JP5824664B2 - Rotary compressor and refrigeration cycle apparatus - Google Patents

Description

  The present invention relates to a rotary compressor and a refrigeration cycle apparatus.

  It is known that the efficiency of a refrigeration cycle apparatus is improved by injecting a gas-phase refrigerant having an intermediate pressure into a compressor (see Patent Document 1). As a compressor that can employ the injection technology, a rolling piston compressor in which a plurality of vanes (blades) are provided so that a first compression chamber and a second compression chamber are formed in a cylinder has been proposed (Patent Literature). 2).

  FIG. 20 is a configuration diagram of the heat pump heating device described in FIG. The heat pump heating apparatus 500 includes a rolling piston compressor 501, a condenser 503, an expansion mechanism 504, a gas-liquid separator 507, and an evaporator 509. The gas-phase refrigerant and vapor-liquid separator 507 from the evaporator 509 The separated intermediate-pressure gas-phase refrigerant is compressed by the compressor 501. A space between the cylinder 522 and the rotor 523 is partitioned into a first compression chamber 526 and a second compression chamber 527 by vanes 525 and 535 attached to the cylinder 522 of the compressor 501. The first compression chamber 526 has a suction hole 526a and a discharge hole 527b. The second compression chamber 527 has a suction hole 527a and a discharge hole 527b. The suction hole 526a is connected to the evaporator 509, and the suction hole 527a is connected to the gas-liquid separator 507. The discharge holes 526 b and the discharge holes 527 b are gathered together and connected to the condenser 503.

JP 2006-112753 A Japanese Examined Patent Publication No. 3-53532

  In the compressor 501 shown in FIG. 20, the ratio of the suction volume of the second compression chamber 527 to the suction volume of the first compression chamber 526 should be appropriately determined according to the application of the compressor 501 and the like. The suction volumes of the compression chambers 526 and 527 are determined by the positions of the two vanes 525 and 535, respectively. For example, when the angle formed by the vane 525 and the vane 535 is increased, the suction volume of the second compression chamber 527 increases. However, according to this method, the suction volume of the first compression chamber 526 is reduced.

  An object of the present invention is to provide a technique for increasing the suction volume of the second compression chamber without reducing the suction volume of the first compression chamber.

That is, the present invention
A cylinder,
A piston disposed in the cylinder so as to form a space between itself and the cylinder;
A shaft to which the piston is attached;
A first vane that is disposed in a first vane groove formed in the cylinder and partitions the space along a circumferential direction of the piston;
A first compression chamber and a second compression chamber having a volume smaller than the volume of the first compression chamber are formed in the cylinder and are disposed in a second vane groove formed in the cylinder. A second vane further dividing the space partitioned by the first vane along a circumferential direction of the piston;
A first suction hole for guiding the working fluid to be compressed in the first compression chamber to the first compression chamber;
A first discharge hole for guiding the working fluid compressed in the first compression chamber from the first compression chamber to the outside of the first compression chamber;
A second suction hole for guiding the working fluid to be compressed in the second compression chamber to the second compression chamber;
A second discharge hole for guiding the working fluid compressed in the second compression chamber from the second compression chamber to the outside of the second compression chamber;
With
The position of the contact point between the movable circle forming the outer peripheral surface of the piston and the fixed circle forming the inner peripheral surface of the cylinder at the moment when the first vane is pushed into the first vane groove to the maximum by the piston. One angular position, a position on the fixed circle 180 degrees opposite to the first angular position passes through the second angular position, the first angular position, and the second angular position, and passes through the rotation axis of the shaft. A virtual plane including a first reference plane, a reciprocating motion direction of the first vane and a rotation plane of the shaft, and a second virtual plane passing through the center of the width direction of the first vane groove. When a reference plane, a position where the second reference plane and the fixed circle intersect with each other is defined as a third angular position,
When the shaft is rotated, the second reference plane is the first reference point so that the contact point between the movable circle and the fixed circle passes in the order of the first angular position, the third angular position, and the second angular position. A rotary compressor is provided that is inclined with respect to a reference plane.

In another aspect, the present invention provides:
The rotary compressor of the present invention;
A radiator for cooling the working fluid compressed by the rotary compressor;
An expansion mechanism for expanding the working fluid cooled by the radiator;
A gas-liquid separator that separates the working fluid expanded by the expansion mechanism into a gaseous working fluid and a liquid working fluid;
An evaporator for evaporating the liquid-phase working fluid separated by the gas-liquid separator;
A suction flow path for guiding the working fluid flowing out of the evaporator to the first suction hole of the rotary compressor;
An injection flow path for guiding the gas-phase working fluid separated by the gas-liquid separator to the second suction hole of the rotary compressor;
A refrigeration cycle apparatus is provided.

  According to the present invention, the suction volume of the second compression chamber can be increased without reducing the suction volume of the first compression chamber. Thereby, the volume of a cylinder can be used effectively and by extension, the operating efficiency of a rotary compressor can be improved.

  In this specification, “suction volume” means the volume of the compression chamber at the moment when the compression stroke starts. In other words, the suction volume means the amount of refrigerant (volume flow rate) to be sucked into the compression chamber during one rotation of the shaft.

The block diagram of the refrigerating-cycle apparatus which concerns on 1st Embodiment of this invention. Longitudinal sectional view of a rotary compressor used in the refrigeration cycle apparatus shown in FIG. FIG. 2 is a cross-sectional view taken along line AA of the rotary compressor shown in FIG. Expanded sectional view of the suction check valve Side view and plan view of the valve body Side view and plan view of valve stop Perspective view of compression mechanism Schematic showing the operation of the rotary compressor for each rotation angle of the shaft Schematic showing the suction volume of the first compression chamber in the reference example Schematic which shows the suction | inhalation volume of the 1st compression chamber in 1st Embodiment. Schematic showing the suction volume of the second compression chamber in the reference example Schematic which shows the suction | inhalation volume of the 2nd compression chamber in 1st Embodiment. A graph showing the relationship between the inclination angle ξ of the second reference plane relative to the first reference plane and the rate of increase of the suction volume of the second compression chamber Schematic showing the maximum volume of the first compression chamber Schematic showing the suction volume of the first compression chamber in consideration of the reverse flow of the refrigerant Longitudinal sectional view of a rotary compressor according to a modification Fig. 12 is a cross-sectional view of the rotary compressor shown in Fig. 12, taken along line BB. The block diagram of the refrigerating-cycle apparatus which concerns on 2nd Embodiment of this invention. The longitudinal cross-sectional view of the rotary compressor used for the refrigeration cycle apparatus shown in FIG. Cross section taken along line DD of the rotary compressor shown in FIG. Cross section along line EE of the rotary compressor shown in FIG. Cross-sectional view showing a modification of the second compression mechanism Schematic showing the relationship between the thickness of the first cylinder and the thickness of the second cylinder Partial configuration diagram showing a modification of the first injection channel and the second injection channel Configuration diagram of conventional heat pump heater

  Hereinafter, embodiments of the present invention will be described with reference to the accompanying drawings. However, the present invention is not limited to the embodiments described below. Each embodiment and each modification can be combined with each other without departing from the scope of the invention.

(First embodiment)
FIG. 1 is a configuration diagram of a refrigeration cycle apparatus according to the present embodiment. The refrigeration cycle apparatus 100 includes a rotary compressor 102, a first heat exchanger 104, a first expansion mechanism 106, a gas-liquid separator 108, a second expansion mechanism 110, and a second heat exchanger 112. These components are annularly connected in the above order by the flow paths 10 a to 10 d so as to form the refrigerant circuit 10. The flow paths 10a to 10d are typically constituted by refrigerant pipes. The refrigerant circuit 10 is filled with a refrigerant such as hydrofluorocarbon or carbon dioxide as a working fluid.

  The refrigeration cycle apparatus 100 further includes an injection flow path 10j. The injection flow path 10j has one end connected to the gas-liquid separator 108 and the other end connected to the rotary compressor 102. The gas-phase refrigerant separated by the gas-liquid separator 108 is exchanged with the rotary compressor 102. Lead directly to. The injection flow path 10j is typically composed of a refrigerant pipe. A pressure reducing valve may be provided in the injection flow path 10j. An accumulator may be provided in the injection flow path 10j.

