to the fourth aspect, sliding contact surfaces in
slidable contact with the vane groove are formed on both sides in the thickness direction
of the vane, chamfering for partially removing the sliding contact surfaces and the
convex arc surface is performed between the sliding contact surfaces and the convex
arc surface of the other end portion of the vane, and the voids are thereby provided.
[0016] Accordingly, it is possible to shave the shoulder portion of the vane or enlarge
voids formed between the other end portion of the vane and the bottom of the vane
groove on both sides in the thickness direction of the vane when the other end portion
of the vane makes contact with the concave arc surface of the vane groove. Accordingly,
when the vane enters the deepest part of the vane groove, the shoulder portion of
the other end portion of the vane has more difficulty in overriding the arc surface
on the side of the concave arc surface of the back pressure chamber.
Advantageous Effects of Invention
[0017] As described above, in the invention, even if the center of the vane groove in the
thickness direction of the vane deviates from the center of the back pressure chamber
in the thickness direction of the vane, voids are formed between the lower end portion
of the vane and the concave arc surface of the back pressure chamber on both sides
in the thickness direction of the vane when the lower end portion of the vane makes
contact with the concave arc surface of the back pressure chamber. Accordingly, when
the vane enters the deepest part of the vane groove, it is possible to prevent the
shoulder portion of the lower end portion of the vane from overriding the arc surface
on the side of the concave arc surface of the back pressure chamber. Accordingly,
it is possible to prevent a defect that causes the upper end portion of the vane to
project from the outer peripheral surface of the rotor, interfere with the inner peripheral
surface of the cylinder, and inhibit the rotation of the rotor.
[0018] According to particularly the third aspect of the invention, when the entire surface
of the other end portion of the vane facing the concave arc surface on the bottom
of the vane groove is the convex arc surface, since the position of the shoulder portion
of the vane is raised toward the outer peripheral surface of the rotor, the width
of the sliding surface of the vane is narrowed. However, since the tangential flat
surfaces are present, the position of the shoulder portion of the vane is prevented
from being raised toward the outer peripheral surface of the rotor more than necessary,
thereby preventing the width of the sliding surface of the vane from being narrowed.
[0019] In addition, according to particularly the third aspect of the invention, since the
radius of the convex arc surface of the other end portion of the vane can be reduced
as compared with the case in which the entire surface facing the concave arc surface
on the bottom of the vane groove is the convex arc surface, contact can be concentrated
on the position at which the other end portion of the vane makes contact with the
bottom of the vane groove. Accordingly, even when, for example, fine foreign matter
enters the back pressure chamber, the foreign matter is sandwiched between the other
end portion of the vane and the bottom of the vane groove, thereby preventing the
possibility that the vane cannot enter the deep part of the bottom of the vane groove.
[0020] According to particularly the fourth aspect of the invention, it is possible to shave
the shoulder portion of the vane or enlarge voids formed between the lower end portion
of the vane and the bottom of the vane groove on both sides in the thickness direction
of the vane when the lower end portion of the vane makes contact with the concave
arc surface of the back pressure chamber. Accordingly, when the vane enters the deepest
part of the vane groove, the shoulder portion of the lower end portion of the vane
has more difficulty in overriding the arc surface on the side of the concave arc surface
of the back pressure chamber.
Brief Description of Drawings
[0021]
[Fig. 1 (a) ] Fig. 1(a) is a cross sectional view illustrating an example of a vane
compressor according to the invention, and a cross sectional view cut so that a discharge
port can be seen.
[Fig. 1(b)] Fig. 1(b) is a cross sectional view illustrating an example of a vane
compressor according to the invention, and a cross sectional view cut so that an intake
port can be seen.
[Fig. 2] Fig. 2 is a cross sectional view taken along line A-A in Fig. 1(b).
[Fig. 3(a)] Fig. 3(a) is a schematic view illustrating the structures of a vane, a
vane groove, and a back pressure chamber according to embodiment 1 of the invention,
and an enlarged view illustrating the vane and the back pressure chamber when the
vane groove does not deviate from the back pressure chamber in the thickness direction
of the vane.
