Technical Field
[0001] The present invention relates to a refrigerant compressor for use in, for example,
a refrigerator or an air conditioner, and also to a refrigeration apparatus using
the refrigerant compressor.
Background Art
[0002] FIG. 12 shows a schematic sectional view of a conventional refrigerant compressor
1. For example, the conventional refrigerant compressor 1 includes a sealed container
11, in which a compression element 6 and an electric element 5 are accommodated. The
compression element 6 includes a crankshaft 7 and a piston 15. The piston 15 is connected
to an eccentric shaft 9 of the crankshaft 7. The electric element 5, which rotates
the crankshaft 7, includes a stator 3 and a rotor 4. A main shaft 8 of the crankshaft
7 is pivotally supported by a main bearing 14. Refrigerating machine oil 2 is fed
to sliding portions in the refrigerant compressor 1.
[0003] During the refrigerant compressor 1 being driven, the crankshaft 7 is rotated together
with the rotor 4 of the electric element 5 by electric power supplied from the outside,
and eccentric motion of the eccentric shaft 9 causes the piston 15 to make reciprocating
motion in a cylinder bore 12 via a connecting rod 17 and a piston pin 16. The piston
15 compresses, in a compression chamber 13, refrigerant gas that is supplied into
the sealed container 11 via a suction tube 20 from the outside. In accordance with
the rotation of the crankshaft 7, the refrigerating machine oil 2 is fed to the sliding
portions from an oil-feeding pump 10 to lubricate the sliding portions and seal between
the piston 15 and the cylinder bore 12.
[0004] In recent years, from the viewpoint of global environment conservation, the development
of a high-efficient refrigerant compressor has been conducted for the purpose of reducing
the use of fossil fuels. For example, a refrigerant compressor as disclosed in Patent
Literature 1 has been developed, in which wear of a sliding portion of, for example,
the crankshaft is prevented by forming an insoluble coating on the surface of the
sliding portion.
[0005] Specifically, in the example shown in FIG. 12, the crankshaft 7 is supported at one
end thereof by the main bearing 14. During the suction of the refrigerant gas into
and the compression of the refrigerant gas in the sealed container 11, a load applied
to the crankshaft 7 in the radial direction varies at least ten times its minimum
value. Such load variation causes run-out of the crankshaft 7, in which the crankshaft
7 rotates in a state where the axis of the crankshaft 7 is tilted relative to the
axis of the main bearing 14. As a result, lubrication at both ends of the main bearing
14 in the axial direction becomes relatively insufficient. In this respect, an insoluble
coating, such as a phosphatic coating, is formed on the surface of the main shaft
8 of the crankshaft 7, and thereby abnormal wear due to direct metal contact between
the main shaft 8 and the main bearing 14 is suppressed.
Citation List
Patent Literature
Summary of Invention
Technical Problem
[0007] However, in recent years, there is a demand for a refrigerant compressor with further
improved efficiency. For example, various design changes have been taken into consideration,
such as expanding the variable speed rotation range at rotating portions of the refrigerant
compressor, adopting low-viscosity refrigerating machine oil, and reducing the area
of the sliding portions. In a case where such design changes have been made, even
if an insoluble coating is formed on the surface of the sliding portions, the coating
becomes scraped particularly at, for example, both ends of the main shaft of the crankshaft
in the axial direction, at which it is difficult to keep the lubricated state. Consequently,
there is a risk that the wear of the sliding portions progresses, which causes reduction
in the durability and reliability of the refrigerant compressor.
[0008] In view of the above, an object of the present invention is to provide a refrigerant
compressor that makes it possible to achieve improvement in efficiency while preventing
reduction in durability and reliability by preventing wear of sliding portions, and
to provide a refrigeration apparatus in which the refrigerant compressor is used.
Solution to Problem
[0009] In order to solve the above-described problems, a refrigerant compressor according
to one aspect of the present invention includes: a sealed container in which refrigerating
machine oil is stored; an electric element accommodated in the sealed container and
driven by electric power supplied from outside; and a compression element accommodated
in the sealed container and covered with the refrigerating machine oil, the compression
element being driven by the electric element to compress refrigerant gas supplied
from outside. The compression element includes: a crankshaft including a main shaft
and an eccentric shaft that are arranged side by side in a longitudinal direction;
a main bearing that pivotally supports the main shaft; and an eccentric bearing that
pivotally supports the eccentric shaft. A shaft part that is at least one of the main
shaft and the eccentric shaft, or a bearing part that is at least one of the main
bearing and the eccentric bearing, is provided with a tapered portion, the tapered
portion being formed on at least one of one end side and another end side of the shaft
part or the bearing part in an axial direction of the bearing part such that a diameter
of the shaft part or the bearing part changes from an outer side toward a central
side in the longitudinal direction of the crankshaft, the tapered portion allowing
the shaft part and the bearing part to come into line contact with each other in a
state where an axis of the shaft part is tilted relative to an axis of the bearing
part. A ratio C / D, which is a ratio of a clearance C between the shaft part and
the bearing part to a diameter D of the shaft part, is set to a value within a range
of not less than 4.0 × 10
-4 and not greater than 3.0 × 10
-3. A taper depth d
B, which corresponds to a distance between one end and another end of the tapered portion
in the axial direction of the bearing part, the distance being in a direction perpendicular
to the axis of the bearing part, is set to a value not less than 2.0 × 10
-3 mm. In a combination of the shaft part and the bearing part corresponding thereto,
a ratio G / D, which is a ratio of a maximum gap G to the diameter D of the shaft
part, is set to a value not greater than 4.0 × 10
-3, the maximum gap G being a sum of the clearance C and a total value of the taper
depth d
B of the tapered portion.
[0010] According to the above configuration, the ratio C / D, the taper depth d
B, and the ratio G / D are set to the values within the aforementioned ranges. With
such settings, the distance between the shaft part and the bearing part can be suitably
set in relation to the diameter D of the shaft part, and also, the tapered portion
having a favorable sloped surface can be formed. Consequently, local metal contact
between the shaft part and the bearing part can be prevented, and the formation of
an oil film between a sliding portion of the shaft part and a sliding portion of the
bearing part can be facilitated. This makes it possible to provide the refrigerant
compressor, which is a low-input and highly efficient refrigerant compressor with
excellent long-term durability.
[0011] A refrigeration apparatus according to another aspect of the present invention includes
a refrigerant circuit including: the above refrigerant compressor; a radiator that
radiates heat of a refrigerant; a decompressor that decompresses the refrigerant;
and a heat absorber that absorbs the heat of the refrigerant. In the refrigerant circuit,
the refrigerant compressor, the radiator, the decompressor, and the heat absorber
are connected by piping in an annular manner.
[0012] Provided by the above configuration is the refrigeration apparatus which can, by
including the above-described refrigerant compressor, reduce electric power consumption,
i.e., realize energy saving, and have improved long-term reliability.
Advantageous Effects of Invention
[0013] The present invention can provide a refrigerant compressor that makes it possible
to achieve improvement in efficiency while preventing reduction in durability and
reliability by preventing wear of sliding portions, and provide a refrigeration apparatus
in which the refrigerant compressor is used.
