TECHNICAL FIELD
The present invention relates to a vane compressor.
BACKGROUND ART
Hitherto, typical vane compressors have been proposed in each of which a rotor portion included in a rotor shaft (a unit including the rotor portion, which has a columnar shape and undergoes a rotational motion in a cylinder, and a shaft that transmits a rotational force to the rotor portion is referred to as rotor shaft) has one or a plurality of vane grooves in which vanes are fitted, respectively, the tips of the vanes being in contact with and sliding on the inner circumferential surface of the cylinder (see Patent Literature 1, for example).
Another proposed vane compressor includes a rotor shaft having a hollow thereinside. A fixed shaft provided for vanes is provided in the hollow. The vanes are rotatably attached to the fixed shaft. Furthermore, the vanes are each held between a pair of nipping members (a bush) provided closely to the outer circumference of the rotor portion, the vanes being held in such a manner as to be rotatable with respect to a rotor portion, the nipping members each having a semicircular stick-like shape (see Patent Literature 2, for example).
CITATION LIST
Patent Literature
Patent Literature 1: Japanese Unexamined Patent Application Publication No. 10-252675 (p. 4 and FIG. 1)
Patent Literature 2: Japanese Unexamined Patent Application Publication No. 2000-352390 (p. 6 and FIG. 1)
SUMMARY OF INVENTION
Technical Problem
In the known typical vane compressor disclosed by Patent Literature 1, there is a large difference between the radius of curvature at the tip of each vane and the radius of curvature of the inner circumferential surface of the cylinder. Therefore, no oil film is formed between the inner circumferential surface of the cylinder and the tip of the vane, producing a state of boundary lubrication instead of hydrodynamic lubrication. In general, the coefficient of friction, which depends on the state of lubrication, is about 0.001 to 0.005 in the case of hydrodynamic lubrication but is much higher, about 0.05 or above, in the case of boundary lubrication.
Hence, the configuration of the known typical vane compressor has a problem in that a significant reduction in the compressor efficiency due to an increase in mechanical loss occurs with an increase in the sliding resistance between the tip of the vane and the inner circumferential surface of the cylinder that slide on each other in a state of boundary lubrication. Moreover, the known typical vane compressor has another problem in that the tip of the vane and the inner circumferential surface of the cylinder are liable to wear, making it difficult to provide a long life.
To ease the above problems, a technology (see Patent Literature 2, for example) has been proposed in which a rotor portion having a hollow thereinside includes a fixed shaft that is provided in the hollow and supports vanes such that the vanes are rotatable about the center of the inner circumferential surface of a cylinder, the vanes being held between nipping members in such a manner as to be rotatable with respect to the rotor portion, the nipping members being provided closely to the outer circumference of the rotor portion.
In the above configuration, the vanes are rotatably supported at the center of the inner circumferential surface of the cylinder. Hence, the longitudinal direction of each of the vanes always corresponds to a direction toward the center of the inner circumferential surface of the cylinder. Accordingly, the vanes rotate with the tips thereof moving along the inner circumferential surface of the cylinder. Therefore, a very small gap is always provided between the tip of each of the vanes and the inner circumferential surface of the cylinder, allowing the vanes and the cylinder to behave without coming into contact with each other. Hence, no loss due to sliding at the tips of the vanes occurs. Thus, a vane compressor in which the tips of vanes and the inner circumferential surface of a cylinder do not wear is provided.
In the technology disclosed by Patent Literature 2, however, since the rotor portion has a hollow thereinside, it is difficult to provide a rotational force to the rotor portion and to rotatably support the rotor portion. According to Patent Literature 2, end plates are provided on two respective end facets of the rotor portion. One of the end plates has a disc-like shape out of the need for transmitting power from a rotating shaft. The rotating shaft is connected to the center of the end plate. The other end plate needs to have a ring shape having a hole in a central part thereof out of the need for avoiding the interference with the areas of rotation of the fixed shaft having the vanes and a vane shaft supporting member. Therefore, a portion that rotatably supports the end plate needs to have a larger diameter than the rotating shaft, leading to a problem of an increase in the loss due to sliding on bearings.
Moreover, since a small gap is provided between the rotor portion and the inner circumferential surface of the cylinder so as to prevent the leakage of a gas that has been compressed, the outside diameter and the center of rotation of the rotor portion need to be defined with high accuracy. Despite such circumstances, since the rotor portion and the end plates are provided as separate components, another problem arises in that the accuracy in the outside diameter and the center of rotation of the rotor portion may be deteriorated by any distortion, misalignment, or the like between the rotor portion and the end plates that may occur when they are connected to each other.
The present invention is to solve the above problems and to provide a vane compressor in which a vane is stably supported, the wear at the tip of the vane is suppressed, the loss due to sliding on bearings is reduced by supporting a rotating shaft portion with a small diameter, and the accuracy in the outside diameter and the center of rotation of a rotor portion is increased.
Solution to Problem
A vane compressor according to the present invention includes a compressing element that compresses a refrigerant. The compressing element includes a cylinder having a cylindrical inner circumferential surface; a rotor shaft provided in the cylinder and including a cylindrical rotor portion and a rotating shaft portion, the rotor portion being configured to rotate about an axis of rotation offset from a central axis of the inner circumferential surface by a predetermined distance, the rotating shaft portion being configured to transmit a rotational force from an outside to the rotor portion; a frame that closes one of openings defined by the inner circumferential surface of the cylinder and supports the rotating shaft portion by a main bearing portion thereof; a cylinder head that closes the other of the openings defined by the inner circumferential surface of the cylinder and supports the rotating shaft portion by a main bearing portion thereof; and at least one vane provided to the rotor portion and whose tip projects from the rotor portion and is shaped as an arc that is convex outward. The vane compressor further includes vane supporting means configured to support the vane such that the refrigerant is compressed in a space defined by the vane, an outer circumference of the rotor portion, and the inner circumferential surface of the cylinder and such that a line normal to the arc at the tip of the vane and a line normal to the inner circumferential surface of the cylinder always substantially coincide with each other, the vane supporting means being configured to support the vane such that the vane is rotatable and movable with respect to the rotor portion, the vane supporting means being configured to hold the vane such that a predetermined gap is provided between the tip of the vane and the inner circumferential surface of the cylinder in a state where the tip of the vane has moved by a maximum length toward the inner circumferential surface of the cylinder. The rotor shaft is an integral body including the rotor portion and the rotating shaft portion. An end facet of the vane that is close to an inner circumferential surface center, which is the center of the inner circumferential surface of the cylinder, is always positioned on an inner side of the rotor portion than a center of rotation of the vane that is rotatable with respect to the rotor portion.
Advantageous Effects of Invention
According to the present invention, providing a predetermined appropriate gap between the tip of the vane and the cylinder inner circumferential surface suppresses the leakage of the refrigerant at the tip, the reduction in the compressor efficiency due to an increase in the mechanical loss, and the wear of the tip. Furthermore, a mechanism that allows the vane necessary for performing the compressing operation to rotate about the center of the cylinder inner circumferential surface such that the line normal to the arc at the tip of the vane and the line normal to the cylinder inner circumferential surface always substantially coincide with each other is provided as an integral body including the rotor portion and the rotating shaft portion. Hence, the rotating shaft portion can be supported with a small diameter. Accordingly, the loss due to sliding on the bearings is reduced, the accuracy in the outside diameter and the center of rotation of the rotor portion is increased, and the loss due to leakage is reduced with a reduced gap provided between the rotor portion and the cylinder inner circumferential surface. Furthermore, since the end facet of the vane that is close to the inner circumferential surface center, which is the center of the inner circumferential surface of the cylinder, is always positioned on an inner side of the rotor portion than the center of rotation of the vane with respect to the rotor portion, the vane is allowed to stably rotate about the center of rotation thereof, whereby the vane is always stably supported.
