Technical Field
[0001] The present invention relates to a scroll compressor.
Background Art
[0003] Scroll compressors have a compressor body including a fixed scroll and an orbiting
scroll.
[0004] The compressor body includes a compression chamber formed by the orbiting scroll
meshing with the fixed scroll. The scroll compressors compress the fluid within the
compression chamber by revolving and driving the orbiting scroll with respect to the
fixed scroll. Such scroll compressors have a ring-like thrust plate as a member that
suppresses seizure resulting from sliding of the orbiting scroll (for example, refer
to PTL 1).
[0005] PTL 1 discloses a configuration in which the orbiting scroll is provided with a ring-like
recessed portion that houses a portion of a thrust plate, and the position of the
thrust plate is restricted by interposing the thrust plate between the orbiting scroll
and the front housing (frame). PTL 2 discloses a thrust plate formed of an abrasion-resistant
material. PTL 3 discloses a minor gap on an inner periphery side of a thrust bearing.
PTL 4 discloses a scroll-type compressor used for a vehicle air conditioner which
includes an orbiting scroll, a stationary scroll, and a thrust plate.
Citation List
Patent Literature
[0006]
[PTL 1] Japanese Unexamined Patent Application Publication No. 2012-225257 [PTL 2] European Patent Application Publication No. EP3081815
[PTL 3] Japanese Patent Application Publication No. JPS57173585
[PTL 4] International Patent Application Publication No. WO2015198516
Summary of Invention
Technical Problem
[0007] As described above, PTL 1 has a configuration in which the thrust plate is interposed
between the orbiting scroll, which is revolved and driven with respect to the fixed
scroll, and the front housing. For this reason, if a centrifugal force becomes large
due to the orbiting of the orbiting scroll and a thrust load is increased, the position
of the thrust plate deviates from the recessed portion and the thrust plate and the
front housing interfere with each other. Therefore, there is a possibility that the
thrust plate and its peripheral components (components disposed around the thrust
plate) may be damaged.
[0008] Thus, an object of the invention is to provide a scroll compressor that can suppress
damage to a thrust plate and its peripheral components.
Solution to Problem
[0009] In order to solve the above problems, a scroll compressor related to an aspect of
the invention includes a housing that has a cylindrical rear housing, and a front
housing including a plate placement surface; a fixed scroll that is provided within
the rear housing and fixed to the rear housing; an orbiting scroll that is provided
within the rear housing, partitions a compression chamber between the orbiting scroll
and the fixed scroll by meshing the fixed scroll, and is revolved and driven around
the fixed scroll; a ring-like thrust plate that is disposed between an end plate,
in the orbiting scroll, disposed on a side opposite to a side where the fixed scroll
is provided and the plate placement surface of the front housing; a plurality of bolts
that are fastened to a plate placement part, of the front housing, which partitions
the plate placement surface and that restricts a position of the thrust plate with
respect to the plate placement part, and the plurality of bolts each include a head
part, and a shaft part having one end connected to the head part, and at least a portion
of the head part is disposed to protrude from the plate placement surface, and the
thrust plate has a plurality of through-holes that allow the head part to pass therethrough.
[0010] According to the invention, by having the plurality of bolts that are fastened to
the plate placement part partitioning the plate placement surface, in the front housing
which does not turn, and that restrict the position of the thrust plate with respect
to the plate placement part, it is possible to suppress the displacement of the thrust
plate even in case where a centrifugal force becomes large due to the orbiting of
the orbiting scroll and a thrust load is increased.
[0011] Accordingly, since any interference between the thrust plate and the front housing
is suppressed, damage to the thrust plate and its peripheral components (components
disposed around the thrust plate) can be suppressed.
[0012] By adopting such a configuration, it is possible to dispose the thrust plate on the
plate placement surface in a state where the plurality of bolts are fastened to the
plate placement part, without detaching the plurality of bolts fastened to the plate
placement part from the plate placement part. Accordingly, positional restriction
of the thrust plate can be enhanced due to the fitting between the head parts of the
bolts and the through-holes of the thrust plate.
[0013] Additionally, by configuring the thrust plate so as not to be directly fastened with
the bolts, occurrence of distortion or deformation of the thrust plate resulting from
the bolt fastening is suppressed. Thus, the reliability of the scroll compressor can
be improved.
[0014] Additionally, in the scroll compressor according to the aspect of the invention,
the head part of each of the plurality of bolts may be disposed outside the orbiting
scroll, and an outer peripheral part of the end plate may be provided with a first
cutout part capable of housing the head part when the orbiting scroll is revolved.
[0015] By providing the first cutout part having such a configuration at the outer peripheral
part of the end plate, the contact between the outer peripheral part of the orbiting
scroll and the head parts of the bolts when the orbiting scroll is revolved can be
suppressed.
[0016] Additionally, in the scroll compressor according to the aspect of the invention,
a material of each of the plurality of bolts may be a material harder than a material
of the orbiting scroll.
[0017] In this way, by using the material harder than the material of the orbiting scroll
as the material of the plurality of bolts, even in case where the outer peripheral
part of the orbiting scroll and the head parts of the bolts are in contact with each
other when the orbiting scroll is revolved, damage to the head parts of the bolts
may be suppressed. Accordingly, even in case where a thrust load is increased, displacement
of the thrust plate can be suppressed by the plurality of bolts.
[0018] Additionally, in the scroll compressor according to the aspect of the above invention,
the rear housing may include a suction port that suctions a fluid within the rear
housing, and the plurality of bolts may be provided at positions separated from the
suction port in a circumferential direction of the plate placement part.
[0019] In this way, by providing the plurality of bolts at positions separated from the
suction port for suctioning the fluid in the circumferential direction of the plate
placement part, the fluid does not easily collide against the head parts of the bolts.
Accordingly, occurrence of turbulence in the airflow of the fluid within the housing
can be suppressed.
[0020] In the scroll compressor according to the aspect of the invention, the plate placement
part of the front housing may be provided with bolt holes to which the plurality of
bolts are fastened, and each of the plurality of bolts may include a protruding part
that is provided at the other end of a shaft part of each of the plurality of bolts,
is made to have an outer diameter smaller than an outer diameter of the shaft part,
and protrudes in an extending direction of the shaft part.
[0021] In this way, by having the protruding part, which has an outer diameter smaller than
the outer diameter of the shaft part and protrudes in the extending direction of the
shaft part, at the other end of the shaft part of each of the plurality of bolts,
it is possible to make the bolts independent from the bolt holes by inserting the
protruding part into each bolt hole when the bolts are fastened to the bolt holes.
Accordingly, the work of fastening the bolts to the plurality of bolt holes can be
easily performed.
[0022] Additionally, the scroll compressor according to the aspect of the invention may
further include a rotation suppressing member that is provided between the orbiting
scroll and the thrust plate, suppresses rotation of the orbiting scroll, and includes
a plurality of engaging projections, the thrust plate may include a plurality of insertion
cutout parts into which the engaging projections are inserted, and the plurality of
through-holes may be provided at positions separated from the plurality of insertion
cutout parts.