Brief Description of Drawings
[0014]
FIG. 1 is a schematic sectional view of a reciprocating refrigerant compressor according
to Embodiment 1.
FIG. 2 is an enlarged sectional view of an E region of the refrigerant compressor
of FIG. 1.
FIG. 3 is a sectional view of main components of the refrigerant compressor of FIG.
1.
FIG. 4A is a characteristic diagram showing an input ratio between the refrigerant
compressor of Example, which is shown in FIG. 1, and a refrigerant compressor of Conventional
Example.
FIG. 4B is a characteristic diagram showing a COP ratio between the refrigerant compressor
of Example, which is shown in FIG. 1, and the refrigerant compressor of Conventional
Example.
FIG. 5 is a functional diagram illustrating a compressive load applied to the refrigerant
compressor of FIG. 1.
FIG. 6 illustrates contact states each between a main shaft of FIG. 1 and a main bearing
when the main shaft is tilted inside the main bearing; FIG. 6 shows, for each contact
state, a correlation between the contact state and relational expressions that hold
true in the contact state.
FIG. 7 is a graph showing setting ranges of Examples and Comparative Examples.
FIG. 8 is a schematic sectional view of a rotating (rotary) refrigerant compressor
according to Embodiment 2.
FIG. 9 is an enlarged sectional view of a B region of the refrigerant compressor of
FIG. 8.
FIG. 10 is a sectional view of the refrigerant compressor of FIG. 8, the sectional
view being taken along line A-A' of FIG. 8 as viewed in the direction of the arrows
of line A-A'.
FIG. 11 is a schematic diagram of a refrigeration apparatus according to Embodiment
3.
FIG. 12 is a schematic sectional view of a conventional refrigerant compressor.
Description of Embodiments
[0015] Hereinafter, embodiments are described with reference to the drawings.
(Embodiment 1)
[Refrigerant Compressor]
[0016] FIG. 1 is a schematic sectional view of a reciprocating refrigerant compressor 100
according to Embodiment 1. As shown in FIG. 1, the refrigerant compressor 100 includes
a sealed container 101, an electric element 106, a compression element 107, and an
oil-feeding pump 120. The inside of the sealed container 101 is filled with refrigerant
gas (e.g., R600a). Refrigerating machine oil 103 (e.g., mineral oil) is stored in
the bottom of the sealed container 101).
[0017] The electric element 106 is accommodated in the sealed container 101, and is driven
by electric power supplied from the outside. The electric element 106 includes a stator
104 and a rotor 105. The compression element 107 is accommodated in the sealed container
101, and is covered with the refrigerating machine oil 103. The compression element
107 is driven by the electric element 106 to compress the refrigerant gas supplied
from the outside. The compression element 107 includes a crankshaft 108, a cylinder
block 112, a piston pin 115, a coupling member 117, a piston 132, a valve plate 139,
and a cylinder head 140.
[0018] As one example, the crankshaft 108 is made of cast iron. The crankshaft 108 is disposed
in a manner to extend vertically. The crankshaft 108 includes a main shaft 109 and
an eccentric shaft 110, which are arranged side by side in the longitudinal direction.
The rotor 105 is fixed to the main shaft 109 by press-fitting. As one example, the
eccentric shaft 110 is disposed above the main shaft 109. The eccentric shaft 110
is disposed eccentrically with respect to the main shaft 109.
[0019] As described below, in the refrigerant compressor 100, the main shaft 109 is pivotally
supported by a main bearing 111, and the eccentric shaft 110 is pivotally supported
by an eccentric bearing 119. The lower side of the crankshaft 108 is provided with
the oil-feeding pump 120, and is fed with the refrigerating machine oil 103.
[0020] As one example, the cylinder block 112 is made of cast iron. A substantially cylindrical
cylinder bore 113 is formed inside the cylinder block 112. The cylinder bore 113 extends
horizontally, and one end thereof is sealed by the valve plate 139. The cylinder block
112 includes the main bearing 111, which pivotally supports the main shaft 109.
[0021] The piston 132 is inserted in the cylinder bore 113 in a reciprocable manner. An
interior space of the cylinder bore 113 between the piston 132 and the valve plate
139 serves as a compression chamber 134. A piston pin hole 116 is formed in the piston
132. The piston pin 115 is locked to the piston pin hole 116 in a non-rotatable manner.
The piston pin 115 has a substantially cylindrical shape, and is disposed parallel
to the eccentric shaft 110.
[0022] The eccentric shaft 110 and the piston 132 are coupled together by the coupling member
117. The coupling member 117 is an aluminum casting product, and includes the eccentric
bearing 119. The coupling member 117 couples the eccentric shaft 110 and the piston
132 via the piston pin 115.
[0023] The cylinder head 140 is disposed on the opposite side of the valve plate 139 from
the cylinder bore 113. The cylinder head 140 forms a high-pressure chamber (not shown),
and is fixed to the valve plate 139.
[0024] A suction tube (not shown) is fixed to the sealed container 101. The suction tube
is connected to the low-pressure side (not shown) of the refrigeration cycle of the
refrigerant compressor 100, such that the suction tube leads the refrigerant gas into
the sealed container 101. A suction muffler 142 is held between the valve plate 139
and the cylinder head 140.
[0025] At the time of driving the refrigerant compressor 100, electric power supplied from
the outside, such as electric power from a commercial power source, is supplied to
the electric element 106 via an external inverter drive circuit (not shown). Accordingly,
the electric element 106 is inverter-driven at a plurality of operating frequencies.
[0026] The crankshaft 108 is rotated by the rotor 105 of the electric element 106. As a
result, the eccentric shaft 110 makes eccentric motion. The coupling member 117 causes,
via the piston pin 115, the piston 132 to make reciprocating motion in the cylinder
bore 113. As a result, the refrigerant gas that has been led into the sealed container
101 through the suction tube is sucked from the suction muffler 142 into the compression
chamber 134, and is compressed in the compression chamber 134.
[0027] In accordance with the rotation of the crankshaft 108, the refrigerating machine
oil 103 is fed to sliding portions from the oil-feeding pump 120 to lubricate the
sliding portions. Also, the refrigerating machine oil 103 seals between the piston
132 and the cylinder bore 113. Hereinafter, a shaft part and a bearing part of the
refrigerant compressor 100 are illustratively described in detail.
[Shaft Part and Bearing Part]
[0028] The refrigerant compressor 100 includes a shaft part and a bearing part. The shaft
part is at least one of the main shaft 109 and the eccentric shaft 110. The bearing
part is at least one of the main bearing 111 and the eccentric bearing 119. Either
the shaft part or the bearing part is provided with a tapered portion. The tapered
portion is formed on at least one of one end side and the other end side of the shaft
part or the bearing part in the axial direction of the bearing part such that the
diameter of the shaft part or the bearing part changes from the outer side toward
the central side in the longitudinal direction of the crankshaft 108. The tapered
portion allows the shaft part and the bearing part to come into line contact with
each other in a state where the axis of the shaft part is tilted relative to the axis
of the bearing part.