BRIEF DESCRIPTION OF DRAWINGS
FIG. 1 is a vertical sectional view of a vane compressor 200 according to Embodiment 1 of the present invention.
FIG. 2 is an exploded perspective view of a compressing element 101 included in the vane compressor 200 according to Embodiment 1 of the present invention.
FIG. 3 includes a plan view and a front view each illustrating a first vane 5 and a second vane 6 included in the vane compressor 200 according to Embodiment 1 of the present invention.
FIG. 4 is a sectional view of the vane compressor 200 according to Embodiment 1 of the present invention that is taken along line I-I illustrated in FIG. 1.
FIG. 5 includes diagrams illustrating a compressing operation performed by the vane compressor 200 according to Embodiment 1 of the present invention.
FIG. 6 includes sectional views each taken along line J-J illustrated in FIG. 1 and illustrating rotational motions of vane aligner portions 5c and 6c included in the vane compressor 200 according to Embodiment 1 of the present invention.
FIG. 7 is a sectional view illustrating a vane portion 5a of the first vane 5 and associated elements included in the vane compressor 200 according to Embodiment 1 of the present invention.
FIG. 8 includes diagrams illustrating configurations and behaviors of a vane portion 6a and associated elements included in the vane compressor 200 according to Embodiment 1 of the present invention.
FIG. 9 includes a plan view and a front view illustrating a first vane 5 and a second vane 6 of a vane compressor 200 according to Embodiment 2 of the present invention.
FIG. 10 includes a plan view and a front view illustrating a modification of the first vane 5 and the second vane 6 of the vane compressor 200 according to Embodiment 2 of the present invention.
FIG. 11 is a plan view illustrating a first vane 5 or a second vane 6 of a vane compressor 200 according to Embodiment 3 of the present invention.
FIG. 12 includes diagrams illustrating a compressing operation performed by the vane compressor 200 according to Embodiment 3 of the present invention.
FIG. 13 is a sectional view of a vane compressor 200 according to Embodiment 4 of the present invention that is taken along line I-I illustrated in FIG. 1 and at “the angle of 0 degrees”.
FIG. 14 includes sectional views illustrating the vane portion 5a of the first vane 5 and associated elements included in the vane compressor 200 according to Embodiment 4 of the present invention at different angles of rotation established after the state illustrated in FIG. 13.
FIG. 15 includes a plan view and a vertical sectional view of a rotor shaft 4 included in the vane compressor 200 according to Embodiment 4 of the present invention.
FIG. 16 is a vertical sectional view illustrating a modification of the rotor shaft 4 included in the vane compressor 200 according to Embodiment 4 of the present invention.
DESCRIPTION OF EMBODIMENTS
Embodiment 1
Configuration of Vane Compressor 200
FIG. 1 is a vertical sectional view of a vane compressor 200 according to Embodiment 1 of the present invention. FIG. 2 is an exploded perspective view of a compressing element 101 included in the vane compressor 200. FIG. 3 includes a plan view and a front view each illustrating a first vane 5 and a second vane 6 included in the vane compressor 200. In FIG. 1, solid-line arrows represent the flow of a gas (refrigerant), and broken-line arrows represent the flow of a refrigerating machine oil 25. Referring to FIGS. 1 to 3, a configuration of the vane compressor 200 will now be described.
The vane compressor 200 according to Embodiment 1 includes a closed container 103 that defines the outer shape thereof, the compressing element 101 that is housed in the closed container 103, an motor element 102 that is provided above the compressing element 101 and drives the compressing element 101, and an oil reservoir 104 that is provided in and at the bottom of the closed container 103 and stores a refrigerating machine oil 25.
The closed container 103 defines the outer shape of the vane compressor 200 and houses the compressing element 101 and the motor element 102 thereinside. The closed container 103 stores the refrigerant and the refrigerating machine oil in a hermetical manner. A suction pipe 26 via which the refrigerant is sucked into the closed container 103 is provided on a side face of the closed container 103. A discharge pipe 24 via which the refrigerant that has been compressed is discharged to the outside is provided on the top face of the closed container 103.
The compressing element 101 compresses the refrigerant that has been sucked into the closed container 103 via the suction pipe 26 and includes a cylinder 1, a frame 2, a cylinder head 3, a rotor shaft 4, the first vane 5, the second vane 6, and bushes 7 and 8.
The cylinder 1 has a substantially cylindrical shape in its entirety and has a through portion 1f having a substantially circular shape and being axially eccentric in the axial direction with respect to a circle defined by the cylindrical shape. A part of a cylinder inner circumferential surface 1b forming the inner circumferential surface that defines the through portion 1f is recessed in a direction from the center of the through portion 1f toward the outer side and in a curved shape, whereby a notch 1c is provided. The notch 1c has a suction port 1a. The suction port 1a communicates with the suction pipe 26. The refrigerant is sucked into the through portion 1f via the suction port 1a. A discharge port 1d in the form of a notch is provided across a closest point 32, to be described below, from the suction port 1a and close to the closest point 32. The discharge port 1d is provided on a side facing the frame 2, to be described below (see FIG. 2). The cylinder 1 has two oil return holes 1e provided in an outer periphery thereof and extending therethrough in the axial direction. The oil return holes 1e are provided at respective positions that are symmetrical to each other with respect to the center of the through portion 1f.
The frame 2 has a substantially T-shaped vertical section. A part of the frame 2 that is in contact with the cylinder 1 has a substantially disc-like shape. The frame 2 closes one of the openings (the upper one in FIG. 2) at the through portion 1f provided in the cylinder 1. The frame 2 has a cylindrical portion in a central part thereof. The cylindrical portion is hollow, thereby forming a main bearing portion 2c. A recess 2a is provided in an end facet of the frame 2 that is close to the cylinder 1 and in a part corresponding to the main bearing portion 2c. The outer circumferential surface of the recess 2a is concentric with respect to the cylinder inner circumferential surface 1b. A vane aligner portion 5c of the first vane 5 and a vane aligner portion 6c of the second vane 6, to be described below, are fitted in the recess 2a. The vane aligner portions 5c and 6c are supported by a vane aligner bearing portion 2b provided by the outer circumferential surface of the recess 2a. The frame 2 also has a discharge port 2d communicating with the discharge port 1d provided in the cylinder 1 and extending through the frame 2 in the axial direction. A discharge valve 27 and a discharge valve stopper 28 that regulates the opening degree of the discharge valve 27 are attached to one of the openings at the discharge port 2d that is farther from the cylinder 1.
The cylinder head 3 has a substantially T-shaped vertical section. A part of the cylinder head 3 that is in contact with the cylinder 1 has a substantially disc-like shape. The cylinder head 3 closes the other one of the openings (the lower one in FIG. 2) at the through portion 1f of the cylinder 1. The cylinder head 3 has a cylindrical portion in a central part thereof. The cylindrical portion is hollow, thereby forming a main bearing portion 3c. A recess 3a is provided in an end facet of the cylinder head 3 that is close to the cylinder 1 and in a part corresponding to the main bearing portion 3c. The outer circumferential surface of the recess 3a is concentric with respect to the cylinder inner circumferential surface 1b. A vane aligner portion 5d of the first vane 5 and a vane aligner portion 6d of the second vane 6, to be described below, are fitted in the recess 3a. The vane aligner portions 5d and 6d are supported by a vane aligner bearing portion 3b formed by the outer circumferential surface of the recess 3a.