[0023] In this way, by providing the plurality of through-holes at the positions separated
from the plurality of insertion cutout parts, a decrease in the strength of the portions
of the thrust plate partitioning the through-holes and the portions of the thrust
plate partitioning the insertion cutout parts can be suppressed.
[0024] Additionally, in the scroll compressor according to the aspect of the invention,
the front housing may include a plurality of second cutout parts that are provided
in the outer peripheral part of the plate placement part in a circumferential direction,
and are formed by cutting out the plate placement part corresponding to the plate
placement surface, and the thrust plate may have claw parts that are provided in the
outer peripheral part of the thrust plate in the circumferential direction and are
respectively disposed within the plurality of second cutout parts in a bent state.
[0025] In this way, by having the claw parts that are respectively disposed in a bent state
within the plurality of second cutout parts, it is possible to restrict the position
of the thrust plate using both members of the claw parts and the head parts of the
bolts. Thus, even in case where the thrust load is increased, the displacement of
the thrust plate can be further suppressed. Additionally, it is possible to restrict
the position of the thrust plate using both members of the claw parts and the head
parts of the bolts. Accordingly, even in case where any one of the claw parts and
the head parts of the bolts lose the function of positional restriction of the thrust
plate due to wear or the like, it is possible to perform the positional restriction
of the thrust plate using the other. Accordingly, the reliability of the scroll compressor
can be improved.
[0026] Additionally, in the scroll compressor according to the aspect of the invention,
the plurality of claw parts may be provided at positions different from formation
positions of a plurality of through-holes provided in the thrust plate in a radial
direction of the thrust plate.
[0027] By providing the plurality of claw parts at such positions, a decrease in the strength
of the plurality of claw parts can be suppressed.
[0028] Additionally, in the scroll compressor according to the aspect of the invention,
the plurality of claw parts may be disposed outside the formation positions of a plurality
of through-holes provided in the thrust plate.
[0029] The plurality of claw parts are configured by bending the thrust plate that is a
thin plate. For this reason, the claw parts may be damaged if the claw parts receive
a large thrust load.
[0030] Thus, by providing the plurality of claw parts outside the formation positions (in
other words, the positions of the plurality of bolts) of the plurality of through-holes
provided in the thrust plate, the thrust plate abuts against the plurality of bolts
disposed inside the plurality of claw parts even in case where a large thrust load
is applied to the thrust plate. Accordingly, since it is possible to reduce the thrust
load in the outer peripheral part of the thrust plate. Accordingly, the plurality
of claw parts do not receive a large thrust load. Hence, the displacement of the thrust
plate can be further suppressed while suppressing damage to the plurality of claw
parts.
[0031] Additionally, in the scroll compressor according to the aspect of the above invention,
a first clearance formed between a head part of each of the bolts and each of through-holes
of the thrust plate may be smaller than a second clearance formed between a position
where the thrust plate is bent and each of the second cutout parts.
[0032] In this way, by making the first clearance smaller than second clearance, the portions
of the thrust plate that partition the through-holes, and the bolts are brought into
contact with each other when the thrust plate is displaced. Accordingly, it is possible
to suppress the collision of the plurality of claw parts against corners of the second
cutout parts. Accordingly, damage to the claw parts resulting from the claw parts
colliding against the corners of the second cutout parts can be suppressed.
Advantageous Effects of Invention
[0033] Accordingly, damage to the thrust plate and its peripheral components (components
disposed around the thrust plate) can be suppressed.
Brief Description of Drawings
[0034]
Fig. 1 is a sectional view schematically illustrating a schematic configuration of
principal parts of a scroll compressor related to a first embodiment of the invention.
Fig. 2 is a schematic view for illustrating a positional relationship between a suction
port constituting a housing, and a plurality of bolts.
Fig. 3 is a sectional view of the scroll compressor illustrated in Fig. 2 taken along
line C1-C2.
Fig. 4 is a plan view schematically illustrating a rotation suppressing member illustrated
in Fig. 1.
Fig. 5 is a sectional view for illustrating a modification example of bolts to be
fastened to a plate placement part.
Fig. 6 is a sectional view schematically illustrating a schematic configuration of
principal parts of a scroll compressor related to a modification example of the first
embodiment.
Fig. 7 is a view schematically illustrating a schematic configuration of principal
parts of a scroll compressor related to a second embodiment of the invention.
Fig. 8 is a sectional view of the scroll compressor illustrated in Fig. 7 taken along
line D1-D2.
Description of Embodiments
[0035] Hereinafter, embodiments to which the invention is applied will be described in detail
with reference to the drawings.
(First embodiment)
[0036] A scroll compressor 10 of a first embodiment of the invention will be described with
reference to Figs. 1 to 3. In addition, O
1 illustrated in Fig. 1 represents an axis (hereinafter referred to as "an axis O1")
of a drive shaft 14. Fig. 2 is a view of a plate placement part 42, a thrust plate
27, a bolt 12, and a rear housing 32, which are illustrated in Fig. 1, as seen from
A. In Fig. 2, for the convenience of description, the rear housing 32 is illustrated
in a section. E illustrated in Fig. 2 represents a circumferential direction (hereinafter
referred to as "a circumferential direction E") of the plate placement part 42.
[0037] In Fig. 2, the same components as those of the structural body illustrated in Figs.
1 and 3 are denoted by the same reference signs. Additionally, for convenience of
description, an end plate 51A (refer to Fig. 1), which is not illustrated in Fig.
2, is illustrated in Fig. 3.
[0038] The scroll compressor 10 has a housing 11, a plurality of the bolts 12, a main bearing
13, the drive shaft 14, a sub-bearing 15, a lip seal 17, a driven crank mechanism
19, a compressor body 21, a rotation suppressing member 23, and the thrust plate 27.
[0039] The housing 11 has a sealed structure and has the rear housing 32 and a front housing
34.
[0040] The rear housing 32 is a cylindrical cup-shaped member. One side of the rear housing
32 is an open end. The rear housing 32 has a suction port 35 for introducing a fluid
into the housing 11 from the outside of the housing 11.
[0041] The front housing 34 is provided on the open end side of the rear housing 32 so as
to block the open end of the rear housing 32. The front housing 34 has a first housing
part 36 and a second housing part 37.
[0042] The first housing part 36 is fitted to the rear housing 32 via a seal member (for
example, an O-ring or the like) on the open end side of the rear housing 32. The first
housing part 36 has a main-bearing housing part 41 and the plate placement part 42.
The main-bearing housing part 41 has a space capable of housing the main bearing 13
therein.
[0043] The plate placement part 42 is disposed between the main-bearing housing part 41
and an orbiting scroll 51 in the axis O
1. The plate placement part 42 protrudes in a direction toward the orbiting scroll
51 from the main-bearing housing part 41 located outside the main bearing 13.
[0044] The shape of the plate placement part 42 is a ring shape. The plate placement part
42 has a plate placement surface 42a that is a plane that faces the orbiting scroll
51. The plate placement surface 42a is a ring-like flat plane. The thrust plate 27
is disposed on the plate placement surface 42a.
[0045] The plate placement part 42 has a plurality of (for example, two as an example, in
the case of Fig. 2) and bolt holes 42A and a plurality of cutout grooves 42B. The
bolts 12 are respectively fastened to the plurality of bolt holes 42A. It is preferable
that the plurality of bolt holes 42A are provided, for example, at positions separated
from the suction port 35 in the circumferential direction E of the plate placement
part 42.