[0029] In the refrigerant compressor 100, a ratio C / D, which is the ratio of a clearance
C between the shaft part and the bearing part to the diameter D of the shaft part,
is set to a value within the range of not less than 4.0 × 10
-4 and not greater than 3.0 × 10
-3. A taper depth d
B, which corresponds to a distance between one end and the other end of the tapered
portion in the axial direction of the bearing part, the distance being in a direction
perpendicular to the axis of the bearing part, is set to a value not less than 2.0
× 10
-3 mm.
[0030] In the refrigerant compressor 100, the shaft part or the bearing part is provided
with a pair of the tapered portions that are formed on both sides of the shaft part
or the bearing part in the axial direction of the bearing part. In a case where the
shaft part is provided with the tapered portions, the external diameter of each tapered
portion changes from its one end toward the other end in the axial direction of the
shaft part. In a case where the bearing part is provided with the tapered portions,
the internal diameter of each tapered portion changes from its one end toward the
other end in the axial direction of the bearing part.
[0031] In the refrigerant compressor 100, the following elements satisfy Math. 1 and Math.
2 indicated below: a taper depth d
BU, which is the taper depth d
B of the tapered portion on the one end side of the shaft part or the bearing part
in the axial direction of the bearing part; a taper width W
BU, which is the width, in the axial direction of the bearing part, of the tapered portion
on the one end side of the shaft part or the bearing part in the axial direction of
the bearing part; a taper depth d
BL, which is the taper depth d
B of the tapered portion on the other end side of the shaft part or the bearing part
in the axial direction of the bearing part; a taper width W
BL, which is the width, in the axial direction of the bearing part, of the tapered portion
on the other end side of the shaft part or the bearing part in the axial direction
of the bearing part; a bearing length B of the bearing part; and the clearance C.

[0032] Here, (C + d
BU + d
BL) corresponds to a maximum gap G, which is the sum of the clearance C, the taper depth
d
BU, and the taper depth d
BL. In other words, in a combination of the shaft part and the bearing part corresponding
thereto, the maximum gap G is the sum of the clearance C and a total value of the
taper depths d
B of the tapered portions. Hereinafter, (C + d
BU + d
BL) is also referred to as the maximum gap G.
[0033] Next, the refrigerant compressor 100 with the above-described configuration is illustratively
described in detail. FIG. 2 is an enlarged sectional view of an E region of the refrigerant
compressor 100 of FIG. 1. FIG. 3 is a sectional view of main components of the refrigerant
compressor 100 of FIG. 1. As shown in FIGS. 1 to 3, the main shaft 109 extends vertically.
[0034] In the refrigerant compressor 100, of the shaft part or the bearing part, an opposite-to-taper
surface that faces the opposite surface of the tapered portion on the one end side
in the axial direction of the bearing part is provided with a first sliding surface
formed thereon. Also, of the shaft part or the bearing part, an opposite-to-taper
surface that faces the opposite surface of the tapered portion on the other end side
in the axial direction of the bearing part is provided with a second sliding surface
formed thereon.
[0035] In the refrigerant compressor 100, at least one of the shaft part and the bearing
part is provided with a pair of the tapered portions that are formed on both sides
of the at least one of the shaft part and the bearing part in the axial direction
of the bearing part, and at least one of the shaft part and the bearing part includes
a small-diameter portion that has a less diameter than the maximum diameter of the
tapered portions.
[0036] As one example, in the refrigerant compressor 100 of the present embodiment, the
main shaft 109 includes a first sliding surface 151, a small-diameter portion 152,
and a second sliding surface 153. The first sliding surface 151 is disposed on the
upper portion of the main shaft 109. The second sliding surface 153 is disposed on
the lower portion of the main shaft 109. The small-diameter portion 152 is disposed
between the first sliding surface 151 and the second sliding surface 153.
[0037] The small-diameter portion 152 has a less diameter than that of the first sliding
surface 151. A diameter D
LO of a portion of the main shaft 109, the portion being provided with the second sliding
surface 153, is equal to a diameter Duo of a portion of the main shaft 109, the portion
being provided with the first sliding surface 151 (see FIG. 5).
[0038] The main bearing 111, which pivotally supports the main shaft 109, is disposed such
that the axis of the main bearing 111 extends vertically. The upper end of the inner
peripheral surface of the main bearing 111 is provided with a tapered portion 170U.
The lower end of the inner peripheral surface of the main bearing 111 is provided
with a tapered portion 170L. That is, in the present embodiment, the bearing part
is provided with a pair of tapered portions. The internal diameter of the main bearing
111, except the tapered portions 170U and 170L, is constant.
[0039] Each tapered portion 170U or 170L has a linear or continuously curved surface when
seen in a direction perpendicular to the axis of the tapered portion 170U or 170L.
FIG. 2 shows a configuration in which the tapered portion 170U has a linear surface
between an inner one end 171 and an outer other end 172 in the axial direction of
the main bearing 111. The tapered portion 170L is configured in the same manner.
[0040] Each tapered portion 170U or 170L is formed over the entire circumferential direction
of the inner peripheral surface of the main bearing 111. The taper depth d
B (d
BU or d
BL), which corresponds to a distance between the one end 171 and the other end 172 of
the tapered portion 170U or 170L in the axial direction of the main bearing 111, the
distance being in a direction perpendicular to the axis of the main bearing 111, is
set to a value in units of µm.
[0041] The method of forming each of the tapered portions 170U and 170L is not particularly
limited. Each of the tapered portions 170U and 170L of the present embodiment is formed
by using a prototype tool. The prototype tool includes a radial needle bearing and
a rotating shaft. The radial needle bearing has an internal diameter of 12 mm, an
external diameter of 16 mm, and a roller diameter of 2 mm. The rotating shaft is provided
with a minute slope. A bearing that is to be formed into the main bearing 111 is prepared.
The prototype tool is, while being rotated, press-fitted into the bearing, and thereby
an end portion of the bearing is deformed. In this manner, each of the tapered portions
170U and 170L is formed.
[0042] Assuming that the tapered portions are absent, the clearance C herein corresponds
to a difference between the internal diameter of the bearing part and the external
diameter of a portion of the shaft part, the portion facing the inner peripheral surface
of the bearing part. There may be a case where the portion of the shaft part, the
portion facing the inner peripheral surface of the bearing part, has an external diameter
that varies at a plurality of positions. In this case, assuming that the tapered portions
are absent, the clearance C corresponds to a difference between the internal diameter
of the bearing part and a maximum external diameter of the portion of the shaft part,
the portion facing the inner peripheral surface of the bearing part.
[0043] Specifically, in a case where the diameters D
LO and Duo of the shaft part are equal to each other as described above, assuming that
the tapered portions are absent, the clearance C corresponds to a difference between
the internal diameter of the bearing part and the external diameter of portions of
the shaft part, the portions being provided with the respective sliding surfaces 151
and 153. In other words, in the present embodiment, the clearance C is a difference
between the internal diameter D
I of a portion of the main bearing 111, the portion including neither the tapered portion
170U nor the tapered portion 170L, and the diameter D
LO or D
UO of a portion of the main shaft 109, the portion being provided with the first or
second sliding surface 151 or 153.