The rotor shaft 4 is an integral body including a substantially cylindrical rotor portion 4a that is provided in the cylinder 1 and undergoes a rotational motion about a central axis that is eccentric with respect to the central axis of the through portion 1f of the cylinder 1, a rotating shaft portion 4b that extends perpendicularly upward from the center of a circular upper surface of the rotor portion 4a, and a rotating shaft portion 4c that extends perpendicularly downward from the center of a circular lower surface of the rotor portion 4a. The rotating shaft portion 4b extends through and is supported by the main bearing portion 2c of the frame 2. The rotating shaft portion 4c extends through and is supported by the main bearing portion 3c of the cylinder head 3. The rotor portion 4a includes bush holding portions 4d and 4e and vane relief portions 4f and 4g each extending through the rotor portion 4a, having a cylindrical shape, in the axial direction of the rotor portion 4a and having a substantially circular cross-sectional shape in a direction perpendicular to the axial direction. The bush holding portions 4d and 4e are provided at respective positions that are symmetrical to each other with respect to the center of the rotor portion 4a. The vane relief portions 4f and 4g are provided on the outer side of the respective bush holding portions 4d and 4e. That is, the centers of the rotor portion 4a, the bush holding portions 4d and 4e, and the vane relief portions 4f and 4g are aligned substantially linearly. Furthermore, the bush holding portion 4d and the vane relief portion 4f communicate with each other, and the bush holding portion 4e and the vane relief portion 4g communicate with each other. Furthermore, the axial ends of each of the vane relief portions 4f and 4g communicate with the recess 2a of the frame 2 and the recess 3a of the cylinder head 3, respectively. Furthermore, an oil pump 31 that utilizes the centrifugal force of the rotor shaft 4, such as that disclosed by, for example, Japanese Unexamined Patent Application Publication No. 2009-62820, is provided at the lower end of the rotating shaft portion 4c of the rotor shaft 4. The oil pump 31 at the lower end of the rotating shaft portion 4c resides in an axially central part of the rotating shaft portion 4c of the rotor shaft 4 and communicates with an oil supply path 4h extending upward from the lower end of the rotating shaft portion 4c through the rotor portion 4a up to a position in the rotating shaft portion 4b. The rotating shaft portion 4b has an oil supply path 4i that allows the oil supply path 4h and the recess 2a to communicate with each other. The rotating shaft portion 4c has an oil supply path 4j that allows the oil supply path 4h and the recess 3a to communicate with each other. Furthermore, the rotating shaft portion 4b has an oil discharge hole 4k at a position thereof above the main bearing portion 2c. The oil discharge hole 4k communicates with the internal space of the closed container 103.
The first vane 5 includes a vane portion 5a that is a substantially rectangular plate-like member; the vane aligner portion 5c provided on the upper end facet of the vane portion 5a that is close to the frame 2 and the rotating shaft portion 4b, the vane aligner portion 5c having an arc shape, that is, shaped as a part of a ring; and the vane aligner portion 5d provided on the lower end facet of the vane portion 5a that is close to the cylinder head 3 and the rotating shaft portion 4c, the vane aligner portion 5d having an arc shape, that is, shaped as a part of a ring. A vane tip 5b as an end facet of the vane portion 5a that is close to the cylinder inner circumferential surface 1b has an arc shape that is convex outward. The radius of curvature of the arc is substantially the same as the radius of curvature of the cylinder inner circumferential surface 1b. As illustrated in FIG. 3, the first vane 5 is configured such that the longitudinal direction of the vane portion 5a and the direction of normal line to the arc at the vane tip 5b pass through the center of the arc defined by each of the vane aligner portions 5c and 5d.
The second vane 6 includes a vane portion 6a that is a substantially rectangular plate-like member; the vane aligner portion 6c provided on the upper end facet of the vane portion 6a that is close to the frame 2 and the rotating shaft portion 4b, the vane aligner portion 6c having an arc shape, that is, shaped as a part of a ring; and the vane aligner portion 6d provided on the lower end facet of the vane portion 6a that is close to the cylinder head 3 and the rotating shaft portion 4c, the vane aligner portion 6d having an arc shape, that is, shaped as a part of a ring. A vane tip 6b as an end facet of the vane portion 6a that is close to the cylinder inner circumferential surface 1b has an arc shape that is convex outward. The radius of curvature of the arc is substantially the same as the radius of curvature of the cylinder inner circumferential surface 1b. As illustrated in FIG. 3, the second vane 6 is configured such that the longitudinal direction of the vane portion 6a and the direction of normal line to the arc at the vane tip 6b pass through the center of the arc defined by each of the vane aligner portions 6c and 6d.
The bushes 7 and 8 each include a pair of members each having a substantially semicircular columnar shape. The bush 7 is fitted in the bush holding portion 4d of the rotor shaft 4. The vane portion 5a having a plate-like shape is held between the pair of members of the bush 7. In this state, the vane portion 5a is held in such a manner as to be rotatable with respect to the rotor portion 4a and movable in the longitudinal direction of the vane portion 5a. The bush 8 is fitted in the bush holding portion 4e of the rotor shaft 4. The vane portion 6a having a plate-like shape is held between the pair of members of the bush 8. In this state, the vane portion 6a is held in such a manner as to be rotatable with respect to the rotor portion 4a and movable in the longitudinal direction of the vane portion 6a.
The bush holding portions 4d and 4e, the vane relief portions 4f and 4g, the bushes 7 and 8, and the vane aligner bearing portions 2b and 3b correspond to “vane supporting means” according to the present invention.
The motor element 102 is, for example, a brushless DC motor and includes, as illustrated in FIG. 1, a stator 21 fixed to the inner circumference of the closed container 103, and a rotor 22 provided on the inner side of the stator 21 and including permanent magnets. The stator 21 receives electric power from a glass terminal 23 fixed to the upper surface of the closed container 103. The electric power drives the rotor 22 to rotate. The rotating shaft portion 4b of the rotor shaft 4 extends through and is fixed to the rotor 22. When the rotor 22 rotates, a rotational force of the rotor 22 is transmitted to the rotating shaft portion 4b, whereby the entirety of the rotor shaft 4 rotates.
Compressing Operation of Vane Compressor 200
FIG. 4 is a sectional view of the vane compressor 200 according to Embodiment 1 of the present invention that is taken along line I-I illustrated in FIG. 1. FIG. 5 includes diagrams illustrating a compressing operation performed by the vane compressor 200. Referring to FIGS. 4 and 5, the compressing operation performed by the vane compressor 200 will now be described.
FIG. 5 illustrates states in each of which the rotor portion 4a of the rotor shaft 4 resides closest to a position (the closest point 32) on the cylinder inner circumferential surface 1b. With the radius of each of the vane aligner bearing portions 2b and 3b labeled as ra (see FIG. 6 to be referred to below) and the radius of the cylinder inner circumferential surface 1b being labeled as rc (see FIG. 4), a distance rv (see FIG. 3) between the outer circumferential side of each of the vane aligner portions 5c and 5d of the first vane 5 and the vane tip 5b is expressed by Expression (1) below.
rv=rc−ra−δ (1)
Here, δ denotes the gap between the vane tip 5b and the cylinder inner circumferential surface 1b. If rv is set as in Expression (1), the first vane 5 rotates with the vane tip 5b thereof being out of contact with the cylinder inner circumferential surface 1b. If rv is set such that δ is minimized, the leakage of the refrigerant at the vane tip 5b is minimized. The relationship expressed by Expression (1) also applies to the second vane 6. That is, the second vane 6 rotates while a small gap is provided between the vane tip 6b of the second vane 6 and the cylinder inner circumferential surface 1b.