[0046] In this way, by providing the plurality of bolt holes 42A at the positions separated
from the suction port 35 in the circumferential direction E of the plate placement
part 42, it is possible to dispose the plurality of bolts 12 at the positions separated
in the circumferential direction E of the plate placement part 42 from the suction
port 35.
[0047] Accordingly, since it is possible to suppress the collision of the fluid immediately
after being suctioned from the suction port 35 against head parts 12A of bolts 12,
occurrence of turbulence in an airflow formed within the housing 11 can be suppressed.
[0048] Additionally, as illustrated in Fig. 2, in case where the plate placement part 42
has two bolt holes 42A, the two bolt holes 42A may be disposed to face each other
with the axis O
1 interposed therebetween. By providing the two bolt holes 42A at such positions, the
position of the thrust plate 27 with respect to the plate placement part 42 can be
firmly restricted using the two bolts 12.
[0049] In addition, although a case where the two bolt holes 42A are provided has been described
as an example in Fig. 2, the number of bolt holes 42A may be plural and is not limited
to two.
[0050] The cutout grooves 42B are formed by being cut out in portions of an inner peripheral
part of the plate placement surface 42a. The plurality of (two as an example, in the
case of Fig. 2) cutout grooves 42B are disposed in the circumferential direction of
the plate placement part 42. As illustrated in Fig. 2, in case where two cutout grooves
42B are provided, the cutout grooves 42B may be disposed to face each other with the
axis O
1 interposed therebetween.
[0051] Each of the plurality of bolts 12 has a head part 12A, and a shaft part 12B having
one end connected to the head part 12A. The plurality of bolts 12 are provided at
the plate placement part 42. The head parts 12A are fastened to the two bolt holes
42A in a state where lower surfaces 12Aa of the bolts 12 are in contact with the plate
placement surface 42a. Accordingly, the entire head parts 12A protrude from the plate
placement surface 42a. The plurality of bolts 12 are disposed in an outer peripheral
part of the thrust plate 27 in a circumferential direction.
[0052] The head parts 12A of the bolts 12 are disposing within through-holes 64 (to be described
below) of the thrust plate 27, so that when the thrust plate 27 is displaced, the
thrust plate 27 partitioning the through-holes 64 abuts against the head parts, thereby
suppressing the displacement of the thrust plate 27.
[0053] The plurality of bolts 12 may be provided, for example, at positions separated from
the suction port 35 in the circumferential direction of the plate placement part 42.
[0054] In this way, by providing the plurality of bolts 12 at positions separated from the
suction port 35 for suctioning the fluid in the circumferential direction of the plate
placement part 42, the fluid does not easily collide against the head parts 12A of
the bolts 12. Accordingly, occurrence of turbulence in the airflow of the fluid within
the housing 11 can be suppressed.
[0055] The second housing part 37 is formed integrally with the first housing part 36 such
that the first housing part 36 is disposed between the second housing part 37 and
the orbiting scroll 51.
[0056] The second housing part 37 is a tubular member extends in the direction of the axis
O
1, and both ends thereof are open ends. The outer diameter and the inner diameter of
the second housing part 37 are configured so as to be smaller than the outer diameter
and the inner diameter of the main-bearing housing part 41.
[0057] The main bearing 13 has an outer ring 13A, an inner ring 13B, and a plurality of
rolling elements 13C. The outer ring 13A is fixed to the main-bearing housing part
41. The inner ring 13B is fixed to an outer peripheral part of a base end part 14A
of the drive shaft 14. The plurality of rolling elements 13C are disposed between
the outer ring 13A and the inner ring 13B.
[0058] The drive shaft 14 extends in the direction of the axis O
1, and has the base end part 14A, a tip part 14B, and a crankpin 14C.
[0059] The drive shaft 14 passes through the second housing part 37 from the inside of the
housing 11. A portion of the tip part 14B of the drive shaft 14 is housed within the
second housing part 37 in a state where a gap allowing the sub-bearing 15 to be disposed
therein is interposed between the tip part and the second housing part 37.
[0060] A remaining portion (a portion located closer to a tip side than a portion of the
tip part 14B) of the tip part 14B of the drive shaft 14 protrudes toward the outside
of the second housing part 37.
[0061] The base end part 14A is larger in diameter than the tip part 14B. The crankpin 14C
is provided at the base end part 14A located on the side opposite to the side where
the tip part 14B is disposed. The crankpin 14C is disposed at a position that is eccentric
by a predetermined dimension with respect to the axis O
1.
[0062] The sub-bearing 15 is provided between the second housing part 37 and a portion of
the tip part 14B of the drive shaft 14. The sub-bearing 15 has an outer ring 15A,
an inner ring 15B, and a plurality of rolling elements 15C. The outer ring 15A is
fixed inside the second housing part 37.
[0063] The inner ring 15B is fixed to a partial outer peripheral part of the tip part 14B
of the drive shaft 14. The plurality of rolling elements 15C are disposed between
the outer ring 15A and the inner ring 15B.
[0064] Accordingly, the sub-bearing 15 rotatably supports the drive shaft 14 together with
the main bearing 13.
[0065] The lip seal 17 is provided on an inner wall of the second housing part 37 located
closer to the base end part 14A side of the drive shaft 14 than the sub-bearing 15.
The lip seal 17 abuts against an outer peripheral surface of the drive shaft 14. The
lip seal 17 is a seal member for maintaining the airtightness within the housing 11
(for preventing entering of the air outside the housing 11) .
[0066] The driven crank mechanism 19 has a drive bush 46 and a turning bearing 47. The drive
bush 46 houses the crankpin 14C and is fixed to the outside of the crankpin 14C. The
turning bearing 47 is provided outside the drive bush 46.
[0067] The compressor body 21 is housed within the housing 11 and has a fixed scroll 49
and the orbiting scroll 51.
[0068] The fixed scroll 49 has an end plate 49A and a wrap part 49B. The end plate 49A is
orthogonal to the axis O
1. The end plate 49A is disposed to face the front housing 34 via the orbiting scroll
51 in the direction of the axis O
1. The end plate 49A is orthogonal to the axis O
1 and has one surface 49Aa that faces the orbiting scroll 51. The end plate 49A of
the fixed scroll 49 is fixed to the rear housing 32 with bolts or the like.
[0069] The wrap part 49B has a spiral shape and is provided on the one surface 49Aa of
the end plate 49A. The wrap part 49B is erected in the direction of the axis O
1.
[0070] The orbiting scroll 51 is disposed between the front housing 34 and the fixed scroll
49. The orbiting scroll 51 has the end plate 51A, a wrap part 51B, and a boss part
51C.
[0071] The end plate 51A is orthogonal to the axis O
1. The end plate 51A has one surface 51Aa that faces the one surface 49Aa of the fixed
scroll 49, the other surface 51Ab, and a first cutout part 51Ac.
[0072] The one surface 51Aa is in contact with an inner peripheral part of the thrust plate
27 and is disposed inside positions where the head parts 12A of the plurality of bolts
12 are provided.