[0044] There may be a case where the diameters D
LO and D
UO of the shaft part are different from each other. In this case, assuming that the
tapered portions are absent, the clearance C may be a difference between the internal
diameter of the main bearing 111 and a greater one of the diameters D
LO and D
UO of the main shaft 109.
[0045] As shown in FIGS. 2 and 3, in the present embodiment, as one example, in a sectional
view of an end portion of the main bearing 111 in a plane including the axis 111c
of the main bearing 111, the taper width W
BU of the tapered portion 170U in a direction parallel to the axis 111c of the main
bearing 111 (in other words, the taper width W
BU, which is the width, in the axial direction of the main bearing 111, of the tapered
portion 170U on the one end side in the axial direction of the main bearing 111) is
set to 10 mm, and the taper depth d
BU is set to 4.0 × 10
-3 mm.
[0046] Also, in the sectional view of the end portion of the main bearing 111 in the plane
including the axis 111c of the main bearing 111, the taper width W
BL of the tapered portion 170L in the direction parallel to the axis 111c of the main
bearing 111 (in other words, the taper width W
BL, which is the width, in the axial direction of the main bearing 111, of the tapered
portion 170L on the other end side in the axial direction of the main bearing 111)
is set to 10 mm, and the taper depth d
BL is set to 4.0 × 10
-3 mm.
[0047] Further, the bearing length B of the main bearing 111 is set to 43.5 mm. The internal
diameter D
I of a portion of the main bearing 111, the portion including neither the tapered portion
170U nor the tapered portion 170L, is set to 16.026 mm. A diameter Do, which is the
diameter of a portion of the main shaft 109, the portion being provided with the first
sliding surface 151, or the diameter of a portion of the main shaft 109, the portion
being provided with the second sliding surface 153, is set to 16.010 mm. The clearance
C between the main shaft 109 and the main bearing 111 is set to 1.6 × 10
-2 mm.
[0048] As a result, d
BU / w
BU and d
BL / w
BL are each set to 4.0 × 10
-4. Also, (C + d
BU + d
BL) / B is set to 5.5 × 10
-4. That is, d
BU / w
BU and d
BL / w
BL are each less than (C + d
BU + d
BL) / B. Also, a ratio C / D
O, which is the ratio of the clearance C to the diameter D
O of the main shaft 109, is set to 1.0 × 10
-3.
[0049] In the refrigerant compressor 100, in a combination of the shaft part and the bearing
part corresponding thereto, a ratio G / D, which is the ratio of the maximum gap G
to the diameter D of the shaft part (in the above example, the diameter Do of the
main shaft 109), is set to a value not greater than 4.0 × 10
-3. The maximum gap G is the sum of the clearance C and a total value of the taper depths
d
B of the tapered portions (in this example, a total value d
BU + d
BL of the taper depths of the two respective tapered portions 170U and 170L in the combination
of the main shaft 109 and the main bearing 111) (i.e., the maximum gap G = C + d
BU + d
BL).
[0050] As described above, the ratio C / D, the taper depths d
B (d
BU, d
BL), and the ratio G / D are set to the values within the aforementioned ranges. With
such settings, the distance between the shaft part and the bearing part can be suitably
set in relation to the diameter D of the shaft part, and also, the tapered portions
170U and 170L each having a favorable sloped surface can be formed. Consequently,
local metal contact between the shaft part and the bearing part can be prevented,
and the formation of an oil film between a sliding portion of the shaft part and a
sliding portion of the bearing part can be facilitated. This makes it possible to
provide the refrigerant compressor 100, which is a low-input and highly efficient
refrigerant compressor with excellent long-term durability.
[0051] In the refrigerant compressor 100, the bearing length B of the bearing part and the
clearance C satisfy the relational expressions Math. 1 and Math. 2. Accordingly, the
degree of the slope of each of the tapered portions 170U and 170L is adjusted to be
suitably small. Therefore, during the refrigerant compressor 200 being driven, when
run-out of the shaft part occurs, the surface of the tapered portion 170U or 170 and
the opposite surface of the shaft part are allowed to extend along with each other
in a more aligned manner (see FIG. 6). Consequently, the formation of an oil film
between the surface of the tapered portion 170U or 170 and the opposite surface of
the shaft part can be further facilitated.
[0052] Further, in the refrigerant compressor 100, as one example, the first sliding surface
151 faces the surface of the tapered portion 170U; a sliding width L
1 of the first sliding surface 151 is less than the taper width W
BU of the tapered portion 170U; the second sliding surface 153 faces the surface of
the tapered portion 170L; and a sliding width L
2 of the second sliding surface 153 is less than the taper width W
BL of the tapered portion 170L. Consequently, the viscous resistance between the shaft
part and the bearing part is reduced effectively.
[0053] Still further, in the refrigerant compressor 100, the ratio G / D is set to a value
not greater than 4.0 × 10
-3. With such a setting, the ratio of the maximum gap G to the diameter D of the shaft
part can be suitably adjusted, which makes it possible to prevent a situation where
tilting of the crankshaft 108 in the bearing part becomes excessively steep, causing
increase in edge contact (the edge contact will be described below). This consequently
makes it possible to prevent, for example, a situation where the edge contact causes
wear at the distal end of the piston 132, and the amount of leakage of the refrigerant
from the worn portion increases, causing deterioration in refrigeration capacity.
[0054] Still further, the shaft part of the refrigerant compressor 100 includes a coating
formed on its surface portion that slides on the bearing part. The hardness of the
coating is higher than or equal to the hardness of the surface of the bearing part
facing the coating. In the present embodiment, at least one of (in this example, both)
the main shaft 109 and the eccentric shaft 110 includes the coating.
[0055] The coating is not limited to a specific type of coating. The coating may be, for
example, an oxide coating. Examples of the oxide coating include an iron oxide coating.
For example, compared to a phosphatic coating, an iron oxide coating is chemically
very stable, and has higher hardness. As a result of the oxide coating being formed,
problems such as the generation of wear debris and the adhesion of wear debris to
the coating can be prevented effectively. This makes it possible to effectively avoid
increase in the amount of wear of the oxide coating, and thereby high wear resistance
can be imparted to the coating.
[0056] The coating is required to be harder than the material that the coating is facing,
as with the oxide coating. Assume that the base material of a portion of the shaft
part, the portion being provided with the coating formed thereon, is a ferrous material.
In this case, the coating may be formed not only by general quenching, but also by
impregnating the surface layer of the shaft part with, for example, carbon or nitrogen.
Alternatively, the coating may be formed by a steam oxidization process, or by an
oxidization process in which a material is immersed in an aqueous solution such as
sodium hydroxide.
[0057] The coating is not limited to a compound layer that is formed by, for example, the
oxidization process mentioned above, carburizing, nitriding, or a different oxidization
process, but may be, for example, a strength reinforced layer whose base material
strength is increased by suppressing dislocation slip by any of, for example, the
following: cold working; work hardening; solid solution strengthening; precipitation
strengthening; dispersion strengthening; and grain refining. The coating may be a
treatment layer formed by a coating technique that is any of, for example, the following:
plating; thermal spraying; PVD; and CVD.