In the above configuration, the closest point 32 where the rotor portion 4a resides closest to the cylinder inner circumferential surface 1b, the vane tip 5b of the first vane 5, and the vane tip 6b of the second vane 6 define three spaces (a suction chamber 9, an intermediate chamber 10, and a compression chamber 11) in the through portion 1f of the cylinder 1. The refrigerant that is sucked from the suction pipe 26 via the suction port 1a provided in the notch 1c flows into the suction chamber 9. As illustrated in FIG. 4 (the angular position of the rotor shaft 4 illustrated in FIG. 4 is defined as 90 degrees), the notch 1c extends from a position close to the closest point 32 to a position corresponding to a close to point A where the vane tip 5b of the first vane 5 and the cylinder inner circumferential surface 1b are close to each other. The compression chamber 11 communicates with the discharge port 2d, provided in the frame 2, via the discharge port 1d of the cylinder 1. The discharge port 2d is closed by the discharge valve 27 when the refrigerant is not discharged. Hence, the intermediate chamber 10 is a space that communicates with the suction port 1a at an angle of rotation of up to 90 degrees but does not communicate with either the suction port 1a or the discharge port 1d at an angle of rotation of over 90 degrees. At an angle of rotation of over 90 degrees, the intermediate chamber 10 communicates with the discharge port 1d and serves as the compression chamber 11. In FIG. 4, bush centers 7a and 8a are the centers of rotation of the respective bushes 7 and 8 and are also the centers of rotation of the respective vane portions 5a and 6a.
Now, a rotational motion of the rotor shaft 4 of the vane compressor 200 will be described.
The rotating shaft portion 4b of the rotor shaft 4 receives a rotational force from the rotor 22 of the motor element 102, whereby the rotor portion 4a rotates in the through portion 1f of the cylinder 1. With the rotation of the rotor portion 4a, the bush holding portions 4d and 4e of the rotor portion 4a move on the circumference of a circle that is centered on the center of the rotor shaft 4. Meanwhile, the pair of members included in each of the bushes 7 and 8 that are held by a corresponding one of the bush holding portions 4d and 4e, and each of the vane portion 5a of the first vane 5 and the vane portion 6a of the second vane 6 that is rotatably held between the pair of members included in a corresponding one of the bushes 7 and 8 also rotate with the rotation of the rotor portion 4a. The first vane 5 and the second vane 6 receive a centrifugal force produced by the rotation of the rotor portion 4a, whereby the vane aligner portions 5c and 6c and the vane aligner portions 5d and 6d are pressed against and slide along the respective vane aligner bearing portions 2b and 3b while rotating about the centers of the respective vane aligner bearing portions 2b and 3b. Here, since the vane aligner bearing portions 2b and 3b are concentric with respect to the cylinder inner circumferential surface 1b, the first vane 5 and the second vane 6 rotate about the center of the cylinder inner circumferential surface 1b. In such a case, the bushes 7 and 8 rotate about the respective bush centers 7a and 8a in the respective bush holding portions 4d and 4e such that the longitudinal direction of each of the vane portion 5a of the first vane 5 and the vane portion 6a of the second vane 6 passes through the center of the cylinder inner circumferential surface 1b. That is, the rotor portion 4a rotates in a state where the line normal to the arc at each of the vane tips 5b and 6b and the line normal to the cylinder inner circumferential surface 1b always substantially coincide with each other.
In the above motion, the bush 7 and the vane portion 5a of the first vane 5 slide on each other by side faces thereof, and the bush 8 and the vane portion 6a of the second vane 6 slide on each other by side faces thereof. Furthermore, the bush holding portion 4d of the rotor shaft 4 and the bush 7 slide on each other, and the bush holding portion 4e of the rotor shaft 4 and the bush 8 slide on each other.
Referring now to FIG. 5, how the capacities of the suction chamber 9, the intermediate chamber 10, and the compression chamber 11 change will be described. In FIG. 5, for easier illustration, the suction port 1a, the notch 1c, and the discharge port 1d are not illustrated. Instead, the suction port 1a and the discharge port 1d are represented by arrows denoted by “suction” and “discharge”, respectively. First, with the rotation of the rotor shaft 4, a low-pressure gas refrigerant flows into the suction port 1a from the suction pipe 26. Here, in FIG. 5, the angle of rotation at which the closest point 32 where the rotor portion 4a of the rotor shaft 4 and the cylinder inner circumferential surface 1b are closest to each other coincides with a position where the vane portion 5a and the cylinder inner circumferential surface 1b face each other is defined as “the angle of 0 degrees”. FIG. 5 illustrates the positions of the vane portion 5a and the vane portion 6a and the states of the suction chamber 9, the intermediate chamber 10, and the compression chamber 11 at “the angle of 0 degrees”, at “the angle of 45 degrees”, at “the angle of 90 degrees”, and at “the angle of 135 degrees”. In the diagram included in FIG. 5 that illustrates the state at “the angle of 0 degrees”, the direction of rotation of the rotor shaft 4 (the clockwise direction in FIG. 5) is represented by an arrow. In the other diagrams included in FIG. 5 that illustrate the states at the other angles, the arrow representing the direction of rotation of the rotor shaft 4 is omitted. States at “the angle of 180 degrees” and larger angles are not illustrated because a state that is the same as that at “the angle of 0 degrees” is established at “the angle of 180 degrees” with the first vane 5 and the second vane 6 being interchanged with each other, and, thereafter, the compression operation progresses in the same manner as for the transition from “the angle of 0 degrees” to “the angle of 135 degrees”.
At “the angle of 0 degrees” illustrated in FIG. 5, the right one of the spaces defined between the closest point 32 and the vane portion 6a of the second vane 6 is the intermediate chamber 10, which communicates with the suction port 1a via the notch 1c and into which the gas refrigerant is sucked. The left one of the spaces defined between the closest point 32 and the vane portion 6a of the second vane 6 is the compression chamber 11, which communicates with the discharge port 1d.
At “the angle of 45 degrees” illustrated in FIG. 5, a space defined between the vane portion 5a of the first vane 5 and the closest point 32 is the suction chamber 9. The intermediate chamber 10 defined between the vane portion 5a of the first vane 5 and the vane portion 6a of the second vane 6 communicates with the suction port 1a via the notch 1c and has a capacity increased from that at “the angle of 0 degrees”. Therefore, the suction of the gas refrigerant continues. A space defined between the vane portion 6a of the second vane 6 and the closest point 32 is the compression chamber 11. The capacity of the compression chamber 11 is reduced from that at “the angle of 0 degrees”. Therefore, the gas refrigerant is compressed, and the pressure thereof gradually increases.
At “the angle of 90 degrees” illustrated in FIG. 5, since the vane tip 5b of the first vane 5 reaches the close to point A on the cylinder inner circumferential surface 1b, the intermediate chamber 10 loses communication with the suction port 1a. Therefore, the suction of the gas refrigerant into the intermediate chamber 10 ends. In this state, the capacity of the intermediate chamber 10 is substantially largest. The capacity of the compression chamber 11 is further reduced from that at “the angle of 45 degrees”, and the pressure of the gas refrigerant increases. The capacity of the suction chamber 9 is increased from that at “the angle of 45 degrees”. Therefore, the suction chamber 9 communicates with the suction port 1a via the notch 1c, and the gas refrigerant is sucked thereinto.
At “the angle of 135 degrees” illustrated in FIG. 5, the capacity of the intermediate chamber 10 is reduced from that at “the angle of 90 degrees”, and the pressure of the refrigerant increases. The capacity of the compression chamber 11 is also reduced from that at “the angle of 90 degrees”, and the pressure of the refrigerant increases. The capacity of the suction chamber 9 is increased from that at “the angle of 90 degrees”. Therefore, the suction of the gas refrigerant continues.