  The refrigerant circuit 10 is provided with a four-way valve 116 as a switching mechanism capable of switching the flow direction of the refrigerant. When the four-way valve 116 is controlled as indicated by a solid line in FIG. 1, the refrigerant compressed by the rotary compressor 102 is supplied to the first heat exchanger 104. In this case, the first heat exchanger 104 functions as a radiator (condenser) that cools the refrigerant compressed by the rotary compressor 102. The second heat exchanger 112 functions as an evaporator that evaporates the liquid-phase refrigerant separated by the gas-liquid separator 108. On the other hand, when the four-way valve 116 is controlled as shown by a broken line in FIG. 1, the refrigerant compressed by the rotary compressor 102 is supplied to the second heat exchanger 112. In this case, the first heat exchanger 104 functions as an evaporator, and the second heat exchanger 112 functions as a radiator. With the four-way valve 116, for example, the air conditioning apparatus employing the refrigeration cycle apparatus 100 can be provided with both functions of cooling and heating.

  The rotary compressor 102 is a device for compressing the refrigerant to a high temperature and a high pressure. The rotary compressor 102 has a first suction hole 19 (main suction hole) and a second suction hole 20 (injection suction hole). A flow path 10 d is connected to the first suction hole 19 so that the refrigerant flowing out from the first heat exchanger 104 or the second heat exchanger 112 is guided to the rotary compressor 102. The injection flow path 10j is connected to the second suction hole 20 so that the gas-phase refrigerant separated by the gas-liquid separator 108 is guided to the rotary compressor 102.

  The first heat exchanger 104 is typically composed of an air-refrigerant heat exchanger or a water-refrigerant heat exchanger. The second heat exchanger 112 is also typically composed of an air-refrigerant heat exchanger or a water-refrigerant heat exchanger. When the refrigeration cycle apparatus 100 is employed in an air conditioner, both the first heat exchanger 104 and the second heat exchanger 112 are configured with an air-refrigerant heat exchanger. When the refrigeration cycle apparatus 100 is employed in a hot water heater or a hot water heater, the first heat exchanger 104 is configured with a water-refrigerant heat exchanger, and the second heat exchanger 112 is configured with an air-refrigerant heat exchanger. .

  The first expansion mechanism 106 and the second expansion mechanism 110 are a refrigerant cooled by the first heat exchanger 104 (or the second heat exchanger 112) as a radiator or a liquid phase separated by the gas-liquid separator 108. It is a device for expanding the refrigerant. The first expansion mechanism 106 and the second expansion mechanism 110 are typically configured by expansion valves. A suitable expansion valve includes a valve whose opening degree can be changed, for example, an electric expansion valve. The first expansion mechanism 106 is provided on the flow path 10 b between the first heat exchanger 104 and the gas-liquid separator 108. The second expansion mechanism 110 is provided on the flow path 10 c between the gas-liquid separator 108 and the second heat exchanger 112. The expansion mechanisms 106 and 110 may each be composed of a positive displacement expander that can recover power from the refrigerant.

  The gas-liquid separator 108 separates the refrigerant expanded by the first expansion mechanism 106 or the second expansion mechanism 110 into a gas phase refrigerant and a liquid phase refrigerant. The gas-liquid separator 108 is provided with an inlet for the refrigerant expanded by the first expansion mechanism 106 or the second expansion mechanism 110, an outlet for the liquid phase refrigerant, and an outlet for the gas phase refrigerant. One end of the injection flow path 10j is connected to the outlet of the gas phase refrigerant.

  The refrigerant circuit 10 may be provided with other devices such as an accumulator and an internal heat exchanger.

  FIG. 2 is a longitudinal sectional view of a rotary compressor used in the refrigeration cycle apparatus shown in FIG. FIG. 3 is a cross-sectional view taken along line AA of the rotary compressor shown in FIG. The rotary compressor 102 includes a sealed container 1, a motor 2, a compression mechanism 3, and a shaft 4. The compression mechanism 3 is disposed in the lower part in the sealed container 1. The motor 2 is disposed on the compression mechanism 3 in the sealed container 1. The compression mechanism 3 and the motor 2 are connected by the shaft 4. A terminal 21 for supplying electric power to the motor 2 is provided on the top of the sealed container 1. An oil sump 22 for holding lubricating oil is formed at the bottom of the sealed container 1.

  The motor 2 includes a stator 17 and a rotor 18. The stator 17 is fixed to the inner wall of the sealed container 1. The rotor 18 is fixed to the shaft 4 and rotates together with the shaft 4.

  A discharge pipe 11 is provided on the top of the sealed container 1. The discharge pipe 11 penetrates the upper part of the sealed container 1 and opens toward the internal space 13 of the sealed container 1. The discharge pipe 11 serves as a discharge flow path that guides the refrigerant compressed by the compression mechanism 3 to the outside of the sealed container 1. That is, the discharge pipe 11 constitutes a part of the flow path 10a shown in FIG. During the operation of the rotary compressor 102, the internal space 13 of the sealed container 1 is filled with the compressed refrigerant. That is, the rotary compressor 102 is a high-pressure shell type compressor. According to the high-pressure shell-type rotary compressor 102, the motor 2 can be cooled with the refrigerant, so that improvement in motor efficiency can be expected. When the refrigerant is heated by the motor 2, the heating capacity of the refrigeration cycle apparatus 100 is also improved.

  The compression mechanism 3 is moved by the motor 2 so as to compress the refrigerant. 2 and 3, the compression mechanism 3 includes a cylinder 5, a main bearing 6, a sub bearing 7, a piston 8, a muffler 9, a first vane 32, a second vane 33, a first discharge valve 43, a second It has a discharge valve 44 and a suction check valve 50. In the present embodiment, the suction check valve 50 is provided only in the second suction hole 20 out of the first suction hole 19 and the second suction hole 20.

  The shaft 4 has an eccentric portion 4a protruding outward in the radial direction. The piston 8 is disposed inside the cylinder 5. Inside the cylinder 5, a piston 8 is attached to the eccentric part 4 a of the shaft 4. A first vane groove 34 and a second vane groove 35 are formed in the cylinder 5.

  A first vane 32 (blade) having a tip in contact with the outer peripheral surface of the piston 8 is attached to the first vane groove 34 so as to be slidable. The first vane 32 partitions the space between the cylinder 5 and the piston 8 along the circumferential direction of the piston 8. A second vane 33 (blade) having a tip contacting the outer peripheral surface of the piston 8 is attached to the second vane groove 35 so as to be slidable. The second vane 33 further partitions the space between the cylinder 5 and the piston 8 along the circumferential direction of the piston 8. Thus, a first compression chamber 25 (main compression chamber) and a second compression chamber 26 (injection compression chamber) having a volume smaller than the volume of the first compression chamber 25 are formed inside the cylinder 5. .

  In the present embodiment, the first vane groove 34 is inclined so that a virtual plane passing through the center in the width direction of the first vane groove 34 is offset from the rotation axis O of the shaft 4. According to this configuration, the suction volume of the second compression chamber 26 can be increased without reducing the suction volume of the first compression chamber 25. Specifically, when the inclination direction of the first vane groove 34 is defined so as to satisfy the following requirements, the suction volume of the second compression chamber 26 can be increased.

  First, the contact point between the movable circle 8a forming the outer peripheral surface of the piston 8 and the fixed circle 5a forming the inner peripheral surface of the cylinder 5 at the moment when the first vane 32 is pushed into the first vane groove 34 to the maximum by the piston 8. Is defined as a first angular position T1. The first vane groove 34 is formed to open toward the inside of the cylinder 5 at the first angular position T1. Next, a position on the fixed circle 5a on the opposite side 180 degrees as viewed from the first angular position T1 is defined as a second angular position T2. Next, a virtual plane that passes through the first angular position T1 and the second angular position T2 and includes the rotation axis O of the shaft 4 is defined as a first reference plane P1. Next, a virtual plane parallel to the reciprocating motion direction of the first vane 32 and the rotation axis O of the shaft 4 and passing through the center in the width direction of the first vane groove 34 is defined as a second reference plane P2. A position where the second reference plane P2 and the fixed circle 5a intersect is defined as a third angular position T3 except for the first angular position T1. When the shaft 4 rotates in the forward direction (clockwise in FIG. 3), the contact point between the movable circle 8a and the fixed circle 5a passes through the first angular position T1, the third angular position T3, and the second angular position T2. As described above, the second reference plane P2 is inclined with respect to the first reference plane P1.