[Validation Test]
[0058] The refrigerant compressor 100 of Embodiment 1 was produced as Example. Another refrigerant
compressor was produced as Conventional Example. The refrigerant compressor of Conventional
Example is the same as the refrigerant compressor 100, except that the refrigerant
compressor of Conventional Example is not provided with the tapered portions 170U
and 170L. The performance of each of these refrigerant compressors was evaluated when
each compressor was inverter-driven to perform low-speed operation (at an operating
frequency of 17Hz).
[0059] FIG. 4A is a characteristic diagram showing an input ratio between the refrigerant
compressor of Example, which is shown in FIG. 1, and the refrigerant compressor of
Conventional Example. FIG. 4B is a characteristic diagram showing a coefficient of
performance (COP) ratio between the refrigerant compressor of Example, which is shown
in FIG. 1, and the refrigerant compressor of Conventional Example.
[0060] The coefficient of performance is a coefficient used as an index indicating the energy
consumption efficiency of refrigerator-freezer equipment or the like. The coefficient
of performance is a value that is obtained by dividing a refrigeration capacity (W)
by an applied input (W). FIG. 4A shows the ratio (input ratio) when the applied input
value in Conventional Example is assumed as 100. FIG. 4B shows the ratio (COP ratio)
when the COP value in Conventional Example is assumed as 100.
[0061] From the results shown in FIGS. 4A and 4B, it has been validated that Example exhibits
a lower input and a higher COP than the comparative Conventional Example for the reason
that the refrigerant compressor of Example is additionally provided with the tapered
portions 170U and 170L.
[0062] FIG. 5 is a functional diagram illustrating a compressive load applied to the refrigerant
compressor 100 of FIG. 1. FIG. 5 schematically shows the compressive load applied
to the refrigerant compressor 100. An analysis of the validation test results on Example
and Conventional Example is given below with reference to FIG. 5.
[0063] In the case of a reciprocating refrigerant compressor such as the refrigerant compressor
100, generally speaking, in the compression chamber 134 formed between the cylinder
bore 113 and the piston 132, the internal pressure of the sealed container 101 is
lower compared to a compressive load P that occurs in the cylinder axial direction
of the cylinder bore 113. While the compressive load P is being applied to the eccentric
shaft 110, the main shaft 109 is supported at one end by the single main bearing 111.
Accordingly, during the refrigerant compressor being driven, run-out of the crankshaft
108, in which the crankshaft 108 rotates in a state where the crankshaft 108 is tilted
inside the main bearing 111, occurs due to the influence of the compressive load P
as described in a literature of
Ito, et al. (Proceedings of The Japan Society of Mechanical Engineers Annual Meeting
Vol. 5-1 (2005) p. 143).
[0064] As a result, component force PI of the compressive load P is applied to a portion
of the main shaft 109, the portion corresponding to the upper end portion of the main
bearing 111, and component force P2 of the compressive load P is applied to a portion
of the main shaft 109, the portion corresponding to the lower end portion of the main
bearing 111. Consequently, so-called edge contact occurs. In a conventional refrigerant
compressor, there is a case where when the main shaft 109 is tilted inside the main
bearing 111, local contact between the main shaft 109 and the main bearing 111 occurs,
which causes increase in surface pressure. When the speed of the operation decreases,
the thickness of the oil film formed between the main shaft 109 and the main bearing
111 becomes thinner, which may even result in breakage of the oil film. Consequently,
solid contact between the main shaft 109 and the main bearing 111 occurs, which causes
increase in sliding loss.
[0065] On the other hand, in the present embodiment (Example), since the main bearing 111
is provided with the tapered portions 170U and 170L, even if the main shaft 109 is
tilted inside the main bearing 111, the surface of the main shaft 109 and the opposite
surface of the main bearing 111 are arranged such that, when seen in a direction perpendicular
to the axis of the main bearing 111, these surfaces extend along with each other.
Accordingly, local metal contact between the main shaft 109 and the main bearing 111
is prevented.
[0066] Further, in the present embodiment (Example), the total value of the clearance C,
the taper depth d
BU, and the taper depth d
BL, i.e., the maximum gap G (= C + d
BU + d
BL), is set to be relatively large. It is considered that, owing to such setting, the
viscous resistance of the refrigerating machine oil 103 is reduced, and sliding loss
is reduced significantly, which effectively lowers the input to the refrigerant compressor.
[0067] From the above results, it is understood that, by providing the bearing part of the
refrigerant compressor with the tapered portions, local metal contact between the
bearing part and the shaft part can be prevented, thereby achieving improvement in
durability, and also, the performance of the refrigerant compressor can be improved.
[Evaluation Test]
[0068] Next, after the above validation test results were obtained, a performance evaluation
test and a reliability evaluation test were performed on the refrigerant compressor,
and thereby numerical value ranges with which to achieve improvement in the performance
of the refrigerant compressor were clarified. In the performance evaluation test,
the clearance C between the main shaft and the main bearing, the bearing length B,
the diameter Do of the main shaft, the ratio C / Do of the clearance C to the diameter
Do, the taper depths d
BU and d
BL of the tapered portions 170U and 170L, and the taper widths W
BU and W
BL were used as parameters. In the performance evaluation test, the refrigerant compressor
was inverter-driven to perform low-speed operation (at an operating frequency of 17
Hz).
[0069] In the reliability evaluation test, the refrigerant compressor was operated for 160
hours in a high-temperature and high-load intermittent operation mode. Thereafter,
the refrigerant compressor was disassembled, and wear of sliding components (such
as the crankshaft and piston) was measured, based on which evaluations were made.
[0070] The description hereinafter refers to a graph (shown in FIG. 7). Plotted in the graph
is a relationship among the taper width W
BU and the taper depth d
BU of the tapered portion 170U, the taper width W
BL and the taper depth d
BL of the tapered portion 170L, the bearing length B of the main bearing 111, and the
clearance C between the main shaft 109 and the main bearing 111. In the graph, a range
that satisfies the aforementioned relational expressions Math. 1 and Math. 2 is referred
to as an area A1, and a range that satisfies relational expressions Math. 3 and Math.
4 shown below is referred to as an area A2.

[0071] In each of these tests, the clearance C between the main shaft 109 and the main bearing
111 was set to 1.6 × 10
-2 mm, and the bearing length B of the main bearing 111 was set to 43.5 mm. FIG. 6 illustrates
contact states each between the main shaft 109 of FIG. 1 and the main bearing 111
when the main shaft 109 is tilted inside the main bearing 111. FIG. 6 shows, for each
contact state, a correlation between the contact state and relational expressions
that hold true in the contact state. FIG. 7 is a graph showing setting ranges of Examples
1 to 2 and Comparative Examples 1 to 2. Table 1 below shows evaluations on Examples
1 to 2 and Comparative Examples 1 to 2 in the performance evaluation test and the
reliability evaluation test.