Subsequently, the vane portion 6a of the second vane 6 comes close to the discharge port 1d. When the pressure of the gas refrigerant in the compression chamber 11 exceeds a high pressure in a refrigeration cycle (including a pressure required for opening the discharge valve 27), the discharge valve 27 opens. Then, the gas refrigerant in the compression chamber 11 flows into the discharge port 1d and the discharge port 2d and is discharged into the closed container 103 as illustrated in FIG. 1. The gas refrigerant discharged into the closed container 103 flows through the motor element 102, the discharge pipe 24 fixed to the upper portion of the closed container 103, and is discharged to the outside (to a high-pressure side of the refrigeration cycle). Accordingly, the inside of the closed container 103 is at a high pressure corresponding to a discharge pressure.
After the vane portion 6a of the second vane 6 passes the discharge port 1d, a small amount of high-pressure gas refrigerant remains (as a loss) in the compression chamber 11. When the compression chamber 11 disappears at “the angle of 180 degrees” (not illustrated), the high-pressure gas refrigerant turns into a low-pressure gas refrigerant in the suction chamber 9. At “the angle of 180 degrees”, the suction chamber 9 turns into the intermediate chamber 10, and the intermediate chamber 10 turns into the compression chamber 11. Subsequently, the above compressing operation is repeated.
With the rotation of the rotor portion 4a of the rotor shaft 4, the capacity of the suction chamber 9 gradually increases. Therefore, the suction of the gas refrigerant continues. Subsequently, the suction chamber 9 turns into the intermediate chamber 10. Before that (before the vane portion (the vane portion 5a or the vane portion 6a) that separates the suction chamber 9 and the intermediate chamber 10 from each other reaches the close to point A), the capacity of the suction chamber 9 gradually increases, and the suction of the gas refrigerant continues further. In this process, the capacity of the intermediate chamber 10 becomes largest, and the intermediate chamber 10 goes out of communication with the suction port 1a, whereby the suction of the gas refrigerant ends. Subsequently, the capacity of the intermediate chamber 10 is gradually reduced, whereby the gas refrigerant is compressed. Subsequently, the intermediate chamber 10 turns into the compression chamber 11, and the compression of the gas refrigerant continues. The gas refrigerant that has been compressed to a predetermined pressure flows through the discharge port 1d and the discharge port 2d, pushes up the discharge valve 27, and is discharged into the closed container 103.
FIG. 6 includes sectional views each taken along line J-J illustrated in FIG. 1 and illustrating the rotational motion of the vane aligner portions 5c and 6c included in the vane compressor 200 according to Embodiment 1 of the present invention.
In the diagram included in FIG. 6 that illustrates “the angle of 0 degrees”, the direction of rotation of the vane aligner portions 5c and 6c (the clockwise direction in FIG. 6) is represented by an arrow. In the other diagrams included in FIG. 6 that illustrate the other angles, the arrow representing the direction of rotation of the vane aligner portions 5c and 6c is omitted. With the rotation of the rotor shaft 4, the vane portion 5a of the first vane 5 and the vane portion 6a of the second vane 6 rotate about the center of the cylinder inner circumferential surface 1b. Hence, as illustrated in FIG. 6, the vane aligner portions 5c and 6c supported by the vane aligner bearing portion 2b rotate in the recess 2a about the center of the cylinder inner circumferential surface 1b. Likewise, the vane aligner portions 5d and 6d supported by the vane aligner bearing portion 3b rotate in the recess 3a about the center of the cylinder inner circumferential surface 1b.
Behavior of Refrigerating Machine Oil 25
In the above motion, referring to FIG. 1, when the rotor shaft 4 rotates, the refrigerating machine oil 25 is sucked from the oil reservoir 104 by the oil pump 31 and is fed into the oil supply path 4h. The refrigerating machine oil 25 that has been fed into the oil supply path 4h is fed into the recess 2a of the frame 2 via the oil supply path 4i and into the recess 3a of the cylinder head 3 via the oil supply path 4j. The refrigerating machine oil 25 that has been fed into the recesses 2a and 3a lubricates the vane aligner bearing portions 2b and 3b and is supplied into the vane relief portions 4f and 4g that communicate with the recesses 2a and 3a. In this step, the inside of the closed container 103 is at a high pressure corresponding to the discharge pressure. Accordingly, the insides of the recesses 2a and 3a and in the vane relief portions 4f and 4g are also at the discharge pressure. Portions of the refrigerating machine oil 25 that have been fed into the recesses 2a and 3a are supplied to and lubricate the main bearing portion 2c of the frame 2 and the main bearing portion 3c of the cylinder head 3, respectively.
FIG. 7 is a sectional view illustrating principal portions of the vane portion 5a of the first vane 5 and associated elements included in the vane compressor 200 according to Embodiment 1 of the present invention.
In FIG. 7, the solid-line arrows represent the flow of the refrigerating machine oil 25. The inside of the vane relief portion 4f is at the discharge pressure that is higher than the pressures in the suction chamber 9 and the intermediate chamber 10. Therefore, the pressure difference and the centrifugal force cause the refrigerating machine oil 25 to be fed into the suction chamber 9 and the intermediate chamber 10 while lubricating sliding portions between the bush 7 and the side faces of the vane portion 5a. The pressure difference and the centrifugal force cause the refrigerating machine oil 25 to also lubricate sliding portions between the bush 7 and the bush holding portion 4d of the rotor shaft 4 while being fed into the suction chamber 9 and the intermediate chamber 10. A portion of the refrigerating machine oil 25 that has been fed into the intermediate chamber 10 flows into the suction chamber 9 while sealing the gap between the vane tip 5b and the cylinder inner circumferential surface 1b.
While the above description concerns a situation where the vane portion 5a of the first vane 5 separates the suction chamber 9 and the intermediate chamber 10 from each other, the same applies to a situation established with further rotation of the rotor shaft 4 where the vane portion 5a of the first vane 5 separates the intermediate chamber 10 and the compression chamber 11 from each other. That is, even in a case where the pressure in the compression chamber 11 has reached the discharge pressure that is the same as the pressure in the vane relief portion 4f, the refrigerating machine oil 25 is fed toward the compression chamber 11 with the centrifugal force.
While the above description concerns the motion of the first vane 5, the same applies to the second vane 6.
As illustrated in FIG. 1, the portion of the refrigerating machine oil 25 that has been supplied to the main bearing portion 2c flows through the gap between the main bearing portion 2c and the rotating shaft portion 4b and is discharged into the space above the frame 2. Subsequently, the refrigerating machine oil 25 flows through the oil return holes 1e provided in the outer periphery of the cylinder 1 and is fed back to the oil reservoir 104. Meanwhile, the portion of the refrigerating machine oil 25 that has been supplied to the main bearing portion 3c flows through the gap between the main bearing portion 3c and the rotating shaft portion 4c and is fed back to the oil reservoir 104. Furthermore, the portions of the refrigerating machine oil 25 that have been fed into the suction chamber 9, the intermediate chamber 10, and the compression chamber 11 via the vane relief portions 4f and 4g are eventually discharged into the space above the frame 2 via the discharge port 2d together with the gas refrigerant and are fed back to the oil reservoir 104 via the oil return holes 1e provided in the outer periphery of the cylinder 1. In the refrigerating machine oil 25 that has been fed into the oil supply path 4h by the oil pump 31, an excessive portion of the refrigerating machine oil 25 is discharged into the space above the frame 2 via the oil discharge hole 4k provided at an upper position of the rotor shaft 4, and is fed back to the oil reservoir 104 via the oil return holes 1e provided in the outer periphery of the cylinder 1.
Configurations and Behaviors of Vane Portions 5a and 6a and Bushes 7 and 8
FIG. 8 includes diagrams illustrating configurations and behaviors of the vane portion 6a and associated elements included in the vane compressor 200 according to Embodiment 1 of the present invention. FIG. 8 illustrates loads acting on the bush 8 that holds the vane portion 6a of the second vane 6 and in the state of “the angle of 0 degrees”. FIG. 8(a) illustrates the configuration of the vane portion 6a and associated elements included in the vane compressor 200 according to Embodiment 1. FIG. 8(b) illustrates a case where an end of the vane portion 6a that is close to the center of the cylinder inner circumferential surface 1b (hereinafter simply referred to as “the inner circumferential surface center”) resides on the outer side with respect to the bush center 8a.