[Fig. 3(b)] Fig. 3(b) is a schematic view illustrating the structures of a vane, a
vane groove, and a back pressure chamber according to embodiment 1 of the invention,
and an overall view illustrating the vane, the vane groove, and the back pressure
chamber when the vane groove deviates from the back pressure chamber in the thickness
direction of the vane.
[Fig. 4(a)] Fig. 4(a) is a schematic view illustrating the structures of a vane, a
vane groove, and a back pressure chamber according to the other example of embodiment
1 of the invention, and an enlarged view illustrating the vane and the back pressure
chamber when the vane groove does not deviate from the back pressure chamber in the
thickness direction of the vane.
[Fig. 4(b)] Fig. 4(b) is a schematic view illustrating the structures of a vane, a
vane groove, and a back pressure chamber according to the other example of embodiment
1 of the invention, and an overall view illustrating the vane, the vane groove, and
the back pressure chamber when the vane groove deviates from the back pressure chamber
in the thickness direction of the vane.
[Fig. 5(a)] Fig. 5(a) is a schematic view illustrating the structures of a vane, a
vane groove, and a back pressure chamber according to embodiment 2 of the invention,
and an enlarged view illustrating the vane and the back pressure chamber when the
vane groove does not deviate from the back pressure chamber in the thickness direction
of the vane.
[Fig. 5(b)] Fig. 5(b) is a schematic view illustrating the structures of a vane, a
vane groove, and a back pressure chamber according to embodiment 2 of the invention,
and an overall view illustrating the vane, the vane groove, and the back pressure
chamber when the vane groove deviates from the back pressure chamber in the thickness
direction of the vane.
[Fig. 6] Fig. 6 is an explanatory diagram illustrating an example of setting the angle
of the tangential flat surfaces of the other end portion of the vane according to
embodiment 2 of the invention illustrated in Fig. 5(a) and Fig. 5(b).
[Fig. 7(a)] Fig. 7(a) is a schematic view illustrating the structures of a vane, a
vane groove, and a back pressure chamber according to embodiment 3 of the invention,
and an enlarged view illustrating the vane and the back pressure chamber when the
vane groove does not deviate from the back pressure chamber in the thickness direction
of the vane.
[Fig. 7(b)] Fig. 7(b) is a schematic view illustrating the structures of a vane, a
vane groove, and a back pressure chamber according to embodiment 3 of the invention,
and an overall view illustrating the vane, the vane groove, and the back pressure
chamber when the vane groove deviates from the back pressure chamber in the thickness
direction of the vane.
[Fig. 8(a)] Fig. 8(a) is a schematic view illustrating the structures of a vane, a
vane groove, and a back pressure chamber according to a comparative example (to be
compared with the embodiment 1, the other example of embodiment 1, embodiment 2, and
embodiment 3 of the invention) having a problem in the lower end portion of the vane,
and an enlarged view illustrating the vane and the back pressure chamber when the
vane groove does not deviate from the back pressure chamber in the thickness direction
of the vane.
[Fig. 8(b)] Fig. 8(b) is a schematic view illustrating the structures of a vane, a
vane groove, and a back pressure chamber according to a comparative example (to be
compared with the embodiment 1, the other example of embodiment 1, embodiment 2, and
embodiment 3 of the invention) having a problem in the lower end portion of the vane,
and an overall view illustrating the vane, the vane groove, and the back pressure
chamber when the vane groove deviates from the back pressure chamber in the thickness
direction of the vane.
Description of Embodiments
[0022] Embodiments of the invention will be described below with reference to the attached
drawings.
[0023] Figs. 1 and 2 illustrate an example of a vane compressor used for the refrigeration
cycle of, for example, an in-vehicle air conditioner. A vane compressor 1 includes
a shaft 3, a rotor 4, fixed to the shaft 3, that rotates as the shaft 3 rotates, and
first and second housing members 8 and 9 that define a compression space 18 (described
later) together with the rotor 4. The first housing member 8 and the second housing
member 9 constitute a housing 2.
[0024] In the embodiment, the first housing member 8 includes a cylinder 8a in which the
rotor 4 is housed and a rear side block 8b positioned on the rear side in the shaft
direction of the shaft 3 with respect to the cylinder 8a, integrally molded with the
cylinder 8a, and closing the rear side of the cylinder 8a.