  In other words, the second reference plane P2 is the shaft so that the rotation angle of the shaft 4 is less than 180 degrees when the contact point between the movable circle 8a and the fixed circle 5a advances from the first angular position T1 to the second angular position T2. 4 is offset from the rotation axis O.

  A virtual plane P3 (third reference plane) that is parallel to the rotation axis O of the shaft 4 and passes through the center in the width direction of the second vane groove 35 passes through the rotation axis O of the shaft 4. When the position of the contact point between the movable circle 8a and the fixed circle 5a at the moment when the second vane 33 is pushed into the second vane groove 35 by the piston 8 to the maximum extent is defined as the fourth angular position T4, the second vane groove 35 is defined. Is formed so as to open toward the inside of the cylinder 5 at the fourth angular position T4.

  According to the rotary compressor 102 of the present embodiment, the tip surfaces of the vanes 32 and 33 slide on the surface of the piston 8. That is, the rotary compressor 102 is configured as a so-called rolling piston compressor. However, the piston 8 and one selected from the first vane 32 and the second vane 33 may be formed of a single component, a so-called swing piston. Further, at least one selected from the first vane 32 and the second vane 33 may be coupled to the piston 8.

  A first spring 36 is disposed behind the first vane 32. A second spring 37 is disposed behind the second vane 33. The first spring 36 and the second spring 37 press the first vane 32 and the second vane 33 toward the piston 8, respectively. The rear part of the first vane groove 34 and the rear part of the second vane groove 35 are each in communication with the internal space 13 of the sealed container 1. Accordingly, the pressure in the internal space 13 of the sealed container 1 is applied to the back surface of the first vane 32 and the back surface of the second vane 33. Further, the lubricating oil stored in the oil reservoir 22 is supplied to the first vane groove 34 and the second vane groove 35.

  In the present specification, the first angular position T1 is defined as a position of “0 degree” along the rotation direction of the shaft 4. In other words, the rotation angle of the shaft 4 at the moment when the first vane 32 is pushed into the first vane groove 34 to the maximum by the piston 8 is defined as “0 degree”. In the present embodiment, the angle θ (degrees) from the first angular position T1 to the fourth angular position T4 is in the range of 270 to 350 degrees with respect to the rotation direction of the shaft 4, for example. When the angle θ is set to 270 degrees or more, in the suction stroke of the first compression chamber 25, the amount of refrigerant that flows back from the first compression chamber 25 to the first suction pipe 14 through the first suction hole 19 is sufficiently small. . Therefore, it is not necessary to provide a check valve in the first suction hole 19. Of course, a check valve may be provided in the first suction hole 19.

  As shown in FIG. 2, the main bearing 6 and the sub-bearing 7 are respectively arranged on the upper side and the lower side of the cylinder 5 so as to close the cylinder 5. The muffler 9 is provided above the main bearing 6 and covers the first discharge valve 43 and the second discharge valve 44. The muffler 9 is formed with a discharge hole 9 a for guiding the compressed refrigerant to the internal space 13 of the sealed container 1. The shaft 4 passes through the center portion of the muffler 9 and is rotatably supported by the main bearing 6 and the sub bearing 7.

  As shown in FIGS. 2 and 3, in the present embodiment, the first suction hole 19 and the second suction hole 20 are formed in the cylinder 5. The first suction hole 19 guides the refrigerant to be compressed in the first compression chamber 25 to the first compression chamber 25. The second suction hole 20 guides the refrigerant to be compressed in the second compression chamber 26 to the second compression chamber 26. The first suction hole 19 and the second suction hole 20 may be formed in the main bearing 6 or the sub bearing 7, respectively.

In the present embodiment, the second suction hole 20 has an opening area smaller than the opening area of the first suction hole 19. The smaller the opening area of the second suction hole 20, the smaller the dimensions of the parts of the suction check valve 50. This is important from the viewpoint of suppressing an increase in dead volume caused by the suction check valve 50 and securing a design margin. When the opening area of the first suction hole 19 is S ₁ and the opening area of the second suction hole 20 is S ₂ , the opening areas S ₁ and S ₂ are, for example, 1.1 ≦ (S ₁ / S ₂ ) ≦ 30. Meet. “Dead volume” means a volume that does not function as a working chamber. In general, large dead volumes are not preferred for positive displacement fluid machines.

  As shown in FIG. 3, the compression mechanism 3 is connected to a first suction pipe 14 (main suction pipe) and a second suction pipe 16 (injection suction pipe). The first suction pipe 14 is fitted into the cylinder 5 through the trunk of the sealed container 1 so that the refrigerant can be supplied to the first suction hole 19. The first suction pipe 14 constitutes a part of the flow path 10d shown in FIG. The second suction pipe 16 is fitted into the cylinder 5 through the trunk portion of the sealed container 1 so that the refrigerant can be supplied to the second suction hole 20. The second suction pipe 16 constitutes a part of the injection flow path 10j shown in FIG.

  The compression mechanism 3 is further provided with a first discharge hole 40 (main discharge hole) and a second discharge hole 41 (injection discharge hole). The first discharge hole 40 and the second discharge hole 41 are respectively formed in the main bearing 6 so as to penetrate the main bearing 6 in the axial direction of the shaft 4. The first discharge hole 40 guides the refrigerant compressed in the first compression chamber 25 from the first compression chamber 25 to the outside of the first compression chamber 25 (in the present embodiment, the internal space of the muffler 9). The second discharge hole 41 guides the refrigerant compressed in the second compression chamber 26 from the second compression chamber 26 to the outside of the second compression chamber 26 (in this embodiment, the internal space of the muffler 9). A first discharge valve 43 and a second discharge valve 44 are provided in the first discharge hole 40 and the second discharge hole 41, respectively. When the pressure in the first compression chamber 25 exceeds the pressure in the internal space 13 of the sealed container 1 (high pressure in the refrigeration cycle), the first discharge valve 43 opens. When the pressure in the second compression chamber 26 exceeds the pressure in the internal space 13 of the sealed container 1, the second discharge valve 44 is opened.

  The muffler 9 serves as a discharge flow path that connects each of the first discharge hole 40 and the second discharge hole 41 and the internal space 13 of the sealed container 1. The refrigerant guided to the outside of the first compression chamber 25 through the first discharge hole 40 and the refrigerant guided to the outside of the second compression chamber 26 through the second discharge hole 41 merge inside the muffler 9. The merged refrigerant flows into the discharge pipe 11 via the internal space 13 of the sealed container 1. A motor 2 is arranged in the sealed container 1 so as to be positioned on the refrigerant flow path from the muffler 9 to the discharge pipe 11. According to such a configuration, the cooling of the motor 2 by the refrigerant and the heating of the refrigerant by the heat of the motor 2 can be performed efficiently.

In the present embodiment, the second discharge hole 41 has an opening area smaller than the opening area of the first discharge hole 40. The smaller the opening area of the second discharge hole 41, the smaller the dead volume caused by the second discharge hole 41. When the opening area of the first discharge hole 40 is S ₃ and the opening area of the second discharge hole 41 is S ₄ , the opening areas S ₃ and S ₄ are, for example, 1.1 ≦ (S ₃ / S ₄ ) ≦ 15. Meet.

Note that the opening area S ₂ of the second suction hole 20 may be equal to the opening area S ₁ of the first suction hole 19. Further, the opening area S ₄ of the second discharge hole 41 may be equal to the opening area S ₃ of the first discharge hole 40. The dimensions of each suction hole and each discharge hole should be appropriately determined in consideration of the flow rate of the refrigerant passing through them. More specifically, it should be determined in consideration of the balance between dead volume and pressure loss.