First, a behavior of the second vane 6 of the second vane 6 according to Embodiment 1 will be described with reference to FIG. 8(a).
As illustrated in FIG. 8(a), a load represented by an arrow 41 (a direction from the compression chamber 11 toward the intermediate chamber 10) produced by the pressure difference between the compression chamber 11 and the intermediate chamber 10 acts on the vane portion 6a of the second vane 6. The load represented by the arrow 41 urges the vane portion 6a to rotate counterclockwise in FIG. 8(a). Hence, a part of a sliding surface of the right one of the members included in the bush 8 that is on a side farther from the inner circumferential surface center and a part of the right side face of the vane portion 6a that is on the outer side with respect to the bush center 8a come into contact with each other. Therefore, a load in a direction represented by an arrow 42 (a direction in which the bush 8 rotates counterclockwise about the bush center 8a) acts on the bush 8. Furthermore, a part of a sliding surface of the left one of the members included in the bush 8 that is on a side close to the inner circumferential surface center and a part of the left side face of the vane portion 6a that is on the inner side with respect to the bush center 8a come into contact with each other. Therefore, a load in a direction represented by an arrow 43 (the direction in which the bush 8 rotates counterclockwise about the bush center 8a) acts on the bush 8. In this case, the bush 8 receives a moment 44 produced by the load represented by the arrow 42 and acting about the bush center 8a and a moment 45 produced by the load represented by the arrow 43 and acting about the bush center 8a. This enables the bush 8 to stably rotate about the bush center 8a.
Referring now to FIG. 8(b), a behavior of the vane portion 6a in a case where the end of the vane portion 6a that is close to the inner circumferential surface center resides on the outer side with respect to the bush center 8a will be described.
In FIG. 8(b) also, the pressure difference between the compression chamber 11 and the intermediate chamber 10 produces a load represented by the arrow 41 (in the direction from the compression chamber 11 toward the intermediate chamber 10) that acts on the vane portion 6a of the second vane 6. The load represented by the arrow 41 urges the vane portion 6a to rotate counterclockwise in FIG. 8(b). Hence, a part of the sliding surface of the right one of the members included in the bush 8 that is on the side farther from the inner circumferential surface center and a part of the right side face of the vane portion 6a that is on the outer side with respect to the bush center 8a come into contact with each other. Therefore, a load in the direction represented by the arrow 42 (the direction in which the bush 8 rotates counterclockwise about the bush center 8a) acts on the bush 8. Furthermore, a part of the sliding surface of the left one of the members included in the bush 8 that is on the side farther from the inner circumferential surface center and a part of the left side face of the vane portion 6a that is on the outer side with respect to the bush center 8a come into contact with each other. Therefore, a load in the direction represented by the arrow 43 (a direction in which the bush 8 rotates clockwise about the bush center 8a) acts on the bush 8. In this case, a moment 44 produced about the bush center 8a by the load represented by the arrow 42 acts counterclockwise, whereas a moment 45 produced about the bush center 8a by the load represented by the arrow 43 acts clockwise. Therefore, it is difficult for the bush 8 to stably rotate about the bush center 8a.
Hence, to allow the bush 8 to stably rotate about the bush center 8a, the end of the vane portion 6a that is close to the inner circumferential surface center needs to be always positioned on the inner side with respect to the bush center 8a as illustrated in FIG. 8(a). The end of the vane portion 6a that is close to the inner circumferential surface center is positioned closest to the bush center 8a in the state illustrated in FIG. 8 (the state at “the angle of 0 degrees”). Therefore, the end of the vane portion 6a that is close to the inside diameter center of the vane portion 6a only needs to be positioned on the inner side with respect to the bush center 8a in that state.
While the configurations and behaviors of the vane portion 6a of the second vane 6 and the bush 8 have been described referring to FIG. 8, the same applies to the vane portion 5a of the first vane 5 and the bush 7. An end of the vane portion 5a that is close to the inner circumferential surface center needs to be always positioned on the inner side with respect to the bush center 7a.
While the end of the vane portion 6a of the second vane 6 that is close to the inner circumferential surface center does not project toward the inner side with respect to an end of the bush 8 that is close to the inner circumferential surface center as illustrated in FIG. 8(a), the present invention is not limited to such a case. Needless to say, the end of the vane portion 6a that is close to the inner circumferential surface center may project toward the inner side with respect to the end of the bush 8 that is close to the inner circumferential surface center. However, to reduce the outside diameter of the rotor portion 4a for a reduction in the diameter of the vane compressor 200, it is desirable to minimize the distance between the bush center 8a and the end of the vane portion 6a of the second vane 6 that is close to the inner circumferential surface center. That is, at “the angle of 0 degrees”, if the end of the vane portion 6a of the second vane 6 that is close to the inner circumferential surface center does not project toward the inner side with respect to the end of the bush 8 that is close to the inner circumferential surface center as illustrated in FIG. 8(a), the outside diameter of the rotor portion 4a can be made much smaller, realizing a reduction in the diameter of the vane compressor 200.
Advantageous Effects of Embodiment 1
As described above, providing a predetermined appropriate gap δ between the cylinder inner circumferential surface 1b and each of the vane tips 5b and 6b such that the relationship of Expression (1) given above holds suppresses the leakage of the refrigerant at the vane tips 5b and 6b, the reduction in the compressor efficiency due to an increase in the mechanical loss, and the wear of the vane tips 5b and 6b.
Furthermore, since the radius of curvature of the arc at each of the vane tip 5b of the first vane 5 and the vane tip 6b of the second vane 6 is substantially the same as the radius of curvature of the cylinder inner circumferential surface 1b, a state of hydrodynamic lubrication is produced between the cylinder inner circumferential surface 1b and each of the vane tips 5b and 6b, whereby the sliding resistance is reduced, and the mechanical loss is thus reduced.
Furthermore, a mechanism that allows the vanes (the first vane 5 and the second vane 6) necessary for performing the compressing operation to rotate about the center of the cylinder inner circumferential surface 1b such that the line normal to the arc at each of the vane tips 5b and 6b and the line normal to the cylinder inner circumferential surface 1b always substantially coincide with each other is provided as an integral body including the rotor portion 4a and the rotating shaft portions 4b and 4c. Hence, the rotating shaft portions 4b and 4c can be each supported with a small diameter. Accordingly, the loss due to sliding on the bearings is reduced, the accuracy in the outside diameter and the center of rotation of the rotor portion 4a is increased, and the loss due to leakage is reduced with a reduced gap provided between the rotor portion 4a and the cylinder inner circumferential surface 1b.
Furthermore, since the end of each of the vane portions 5a and 6a that is close to the inner circumferential surface center is always positioned on the inner side with respect to a corresponding one of the bush centers 7a and 8a, the bushes 7 and 8 stably rotate about the respective bush centers 7a and 8a, whereby the vane portions 5a and 6a are always stably supported. In this case, at an angle of rotation of the rotor portion 4a at which the end of each of the vane portions 5a and 6a that is close to the inner circumferential surface center resides closest to a corresponding one of the bush centers 7a and 8a, if the end of each of the vane portions 5a and 6a that is close to the inner circumferential surface center does not project toward the inner side with respect to the end of a corresponding one of the bushes 7 and 8 that is close to the inner circumferential surface center, the outside diameter of the rotor portion 4a can be reduced, whereby the size of the vane compressor 200 can be reduced.