[0025] The rotor 4 housed in the cylinder 8a is a cylinder having a perfect circular cross
section and a center point P1 of the perfect circle is provided with a through hole
4a to which the shaft 3 can be press-fitted, as illustrated in Fig. 2. In addition,
the rotor 4 has two vanes 6 to be inserted into two vane grooves 5 opened in the outer
peripheral surface of the rotor 4.
[0026] Although the structures of the vanes 6 in the examples illustrated in Figs. 3 to
8 will be described later, any of the vanes 6 includes one end portion having sliding
contact surfaces 6a and 6a (described later) in slidable contact with the inner peripheral
surface of the vane groove 5 described below on both sides in the thickness direction
of the vane 6 and the other end portion having a convex arc surface 611a (described
later) and slides on the inner peripheral surface of the cylinder 8a by moving forward
or backward from the vane groove 5.
[0027] In any of the examples illustrated in Figs. 3 to 8, the vane groove 5 extends radially
inward from the outer peripheral surface of the rotor 4. In addition, a back pressure
chamber 10 having a concave arc surface 101, which will be described later, is formed
on the bottom of the vane groove 5. The vane groove 5 and the back pressure chamber
10 are formed so as to penetrate from front side to the rear side along the shaft
direction of the rotor 4.
[0028] As illustrated in Fig. 2, in the embodiment, the inner peripheral surface of the
cylinder 8a has an inner diameter larger than the outer diameter of the rotor 4 and
is formed in a perfect circle about a center point P2. The rotor 4 is housed in the
cylinder 8a so that the outer peripheral surface of the rotor 4 and the inner peripheral
surface of the cylinder 8a form a fine clearance (radial seal portion P3 at which
the cylinder 8a is closest to the rotor 4) at one position in the peripheral direction.
Since the rotor 4 about the center point P1 is housed in the cylinder 8a as described
above, a compression space 18 is defined between the inner peripheral surface of the
cylinder 8a and the outer peripheral surface of the rotor 4. This compression space
18 is partitioned by the two vanes 6 housed in the two vane grooves 5 formed in the
rotor 4 into two compression chambers 19 and the volumes of the compression chambers
19 are changed as the rotor 4 rotates.
[0029] The second housing member 9 is configured by integrating a front side block 9a in
contact with the front side end surface of the cylinder 8a with a shell 9b, extending
in the shaft direction of the shaft 3 from the front side block 9a, that surrounds
the outer peripheral surfaces of the cylinder 8a and the rear side block 8b. In addition,
the second housing member 9 is coupled to the first housing member 8 via a coupling
tool 7 such as a bolt. By inserting the first housing member 8 from a rear side opening
9d of the shell 9b and fitting the first housing member 8 to the shell 9b, the front
side of the cylinder 8a is closed by the front side block 9a and the rear side opening
9d of the shell 9b is closed by the rear side block 8b.
[0030] In addition, in the second housing member 9, a pulley 20 to which rotational power
is transmitted from the power source (not illustrated) of a vehicle via a belt (not
illustrated) is rotatably mounted onto a boss section 9c integrated with the front
side block 9a and the rotational power is transmitted from the pulley 20 to the shaft
3 via an electromagnetic clutch 21. In addition, the second housing member 9 is provided
with an intake port 11 and a discharge port 12 of the working fluid (refrigerant gas)
and the intake port 11 communicates with an intake space 14 including a space 14a
formed in the second housing member 9 and a concavity 14b formed in the cylinder 8a.
[0031] The shaft 3 is rotatably supported via plain bearings 23 and 24 that are bearing
portions held and formed by the front side block 9a of the second housing member 9
and the rear side block 8b of the first housing member 8. In addition, a seal member
13 is present between the shaft 3 and the inner side surface of the second housing
member 9 in the part close to the base end of the boss section 9C of the second housing
member 9 to prevent the working fluid from leaking externally from the opening of
the boss section 9c.