  As shown in FIG. 4, the suction check valve 50 includes a valve body 51 and a valve stop 52. A shallow groove 5g having a strip shape in plan view is formed on the upper surface 5p of the cylinder 5, and a valve body 51 and a valve stopper 52 are mounted in the groove 5g. The groove 5g extends outward in the radial direction of the cylinder 5 and communicates with the second compression chamber 26. The second suction hole 20 opens at the bottom of the groove 5g. Specifically, the second suction hole 20 is formed of a bottomed hole formed in the cylinder 5, and the bottomed hole opens at the bottom of the groove 5g. A suction flow path 5 f extending from the outer peripheral surface of the cylinder 5 toward the center of the cylinder 5 is formed in the cylinder 5 so that the refrigerant can be supplied to the second suction hole 20. A suction pipe 16 is connected to the suction flow path 5f.

  As shown in FIG. 5A, the valve body 51 has a back surface 51q that closes the second suction hole 20, and a surface 51p that is exposed to the atmosphere in the second compression chamber 26 when the second suction hole 20 is closed. . A movable range of the valve main body 51 of the suction check valve 50 is set in the second compression chamber 26. The valve body 51 has a thin plate shape as a whole, and is typically composed of a thin metal plate (reed valve).

  As shown in FIG. 5B, the valve stop 52 has a support surface 52q that restricts the amount of displacement in the thickness direction of the valve body 51 when the second suction hole 20 is opened. The support surface 52q forms a gentle curved surface so that the thickness of the valve stop 52 decreases as it approaches the second compression chamber 26. That is, the valve stop 52 has a shoe-like shape as a whole. The distal end surface 52 t of the valve stop 52 has an arc shape having the same radius of curvature as the inner diameter of the cylinder 5.

  The valve body 51 is disposed in the groove 5g so that the second suction hole 20 can be opened and closed. The valve stopper 52 is disposed in the groove 5g so that the support surface 52q is exposed to the atmosphere in the second compression chamber 26 when the valve body 51 closes the second suction hole 20. The valve main body 51 and the valve stopper 52 are fixed to the cylinder 5 by a fastener 54 such as a bolt. The rear end portion of the valve main body 51 is sandwiched between the valve stopper 52 and the groove 5g and cannot move, but the front end portion of the valve main body 51 is not fixed and swings. When the valve stop 52 and the second suction hole 20 are viewed in plan, the second suction hole 20 overlaps the support surface 52q of the valve stop 52.

  In the vicinity of the rear end of the valve stop 52, the total thickness of the valve main body 51 and the valve stop 52 substantially matches the depth of the groove 5g. When the valve body 51 and the valve stop 52 are mounted in the groove 5g, the position of the upper surface 52p of the valve stop 52 coincides with the position of the upper surface of the cylinder 5 in the thickness direction of the cylinder 5.

As shown in FIG. 5A, the valve body 51 has a wide portion 55 for opening and closing the second suction hole 20. The maximum width W ₁ of the wide portion 55 is wider than the width W ₂ of the tip of the valve stop 52, in other words, the width of the groove 5 g at the position facing the cylinder 5. The wide portion 55 can suppress an increase in dead volume while securing a seal width for closing the second suction hole 20.

  As shown in FIGS. 4 and 6, the depth of the groove 5 g is smaller than half of the thickness of the cylinder 5, for example. Most of the groove 5g is filled with a valve stop 52. A very small part of the groove 5g is left as a movable range of the valve body 51.

  The suction check valve 50 operates as follows with the rotation of the shaft 5. When the pressure in the second compression chamber 26 falls below the pressure in the suction flow path 5f and the second suction pipe 16, the valve body 51 is displaced into a shape along the support surface 52q of the valve stop 52. In other words, the valve body 51 is pushed up. Thereby, the second suction hole 20 and the second compression chamber 26 communicate with each other, and the refrigerant is supplied to the second compression chamber 26 through the second suction hole 20. On the other hand, when the pressure in the second compression chamber 26 exceeds the pressure in the suction flow path 5f and the second suction pipe 16, the valve body 51 returns to the original flat shape. As a result, the second suction hole 20 is closed. Therefore, it is possible to prevent the refrigerant sucked into the second compression chamber 26 from flowing back to the suction flow path 5f and the second suction pipe 16 through the second suction hole 20.

  In addition, the suction check valve 50 is configured so that the refrigerant sucked into the second compression chamber 26 through the second suction hole 20 is outside the second compression chamber 26 during the period specified by (i), (ii), or (iii). To prevent backflow. (I) The suction check valve 50 prevents backflow from the time when the second compression chamber 26 reaches the maximum volume to the time when the second compression chamber 26 reaches the minimum volume (≈0). (Ii) The suction check valve 50 flows backward from the time when the second compression chamber 26 reaches the maximum volume until the time when the compressed refrigerant starts to be discharged out of the second compression chamber 26 through the second discharge hole 41. To prevent. (Iii) The suction check valve 50 extends from the time when the second compression chamber 26 reaches the maximum volume to the time when the contact point between the cylinder 5 and the piston 8 passes through the second suction hole 20 as the shaft 4 rotates. To prevent backflow. When the angle θ is relatively large, the suction check valve 50 moves (i). When the angle θ is relatively small, the suction check valve 50 moves (ii) or (iii).

  According to the suction check valve 50 of the present embodiment, an increase in dead volume due to the provision of the check valve in the suction hole can be suppressed by the above-described some characteristic structures. That is, the suction check valve 50 contributes to achievement of high compressor efficiency. Therefore, the refrigeration cycle apparatus 100 using the rotary compressor 102 of the present embodiment has a high COP.

  Note that the second suction hole 20 may be formed in the main bearing 6 or the sub-bearing 7. In this case, the suction check valve 50 having the structure described with reference to FIGS. 3 to 6 can be provided in the main bearing 6 or the sub-bearing 7. A member (closing member) for closing the cylinder 5 may be provided between the main bearing 6 (or the auxiliary bearing 7) and the cylinder 5, and the suction check valve 50 may be provided on this member.

  The suction check valve 50 is not essential for the rotary compressor 102, but it is desirable to provide the suction check valve 50 in order to improve the compressor efficiency.

  Next, the operation of the rotary compressor will be described in time series with reference to FIG. The angle in FIG. 7 represents the rotation angle of the shaft 4. The angle shown in FIG. 7 is merely an example, and each stroke does not necessarily start or end at the angle shown in FIG. The process of sucking the refrigerant into the first compression chamber 25 is performed from when the shaft 4 occupies a rotation angle of 0 degrees to when it occupies a rotation angle of approximately 360 degrees. That is, the amount of refrigerant sucked into the first compression chamber 25 is equal to the volume of the first compression chamber 25 when the shaft 4 occupies a rotation angle of 360 degrees.

  The refrigerant sucked into the first compression chamber 25 is compressed as the shaft 4 rotates. The compression stroke continues until the pressure in the first compression chamber 25 exceeds the pressure in the internal space 13 of the sealed container 1. In FIG. 7, the compression stroke is performed from when the shaft 4 occupies a rotation angle of 360 degrees to when it has a rotation angle of 540 degrees. The process of discharging the compressed refrigerant out of the first compression chamber 25 is performed until the contact point between the cylinder 5 and the piston 8 passes through the first discharge hole 40. In FIG. 7, the discharge stroke is performed from when the shaft 4 occupies a rotation angle of 540 degrees to when it occupies a rotation angle of (630 + α) degrees. “Α” represents an angle from an angular position of 270 degrees to a fourth angular position T4 where the second vane 33 is disposed.

On the other hand, the process of sucking the refrigerant into the second compression chamber 26 is performed from when the shaft 4 occupies a rotation angle of (270 + α) degrees to when it occupies a rotation angle of θ ₂ degrees. “Θ ₂ ” represents the rotation angle of the shaft 4 when the volume of the second compression chamber 26 is maximized. In FIG. 3, assuming that the second reference plane P2 coincides with the first reference plane P1, θ ₂ is represented by (495 + α / 2) using α. The amount of refrigerant sucked into the second compression chamber 26 is equal to the volume of the second compression chamber 26 when the shaft 4 occupies a rotation angle of θ ₂ degrees.