While Embodiment 1 concerns a case where two vanes, which are the first vane 5 and the second vane 6, are provided to the rotor portion 4a of the rotor shaft 4, the present invention is not limited to such a case. One vane or three or more vanes may be provided.
Furthermore, while the vane relief portions 4f and 4g each have a substantially circular cross-sectional shape as illustrated in FIGS. 4, 7, and 8, the present invention is not limited to such a case. The vane relief portions 4f and 4g may each have any shape (for example, an oblong shape or a rectangular shape) as long as the vane portions 5a and 6a are out of contact with the inner circumferential surfaces of the respective vane relief portions 4f and 4g.
Furthermore, while FIG. 1 illustrates a configuration in which the frame 2 and the cylinder head 3 have the respective recesses 2a and 3a whose outer circumferential surfaces form the respective vane aligner bearing portions 2b and 3b that are concentric with respect to the cylinder inner circumferential surface 1b, the present invention is not limited to such a case. That is, the recesses 2a and 3a may each have any shape as long as the vane aligner bearing portions 2b and 3b are concentric with respect to the cylinder inner circumferential surface 1b and the vane aligner portions 5c, 6c, 5d, and 6d are fittable into the recesses 2a and 3a. For example, the recesses 2a and 3a may be ring-shaped grooves into which the vane aligner portions 5c, 6c, 5d, and 6d are fittable.
Embodiment 2
A vane compressor 200 according to Embodiment 2 will now be described, focusing on differences from the vane compressor 200 according to Embodiment 1.
Configurations of First Vane 5 and Second Vane 6
FIG. 9 includes a plan view and a front view illustrating a first vane 5 and a second vane 6 of the vane compressor 200 according to Embodiment 2 of the present invention.
As illustrated in FIG. 9, the end of each of a vane portion 5a of the first vane 5 and a vane portion 6a of the second vane 6 that is close to the inner circumferential surface center projects toward the inner circumferential surface center with respect to the inner sides of the vane aligner portions 5c and 5d or the vane aligner portions 6c and 6d. Thus, the end of each of the vane portions 5a and 6a that is close to the inner circumferential surface center project more toward the inner circumferential surface center than in Embodiment 1. Consequently, the outer size of the rotor portion 4a can be made smaller than in Embodiment 1, realizing a reduction in the size of the vane compressor 200.
FIG. 10 includes a plan view and a front view illustrating a modification of the first vane 5 and the second vane 6 of the vane compressor 200 according to Embodiment 2 of the present invention.
As illustrated in FIG. 10, the vane portion 5a of the first vane 5 and the vane portion 6a of the second vane 6 include respective vane inward projections 5e and 6e each projecting from a part of an end facet of the vane portion 5a or 6a that is close to the inner circumferential surface center toward the inner circumferential surface center with respect to the inner sides of the vane aligner portions 5c and 5d or the vane aligner portions 6c and 6d. In such a configuration, even if the end of each of the vane portions 5a and 6a that is close to the inner circumferential surface center does not project toward the inner side with respect to the bush center 7a or 8a during the rotation of the rotor portion 4a, the vane inward projection 5e or 6e is always positioned on the inner side with respect to the bush center 7a or 8a. Hence, the bushes 7 and 8 are allowed to stably rotate about the respective bush centers 7a and 8a and to always stably support the respective vane portions 5a and 6a, producing substantially the same effects as in the case illustrated in FIG. 9.
Advantageous Effects of Embodiment 2
In the above configuration, the outer size of the rotor portion 4a can be made smaller than in Embodiment 1, realizing a reduction in the size of the vane compressor 200.
Embodiment 3
A vane compressor 200 according to Embodiment 3 will now be described, focusing on differences from the vane compressor 200 according to Embodiment 1.
Configuration of Vane Compressor 200
FIG. 11 is a plan view illustrating a first vane 5 or a second vane 6 of the vane compressor 200 according to Embodiment 3 of the present invention. FIG. 12 includes diagrams illustrating a compressing operation performed by the vane compressor 200.
As illustrated in FIG. 11, reference character B denotes a line extending in the longitudinal direction of a vane portion 5a or 6a, and reference character C denotes a line normal to the arc at a vane tip 5b or 6b. That is, the vane portion 5a or 6a is at an angle with respect to the vane aligner portions 5c and 5d or 6c and 6d in such a manner as to extend in the direction B. Furthermore, the line C normal to the arc at the vane tip 5b or 6b is at an angle with respect to the line B and passes through the center of the arc defined by the vane aligner portions 5c and 5d or 6c and 6d.
Furthermore, in Embodiment 3, the centers of the rotor portion 4a and the bush holding portions 4d and 4e are aligned on a substantially straight line. As illustrated in the diagram included in FIG. 12 illustrating “the angle of 0 degrees”, the vane relief portion 4f is provided slightly on the right side with respect to the straight line, whereas the vane relief portion 4g is provided slightly on the left side with respect to the straight line.
Compressing Operation of Vane Compressor 200
In the above configuration also, a compressing operation is performed in a state where the line normal to the arc at each of the vane tips 5b and 6b and the line normal to the cylinder inner circumferential surface 1b always substantially coincide with each other, as in Embodiment 1 illustrated in FIG. 5. Hence, a very small gap is always provided between the cylinder inner circumferential surface 1b and each of the vane tips 5b and 6b, allowing the non-contact rotation. Furthermore, at “the angle of 0 degrees” illustrated in FIG. 12, the end of the vane portion 6a of the second vane 6 that is close to the inner circumferential surface center projects toward the inner side with respect to the bush center 8a in the bush 8 as in Embodiment 1, allowing the bush 8 to stably rotate about the bush center 8a, whereby the vane is always stably supported.
Advantageous Effects of Embodiment 3
In Embodiment 3 also, a compressing operation is performed in a state where the line normal to the arc at each of the vane tips 5b and 6b and the line normal to the cylinder inner circumferential surface 1b always substantially coincide with each other, producing substantially the same effects as in Embodiment 1.
Embodiment 4
A vane compressor 200 according to Embodiment 4 will now be described, focusing on differences from the vane compressor 200 according to Embodiment 2.
Configuration of Vane Compressor 200
FIG. 13 is a sectional view of the vane compressor 200 according to Embodiment 4 of the present invention that is taken along line I-I illustrated in FIG. 1 and at “the angle of 0 degrees”. In FIG. 13, the suction port 1a, the notch 1c, and the discharge port 1d are not illustrated.
As illustrated in FIG. 13, the end of each of the vane portion 5a of the first vane 5 and the vane portion 6a of the second vane 6 that is close to the inner circumferential surface center extends toward the inner side. Furthermore, the rotor portion 4a is configured such that, at “the angle of 0 degrees”, the end of the vane portion 5a or 6a that is close to the inner circumferential surface center projects toward the inner side with respect to a line defined by the outer circumferences of the rotating shaft portions 4b and 4c (toward the center of the rotor shaft 4) in the rotor portion 4a. Correspondingly, second vane relief portions 4l and 4m extend from the respective vane relief portions 4f and 4g toward the center of the rotor portion 4a. The second vane relief portions 4l and 4m reside on the inner side with respect to the line defined by the outer circumferences of the rotating shaft portions 4b and 4c. Sections of the second vane relief portions 4l and 4m taken vertically to the central axis of the rotor portion 4a each have a rectangular shape. A circumferential-direction width a denotes the width of each of the second vane relief portions 4l and 4m that are seen in a direction of the central axis of the rotor portion 4a, and a circumferential-direction smallest width b denotes the width of each of openings provided in the side face of the rotor portion 4a at the bush holding portions 4d and 4f that are seen in the direction of the central axis of the rotor shaft 4. The circumferential-direction width a is substantially the same as the circumferential-direction smallest width b.