[0032] The peripheral surface of the cylinder 8a is provided with an intake port 25 communicating
with the intake space 14 so as to correspond to the compression space 18 and a discharge
port 26 communicating with a discharge space 15. Accordingly, when the cylinder 8a
is fitted to the shell 9b, the intake space 14 communicates with the compression chambers
19 via the intake port 25, the discharge space 15 having both ends separated by flange
sections 8c and 8d is formed between the outer peripheral surface of the cylinder
8a and the inner side surface of the shell 9b, and the discharge space 15 can communicate
with the compression chambers 19 via the discharge port 26. The discharge port 26
is opened or closed by a discharge valve 27 housed in the discharge space 15. In addition,
the discharge space 15 communicates with an oil separator 16 via a passing hole 28
formed in the flange section 8d. In addition, the oil separator 16 communicates with
the discharge port 12.
[0033] In the structure described above, in the vane compressor 1, the rotational power
from the power source (not illustrated) is transmitted to the shaft 3 via the pulley
20 and the electromagnetic clutch 21 and, when the rotor 4 rotates, the working fluid
having flowed to the intake space 14 from the intake port 11 is sucked by the compression
space 18 via the intake port 25. Since the volumes of the compression chambers 19
partitioned by the vanes 6 in the compression space 18 are changed as the rotor 4
rotates, the working fluid between the vanes 6 is compressed and discharged from the
discharge port 26 to the discharge space 15 via the discharge valve 27. The working
fluid discharged to the discharge space 15 moves in the peripheral direction along
the outer peripheral surface (inner side surface of the shell 9b) of the cylinder
8a and is introduced to the oil separating chamber of the oil separator 16 formed
in the rear side block 8b via the passing hole 28 formed in the flange section 8d.
After that, oil is separated from the working fluid during rotation in the oil separating
chamber of the oil separator 16 and then the working fluid is discharged to an external
circuit through the discharge port 12.
[0034] By the way, Fig. 3 illustrates embodiment 1 of the invention, Fig. 4 illustrates
the other example of embodiment 1 of the invention, Figs. 5 and 6 illustrate embodiment
2 of the invention, Fig. 7 illustrates embodiment 3 of the invention, and Fig. 8 illustrates
a comparative example to be compared with embodiment 1, the other example of embodiment
1, embodiment 2, and embodiment 3. Embodiment 1, the other example of embodiment 1,
embodiment 2, and embodiment 3 will be described while being compared with the comparative
example.
Embodiment 1
[0035] The vane groove 5 in embodiment 1 extends radially inward from the outer peripheral
surface of the rotor 4 as described above and has the inner side surfaces in contact
with the sliding contact surfaces 6a and 6a of the vane 6 on both sides in the thickness
direction of the vane 6. Fig. 3 (a) illustrates a center line C passing through the
center in the thickness direction of the vane 6.
[0036] As illustrated in Fig. 3, the back pressure chamber 10 in embodiment 1 includes two
side arc surfaces 101a and 101b and one bottom side arc surface 101c positioned between
the two side arc surfaces 101a and 101b.
[0037] The side arc surface 101a, the bottom side arc surface 101c, and the side arc surface
101b that form the back pressure chamber 10 are disposed along an arc S1 assumed about
a center point P5 of the back pressure chamber 10 and constitute the concave arc surface
101 of the back pressure chamber 10. A diameter L1 of the back pressure chamber 10
is larger than a dimension L2 (illustrated in Fig. 3(b)) of the vane groove 5 in the
thickness direction of the vane 6. Reference numeral 103 in Fig. 3 indicates the center
in the arc of the arc S1 that forms the concave arc surface 101 of the back pressure
chamber 10.
[0038] Also in the comparative example illustrated in Fig. 8, the back pressure chamber
10 has the concave arc surface 101, reference numeral 103 indicates the center in
the arc of the arc S1 that forms the concave arc surface 101 of the back pressure
chamber 10, and the center line C passing through the center in the thickness direction
of the vane 6 is illustrated.