The refrigerant sucked into the second compression chamber 26 is compressed as the shaft 4 rotates. The compression stroke continues until the pressure in the second compression chamber 26 exceeds the pressure in the internal space 13 of the sealed container 1. In FIG. 7, the compression stroke is performed from when the shaft 4 occupies a rotation angle of θ ₂ degrees to when it occupies a rotation angle of 630 degrees. The process of discharging the compressed refrigerant out of the second compression chamber 26 is performed until the contact point between the cylinder 5 and the piston 8 passes through the second discharge hole 41. In FIG. 7, the discharge stroke is performed from when the shaft 4 occupies a rotation angle of 630 degrees to when it occupies a rotation angle of 720 degrees.

  The suction volume of the first compression chamber 25 and the suction volume of the second compression chamber 26 will be described in detail.

  As shown in FIGS. 8A and 9A as a reference example, it is assumed that the second reference plane P2 coincides with the first reference plane P1. On the other hand, as shown in FIGS. 8B and 9B, in the present embodiment, the second reference plane P2 is inclined with respect to the first reference plane P1.

  The areas of the portions indicated by dots in FIGS. 8A and 8B represent the suction volume of the first compression chamber 25, respectively. The suction volume of the first compression chamber 25 in the present embodiment (FIG. 8B) is equal to the suction volume of the first compression chamber 25 in the reference example (FIG. 8A). More precisely, the suction volume of the first compression chamber 25 is the moment when the contact point between the piston 8 and the cylinder 5 (the contact point between the movable circle 8a and the fixed circle 5a) passes through the first suction hole 19 (see FIG. 3). That is, it is equal to the volume of the first compression chamber 25 at the moment when the compression stroke starts. At that moment, the shaft 4 occupies, for example, a rotation angle of 30 degrees.

9A and 9B, the shaft 4 occupies a rotation angle of θ ₂ degrees. However, the angle θ ₂ when the volume of the second compression chamber 26 is maximized is different between the reference example and the present embodiment. The areas of the portions indicated by dots in FIGS. 9A and 9B represent the suction volume of the second compression chamber 26, respectively. The suction volume of the second compression chamber 26 in this embodiment (FIG. 9B) is larger than the suction volume of the second compression chamber 26 in the reference example (FIG. 9A). Thus, according to the present embodiment, the suction volume of the second compression chamber 26 can be increased without reducing the suction volume of the first compression chamber 25. When the suction check valve 50 is provided, the suction volume of the second compression chamber 26 is equal to the maximum volume of the second compression chamber 26. If a suction check valve is provided in the first suction hole 19, the suction volume of the first compression chamber 25 is equal to the maximum volume of the first compression chamber 25.

  FIG. 10 is a graph showing the relationship between the inclination angle ξ of the second reference plane P2 with respect to the first reference plane P1 and the increasing rate of the suction volume of the second compression chamber 26. The increase rate of the suction volume is expressed as a ratio to the suction volume of the second compression chamber 26 in the reference example shown in FIG. 9A. As the inclination angle ξ increases, the suction volume of the second compression chamber 26 increases. The effect of increasing the suction volume of the second compression chamber 26 is obtained when the inclination angle ξ is larger than 0 degrees. The upper limit value of the tilt angle ξ is not particularly limited. Considering the reliability of the rotary compressor 102, design restrictions, etc., the upper limit value of the tilt angle ξ is, for example, 20 degrees. Specifically, the tilt angle ξ can be set to a range greater than 0 degree and 5 degrees or less, or greater than 1 degree and 5 degrees or less.

  Next, the effect of suppressing the back flow of the refrigerant from the first compression chamber 25 to the first suction pipe 14 will be described in detail.

  When the angle θ from the first reference position T1 to the fourth reference position T4 is set to 270 degrees or more, the reverse flow rate of the refrigerant from the first compression chamber 25 to the first suction pipe 14 is small. Therefore, it is not always necessary to provide a check valve in the first suction hole 19. However, a small amount of refrigerant flows backward from the first compression chamber 25 to the first suction pipe 14 through the first suction hole 19. The pulsation caused by this backflow can cause noise and vibration problems.

As shown in FIG. 11A, when the shaft 4 occupies a rotation angle of θ ₁ degree, the first compression chamber 25 has a maximum volume. As shown in FIG. 11B, when the shaft 4 occupies a rotation angle of 0 degrees, the volume of the first compression chamber 25 is equal to the suction volume. The amount of refrigerant flowing backward from the first compression chamber 25 to the first suction pipe 14 is equal to the volume obtained by subtracting the suction volume of the first compression chamber 25 from the maximum volume of the first compression chamber 25. Note that “θ ₁ ” is smaller than 360 degrees (= 0 degrees). Assuming that the second reference plane P2 coincides with the first reference plane P1, θ ₁ is represented by (270 + α / 2) using α.

  In order to reduce the reverse flow rate of the refrigerant, it is necessary to increase the angle θ from the first angular position T1 to the fourth angular position T4. However, when the angle θ is increased, the suction volume of the second compression chamber 26 is reduced. An appropriate ratio of the suction volume of the second compression chamber 26 to the suction volume of the first compression chamber 25 is determined according to the use of the refrigeration cycle apparatus 100 and the like. For this reason, there may be a case where a decrease in the suction volume of the second compression chamber 26 is not acceptable.

  According to the present embodiment, the first vane groove 34 is formed so that the second reference plane P2 is inclined with respect to the first reference plane P1, that is, the posture of the first vane 32 is appropriately adjusted. . Therefore, the suction volume of the second compression chamber 26 can be increased without increasing the angle θ from the first angular position T1 to the fourth angular position T4. Therefore, the reverse flow of the refrigerant from the first compression chamber 25 to the first suction pipe 14 can be suppressed while sufficiently securing the suction volume of the second compression chamber 26.

(Modification)
FIG. 12 is a longitudinal sectional view of a rotary compressor according to a modification. The rotary compressor 202 has a structure in which components such as a cylinder are added to the rotary compressor 102 shown in FIG. In this modification, the compression mechanism 3, the cylinder 5, the piston 8, and the eccentric portion 4a shown in FIG. 2 are defined as the first compression mechanism 3, the first cylinder 5, the first piston 8, and the first eccentric portion 4a, respectively. The detailed structure of the first compression mechanism 3 is as described with reference to FIGS.

  As shown in FIGS. 12 and 13, the rotary compressor 202 includes a second compression mechanism 30 in addition to the first compression mechanism 3. The second compression mechanism 30 includes a second cylinder 65, an intermediate plate 66, a second piston 68, a sub bearing 67, a muffler 70, a third vane 72, a third suction hole 69, and a third discharge hole 73. The second cylinder 65 is disposed concentrically with respect to the first cylinder 5, and is separated from the first cylinder 5 by an intermediate plate 66.

  The shaft 4 has a second eccentric portion 4b protruding outward in the radial direction. The second piston 68 is disposed inside the second cylinder 65. Inside the second cylinder 65, the second piston 68 is attached to the second eccentric portion 4 b of the shaft 4. The intermediate plate 66 is disposed between the first cylinder 5 and the second cylinder 65. A vane groove 74 is formed in the second cylinder 65. A third vane 72 (blade) having a tip in contact with the outer peripheral surface of the second piston 68 is attached to the vane groove 74 so as to be slidable. The third vane 72 partitions the space between the second cylinder 65 and the second piston 68 along the circumferential direction of the second piston 68. Thereby, the third compression chamber 71 is formed inside the second cylinder 65. The second piston 68 and the third vane 72 may be configured as a single component, a so-called swing piston. Further, the third vane 72 may be coupled to the second piston 68. A third spring 76 that pushes the third vane 72 toward the center of the shaft 4 is disposed behind the third vane 72.

  The third suction hole 69 guides the refrigerant to be compressed in the third compression chamber 71 to the third compression chamber 71. A third suction pipe 64 is connected to the third suction hole 69. The third discharge hole 73 passes through the auxiliary bearing 67 and opens toward the inner space of the muffler 70. The refrigerant compressed in the third compression chamber 71 passes through the third discharge hole 73 and is guided from the third compression chamber 71 to the outside of the third compression chamber 71, specifically, to the internal space of the muffler 70. The inside of the sealed container 1 is passed from the inner space of the muffler 70 through the flow path 63 that passes through the main bearing 6, the first cylinder 5, the middle plate 66, the second cylinder 65, and the auxiliary bearing 67 in the axial direction of the shaft 4. The refrigerant is guided to the space 13. The channel 63 may open toward the internal space 13 of the sealed container 1 or may open toward the internal space of the muffler 9.