FIG. 14 includes sectional views illustrating the vane portion 5a of the first vane 5 and associated elements included in the vane compressor 200 according to Embodiment 4 of the present invention at different angles of rotation established after the state illustrated in FIG. 13.
An angle β illustrated in FIG. 14 is an angle formed between a line connecting the center of the rotor portion 4a and the bush center 7a and the longitudinal direction of the vane portion 5a of the first vane 5 toward the center of the cylinder inner circumferential surface 1b.
FIG. 14(
a) illustrates a state where the rotor portion 4a has rotated slightly from the state at “the angle of 0 degrees” illustrated in FIG. 13. The angle β gradually increases with the rotation of the rotor portion 4a. FIG. 14(b) illustrates a state where the rotor portion 4a has rotated further from the state illustrated in FIG. 14(a). The end of the vane portion 5a that is close to the inner circumferential surface center comes close to a side face of the second vane relief portion 4l (a face substantially parallel to the line connecting the center of the rotor shaft 4 and the bush center 7a) but moves away from the bottom face of the second vane relief portion 4l (a face substantially perpendicular to the line connecting the center of the rotor shaft 4 and the bush center 7a). In this state, the angle β has increased further, and a corner of the vane portion 5a at the end close to the inner circumferential surface center and on a leading side in the direction of rotation has gone out of the second vane relief portion 4l and has moved into the vane relief portion 4f. As illustrated in FIG. 14, the circumferential-direction width of the vane relief portion 4f (the width of the vane relief portion 4f that is seen in the direction of the central axis of the rotor portion 4a) is much larger than the circumferential-direction width a of the second vane relief portion 4l. Hence, there is no chance of the vane portion 5a coming into contact with the rotor portion 4a. FIG. 14(c) illustrates a state where the angle of rotation of the rotor portion 4a has increased further from “the angle of 90 degrees”, and the angle formed between the longitudinal direction of the vane portion 5a and the line connecting the center of the rotor shaft 4 and the center of the cylinder inner circumferential surface 1b is 90 degrees. In this state, the angle β is largest. In this state, the end of the vane portion 5a that is close to the inner circumferential surface center is positioned in the vane relief portion 4f and is therefore out of contact with the rotor portion 4a.
The behavior of the vane portion 5a of the first vane 5 illustrated in FIG. 14 also applies to the case of the vane portion 6a of the second vane 6.
FIG. 15 includes a plan view and a vertical sectional view of the rotor shaft 4 included in the vane compressor 200 according to Embodiment 4 of the present invention. FIG. 15(a) is the plan view of the rotor shaft 4. FIG. 15(b) is the vertical sectional view of the rotor shaft 4.
The bush holding portions 4d and 4e and the vane relief portions 4f and 4g are processed in the direction of the central axis of the rotor shaft 4 as represented by arrows D in FIG. 15. In contrast, the second vane relief portions 4l and 4m are processed from the side face of the rotor portion 4a as represented by arrows E in FIG. 15 because the second vane relief portions 4l and 4m extend from the respective vane relief portions 4f and 4g toward the central axis of the rotor portion 4a and are provided on the inner side with respect to the line defined by the outer circumferences of the rotating shaft portions 4b and 4c. In Embodiment 4, since the circumferential-direction width a of each of the second vane relief portions 4l and 4m substantially coincides with the circumferential-direction smallest width b of each of the bush holding portions 4d and 4e, the second vane relief portions 4l and 4m are easy to process.
As long as the end of each of the vane portions 5a and 6a that is close to the inner circumferential surface center is kept out of contact with the side face of a corresponding one of the second vane relief portions 4l and 4m, the circumferential-direction width a of the second vane relief portions 4l and 4m may be smaller than the circumferential-direction smallest width b of the bush holding portions 4d and 4e.
Advantageous Effects of Embodiment 4
In the rotor portion 4a configured as above, if the second vane relief portions 4l and 4m are provided in such a manner as to allow the vane portions 5a and 6a to rotate without coming into contact with the rotor portion 4a even in a case where the end of each of the vane portions 5a and 6a that is close to the inner circumferential surface center projects toward the inner side with respect to the line corresponding to the diameters of the rotating shaft portions 4b and 4c, the end of each of the vane portions 5a and 6a that is close to the inner circumferential surface center can be made to extend further toward the inner circumferential surface center. Hence, the outer size of the rotor portion 4a can be made smaller than in Embodiment 1, realizing a reduction in the size of the vane compressor 200.
Furthermore, since the circumferential-direction width a of the second vane relief portions 4l and 4m is substantially the same as or smaller than the circumferential-direction smallest width b of the bush holding portions 4d and 4e, the second vane relief portions 4l and 4m are easy to process.
While the second vane relief portions 4l and 4m provided in the rotor shaft 4 illustrated in FIG. 15 extend over the entirety of the rotor portion 4a in the axial direction of the rotor portion 4a, the present invention is not limited to such a case. That is, in a modification, illustrated in FIG. 16, of the rotor shaft 4 included in the vane compressor 200 according to Embodiment 4, the length of the second vane relief portions 4l and 4m in the axial direction may be smaller than the length of the rotor portion 4a in the axial direction (the second vane relief portions 4l and 4m illustrated in FIG. 16 each extend over a region of the rotor portion 4a excluding regions at two axial ends of the rotor portion 4a). In such a case, the first vane 5 and the second vane 6 according to Embodiment 2 illustrated in FIG. 10 may be employed. If so, an end facet of the vane inward projection 5e of the vane portion 5a that is close to the inner circumferential surface center is positioned in the second vane relief portion 4l, and an end facet of the vane inward projection 6e of the vane portion 6a that is close to the inner circumferential surface center is positioned in the second vane relief portion 4m.
In such a configuration, since the second vane relief portions 4l and 4m are not necessarily extend over the entirety of the rotor portion 4a in the axial direction, the rigidity of the shaft is increased without reducing the areas of contact between the rotor portion 4a and the rotating shaft portion 4b and between the rotor portion 4a and the rotating shaft portion 4c. Hence, a highly reliable vane compressor 200 exhibiting higher axial strength and smaller axial warpage than those provided by the rotor shaft 4 illustrated in FIG. 15 is provided.
While Embodiments 1 to 4 each concern a case where the oil pump 31 utilizing the centrifugal force of the rotor shaft 4 is employed, the oil pump 31 may be of any type. For example, a positive-offset pump disclosed by Japanese Unexamined Patent Application Publication No. 2009-62820 may be employed as the oil pump 31.
REFERENCE SIGNS LIST
1 cylinder 1a suction port 1b cylinder inner circumferential surface 1c notch 1d discharge port 1e oil return hole 1f through portion 2 frame 2a recess 2b vane aligner bearing portion 2c main bearing portion 2d discharge port 2f, 2g stopper 3 cylinder head 3a recess 3b vane aligner bearing portion 3c main bearing portion 3f, 3g stopper 4 rotor shaft 4a rotor portion 4b, 4c rotating shaft portion 4d, 4e bush holding portion 4f, 4g vane relief portion 4h to 4j oil supply path 4k oil discharge hole 4l, 4m second vane relief portion 5 first vane 5a vane portion 5b vane tip 5c, 5d vane aligner portion 5e, 6e vane inward projection 6 second vane 6a vane portion 6b vane tip 6c, 6d vane aligner portion 7 bush 7a bush center 8 bush 8a bush center 9 suction chamber 10 intermediate chamber 11 compression chamber 21 stator 22 rotor 23 glass terminal 24 discharge pipe refrigerating machine oil 26 suction pipe 27 discharge valve 28 discharge valve stopper 31 oil pump 32 nearest point 41 to 43 arrow 44, 45 moment 101 compressing element 102 motor element 103 closed container 104 oil reservoir 200 vane compressor
Patent Application
20140271315