[0039] The vane 6 in embodiment 1 has a lower end portion 61 close to the lower end in the
forward or backward travel direction of the vane 6 as the other end portion described
above. The lower end portion 61 has the convex arc surface 611a in which an entire
contact surface 611 facing a bottom side arc surface 102c of the back pressure chamber
10 is along an arc S2. Accordingly, shoulder portions K1 and K2 of the lower end portion
61 coincide with the start end and the terminal end of the arc S2 about the center
point P5. A curvature radius L4 of the arc S2 forming the convex arc surface 611a
of the lower end portion 61 is smaller than a curvature radius L3 of the arc S1 forming
the concave arc surface 101 of the back pressure chamber 10. Reference numeral 63
in Fig. 3 indicates the center in the arc of the arc S2 forming the convex arc surface
611a of the lower end portion 61. In Fig. 3, for example, the curvature radius L4
of the arc S2 forming the convex arc surface 611a is substantially half the dimension
L2 in the thickness direction of the vane 6. Accordingly, the convex arc surface 611a
of the lower end portion 61 is a half peripheral surface and the center point P5 of
the arc S2 and the shoulder portions K1 and K2 of the lower end portion 61 are positioned
in a single line. When the position of the vane groove 5 does not deviate from the
position of the back pressure chamber 10, a center point P4 of the arc S1 does not
deviate from the center point P5 of the arc S2 as illustrated in Fig. 3(a), these
points are present in the center line C of the same vane groove 5, and the center
63 in the arc of the convex arc surface 611a of the lower end portion 61 can coincide
with the center 103 in the arc of the concave arc surface 101 of the back pressure
chamber 10.
[0040] Although the entire contact surface 611 facing a bottom side arc surface 102 of the
back pressure chamber 10 is the convex arc surface 611a along the arc S2 in the lower
end portion 61 of the vane 6 in the comparative example, the curvature radius L4 of
the arc S2 forming the convex arc surface 611a of the lower end portion 61 is the
same as the curvature radius L3 of the arc S1 forming the concave arc surface 101
of the back pressure chamber 10. Also in this case, when the position of the vane
groove 5 does not deviate from the position of the back pressure chamber 10, the center
point P4 of the arc S1 does not deviate from the center point P5 of the arc S2 as
illustrated in Fig. 8 (a), these points are present in the center line C of the same
vane groove 5, and the center 63 in the arc of the convex arc surface 611a of the
lower end portion 61 can coincide with the center 103 in the arc of the concave arc
surface 101 of the back pressure chamber 10.
[0041] However, in the comparative example, even when the convex arc surface 611a of the
lower end portion 61 is brought into contact with the bottom side arc surface 101c
of the back pressure chamber 10 so that the center 63 in the arc of the convex arc
surface 611a of the lower end portion 61 coincides with the center 103 in the arc
of the concave arc surface 101 of the back pressure chamber 10, voids D are not formed
between the vane 6 and the concave arc surface 101 of the back pressure chamber 10,
as illustrated in Fig. 8(a). In contrast, in embodiment 1, when the convex arc surface
611a of the lower end portion 61 is brought into contact with the bottom side arc
surface 101c of the back pressure chamber 10 so that the center 63 in the arc of the
convex arc surface 611a of the lower end portion 61 coincides with the center 103
in the arc of the concave arc surface 101 of the back pressure chamber 10, the voids
D are formed between the vane 6 and the concave arc surface 101 of the back pressure
chamber 10 on both sides in the thickness direction of the vane, as illustrated in
Fig. 3(a).
[0042] On the other hand, in manufacturing the rotor 4 of the invention using the manufacturing
method described above, when the vane groove 5 is polished, the position of the vane
groove 5 deviates from the position of the back pressure chamber 10, the center line
C of the vane groove 5 in the thickness direction of the vane 6 and the center point
P5 of the back pressure chamber 10 may deviate by approximately a predetermined dimension
X1 along the thickness direction of the vane 6 from a set position, as illustrated
in Figs. 3 (b) and 8 (b). In addition, the center 63 in the arc of the convex arc
surface 611a of the contact surface 611 and the center 103 in the arc of the concave
arc surface 101 of the back pressure chamber 10 also deviate by the predetermined
dimension X1 along the thickness direction of the vane 6, as illustrated in Figs.
3(b) and 8(b).