[Table 1]
| |
Surface Treatment on Crankshaft |
| Coating softer than the opposite side |
Coating harder than the opposite side |
| Performance |
Reliability |
Performance |
Reliability |
| Comp. Ex. 1 |
Area A1 |
C |
C |
C |
B |
| Area A2 |
C |
C |
C |
B |
| Ex. 1 |
Area A1 |
A |
B |
A |
A |
| Ex. 2 |
Area A2 |
B |
B |
B |
A |
| Comp. Ex. 2 |
Area A1 |
C |
C |
C |
C |
| Area A2 |
C |
C |
C |
C |
[0072] In the graph of FIG. 7, the lower horizontal axis represents each of the taper depths
d
BU and d
BL, and the upper horizontal axis represents the ratio of the maximum gap G to the diameter
D of the shaft part, i.e., (C + d
BU + d
BL) / D. In FIG. 7, the vertical axis represents each of the taper widths W
BU and W
BL. FIG. 7 shows a solid line representing positions that satisfy relational expressions
Math. 5 and Math. 6 shown below.

[0073] In the tests of FIG. 7, Example 1 was the refrigerant compressor 100 with such settings
that the relational expressions Math. 1 and Math. 2 are satisfied in an area in which
each of the taper depths d
BU and d
BL is not less than 2.0 × 10
-3 mm and the ratio of the maximum gap G to the diameter D of the shaft part, i.e.,
(C + d
BU + d
BL) / D, is not greater than 4.0 × 10
-3. On the other hand, Example 2 was a refrigerant compressor with such settings that
the relational expressions Math. 3 and Math. 4 are satisfied in an area in which each
of the taper depths d
BU and d
BL is not less than 2.0 × 10
-3 mm and the ratio of the maximum gap G to the diameter D of the shaft part, i.e.,
(C + d
BU + d
BL) / D, is not greater than 4.0 × 10
-3.
[0074] Comparative Example 1 was a refrigerant compressor with each of the taper depths
d
BU and d
BL set to a value less than 2.0 × 10
-3 mm. Comparative Example 2 was a refrigerant compressor with the ratio of the maximum
gap G to the diameter D of the shaft part, i.e., (C + d
BU + d
BL) / D, set to a value greater than 4.0 × 10
-3.
[0075] In each of Examples 1 to 2 and Comparative Examples 1 to 2, a coating was formed
on a surface portion of the shaft part, the surface portion sliding on the bearing
part. Formed as the coating was a manganese phosphate coating whose hardness is lower
than the hardness of the material of the opposite main bearing, or an iron oxide coating
whose hardness is higher than the hardness of the material of the opposite main bearing.
[0076] The evaluations shown in Table 1 were made with reference to the performance of the
refrigerant compressor of Conventional Example provided with no tapered portions and
to the wear result of the refrigerant compressor of Conventional Example in the reliability
test. In Table 1, "A" indicates significant improvement in characteristics compared
to Conventional Example. Specifically, "A" indicates an evaluation that the compressor
performance has improved and that the wear between the shaft part and the bearing
part has been reduced to the greatest degree. Indicated by "B" is an evaluation next
to "A", and "B" indicates an evaluation that slight improvement in characteristics
has been made compared to the refrigerant compressor of Conventional Example. Indicated
by "C" is an evaluation next to "B", and "C" indicates an evaluation that no improvement
in characteristics has been made compared to the refrigerant compressor of Conventional
Example.
[0077] It is understood from FIG. 7 and Table 1 that both Examples 1 and 2 exhibit improvement
in performance and reliability compared to Comparative Examples 1 and 2. Example 1
exhibits higher performance and reliability than Example 2. It has been confirmed
that particularly when the coating of the shaft part is formed as a coating whose
hardness is higher than the hardness of the material of the opposite main bearing,
excellent compressor performance is obtained and the wear between the shaft part and
the bearing part is reduced significantly, realizing further improvement in reliability.
[0078] On the other hand, Comparative Example 1 with the taper depths d
BU and d
BL set to a value less than 2.0 × 10
-3 mm exhibits no improvement in performance compared to Conventional Example, regardless
of the areas A1 and A2. The reason for this is considered that, in Comparative Example
1, for example, the taper depths of the tapered portions are too shallow, and therefore,
advantages owing to shape differences from the tapered portions of Examples 1 and
2 cannot be obtained.
[0079] Also, Comparative Example 2 with the ratio (C + d
BU + d
BL) / D set to a value greater than 4.0 × 10
-3 exhibits no improvement in performance compared to Conventional Example, regardless
of the areas A1 and A2. The reason for this is considered that, in Comparative Example
2, for example, the tilting of the crankshaft 108 inside the bearing part was excessively
steep, and edge contact occurred. Specifically, in Comparative Example 2, it is considered
that the occurrence of edge contact caused wear at the distal end of the piston 132,
and the amount of leakage of the refrigerant from the worn portion increased, causing
deterioration in refrigeration capacity. It is considered that, for these reasons,
no improvement in performance was observed in Comparative Example 2.
[0080] Also in the separately performed compressor reliability test, significant wear on
the distal end portion of the piston was found in Comparative Example 2, which appeared
to have been caused by edge contact. This backs up the above analysis.
[0081] In the above tests, the clearance C between the main shaft 109 and the main bearing
111 was set to 1.6 × 10
-2 mm, and the bearing length B of the main bearing 111 was set to 43.5 mm, and the
test results obtained under these conditions are indicated herein. It should be noted
that it has been confirmed that the same advantageous effects are obtained also in
a case where the ratio C / D is set to a value within the range of not less than 4.0
× 10
-4 and not greater than 3.0 × 10
-3.
[0082] The diameter D
O of the main shaft 109 can be suitably set. For example, the diameter D
O can be set to a value within the range of not less than 10 mm and not greater than
28 mm. For example, desirably, in accordance with the shaft part diameter D thus set,
the clearance C, the taper depths d
BU and d
BL, and the taper widths W
BU and W
BL are set such that the ratio C / D and the ratio (C + d
BU + d
BL) / D fall within suitable value ranges, respectively.
[0083] In the refrigerant compressor 100 of the present embodiment, the inner peripheral
surface of the main bearing 111 is provided with the tapered portions 170U and 170L.
However, as an alternative, the outer peripheral surface of the main shaft 109 may
be provided with the tapered portions. Also in this case, the same advantageous effects
are obtained. As another alternative, the inner peripheral surface of the eccentric
bearing 119 may be provided with the tapered portions. Yet another alternative, the
outer peripheral surface of the eccentric shaft 110 may be provided with the tapered
portions. In these cases, in a combination of the eccentric shaft 110 and the eccentric
bearing 119, the ratio C / D, the taper depths, and the ratio G / D are set in the
same manner as in the above-described combination of the main shaft 109 and the main
bearing 111. These configurations can also contribute to improvement in the performance
and reliability of the refrigerant compressor as with the present embodiment.
[0084] The present embodiment has described an advantageous effect that the performance
of the refrigerant compressor 100 is improved in a case where the refrigerant compressor
100 is driven to perform low-speed operation (e.g., at an operating frequency of 17
Hz). However, the same advantageous effect is obtained not only when the refrigerant
compressor 100 performs low-speed operation, but also when the refrigerant compressor
100 operates at a commercial rotation speed or when the refrigerant compressor 100
performs high-speed operation at an even higher rotation speed.