[0073] The other surface 51Ab is disposed on the side opposite to the one surface 51Aa and
is orthogonal to the axis O
1. The other surface 51Ab faces the driven crank mechanism 19. The first cutout part
51Ac is provided at an outer peripheral part of the end plate 51A so as to be capable
of housing the head parts 12A of the bolts 12 when the orbiting scroll 51 is revolved.
[0074] By providing the first cutout part 51Ac having such a configuration at the outer
peripheral part of the end plate 51A, the contact between the outer peripheral part
of the orbiting scroll 51 and the head parts 12A of the bolts 12 when the orbiting
scroll 51 is revolved can be suppressed.
[0075] The wrap part 51B has a spiral shape and is provided on the one surface 51Aa of the
end plate 51A. The wrap part 51B is erected in the direction of the axis O
1 (a direction toward the end plate 49A). The wrap part 51B meshes with the wrap part
49B. Accordingly, a compression chamber 21A that compresses the fluid is partitioned
between the fixed scroll 49 and the orbiting scroll 51.
[0076] The boss part 51C is provided on the other surface 51Ab of the end plate 51A. The
boss part 51C protrudes in a direction toward the front housing 34 from the other
surface 51Ab of the end plate 51A. The boss part 51C houses a portion of the driven
crank mechanism 19. The boss part 51C is coupled to the crankpin 14C via the driven
crank mechanism 19.
[0077] Accordingly, the orbiting scroll 51 is configured to be capable of being revolved
and driven with respect to the fixed scroll 49.
[0078] In addition, as the material of the plurality of bolts 12 described earlier, for
example, a material harder than the material of the orbiting scroll 51 may be used.
[0079] In this way, by using the material harder than the material of the orbiting scroll
51 as the material of the plurality of bolts 12, even in case where the outer peripheral
part of the orbiting scroll 51 and the head parts 12A of the bolts 12 are in contact
with each other when the orbiting scroll 51 is revolved, damage to the head parts
12A of the bolts 12 may be suppressed. Accordingly, even in case where a thrust load
is increased, displacement of the thrust plate 27 can be suppressed by the plurality
of bolts 12.
[0080] Next, the rotation suppressing member 23 will be described with reference to Figs.
1, 2, and 4. In Fig. 4, the rotation suppressing member 23 as seen in a plan view
from the front housing 34 side is illustrated. Additionally, in Fig. 4, an Oldham
ring is illustrated as an example of the rotation suppressing member 23.
[0081] The rotation suppressing member 23 is provided between the plate placement part 42
and the orbiting scroll 51. The rotation suppressing member 23 has a ring-like member
55, first engaging projections 56, and second engaging projections 57. The ring-like
member 55 has a surface in contact with the end plate 51A of the orbiting scroll 51
and a surface 55a disposed on the side opposite to this surface. The surface 55a is
a surface that faces the front housing 34.
[0082] The first engaging projections 56 are provided by the same number as that of the
cutout grooves 42B on the surface 55a of the ring-like member 55. The first engaging
projections 56 protrude in a direction orthogonal to the surface 55a of the ring-like
member 55. The first engaging projections 56 are disposed at positions where the projections
are insertable into the cutout grooves 42B.
[0083] A plurality of (two as an example in the case of Fig. 3) the second engaging projections
57 are provided on the surface 55a of the ring-like member 55 located on the side
opposite to the surface 55a. The second engaging projections 57 protrude from the
surface 55a of the ring-like member 55 located on the side opposite to the surface
55a. The second engaging projections 57 have a shape wider than the ring-like member
55. The second engaging projections 57 are inserted into groove parts formed in the
end plate 51A.
[0084] The rotation suppressing member 23 having the above configuration suppresses the
rotation of the orbiting scroll 51.
[0085] In addition, although the Oldham ring has been described as an example of the rotation
suppressing member 23 in Fig. 4, for example, a pin/link type rotation suppressing
member, or other types of rotation suppressing members may be used.
[0086] Next, the thrust plate 27 will be described with reference to Figs. 1 to 4.
[0087] The thrust plate 27 is a thin metallic plate and is provided between the plate placement
part 42 and the orbiting scroll 51. The thrust plate 27 has a plate body 61, a plurality
of insertion cutout parts 62, and a plurality of through-holes 64.
[0088] The plate body 61 is a ring-like plate material. In the plate body 61, one entire
overall surface is in contact with the plate placement surface 42a, and an inner peripheral
part of the other surface is in contact with the end plate 51A of the orbiting scroll
51. Accordingly, the outer peripheral part of the plate body 61 is exposed from the
end plate 51A.
[0089] The plurality of (two as an example in the case of Fig. 2) insertion cutout parts
62 are provided at an inner peripheral part of the plate body 61. The plurality of
insertion cutout parts 62 are provided so as to correspond to the formation positions
of the cutout grooves 42B.
[0090] Portions of the first engaging projections 56 are inserted into the plurality of
insertion cutout parts 62. By inserting the first engaging projections 56 into the
insertion cutout parts 62 and the cutout grooves 42B, the positions of the plate placement
part 42, the thrust plate 27, and the rotation suppressing member 23 are restricted.
[0091] As illustrated in Fig. 2, in case where the two insertion cutout parts 62 are provided,
two insertion cutout parts 62 may be disposed so as to face each other with the axis
O
1 interposed therebetween. In addition, the number of insertion cutout parts 62 may
be plural and is not limited to two.
[0092] The plurality of (two as an example in the case of Fig. 2) 64 are circular holes
formed by passing through the outer peripheral part of the plate body 61. The diameter
of the plurality of through-holes 64 is set to such a size that the through-holes
allow the head parts 12A of the bolts 12 to pass therethrough. A first clearance CL
1 is provided between the plurality of through-holes 64 and the head parts 12A of the
bolts 12. The plurality of through-holes 64 surround the head parts 12A of the bolts
12 via the first clearance CL
1.
[0093] In this way, by having the thrust plate 27 including the plurality of through-holes
64 having such a size that the head parts 12A of the bolts 12, which are disposed
on the plate placement surface 42a of the plate placement part 42 and protrude from
the plate placement surface 42a, can pass through the through-holes, it is possible
to dispose the thrust plate 27 on the plate placement surface 42a in a state where
the plurality of bolts 12 are fastened to the plate placement part 42, without detaching
the plurality of bolts 12 fastened to the plate placement part 42 from the plate placement
part 42.
[0094] Accordingly, positional restriction of the thrust plate 27 can be enhanced due to
the fitting between the head parts 12A of the bolts 12 and the through-holes 64 of
the thrust plate 27.
[0095] Additionally, by configuring the thrust plate 27 so as not to be directly fastened
with the bolts 12, occurrence of distortion or deformation of the thrust plate 27
resulting from the bolt fastening is suppressed. Thus, the reliability of the scroll
compressor 10 can be improved.
[0096] Additionally, the plurality of through-holes 64 may be provided, for example, at
positions separated from the plurality of insertion cutout parts 62.
[0097] In this way, by providing the plurality of through-holes 64 at the positions separated
from the plurality of insertion cutout parts 62, a decrease in the strength of the
portions of the thrust plate 27 partitioning the through-holes 64 and the portions
of the thrust plate 27 partitioning the insertion cutout parts 62 can be suppressed.