[0043] Since the voids D are not formed between the vane 6 and the concave arc surface of
the back pressure chamber 10 on both sides in the thickness direction of the vane
in the comparative example in Fig. 8, the shoulder portions K1 and K2 of the lower
end portion 61 override the side arc surfaces 101a and 101b of the back pressure chamber
10 as illustrated in Fig. 8(b) when the vane 6 enters the deepest part of the vane
groove 5. A clearance G1 is generated between the center 63 in the arc of the convex
arc surface 611a of the lower end portion 61 and the center 103 in the arc of the
concave arc surface 101 of the back pressure chamber 10 along the forward or backward
travel direction of the vane 6. Since this clearance G1 is large, the upper end portion
of the vane 6 projects from the outer peripheral surface of the rotor 4, the vane
6 interferes with the inner peripheral surface of the cylinder 8a, possibly disabling
the rotation of the rotor 4.
[0044] In contrast, since the voids D are formed between the vane 6 and the concave arc
surface 101 of the back pressure chamber 10 on both sides in the thickness direction
of the vane in embodiment 1, the shoulder portions K1 and K2 of the lower end portion
61 have difficulty in overriding the arc surface on the side arc surfaces 101a and
101b of the back pressure chamber 10 as illustrated in Fig. 3(b). Since the convex
arc surface 611a of the lower end portion 61 is raised along the arc of the concave
arc surface 101 of the back pressure chamber 10, a clearance G2 is generated along
the forward or backward travel direction of the vane 6 between the center 63 of the
arc surface of the lower end portion 61 and the center 103 of the arc surface of the
concave arc surface 101 of the back pressure chamber 10, as illustrated in Fig. 3(b).
However, since this clearance G2 is small, the upper end portion of the vane 6 does
not project from the outer peripheral surface of the rotor 4 in embodiment 1, the
vane 6 does not interfere with the inner peripheral surface of the cylinder 8a, thereby
preventing the rotation of the rotor 4 from being disabled.
[0045] Fig. 4 illustrates the other example of embodiment 1 illustrated in Fig. 3. The other
example of embodiment 1 will be described below with reference to Fig. 3. However,
the same components as in embodiment 1 are given the same reference numerals in principle
and descriptions are omitted.
[0046] The lower end portion 61 of the vane 6 in the other example of embodiment 1 is the
same as the lower end portion 61 illustrated in Fig. 3 in that the entire contact
surface 611 facing the bottom side arc surface 101c of the back pressure chamber 10
is the convex arc surface 611a along the arc S2. In contrast, in the lower end portion
61 of the vane 6 in the other example of embodiment 1, the curvature radius L4 of
the arc S2 forming the convex arc surface 611a is larger than substantially the half
of the dimension L2 in the thickness direction of the vane 6 and smaller than the
curvature radius L3 of the arc S1 forming the concave arc surface 101 of the back
pressure chamber 10. Accordingly, the convex arc surface 611a of the lower end portion
61 is smaller than a half peripheral surface and the center point P5 of the arc S2
is disposed closer to the sliding contact surface 6a of the vane 6 than the shoulder
portions K1 and K2 of the lower end portion 61.
[0047] Also in the other example of embodiment 1, when the position of the vane grooves
5 does not deviate from the position of the back pressure chamber 10, as illustrated
in Fig. 4(a), the center point P4 of the arc S1 does not deviate from the center point
P5 of the arc S2, these center points are present in the center line C of the same
vane groove 5, and the center 63 in the arc of the convex arc surface 611a of the
lower end portion 61 can coincide with the center 103 in the arc of the concave arc
surface 101 of the back pressure chamber 10.
[0048] In addition, also in the other example of embodiment 1, when the convex arc surface
611a of the lower end portion 61 is brought into contact with the bottom side arc
surface 101c of the back pressure chamber 10 so that the center 63 in the arc of the
convex arc surface 611a of the lower end portion 61 coincides with the center 103
in the arc of the concave arc surface 101 of the back pressure chamber 10 as illustrated
in Fig. 4(a), the voids D are formed between the vane 6 and the concave arc surface
of the back pressure chamber 10 on both sides in the thickness direction of vane,
unlike the comparative example in Fig. 8.