[0085] The refrigerant compressor is not limited to a reciprocating compressor, but may
be a different type of compressor, such as a rotary compressor or a scroll compressor.
That is, in the case of a different type of refrigerant compressor, such as a rotary
refrigerant compressor or a scroll refrigerant compressor, the same performance-improving
and reliability-improving effects are obtained when the tapered portion is applied
to a sliding portion (a journal bearing sliding portion) that is constituted by the
outer peripheral surface of a shaft and the inner peripheral surface of a bearing.
Hereinafter, other embodiments are described focusing on differences from Embodiment
1.
(Embodiment 2)
[0086] FIG. 8 is a schematic sectional view of a rotating (rotary) refrigerant compressor
200 according to Embodiment 2. FIG. 9 is an enlarged sectional view of a B region
of the refrigerant compressor 200 of FIG. 8. FIG. 9 is an enlarged sectional view
of the B region (positioned at the lower side of a main bearing 209) surrounded by
a dashed circle in FIG. 8. FIG. 10 is a sectional view of the refrigerant compressor
200 of FIG. 8, the sectional view being taken along line A-A' of FIG. 8 as viewed
in the direction of the arrows of line A-A'.
[0087] As shown in FIGS. 8 to 10, the refrigerant compressor 200 includes a sealed container
201, an electric element 202, and a compression element 203. Refrigerating machine
oil 220 is stored in the bottom of the sealed container 101. The electric element
202 and the compression element 203 are accommodated in the sealed container 201.
The electric element 202 includes a stator 202a and a rotor 202b. The compression
element 203 includes a crankshaft 208, the main bearing 209, an auxiliary bearing
211, a cylinder 210, and a roller 213.
[0088] The crankshaft 208 extends vertically, and includes a main shaft 206 and an eccentric
shaft 212. The eccentric shaft 212 is disposed on a non-end portion of the main shaft
206. The main shaft 206 is, above the eccentric shaft 212, pivotally supported by
the main bearing 209, and below the eccentric shaft 212, pivotally supported by the
auxiliary bearing 211. The rotor 202b of the electric element 202 is fixed to the
main shaft 206. The outer periphery of the rotor 202b is surrounded by the stator
202a.
[0089] The eccentric shaft 212 is disposed inside the cylinder 210, which extends vertically.
The roller 213 is formed in a cylindrical shape, and is disposed such that the axis
thereof extends vertically. Inside the cylinder 210, the main shaft 206 and the eccentric
shaft 212 are inserted in the roller 213. The eccentric shaft 212 is supported by
the inner peripheral surface of the cylinder 210 via the roller 213. In the present
embodiment, the roller 213 corresponds to the eccentric bearing of the eccentric shaft
212. During the refrigerant compressor 200 being driven, the roller 213 makes planetary
motion about the axis of the main shaft 206 of the crankshaft 208.
[0090] The cylinder 210 is provided with a through groove 222 extending horizontally. A
shaft-shaped vane 214 is inserted in the through groove 222. One end (distal end)
of the vane 214 in the longitudinal direction is pressed against a peripheral surface
231 of the roller 213 by a spring 215 and back pressure (delivery pressure). Accordingly,
the space between the cylinder 210 and the roller 213 is divided into a suction chamber
216 and a compression chamber 217. The suction chamber 216 sucks refrigerant gas from
the outside. The compression chamber 217 compresses the refrigerant gas.
[0091] The cylinder 210 is further provided with a suction hole 205. One end of a suction
tube 204 is inserted in the suction hole 205. The refrigerant compressor 200 is connected
to an accumulator (not shown) via the suction tube 204. The inner peripheral surface
of the cylinder 210 is provided with a delivery notch 219.
[0092] During the refrigerant compressor 200 being driven, the electric element 202 causes
the crankshaft 208 to rotate about the axis of the main shaft 206, and the roller
213 makes planetary motion (left rotation in FIG. 10). Consequently, the refrigerant
gas is sucked into the suction chamber 216 from the outside through the suction tube
204 and the suction hole 205. As a result of the internal pressure of the compression
chamber 217 increasing, the refrigerant gas is compressed, and the compressed refrigerant
gas is, after passing through the delivery notch 219, delivered into the sealed container
201 through an unshown delivery hole.
[0093] The vane 214, which partitions off the suction chamber 216 and the compression chamber
217 from each other, has its one end in the longitudinal direction pressed against
the peripheral surface 231 of the roller 213 by the spring 215 and back pressure.
As a result, the vane 214 moves while sliding at a contact point with the peripheral
surface 231 of the roller 213. Due to such motion of the vane 214, the crankshaft
208 receives pressure from a direction perpendicular to the axis of the main shaft
206, and thereby deflects. Consequently, the crankshaft 208 rotates in such a manner
that run-out occurs in each clearance between the main bearing 209 and the auxiliary
bearing 211.
[0094] Due to the run-out, the crankshaft 208 may make edge contact with at least one of
the following: the upper end of the main bearing 209 (in FIG. 8, an end portion on
the electric element 202 side); the lower end of the main bearing 209 (in FIG. 8,
an end portion on the roller 213 side); the upper end of the auxiliary bearing 211
(in FIG. 8, an end portion on the roller 213 side); and the lower end of the auxiliary
bearing 211 (in FIG. 8, an end portion on an oil feeder 221 side, the oil feeder 221
being provided at the lower end of the crankshaft 208). Due to the edge contact, there
are risks that the sliding surface may get damaged and adhesive wear may occur. Adhesive
wear is a phenomenon in which the sliding surface gets cut and worn by minute wear
debris.
[0095] In view of the above, in the refrigerant compressor 200, a tapered portion 270U is
provided at the upper end of the main bearing 209, which pivotally supports the crankshaft
208, and a tapered portion 270L is provided at the lower end of the main bearing 209.
Also, a tapered portion 280U is provided at the upper end of the auxiliary bearing
211, and a tapered portion 280L is provided at the lower end of the auxiliary bearing
211. The tapered portions 270U and 280U correspond to the tapered portion 170U, and
the tapered portions 270L and 280L correspond to the tapered portion 170L. It should
be noted that FIG. 9 shows only the tapered portion 270L among these tapered portions.
[0096] Each of the tapered portions 270U and 270L is formed over the entire circumferential
direction of the inner peripheral surface of the main bearing 209. The taper depth
d
B (d
BU or d
BL), which corresponds to a distance between one end 271 and the other end 272 of the
tapered portion 270U or 270L in the axial direction of the main bearing 209, the distance
being in a direction perpendicular to the axis of the main bearing 209, is set to
a value in units of µm.
[0097] As shown in FIGS. 8 and 9, the ratio C / D of the clearance C between the crankshaft
208 (the main shaft 206) and the bearing part (the main bearing 209) to the diameter
D of the crankshaft 208 (the main shaft 206) is set to a value within the range of
not less than 4.0 × 10
-4 and not greater than 3.0 × 10
-3. The ratio G / D in a combination of the shaft part and the bearing part corresponding
thereto (in this example, a combination of the main shaft 206 and the main bearing
209) is set to a value not greater than 4.0 × 10
-3.