[0098] In the scroll compressor 10 having the above configuration, the orbiting scroll 51
is separated from the thrust plate 27 and replacement work (maintenance) of the thrust
plate 27 is performed, in a state where the plurality of bolts 12 are fastened to
the bolt holes 42A of the plate placement part 42.
[0099] According to the scroll compressor 10 of the first embodiment, by having the plurality
of bolts 12 that are fastened to the plate placement part 42 partitioning the plate
placement surface 42a, in the front housing 34 which does not turn, and that restrict
the position of the thrust plate 27 with respect to the plate placement part 42, it
is possible to suppress the displacement of the thrust plate 27 even in case where
a centrifugal force becomes large due to the orbiting of the orbiting scroll 51 and
a thrust load is increased.
[0100] Accordingly, since any interference between the thrust plate 27 and the front housing
34 is suppressed, damage to the thrust plate 27 and its peripheral components (components
disposed around the thrust plate 27) can be suppressed.
[0101] Next, the modification example of the bolt fastened to the plate placement part 42
will be described with reference to Fig. 5. In Fig. 5, the same components as those
of the structural body illustrated in Fig. 3 are denoted by the same reference signs.
[0102] A bolt 67 is configured to each bolt 12 except that the configuration of each bolt
12 illustrated in Fig. 3 is further provided with a protruding part 68. A plurality
of the bolts 67 are fastened to the bolt holes 42A. The protruding part 68 is provided
at the other end of the shaft part 12B.
[0103] The protruding part 68 protrudes in an extending direction of the shaft part 12B.
The outer diameter of the protruding part 68 is configured so as to be smaller than
the outer diameter of the shaft part 12B.
[0104] In this way, by having the protruding part 68, which has an outer diameter smaller
than the outer diameter of the shaft part 12B and protrudes in the extending direction
of the shaft part 12B, at the other end of the shaft part 12B of each of the plurality
of bolts 67, it is possible to make the bolts 67 independent from the bolt holes 42A
by inserting the protruding part 68 into each bolt hole 42A when the bolts 67 are
fastened to the bolt holes 42A. Accordingly, the work of fastening the bolts 67 to
the plurality of bolt holes 42A can be easily performed.
[0105] Next, a scroll compressor 70 related to a modification example of the first embodiment
will be described with reference to Fig. 6. In Fig. 6, some of constituent elements
of the scroll compressor 70 are illustrated. In Fig. 6, the same components as those
of the structural body illustrated in Fig. 3 are denoted by the same reference signs.
[0106] The scroll compressor 70 is configured similarly to the scroll compressor 10 except
having bolt holes 71 instead of the bolt holes 42A that constitute the scroll compressor
10 of the first embodiment.
[0107] Each bolt hole 71 has a head part housing part 71A and a shaft part hole 71B. The
head part housing part 71A is provided on the plate placement surface 42a side of
the plate placement part 42. The head part housing part 71A houses a portion of the
head part 12A of each bolt 12. The shaft part hole 71B is a hole threadedly engaged
with the shaft part 12B of the bolt 12 and is formed integrally with the head part
housing part 71A.
[0108] By providing the bolt holes 71 considered as such a configuration in the plate placement
part 42 and fastening the bolts 12 to the bolt holes 71, it is possible to reduce
the amount of protrusion of the head parts 12A that protrude from the plate placement
surface 42a.
[0109] Accordingly, a width W of the first cutout part 51Ac (the width in the direction
of the axis O
1 illustrated in Fig. 1) can be made smaller as compared to a structural body (a structural
body in which the entire head parts 12A protrude from the plate placement surface
42a) illustrated in Fig. 3.
(Second Embodiment)
[0110] A scroll compressor 75 of a second embodiment will be described with reference to
Figs. 3, 7, and 8. In Fig. 7, only principal parts of the scroll compressor 75 are
schematically illustrated. Additionally, in Fig. 7, the same components as those of
the structural body illustrated in Fig. 2 are denoted by the same reference signs.
Additionally, in Fig. 8, the same components as those of the structural body illustrated
in Fig. 1 and 7 are denoted by the same reference signs.
[0111] The scroll compressor 75 of the second embodiment is configured similarly to the
scroll compressor 10 except that the plate placement part 42 described in the first
embodiment is provided with a plurality of second cutout parts 76 and a thrust plate
78 is provided instead of the thrust plate 27 that constitutes the scroll compressor
10 of the first embodiment.
[0112] The plurality of second cutout parts 76 are provided in the outer peripheral part
of the plate placement part 42 that partitions the plate placement surface 42a, in
the circumferential direction.
[0113] Each second cutout part 76 has a surface 76a orthogonal to the plate placement surface
42a. The second cutout part 76 can be disposed, for example, between a bolt 12 and
a cutout groove 42B.
[0114] By providing the second cutout part 76 at such a position, the second cutout part
76 can be disposed at a position where an insertion cutout part 62 and a through-hole
64 are not provided.
[0115] The thrust plate 78 is configured similarly to the scroll compressor 10 described
in the first embodiment except for having a plurality of claw parts 79.
[0116] The plurality of claw parts 79 are configured such that portions protruding from
an outer peripheral edge of the plate body 61 are bent toward the second cutout parts
76 side. The claw parts 79 are disposed within the plurality of second cutout parts
76.
[0117] In this way, by having the claw parts 79 that are respectively disposed in a bent
state within the plurality of second cutout parts 76, it is possible to restrict the
position of the thrust plate 78 using both members of the claw parts 79 and the head
parts 12A of the bolts 12. Thus, even in case where the thrust load is increased,
the displacement of the thrust plate 78 can be further suppressed.
[0118] Additionally, it is possible to restrict the position of the thrust plate 78 using
both members of the claw parts 79 and the head parts 12A of the bolts 12. Accordingly,
even in case where any one of the claw parts 79 and the head parts 12A of the bolts
12 lose the function of positional restriction of the thrust plate 78 due to wear
or the like, it is possible to perform the positional restriction of the thrust plate
78 using the other. Accordingly, the reliability of the scroll compressor 75 can be
improved.
[0119] Additionally, the plurality of claw parts 79 may be disposed, for example, outside
the formation positions of the plurality of through-holes 64 provided in the thrust
plate 78.
[0120] The plurality of claw parts 79 are configured by bending the thrust plate 78 that
is a thin metallic plate. For this reason, the claw parts 79 may be damaged if the
claw parts receive a large thrust load.
[0121] Thus, by providing the plurality of claw parts 79 outside the formation positions
(in other words, the positions of the plurality of bolts 12) of the plurality of through-holes
64 provided in the thrust plate 78, the thrust plate 78 abuts against the plurality
of bolts 12 disposed inside the plurality of claw parts 79 even in case where a large
thrust load is applied to the thrust plate 78. Accordingly, since it is possible to
reduce the thrust load in the outer peripheral part of the thrust plate 78, the plurality
of claw parts 79 do not receive a large thrust load.
[0122] Accordingly, the displacement of the thrust plate 78 can be further suppressed while
suppressing damage to the plurality of claw parts 79.