[0049] Accordingly, even when the vane groove 5 deviates from the back pressure chamber
10 along the thickness direction of the vane, since the voids D are generated between
the vane 6 and the concave arc surface 101 of the back pressure chamber 10 on both
sides in the thickness direction of the vane, the shoulder portions K1 and K2 of the
lower end portion 61 have difficulty in overriding the side arc surfaces 101a and
101b of the back pressure chamber 10 as illustrated in Fig. 4(b). In addition, the
clearance G2 in Fig. 4(b) generated because the convex arc surface 611a of the lower
end portion 61 is raised along the arc of the concave arc surface 101 of the back
pressure chamber 10 is small as in embodiment 1 in Fig. 3, so the upper end portion
of the vane 6 does not project from the outer peripheral surface of the rotor 4 also
in the other example of embodiment 1, the vane 6 does not interfere with the inner
peripheral surface of the cylinder 8a, thereby preventing the rotation of the rotor
4 from being disabled.
Embodiment 2
[0050] Figs. 5 and 6 illustrate embodiment 2 as described above. Embodiment 2 will be described
below with reference to Figs. 5 and 6. However, the same components as in embodiment
1 and the other example of embodiment 1 are given the same reference numerals in principle
and descriptions are omitted.
[0051] In the lower end portion 61 of the vane 6 in embodiment 2, the contact surface 611
includes the convex arc surface 611a and two tangential flat surfaces 611b continued
to the convex arc surface 611a.
[0052] As illustrated in Fig. 5, the convex arc surface 611a is formed along an arc S3a
of a circle S3, centered at P6, that has a radius L5 smaller than the radius L3 of
the arc S1 forming the concave arc surface 101 of the back pressure chamber 10, the
arc S3a facing the bottom side arc surface 101c. The tangential flat surfaces 611b
are formed so as to make contact with the arc S3a forming the convex arc surface 611a
in embodiment 2 and the contact flat surfaces 611b are flat surfaces extending from
both ends of the arc S3 toward the shoulder portions K1 and K2 while being inclined
toward the sliding contact surfaces 6a of the vane 6.
[0053] As illustrated in Fig. 6, the shape of the lower end portion 61 of the vane 6 in
embodiment 2 can also be formed by, for example, providing the flat surfaces 611b
on both sides in the thickness direction of the lower end portion 61 at the same angle
as the oblique angle of the tangential flat surface of the arc surface (arc S1) passing
through a point P7 at which the arc S1 forming the concave arc surface 101 of the
back pressure chamber 10 and a virtual line V extending from the inner side surface
of the vane groove 5 intersect and by connecting the intersection of the flat surface
611b and the flat surface 611b via the arc S3a of the contact circle S3 having the
curvature radius L5 smaller than the curvature radius L3 of the arc S1 forming the
concave arc surface of the back pressure chamber 10. It should be noted that the flat
surface 611b may be slightly inclined toward the shaft line of the vane groove 5 from
the same angle as the oblique angle of the tangential flat surface of the arc surface
(arc S1) passing through the point P7, which is not illustrated.
[0054] Also in embodiment 2, when the position of the vane grooves 5 does not deviate from
the position of the back pressure chamber 10, the center point P4 of the arc S1 does
not deviate from the center point P6 of the circle S3 (arc S3a) as illustrated Fig.
5(a), these center points are present in the center line C in the same vane groove
5, and the center 63 in the arc of the convex arc surface 611a of the lower end portion
61 can coincide with the center 103 in the arc of the concave arc surface 101 of the
back pressure chamber 10.
[0055] In addition, also in embodiment 2, as illustrated in Fig. 5 (a), when the convex
arc surface 611a of the lower end portion 61 makes contact with the bottom side arc
surface 101c of the back pressure chamber 10 so that the center 63 in the arc of the
convex arc surface 611a of the lower end portion 61 coincides with the center 103
in the arc of the concave arc surface 101 of the back pressure chamber 10, the voids
D are formed between the vane 6 and the concave arc surface of the back pressure chamber
10 on both sides in the thickness direction of the vane, unlike the comparative example
in Fig. 8.
[0056] Accordingly, even when the vane groove 5 deviates from the back pressure chamber
10 along the thickness direction of the vane, since the voids D are generated between
the vane 6 and the concave arc surface 101 of the back pressure chamber 10 on both
sides in the thickness direction of the vane, the shoulder portions K1 and K2 of the
lower end portion 61 have difficulty in overriding the side arc surfaces 101a and
101b of the back pressure chamber 10 as illustrated in Fig. 5(b). In addition, the
clearance G2 in Fig. 5(b) generated because the convex arc surface 611a of the lower
end portion 61 is raised along the arc of the concave arc surface 101 of the back
pressure chamber 10 is small as in the above embodiments, so the upper end portion
of the vane 6 does not project from the outer peripheral surface of the rotor 4 also
in embodiment 2, the vane 6 does not interfere with the inner peripheral surface of
the cylinder 8a, thereby preventing the rotation of the rotor 4 from being disabled.