[0098] Although not illustrated, the ratio C / D of the clearance C between the crankshaft
208 (the main shaft 206) and the bearing part (the auxiliary bearing 211) to the diameter
D of the crankshaft 208 (the main shaft 206) is also set to a value within the range
of not less than 4.0 × 10
-4 and not greater than 3.0 × 10
-3.
[0099] Further, at least one of the taper depth d
BU (not shown) of each of the tapered portions 270U and 280U and the taper depth d
BL of each of the tapered portions 270L and 280L is (in this example, both the taper
depth d
BU and the taper depth d
BL are) set to a value within the range of not less than 2.0 × 10
-3 mm. The crankshaft 208 includes a coating formed on its surface portions that slide
on the main bearing 209 and the auxiliary bearing 211. This coating is the same as
the coating described in Embodiment 1.
[0100] By adopting these settings, even if run-out of the crankshaft 208 occurs and the
aforementioned edge contact occurs, the surface of the main shaft 206 and the opposite
surface of the main bearing 209 are arranged such that, when seen in a direction perpendicular
to the axis of the crankshaft 208, these surfaces extend along with each other, and
also, the surface of the main shaft 206 and the opposite surface of the auxiliary
bearing 211 are arranged such that, when seen in the direction perpendicular to the
axis of the crankshaft 208, these surfaces extend along with each other. Accordingly,
local metal contact is prevented between the main shaft 206 and the main bearing 209,
and between the main shaft 206 and the auxiliary bearing 211. Therefore, the refrigerant
compressor 200 has favorable frictional wear characteristics, high performance, and
high reliability.
[0101] The tapered portion 270L shown in FIG. 9 is, when seen in a direction perpendicular
to the axis thereof, formed to have a curved shape that has a continuously curved
surface. However, as an alternative, the tapered portion 270L may be formed to have
a linear surface. In a case where a plurality of tapered portions are provided, the
tapered portions may have different shapes from each other. Although the refrigerant
compressor 200 described above includes the four tapered portions 270U, 270L, 280U,
and 280L, the refrigerant compressor 200 is only required to include at least one
of these tapered portions.
[0102] An object on which the above-described coating is formed is not limited to the crankshaft
208. The coating may be provided on a sliding portion of any of the components (e.g.,
mechanical parts, devices, and units such as a pump and a motor) of a refrigerant
compressor or a refrigeration apparatus in which the refrigerant compressor is used.
Next, the configuration of a refrigeration apparatus in which the refrigerant compressor
100 or 200 is used is illustratively described.
(Embodiment 3)
[0103] FIG. 11 is a schematic diagram of a refrigeration apparatus 300 according to Embodiment
3. Hereinafter, a fundamental configuration of the refrigeration apparatus 300 is
described briefly. As shown in FIG. 11, the refrigeration apparatus 300 includes a
body 301, a dividing wall 307, and a refrigerant circuit 309.
[0104] The body 301 includes a thermally insulated box and a door. The box is provided with
an opening that communicates with the inside of the box. The opening of the box is
opened and closed by the door. The body 301 includes a storage space 303 and a machinery
room 305. The storage space 303 is a space in which a product is stored. In the machinery
room 305, the refrigerant circuit 309 is disposed, which cools the inside of the storage
space 303. The storage space 303 and the machinery room 305 are divided by the dividing
wall 307. An air feeder (not shown) is disposed in the storage space 303. FIG. 11
is a partially cutaway view of the box, showing the inside of the body 301.
[0105] The refrigerant circuit 309 includes: the refrigerant compressor 100 or 200; a radiator
313; a decompressor 315; and a heat absorber 317. The refrigerant compressor 100 or
200, the radiator 313, the decompressor 315, and the heat absorber 317 are connected
by piping in an annular manner.
[0106] The radiator 313 radiates the heat of the refrigerant. The decompressor 315 decompresses
the refrigerant. The heat absorber 317 absorbs the heat of the refrigerant. The heat
absorber 317 is disposed in the storage space 303, and generates cooling heat. As
indicated by arrows in FIG. 11, the air feeder causes the cooling heat generated by
the heat absorber 317 to circulate inside the storage space 303. In this manner, the
air in the storage space 303 is stirred, and the inside of the storage space 303 is
cooled.
[0107] In the refrigeration apparatus 300 configured as above, high wear resistance between
the shaft part and the bearing part is obtained in the refrigerant compressor 100
or 200. Also, since the formation of the oil film between the shaft part and the bearing
part is facilitated, local metal contact between the shaft part and the bearing part
can be prevented, and thereby high reliability and high compressor performance are
obtained. Accordingly, by including the refrigerant compressor 100 or 200, the refrigeration
apparatus 300 can reduce electric power consumption, i.e., realize energy saving,
and can have improved long-term reliability.
[0108] The present invention is not limited to the above-described embodiments. Various
modifications, additions, or deletions can be made to the configurations without departing
from the scope of the present invention. The above-described embodiments may be combined
with each other in any manner. For example, part of a configuration in one embodiment
may be applied to another embodiment. The scope of the present invention is defined
by the appended claims, and all changes that fall within metes and bounds of the claims,
or equivalence of such metes and bounds thereof are therefore intended to be embraced
by the claims.
Industrial Applicability
[0109] As described above, the present invention has an excellent advantageous effect of
being able to provide a refrigerant compressor that makes it possible to achieve improvement
in efficiency while preventing reduction in durability and reliability by preventing
wear of sliding portions, and to provide a refrigeration apparatus in which the refrigerant
compressor is used. Therefore, the present invention is useful when widely applied
to refrigerant compressors and refrigeration apparatuses using the same, because such
applications make it possible to exert the above advantageous effect meaningfully.
Reference Signs List
[0110]
- 100, 200
- refrigerant compressor
- 101, 201
- sealed container
- 103, 220
- refrigerating machine oil
- 106, 202
- electric element
- 107, 203
- compression element
- 108, 208
- crankshaft
- 109, 206
- main shaft (shaft part)
- 110, 212
- eccentric shaft (shaft part)
- 111, 209
- main bearing (bearing part)
- 111c
- axis of the main bearing
- 119
- eccentric bearing (bearing part)
- 151
- first sliding surface
- 152
- small-diameter portion
- 153
- second sliding surface
- 170U, 170L, 270U, 270L, 280U, 280L
- tapered portion
- 211
- auxiliary bearing (bearing part)
- 300
- refrigeration apparatus
- 309
- refrigerant circuit
- 313
- radiator
- 315
- decompressor
- 317
- heat absorber
- B
- bearing width
- C
- clearance
- D
- diameter of the shaft part
- DO
- diameter of the main shaft
- DI
- diameter (internal diameter) of the main bearing
- dB, dBU, dBL
- taper depth
- L1
- sliding width of the first sliding surface
- L2
- sliding width of the second sliding surface
- wBU, wBL
- taper width