[0123] Moreover, the plurality of claw parts 79 may be provided at positions different from
the formation positions of the plurality of through-holes 64 provided in the thrust
plate 78 in a radial direction of the thrust plate 78.
[0124] By providing the plurality of claw parts 79 at such positions, a decrease in the
strength of the plurality of claw parts 79 can be suppressed.
[0125] A second clearance CL
2 is formed between the surface 76a of a second cutout part 76 and a claw part 79.
The first clearance CL
1 described earlier may be, for example, made smaller than the second clearance CL
2.
[0126] In this way, by making the first clearance CL
1 smaller than second clearance CL
2, the portions of the thrust plate 78 that partition the through-holes 64, and the
bolts 12 are brought into contact with each other when the thrust plate 78 is displaced.
Accordingly, it is possible to suppress the collision of the claw parts 79 against
corners 76A of the second cutout parts 76. Accordingly, damage to the claw parts 79
resulting from the claw parts 79 colliding against the corners 76A of the second cutout
parts 76 can be suppressed.
[0127] According to the scroll compressor 75 of the second embodiment, the plurality of
claw parts 79 disposed in the outer peripheral edge of the thrust plate 78 in the
circumferential direction are provided in addition to the plurality of bolts 12 that
restrict the position of the thrust plate 78 with respect to the plate placement part
42. Accordingly, the displacement of the thrust plate 78 can be further suppressed
while suppressing the damage to the plurality of claw parts 79.
[0128] In addition, in the second embodiment, the bolts 67 illustrated in Fig. 5 may be
used instead of the plurality of bolts 12. Additionally, in the second embodiment,
the bolt holes 71 illustrated in Fig. 6 may be used.
[0129] Although the preferable embodiments for carrying out invention have been described
above in detail, the invention is not limited to the relevant specific embodiments,
and various deformations and changes can be made within the scope of the invention
described in the claims.
Industrial Applicability
[0130] The invention is applicable to the scroll compressor.
Reference Signs List
[0131]
- 10, 70, 75:
- scroll compressor
- 11:
- housing
- 12, 67:
- bolt
- 12A:
- head part
- 12B:
- shaft part
- 12Aa:
- lower surface
- 13:
- main bearing
- 13A, 15A:
- outer ring
- 13B, 15B:
- inner ring
- 13C, 15C:
- rolling element
- 14:
- drive shaft
- 14A:
- base end part
- 14B:
- tip part
- 14C:
- crankpin
- 15:
- sub-bearing
- 17:
- lip seal
- 19:
- driven crank Mechanism
- 21:
- compressor body
- 21A:
- compression chamber
- 23:
- rotation suppressing member
- 27, 78:
- thrust plate
- 32:
- rear housing
- 34:
- front housing
- 35:
- suction port
- 36:
- first housing part
- 37:
- second housing part
- 41:
- main-bearing housing part
- 42:
- plate placement part
- 42a:
- plate placement surface
- 42A, 71:
- bolt hole
- 42B:
- cutout groove
- 46:
- drive bush
- 47:
- turning bearing
- 49:
- fixed scroll
- 49A, 51A:
- end plate
- 49Aa, 51Aa:
- one surface
- 49B, 51B:
- wrap part
- 51:
- orbiting scroll
- 51A:
- end plate
- 51Ab:
- other surface
- 51Ac:
- first cutout part
- 51B:
- wrap part
- 51C:
- boss part
- 55:
- ring-like member
- 55a, 76a:
- surface
- 56:
- first engaging projection
- 57:
- second engaging projection
- 61:
- plate body
- 62:
- insertion cutout part
- 64:
- through-hole
- 68:
- protruding part
- 71:
- head part housing part
- 71B:
- shaft part hole
- 76:
- second cutout part
- 76A:
- corner
- 79:
- claw part
- B:
- region
- E:
- circumferential direction
- CL1:
- first clearance
- CL2:
- second clearance
- O1:
- axis
- W:
- width
1. A scroll compressor (10, 70, 75) comprising:
a housing (11) that has a cylindrical rear housing (32), and a front housing (34)
including a plate placement surface (42a);
a fixed scroll (49) that is provided within the rear housing (32) and fixed to the
rear housing (32);
an orbiting scroll (51) that is provided within the rear housing (32), which forms
a compression chamber (21A) between the orbiting scroll (51) and the fixed scroll
(49) by meshing the fixed scroll (49), and is revolved and driven around the fixed
scroll (49);
a ring-like thrust plate (27, 78) that is disposed between an end plate (51A), in
the orbiting scroll (51), disposed on a side opposite to a side where the fixed scroll
(49) is provided and the plate placement surface (42a) of the front housing (34);
and
a plurality of bolts (12, 67) that are fastened to a plate placement part (42), of
the front housing (34), which partitions the plate placement surface (42a) and that
restricts a position of the thrust plate (27, 78) with respect to the plate placement
part (42),
characterized in that the plurality of bolts (12, 67) each include a head part (12A), and a shaft part
(12B) having one end connected to the head part (12A), and at least a portion of the
head part (12A) is disposed to protrude from the plate placement surface (42a), and
the thrust plate (27, 78) has a plurality of through-holes (64) that allow the head
part (12A) to pass therethrough.
2. The scroll compressor (10, 70, 75) according to Claim 1,
wherein the head part (12A) of each of the plurality of bolts (12, 67) is disposed
outside the orbiting scroll (51), and
wherein an outer peripheral part of the end plate (51A) is provided with a first cutout
part (51Ac) capable of housing the head part (12A) when the orbiting scroll (51) is
revolved.
3. The scroll compressor (10, 70, 75) according to any of Claim 1 or 2,
wherein a material of each of the plurality of bolts (12, 67) is a material harder
than a material of the orbiting scroll (51).
4. The scroll compressor (10, 70, 75) according to any of Claims 1 to 3,
wherein the rear housing (32) includes a suction port (35) that suctions a fluid within
the rear housing (32), and
wherein the plurality of bolts (12, 67) are provided at positions separated from the
suction port (35) in a circumferential direction of the plate placement part (42).
5. The scroll compressor (10, 70, 75) according to any of Claims 1 to 4,
wherein the plate placement part (42) of the front housing (34) is provided with bolt
holes (42A, 71) to which the plurality of bolts (12, 67) are fastened, and
wherein each of the plurality of bolts (12, 67) includes a protruding part (68) that
is provided at the other end of a shaft part (12B) of each of the plurality of bolts
(12, 67), and that is configured to have an outer diameter smaller than an outer diameter
of the shaft part (12B), and protrudes in an extending direction of the shaft part
(12B).
6. The scroll compressor (10, 70, 75) according to any of Claims 1 to 5, further comprising:
a rotation suppressing member (23) that is provided between the orbiting scroll (51)
and the thrust plate (27, 78), which is configured to suppress rotation of the orbiting
scroll (51), and which includes a plurality of engaging projections (56, 57),
wherein the thrust plate (27, 78) includes a plurality of insertion cutout parts (62)
into which the engaging projections (56, 57) are inserted, and
wherein the plurality of through-holes (64) are provided at positions separated from
the plurality of insertion cutout parts (62).