  As described above, the second compression mechanism 30 has the same structure as the compression mechanism of a normal rolling piston compressor having only one vane.

  In the rotary compressor 202, the height, inner diameter, and outer diameter of the second cylinder 65 are equal to the height, inner diameter, and outer diameter of the first cylinder 5, respectively. The outer diameter of the first piston 8 is equal to the outer diameter of the second piston 68. Since only the third compression chamber 71 is formed inside the second cylinder 65, the first compression chamber 25 has a volume smaller than the volume of the third compression chamber 71. That is, by sharing parts between the first compression mechanism 3 and the second compression mechanism 30, it is possible to reduce costs and improve assembly ease.

  According to this modification, the first compression mechanism 3 is disposed on the upper side and the second compression mechanism 30 is disposed on the lower side with respect to the axial direction of the shaft 4. The refrigerant compressed by the first compression mechanism 3 is guided to the internal space of the muffler 9 through the discharge holes 40 and 41 provided in the main bearing 6. The first compression mechanism 3 has two discharge holes 40 and 41. Therefore, it is desirable to shorten the distance from the discharge holes 40 and 41 to the internal space 13 of the sealed container 1 as much as possible, thereby reducing the pressure loss of the refrigerant in the discharge holes 40 and 41 as much as possible. From this viewpoint, it is preferable that the first compression mechanism 3 is disposed on the upper side in the axial direction.

  However, from another viewpoint, the first compression mechanism 3 may be disposed on the lower side in the axial direction. The reason is as follows. The closer to the motor 2, the higher the temperature inside the sealed container 1. That is, during the operation of the rotary compressor 202, the main bearing 6 has a temperature higher than the temperatures of the auxiliary bearing 67 and the muffler 70. Therefore, when the first compression mechanism 3 is disposed on the upper side and the second compression mechanism 30 is disposed on the lower side, the refrigerant to be guided to the second compression chamber 26 is easily heated. Then, since the mass flow rate of the refrigerant to be compressed in the second compression chamber 26 is reduced, the effect of the injection is also reduced. In order to obtain a higher injection effect, the first compression mechanism 3 having the second compression chamber 26 may be disposed on the lower side, and the second compression mechanism 30 may be disposed on the upper side.

  As shown in FIG. 12, with respect to the rotation direction of the shaft 4, the angular difference between the protruding direction of the first eccentric portion 4a and the protruding direction of the second eccentric portion 4b is 180 degrees. In other words, the phase difference between the first piston 8 and the second piston 68 is 180 degrees with respect to the rotation direction of the shaft 4. In other words, the timing of the top dead center of the first piston 8 is shifted by 180 degrees from the timing of the top dead center of the second piston 68. According to such a configuration, vibration generated based on the rotation of the first piston 8 can be canceled out by the rotation of the second piston 68. Further, the compression stroke of the first compression chamber 25 and the compression stroke of the third compression chamber 71 are substantially alternately performed, and the discharge stroke of the first compression chamber 25 and the discharge stroke of the third compression chamber 71 are substantially alternately alternated. Done. Therefore, the torque fluctuation of the shaft 4 can be reduced, which is advantageous in reducing motor loss and mechanical loss. In addition, vibration and noise of the rotary compressor 202 can be reduced. The “timing of the top dead center of the piston” means the timing at which the vane is pushed into the vane groove to the maximum by the piston.

  When the rotary compressor 202 is used in the refrigeration cycle apparatus 100 shown in FIG. 1, the following configuration can be adopted. The refrigeration cycle apparatus 100 includes a suction flow path 10d that guides the refrigerant flowing out from the first heat exchanger 104 or the second heat exchanger 112 as an evaporator to the first suction hole 19 of the rotary compressor 202. As shown in FIG. 12, the refrigerant flowing out from the first heat exchanger 104 or the second heat exchanger 112 is sucked so that it is led to both the first suction hole 19 and the third suction hole 69 of the rotary compressor 202. The flow path 10 d includes a branch portion 14 that extends toward the first suction hole 19 and a branch portion 64 that extends toward the third suction hole 69. In the present embodiment, the first suction pipe 14 constitutes the branch portion 14, and the third suction pipe 64 constitutes the branch portion 64. According to such a configuration, the refrigerant can be smoothly guided to the first compression chamber 25 and the third compression chamber 71. Note that the suction channel 10 d may be branched inside the sealed container 1.

(Second Embodiment)
FIG. 14 is a configuration diagram of a refrigeration cycle apparatus according to the second embodiment. The refrigeration cycle apparatus 200 of the present embodiment is different from the refrigeration cycle apparatus 100 of the first embodiment in that the injection is performed in two stages. Since the injection is performed in two stages, a particularly high effect can be obtained when the refrigeration cycle apparatus 200 is used for heating or hot water supply. Hereinafter, the same reference numerals are assigned to the components described in the first embodiment, and the description thereof is omitted.

  The refrigeration cycle apparatus 200 includes a rotary compressor 302, a first heat exchanger 104, a first expansion mechanism 106, a first gas-liquid separator 108, a second expansion mechanism 110, a second gas-liquid separator 109, and a third expansion mechanism. 111 and a second heat exchanger 112 are provided. These components are annularly connected in the above order by the flow paths 10 a to 10 e so as to form the refrigerant circuit 10. The refrigerant circuit 10 is provided with a four-way valve 116 as a switching mechanism capable of switching the flow direction of the refrigerant.

  The 1st expansion mechanism 106 expands the refrigerant | coolant cooled with the 1st heat exchanger 104 as a heat radiator. The first gas-liquid separator 108 separates the refrigerant expanded by the first expansion mechanism 106 into a gas phase refrigerant and a liquid phase refrigerant. The second expansion mechanism 110 expands the liquid-phase refrigerant separated by the first gas-liquid separator 108. The second gas-liquid separator 109 separates the refrigerant expanded by the second expansion mechanism 110 into a gas phase refrigerant and a liquid phase refrigerant. The third expansion mechanism 111 expands the liquid-phase refrigerant separated by the second gas-liquid separator 109. The refrigerant that has passed through the third expansion mechanism 111 flows into the second heat exchanger 112 serving as an evaporator. Due to the function of the four-way valve 116, the refrigerant can also flow in the opposite direction.

  The rotary compressor 302 has a first suction hole 19, a second suction hole 20, a third suction hole 23, and a fourth suction hole 24. The suction flow path 10d guides the refrigerant flowing out from the first heat exchanger 104 or the second heat exchanger 112 to the first suction hole 19 and the third suction hole 23 of the rotary compressor 302, respectively.

  The refrigeration cycle apparatus 200 further includes a first injection flow path 10j and a second injection flow path 10k. The first injection flow path 10j has one end connected to the first gas-liquid separator 108 and the other end connected to the rotary compressor 302. The first injection flow path 10j has a gas phase separated by the first gas-liquid separator 108. The refrigerant is guided to the rotary compressor 302. The second injection flow path 10k has one end connected to the second gas-liquid separator 109 and the other end connected to the rotary compressor 302, and the gas phase separated by the second gas-liquid separator 109 is The refrigerant is guided to the rotary compressor 302.

  The refrigeration cycle apparatus 200 of the present embodiment is the first in that it has a second gas-liquid separator 109 and a second injection path 10k in addition to the first gas-liquid separator 108 and the first injection flow path 10j. It differs from the refrigeration cycle apparatus 100 of the embodiment. Further, the rotary compressor 302 used in the refrigeration cycle apparatus 200 of the second embodiment is configured to perform injection in two stages.

  As shown in FIGS. 15, 16 </ b> A, and 16 </ b> B, the rotary compressor 302 includes the compression mechanism 3 described in the first embodiment and a second compression mechanism 90 having the same structure as the compression mechanism 3. The compression mechanism 3, the cylinder 5, the piston 8, and the eccentric portion 4a of the rotary compressor 102 described in the first embodiment are defined as the first compression mechanism 3, the first cylinder 5, the first piston 8, and the first eccentric portion 4a, respectively. To do.