Embodiment 3
[0057] Fig. 7 illustrate embodiment 3 as described above. Embodiment 3 will be described
below with reference to Fig. 7. However, the same components as in the embodiments
described above are given the same reference numerals in principle and descriptions
are omitted.
[0058] The lower end portion 61 of the vane 6 in embodiment 3 is tapered by partially removing
the sliding contact surface 6a and a part of the convex arc surface 611a of the vane
6 and forming the chamfered oblique surface 101c with respect to the convex arc surface
611a (the curvature radius L4 of the arc S2 is the same as the curvature radius L3
of the arc S1 forming the concave arc surface 101 of the back pressure chamber 10)
having the entire contact surface 611 facing the bottom side arc surface 101c of the
back pressure chamber 10 disposed along the arc S2 about the center point P5. However,
although not illustrated, the curvature radius L4 of the arc S2 may be smaller than
the curvature radius L3 of the arc S1 forming the concave arc surface 101 of the back
pressure chamber 10. In addition, the chamfered oblique surface 101c may be formed
by partially removing the sliding contact surface 6a of the vane 6 or the convex arc
surface 611a.
[0059] When the position of the vane grooves 5 does not deviate from the position of the
back pressure chamber 10, the center point P4 of the arc S1 does not deviate from
the center point P5 of the circle S2 as illustrated in Fig. 7(a), these center points
are present in the center line C in the same vane groove 5, and the center 63 in the
arc of the convex arc surface 611a of the lower end portion 61 can coincide with the
center 103 in the arc of the concave arc surface 101 of the back pressure chamber
10.
[0060] In addition, also in embodiment 3, as illustrated in Fig. 7 (a), when the convex
arc surface 611a of the lower end portion 61 makes contact with the bottom side arc
surface 101c of the back pressure chamber 10 so that the center 63 in the arc of the
convex arc surface 611a of the lower end portion 61 coincides with the center 103
in the arc of the concave arc surface 101 of the back pressure chamber 10, the voids
D are formed between the vane 6 and the concave arc surface of the back pressure chamber
10 on both sides in the thickness direction of the vane, unlike the comparative example
in Fig. 8.
[0061] Accordingly, even when the vane groove 5 deviates from the back pressure chamber
10 along the thickness direction of the vane, since the voids D are generated between
the vane 6 and the concave arc surface 101 of the back pressure chamber 10 on both
sides in the thickness direction of the vane, the shoulder portions K1 and K2 of the
lower end portion 61 have difficulty in overriding the side arc surfaces 101a and
101b of the back pressure chamber 10 as illustrated in Fig. 7(b). In addition, the
clearance G2 in Fig. 7(b) generated because the convex arc surface 611a of the lower
end portion 61 is raised along the arc of the concave arc surface 101 of the back
pressure chamber 10 is small as in the above embodiments, so the upper end portion
of the vane 6 does not project from the outer peripheral surface of the rotor 4 also
in embodiment 3, the vane 6 does not interfere with the inner peripheral surface of
the cylinder 8a, thereby preventing the rotation of the rotor 4 from being disabled.
Reference Signs List
[0062]
- 1:
- vane compressor
- 4:
- rotor
- 5:
- vane groove
- 6:
- vane
- 6a:
- sliding contact surface
- 61:
- lower end portion (other end portion)
- 611:
- contact surface
- 611a:
- convex arc surface
- 611b:
- tangential flat surface, flat surface
- 611c:
- chamfered oblique surface
- 63:
- center in arc of convex arc surface
- 8a:
- cylinder
- 10:
- back pressure chamber
- 101:
- concave arc surface
- 101a, 101b:
- side arc surface
- 101c:
- bottom side arc surface
- 103:
- center in arc of concave arc surface
- K1, K2:
- shoulder portion of vane
- D:
- void