7. The scroll compressor (10, 70, 75) according to any of Claims 1 to 6,
wherein the front housing (34) includes a plurality of second cutout parts (76) that
are provided in the outer peripheral part of the plate placement part (42) in a circumferential
direction, and are formed by cutting out the plate placement part (42) corresponding
to the plate placement surface (42a), and
wherein the thrust plate has claw parts (79) that are provided in the outer peripheral
part of the thrust plate (27, 78) in the circumferential direction and are respectively
disposed within the plurality of second cutout parts (76) in a bent state.
8. The scroll compressor (10, 70, 75) according to Claim 7,
wherein the plurality of claw parts (79) are provided at positions different from
formation positions of a plurality of through-holes (64) provided in the thrust plate
(27, 78) in a radial direction of the thrust plate (27, 78).
9. The scroll compressor (10, 70, 75) according to Claim 7 or 8,
wherein the plurality of claw parts (79) are disposed outside the formation positions
of a plurality of through-holes (64) provided in the thrust plate (27, 78).
10. The scroll compressor (10, 70, 75) according to any of Claims 7 to 9,
wherein a first clearance (CL1) formed between a head part (12A) of each of the bolts (12, 67) and each of through-holes
(64) of the thrust plate (27, 78) is smaller than a second clearance (CL2) formed between a position where the thrust plate (27, 78) is bent and each of the
second cutout parts (76).
1. Scrollverdichter (10, 70, 75), der Folgendes umfasst:
ein Gehäuse (11), das ein zylindrisches hinteres Gehäuse (32) und ein vorderes Gehäuse
(34), das eine Plattenplatzierungsfläche (42a) beinhaltet, umfasst;
eine feste Spirale (49), die im hinteren Gehäuse (32) bereitgestellt und am hinteren
Gehäuse (32) fixiert ist;
eine umlaufende Spirale (51), die im hinteren Gehäuse (32), das durch Eingreifen in
die feste Spirale (49) zwischen der umlaufenden Spirale (51) und der festen Spirale
(49) eine Verdichtungskammer (21A) bildet, bereitgestellt ist und um die feste Spirale
(49) gedreht und angetrieben wird;
eine ringförmige Druckplatte (27, 78), die zwischen einer Endplatte (51A), in der
umlaufenden Spirale (51), die auf einer Seite angeordnet ist, die einer Seite gegenüberliegt,
auf der die feste Spirale (49) bereitgestellt ist, und der Plattenplatzierungsfläche
(42a) des vorderen Gehäuses (34) angeordnet ist; und
eine Vielzahl von Bolzen (12, 67), die an einem Plattenplatzierungsteil (42) des vorderen
Gehäuses (34) befestigt sind, das die Plattenplatzierungsfläche (42a) teilt und das
eine Position der Druckplatte (27, 78) mit Bezug auf das Plattenplatzierungsteil (42)
beschränkt,
dadurch gekennzeichnet, dass die Vielzahl von Bolzen (12, 67) jeweils einen Kopfteil (12A) und einen Schaftteil
(12B), dessen eines Ende mit dem Kopfteil (12A) verbunden ist, beinhalten, und mindestens
ein Abschnitt des Kopfteils (12A) derart angeordnet ist, dass er von der Plattenplatzierungsfläche
(42a) vorsteht, und die Druckplatte (27, 78) eine Vielzahl von Durchgangslöchern (64)
aufweist, die es erlauben, dass der Kopfteil (12A) dadurch geführt wird.
2. Scrollverdichter (10, 70, 75) nach Anspruch 1,
wobei der Kopfteil (12A) von jedem der Vielzahl von Bolzen (12, 67) außerhalb der
umlaufenden Spirale (51) angeordnet ist, und
wobei ein Außenperipherieteil der Endplatte (51A) mit einem ersten Ausschnittsteil
(51Ac) versehen ist, der in der Lage ist, den Kopfteil (12A) aufzunehmen, wenn die
umlaufende Spirale (51) gedreht wird.
3. Scrollverdichter (10, 70, 75) nach einem der Ansprüche 1 oder 2,
wobei ein Material von jedem der Vielzahl von Bolzen (12, 67) ein Material ist, das
härter als ein Material der umlaufenden Spirale (51) ist.
4. Scrollverdichter (10, 70, 75) nach einem der Ansprüche 1 bis 3,
wobei das hintere Gehäuse (32) einen Ansauganschluss (35) beinhaltet, der ein Fluid
im hinteren Gehäuse (32) angesaugt, und
wobei die Vielzahl von Bolzen (12, 67) in Positionen bereitgestellt sind, die vom
Ansauganschluss (35) in einer Umfangsrichtung des Plattenplatzierungsteils (42) getrennt
sind.
5. Scrollverdichter (10, 70, 75) nach einem der Ansprüche 1 bis 4,
wobei das Plattenplatzierungsteil (42) des vorderen Gehäuses (34) mit Bolzenlöchern
(42A, 71) versehen ist, an denen die Vielzahl von Bolzen (12, 67) befestigt sind,
und
wobei jeder der Vielzahl von Bolzen (12, 67) einen vorstehenden Teil (68) beinhaltet,
der am anderen Ende des Schaftteils (12B) jedes der Vielzahl von Bolzen (12, 67) bereitgestellt
ist und der dazu ausgelegt ist, einen Außendurchmesser aufzuweisen, der kleiner ist
als ein Außendurchmesser des Schaftteils (12B), und in eine Erstreckungsrichtung des
Schaftteils (12B) vorsteht.
6. Scrollverdichter (10, 70, 75) nach einem der Ansprüche 1 bis 5, der ferner Folgendes
umfasst:
ein Rotationsunterdrückungselement (23), das zwischen der umlaufenden Spirale (51)
und der Druckplatte (27, 78) bereitgestellt ist und das dazu ausgelegt ist, eine Rotation
der umlaufenden Spirale (51) zu unterdrücken, und das eine Vielzahl von eingreifenden
Vorsprüngen (56, 57) beinhaltet,
wobei die Druckplatte (27, 78) eine Vielzahl von Einsetzausschnittsteilen (62) beinhaltet,
in die die eingreifenden Vorsprünge (56, 57) eingesetzt werden, und
wobei die Vielzahl von Durchgangslöchern (64) in Positionen bereitgestellt sind, die
von der Vielzahl von Einsetzausschnittsteilen (62) getrennt sind.
7. Scrollverdichter (10, 70, 75) nach einem der Ansprüche 1 bis 6,
wobei das vordere Gehäuse (34) eine Vielzahl von zweiten Ausschnittsteilen (76) beinhaltet,
die im Außenperipherieteil des Plattenplatzierungsteils (42) in einer Umfangsrichtung
bereitgestellt und durch Ausschneiden des Plattenplatzierungsteils (42) entsprechend
der Plattenplatzierungsfläche (42a) gebildet sind, und
wobei die Druckplatte Klauenteile (79) aufweist, die im Außenperipherieteil der Druckplatte
(27, 78) in der Umfangsrichtung bereitgestellt und jeweils in der Vielzahl von zweiten
Ausschnittsteilen (76) in einem gebogenen Zustand angeordnet sind.