  As shown in FIGS. 15 and 16B, the second compression mechanism 90 includes a second cylinder 75, a second piston 78, a third vane 92, a fourth vane 93, a third suction hole 23, a third discharge hole 45, A third discharge valve 47, a fourth suction hole 24, a fourth discharge hole 46, a fourth discharge valve 48, and a second suction check valve 56; The second compression mechanism 90 has basically the same structure as the first compression mechanism 3. The second compression mechanism 90 is concentrically arranged with respect to the first compression mechanism 3 so as to share the shaft 4.

  That is, the first cylinder 5, the first piston 8, the first vane 32, the second vane 33, the first suction hole 19, the first discharge hole 40, the first discharge valve 43, and the second suction hole of the first compression mechanism 3. 20, the second discharge hole 41, the second discharge valve 44, and the first suction check valve 50 are respectively the second cylinder 75, the second piston 78, the third vane 92, and the fourth vane 93 of the second compression mechanism 90. , Corresponding to the third suction hole 23, the third discharge hole 45, the third discharge valve 47, the fourth suction hole 24, the fourth discharge hole 46, the fourth discharge valve 48, and the second suction check valve 56. Further, the first vane groove 34, the first spring 36, the second vane groove 35, and the second spring 37 of the first compression mechanism 3 are respectively connected to the third vane groove 94, the third spring 96, and the like of the second compression mechanism 90. This corresponds to the fourth vane groove 95 and the fourth spring 97. Furthermore, the first compression chamber 25 and the second compression chamber 26 of the first compression mechanism 3 correspond to the third compression chamber 27 and the fourth compression chamber 28 of the second compression mechanism 90, respectively. Further, the first suction pipe 14 and the second suction pipe 16 of the rotary compressor 102 correspond to the third suction pipe 84 and the fourth suction pipe 86 of the rotary compressor 302, respectively. All the structures related to the first compression mechanism 3 and the description thereof can be applied to those of the second compression mechanism 90.

  In addition, as shown in FIG. 17, the 3rd vane groove | channel 94 may be formed so that the front-end | tip of the 3rd vane 92 may face the direction of the rotating shaft O of the shaft 4. As shown in FIG. That is, the third vane groove 94 is formed so that a virtual plane parallel to the rotation axis O of the shaft 4 and passing through the center in the width direction of the third vane groove 94 includes the rotation axis O of the shaft 4. May be.

  According to the rotary compressor 302, the angular difference between the protruding direction of the first eccentric portion 4a and the protruding direction of the second eccentric portion 4b with respect to the rotation direction of the shaft 4 is 180 degrees. In other words, the phase difference between the first piston 8 and the second piston 78 is 180 degrees with respect to the rotation direction of the shaft 4. The effects based on this configuration are the same as those described for the rotary compressor 202 shown in FIG.

  The first injection flow path 10 j guides the gas-phase refrigerant separated by the first gas-liquid separator 108 to the second suction hole 20 of the rotary compressor 302. The second injection flow path 10k guides the gas-phase refrigerant separated by the second gas-liquid separator 109 to the fourth suction hole 24 of the rotary compressor 302. Since both the 1st compression mechanism 3 and the 2nd compression mechanism 90 can compress the refrigerant | coolant which has intermediate pressure, the improvement of the further efficiency of the rotary compressor 302 can be anticipated.

(Modification)
The first compression chamber 25 may have a volume different from the volume of the third compression chamber 27. The second compression chamber 26 may have a volume different from the volume of the fourth compression chamber 28. For example, in the modification shown in FIG. 18, the thickness H ₂ of the second cylinder 75 is larger than the thickness H ₁ of the first cylinder 5. Therefore, the fourth compression chamber 28 (second injection compression chamber) has a volume larger than that of the second compression chamber 26 (first injection compression chamber). In this case, the refrigerant is supplied to the second compression chamber 26 from the high-pressure side injection flow path (for example, the first injection flow path 10j), and the low-pressure side injection flow path (for example, the second injection flow path 10k) is supplied to the fourth compression chamber 28. ) Can be supplied with refrigerant. That is, a relatively low pressure refrigerant is compressed in the fourth compression chamber 28 having a relatively large volume, and a relatively high pressure refrigerant is compressed in the second compression chamber 26 having a relatively small volume. In this way, the second compression chamber 26 and the fourth compression chamber 28 can suck the gas refrigerant generated by the first gas-liquid separator 108 and the second gas-liquid separator 109 without excess or deficiency, respectively. When the gas refrigerant is injected into the rotary compressor 302 without excess or deficiency, the refrigeration cycle apparatus 200 can be operated with high efficiency.

Since the ratio of the volume of the fourth compression chamber 28 to the volume of the second compression chamber 26 depends on the type of refrigerant, the use of the refrigeration cycle apparatus 100, etc., it is not unconditionally determined. As an example, when the volume of the second compression chamber 26 is V ₁ and the volume of the fourth compression chamber 28 is V ₂ , the volumes V ₁ and V ₂ satisfy 1.1 ≦ (V ₂ / V ₁ ) ≦ 30. In addition, the compression mechanisms 3 and 90 can be designed. The volume of the compression chamber can be adjusted by changing various design values such as the height of the cylinder, the inner diameter of the cylinder, the outer diameter of the piston, and the amount of protrusion of the eccentric portion of the shaft. Of course, the volume of the compression chamber can also be adjusted by changing the positional relationship between the two vanes. By making at least one design value selected from the height of the cylinder, the inner diameter of the cylinder, the outer diameter of the piston, and the protruding amount of the eccentric portion of the shaft different between the first compression mechanism 3 and the second compression mechanism 90, When the volume of the second compression chamber 26 and the volume of the fourth compression chamber 28 are adjusted to the above relationship, the volume of the compression chamber can be optimized without changing the position of the vane.

  According to the refrigeration cycle apparatus 200 shown in FIG. 14, the refrigerant flow direction is switched by controlling the four-way valve 116. Accordingly, as shown in FIG. 19, the refrigerant in the first injection flow path 10j can be guided to one selected from the second suction hole 20 and the fourth suction hole 24 of the rotary compressor 302, and the second injection flow path. The flow path switching unit 122 can be provided so that the 10 k refrigerant can be guided to the other selected from the second suction hole 20 and the fourth suction hole 24 of the rotary compressor 302.

  The channel switching unit 122 includes a first three-way valve 118, a second three-way valve 119, a first bypass channel 120, and a second bypass channel 121. The first three-way valve 118 is provided on the first injection flow path 10j. The second three-way valve 119 is provided on the second injection flow path 10k. The first bypass flow channel 120 connects one outlet of the first three-way valve 118 and the second injection flow channel 10k. The second bypass passage 121 connects one outlet of the second three-way valve 119 and the first injection passage 10j. When the three-way valves 118 and 119 are controlled as indicated by solid lines, the refrigerant in the first injection flow path 10j is guided to the second suction hole 20 and the refrigerant in the second injection flow path 10k is guided to the fourth suction hole 24. It is burned. When the three-way valves 118 and 119 are controlled as indicated by broken lines, the refrigerant in the first injection flow path 10j is guided to the fourth suction hole 24, and the refrigerant in the second injection flow path 10k is guided to the second suction hole 20. It is burned. In this way, even if the flow direction of the refrigerant changes, it is possible to supply the refrigerant with an appropriate pressure to each of the second compression chamber 26 and the fourth compression chamber 28.

  The refrigeration cycle apparatus of the present invention can be used for a water heater, a hot water heater, an air conditioner, and the like.