8. Scrollverdichter (10, 70, 75) nach Anspruch 7,
wobei die Vielzahl von Klauenteilen (79) in Positionen bereitgestellt sind, die sich
von Bildungspositionen einer Vielzahl von Durchgangslöchern (64), die in der Druckplatte
(27, 78) in einer Radialrichtung der Druckplatte (27, 78) bereitgestellt sind, unterscheiden.
9. Scrollverdichter (10, 70, 75) nach Anspruch 7 oder 8,
wobei die Vielzahl von Klauenteilen (79) außerhalb der Bildungspositionen einer Vielzahl
von Durchgangslöchern (64), die in der Druckplatte (27, 78) bereitgestellt sind, angeordnet
sind.
10. Scrollverdichter (10, 70, 75) nach einem der Ansprüche 7 bis 9,
wobei ein erstes Spiel (CL1), das zwischen einem Kopfteil (12A) jedes der Bolzen (12, 67) und jedem der Durchgangslöcher
(64) der Druckplatte (27, 78) gebildet ist, kleiner ist als ein zweites Spiel (CL2), das zwischen einer Position, in der die Druckplatte (27, 78) gebogen ist, und jedem
der zweiten Ausschnittsteile (76) gebildet ist.
1. Compresseur à spirales (10, 70, 75) comprenant :
un boîtier (11) qui a un boîtier arrière cylindrique (32), et un boîtier avant (34)
comprenant une surface de mise en place de plaque (42a) ;
une spirale fixe (49) qui est prévue à l'intérieur du boîtier arrière (32) et fixée
sur le boîtier arrière (32) ;
une spirale orbitale (51) qui est prévue à l'intérieur du boîtier arrière (32), qui
forme une chambre de compression (21A) entre la spirale orbitale (51) et la spirale
fixe (49) en engrenant la spirale fixe (49), et est entraînée en rotation et entraînée
autour de la spirale fixe (49) ;
une plaque de poussée de forme annulaire (27, 78) qui est disposée entre une plaque
d'extrémité (51A), dans la spirale orbitale (51), disposée sur un côté opposé à un
côté où la spirale fixe (49) est prévue et la surface de mise en place de plaque (42a)
du boîtier avant (34) ; et
une pluralité de boulons (12, 67) qui sont fixés sur une partie de mise en place de
plaque (42), du boîtier avant (34), qui sépare la surface de mise en place de plaque
(42a) et qui limite une position de la plaque de poussée (27, 78) par rapport à la
partie de mise en place de plaque (42),
caractérisé en ce que la pluralité de boulons (12, 67) comprennent chacun une partie de tête (12A) et une
partie d'arbre (12B) ayant une extrémité raccordée à la partie de tête (12A), et au
moins une partie de la partie de tête (12A) est disposée pour faire saillie de la
surface de mise en place de plaque (42a), et la plaque de poussée (27, 78) a une pluralité
de trous débouchants (64) qui permettent à la partie de tête (12A) de passer à travers.
2. Compresseur à spirales (10, 70, 75) selon la revendication 1,
dans lequel la partie de tête (12A) de chacun de la pluralité de boulons (12, 67)
est disposée à l'extérieur de la spirale orbitale (51), et
dans lequel une partie périphérique externe de la plaque d'extrémité (51A) est prévue
avec une première partie découpée (51Ac) capable de loger la partie de tête (12A)
lorsque la spirale orbitale (51) est entraînée en rotation.
3. Compresseur à spirales (10, 70, 75) selon l'une quelconque des revendications 1 ou
2,
dans lequel un matériau de chacun de la pluralité de boulons (12, 67) est un matériau
plus dur qu'un matériau de la spirale orbitale (51).
4. Compresseur à spirales (10, 70, 75) selon l'une quelconque des revendications 1 à
3,
dans lequel le boîtier arrière (32) comprend un orifice d'aspiration (35) qui aspire
un fluide dans le boîtier arrière (32), et
dans lequel la pluralité de boulons (12, 67) sont prévus dans des positions séparées
de l'orifice d'aspiration (35) dans une direction circonférentielle de la partie de
mise en place de plaque (42).
5. Compresseur à spirales (10, 70, 75) selon l'une quelconque des revendications 1 à
4,
dans lequel la partie de mise en place de plaque (42) du boîtier avant (34) est prévue
avec des trous de boulon (42A, 71) auxquels la pluralité de boulons (12, 67) sont
fixés, et
dans lequel chacun de la pluralité de boulons (12, 67) comprend une partie en saillie
(68) qui est prévue au niveau de l'autre extrémité d'une partie d'arbre (12B) de chacun
de la pluralité de boulons (12, 67), et qui est configurée pour avoir un diamètre
externe inférieur à un diamètre externe de la partie d'arbre (12B), et fait saillie
dans une direction d'extension de la partie d'arbre (12B).
6. Compresseur à spirales (10, 70, 75) selon l'une quelconque des revendications 1 à
5, comprenant en outre :
un élément de suppression de rotation (23) qui est prévu entre la spirale orbitale
(51) et la plaque de poussée (27, 78), qui est configuré pour supprimer la rotation
de la spirale orbitale (51), et qui comprend une pluralité de saillies de mise en
prise (56, 57),
dans lequel la plaque de poussée (27, 78) comprend une pluralité de parties découpées
d'insertion (62) dans lesquelles les saillies de mise en prise (56, 57) sont insérées,
et
dans lequel la pluralité de trous débouchants (64) sont prévus dans des positions
séparées de la pluralité de parties découpées d'insertion (62).
7. Compresseur à spirales (10, 70, 75) selon l'une quelconque des revendications 1 à
6,
dans lequel le boîtier avant (34) comprend une pluralité de secondes parties découpées
(76) qui sont prévues dans la partie périphérique externe de la partie de mise en
place de plaque (42) dans une direction circonférentielle, et sont formées en découpant
la partie de mise en place de plaque (42) correspondant à la surface de mise en place
de plaque (42a), et
dans lequel la plaque de poussée a des parties de griffe (79) qui sont prévues dans
la partie périphérique externe de la plaque de poussée (27, 78) dans la direction
circonférentielle et sont respectivement disposées dans la pluralité des secondes
parties découpées (76) dans un état plié.
8. Compresseur à spirales (10, 70, 75) selon la revendication 7,
dans lequel la pluralité de parties de griffe (79) sont prévues dans des positions
différentes des positions de formation d'une pluralité de trous débouchants (64) prévus
dans la plaque de poussée (27, 78) dans une direction radiale de la plaque de poussée
(27, 78).
9. Compresseur à spirales (10, 70, 75) selon la revendication 7 ou 8,
dans lequel la pluralité de parties de griffe (79) sont disposées à l'extérieur des
positions de formation d'une pluralité de trous débouchants (64) prévus dans la plaque
de poussée (27, 78).
10. Compresseur à spirales (10, 70, 75) selon l'une quelconque des revendications 7 à
9,
dans lequel un premier jeu (CL1) formé entre une partie de tête (12A) de chacun des boulons (12, 67) et chacun des
trous débouchants (64) de la plaque de poussée (27, 78) est inférieur à un second
jeu (CL2) formé entre une position dans laquelle la plaque de poussée (27, 78) est pliée et
chacune des secondes parties découpées (76).