DESCRIPTION OF SYMBOLS 1 Airtight container 2 Motor 3 Compression mechanism 30,90 2nd compression mechanism 4 Shaft 4a, 4b Eccentric part 5 Cylinder 5a The fixed circle 65 and 75 which make the inner peripheral surface of a cylinder 2nd cylinder 5g Groove 6 Main bearings 7, 67 Sub bearing 8 Piston 8a Movable circles 68, 78 forming the outer peripheral surface of the piston Second piston 9, 70 Mufflers 10a to 10e Flow path 10j Injection flow path 10k Second injection flow path 11 Discharge pipe 13 Internal space 14 First suction pipe 16 Second Suction pipe 19 First suction hole 20 Second suction hole 23, 69 Third suction hole 24 Fourth suction hole 25 First compression chamber 26 Second compression chamber 27, 71 Third compression chamber 28 Fourth compression chamber 32 First vane 33 2nd vane 34 1st vane groove 35 2nd vane groove 40 1st discharge hole 41 2nd discharge hole 43 1st discharge valve 44 2nd discharge valve 45, 73 3rd discharge hole 46 1st Discharge hole 47 Third discharge valve 48 Fourth discharge valve 50, 56 Suction check valve 51 Valve body 51p Valve body surface 51q Valve body back surface 52 Valve stop 52q Support surface 84 Third suction pipe 86 Fourth suction pipe 72, 92 3rd vane 93 4th vane 94 3rd vane groove 95 4th vane groove 100,200 Refrigeration cycle apparatus 102,202,302 Rotary compressor 104 1st heat exchanger 106 1st expansion mechanism 108 1st gas-liquid separator 109 Second gas-liquid separator 110 Second expansion mechanism 111 Third expansion mechanism 112 Second heat exchanger 116 Four-way valve P1 First reference plane P2 Second reference plane P3 Third reference plane T1 First angular position T2 Second angle Position T3 Third angle position T4 Fourth angle position O Rotation axis

Claims (12)

A cylinder,
A piston disposed in the cylinder so as to form a space between itself and the cylinder;
A shaft to which the piston is attached;
A first vane that is disposed in a first vane groove formed in the cylinder and partitions the space along a circumferential direction of the piston;
A first compression chamber and a second compression chamber having a volume smaller than the volume of the first compression chamber are formed in the cylinder and are disposed in a second vane groove formed in the cylinder. A second vane further dividing the space partitioned by the first vane along a circumferential direction of the piston;
A first suction hole for guiding the working fluid to be compressed in the first compression chamber to the first compression chamber;
A first discharge hole for guiding the working fluid compressed in the first compression chamber from the first compression chamber to the outside of the first compression chamber;
A second suction hole for guiding the working fluid to be compressed in the second compression chamber to the second compression chamber;
A second discharge hole for guiding the working fluid compressed in the second compression chamber from the second compression chamber to the outside of the second compression chamber;
With
The position of the contact point between the movable circle forming the outer peripheral surface of the piston and the fixed circle forming the inner peripheral surface of the cylinder at the moment when the first vane is pushed into the first vane groove to the maximum by the piston. One angular position, a position on the fixed circle 180 degrees opposite to the first angular position passes through the second angular position, the first angular position, and the second angular position, and passes through the rotation axis of the shaft. A virtual plane including a first reference plane, a reciprocating motion direction of the first vane and a rotation plane of the shaft, and a second virtual plane passing through the center of the width direction of the first vane groove. When a reference plane, a position where the second reference plane and the fixed circle intersect with each other is defined as a third angular position,
When the shaft is rotated, the second reference plane is the first reference point so that the contact point between the movable circle and the fixed circle passes in the order of the first angular position, the third angular position, and the second angular position. We are inclined relative to the reference plane,
The position of the contact point between the movable circle and the fixed circle at the moment when the second vane is pushed into the second vane groove as much as possible passes through the fourth angular position, the fourth angular position, and the shaft. A rotary compressor in which a reciprocating direction of the second vane is parallel to the third reference plane when a virtual plane including a rotation axis is defined as a third reference plane .   2. The rotary compressor according to claim 1, wherein the second reference plane is inclined with respect to the first reference plane in a range of greater than 0 degrees and less than or equal to 5 degrees.   The rotary compressor according to claim 1, further comprising a suction check valve provided in the second suction hole.   (I) the second compression chamber reaches the maximum volume from the time when the second compression chamber reaches the maximum volume until the time when the second compression chamber reaches the minimum volume; Until the time when the compressed working fluid starts to be discharged out of the second compression chamber through the second discharge hole, or (iii) from the time when the second compression chamber reaches the maximum volume, The working fluid sucked into the second compression chamber passes through the second suction hole until the contact point between the piston and the piston passes through the second suction hole as the shaft rotates. The rotary compressor according to claim 3, wherein the rotary compressor is prevented from flowing backward.   The rotary compressor according to any one of claims 1 to 4, wherein the second suction hole has an opening area smaller than an opening area of the first suction hole.   The rotary compressor according to any one of claims 1 to 4, wherein the second discharge hole has an opening area smaller than an opening area of the first discharge hole. When the position of the contact point between the movable circle and the fixed circle at the moment when the second vane is pushed into the second vane groove to the maximum by the piston is defined as a fourth angular position,
With respect to the rotation direction of the shaft, an angle θ from the first angular position to the fourth angular position is set to 270 degrees or more ,
The rotary compressor according to claim 3 , wherein a suction check valve is not provided in the first suction hole . A sealed container containing a compression mechanism including the cylinder, the piston, the first vane and the second vane;
A discharge pipe opening toward the internal space of the sealed container;
The working fluid led to the outside of the first compression chamber through the first discharge hole and the working fluid led to the outside of the second compression chamber through the second discharge hole pass through the internal space of the sealed container. A discharge flow path connecting each of the first discharge hole and the second discharge hole and the internal space of the sealed container so as to flow into the discharge pipe.
A motor disposed in the sealed container so as to be positioned on the flow path of the working fluid from the discharge flow path to the discharge pipe;
The rotary compressor according to any one of claims 1 to 7, further comprising: When the cylinder is defined as a first cylinder and the piston is defined as a first piston,
The rotary compressor further includes
A second cylinder disposed concentrically with respect to the first cylinder;
A second piston disposed within the second cylinder and attached to the shaft;
A third vane for partitioning a space between the second cylinder and the second piston along a circumferential direction of the second piston so that a third compression chamber is formed in the second cylinder;
A third suction hole for guiding the working fluid to be compressed in the third compression chamber to the third compression chamber;
A third discharge hole for guiding the working fluid compressed in the third compression chamber from the third compression chamber to the outside of the third compression chamber;
The rotary compressor of any one of Claims 1-8 provided with these. When the cylinder is defined as a first cylinder and the piston is defined as a first piston,
The rotary compressor further includes
A second cylinder disposed concentrically with respect to the first cylinder;
A second piston disposed in the second cylinder and attached to the shaft so as to form a second space between itself and the second cylinder;
A third vane which is disposed in a third vane groove formed in the second cylinder and partitions the second space along a circumferential direction of the second piston;
A third compression chamber and a fourth compression chamber having a volume smaller than the volume of the third compression chamber are formed in the second cylinder and are disposed in a fourth vane groove formed in the second cylinder. A fourth vane that further partitions the second space partitioned by the third vane along a circumferential direction of the second piston;
A third suction hole for guiding the working fluid to be compressed in the third compression chamber to the third compression chamber;
A third discharge hole for guiding the working fluid compressed in the third compression chamber from the third compression chamber to the outside of the third compression chamber;
A fourth suction hole for guiding the working fluid to be compressed in the fourth compression chamber to the fourth compression chamber;
A fourth discharge hole for guiding the working fluid compressed in the fourth compression chamber from the fourth compression chamber to the outside of the fourth compression chamber;
A second suction check valve provided in the fourth suction hole;
The rotary compressor of any one of Claims 1-8 provided with these. The shaft includes a first eccentric part to which the first piston is attached, and a second eccentric part to which the second piston is attached.
The rotary compressor according to claim 9 or 10, wherein an angular difference between a protruding direction of the first eccentric portion and a protruding direction of the second eccentric portion is 180 ° with respect to the rotation direction of the shaft. The rotary compressor according to any one of claims 1 to 11,
A radiator for cooling the working fluid compressed by the rotary compressor;
An expansion mechanism for expanding the working fluid cooled by the radiator;
A gas-liquid separator that separates the working fluid expanded by the expansion mechanism into a gaseous working fluid and a liquid working fluid;
An evaporator for evaporating the liquid-phase working fluid separated by the gas-liquid separator;
A suction flow path for guiding the working fluid flowing out of the evaporator to the first suction hole of the rotary compressor;
An injection flow path for guiding the gas-phase working fluid separated by the gas-liquid separator to the second suction hole of the rotary compressor;
A refrigeration cycle apparatus comprising:

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