EP3318760A1 - Vane compressor - Google Patents
Vane compressor Download PDFInfo
- Publication number
- EP3318760A1 EP3318760A1 EP16817893.7A EP16817893A EP3318760A1 EP 3318760 A1 EP3318760 A1 EP 3318760A1 EP 16817893 A EP16817893 A EP 16817893A EP 3318760 A1 EP3318760 A1 EP 3318760A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- vane
- arc surface
- end portion
- pressure chamber
- back pressure
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
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- 230000002093 peripheral effect Effects 0.000 claims abstract description 48
- 230000000052 comparative effect Effects 0.000 description 11
- 230000006835 compression Effects 0.000 description 11
- 238000007906 compression Methods 0.000 description 11
- 239000012530 fluid Substances 0.000 description 8
- 238000005242 forging Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 4
- 230000007547 defect Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 239000003507 refrigerant Substances 0.000 description 2
- 238000005057 refrigeration Methods 0.000 description 2
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/30—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F04C18/34—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members
- F04C18/344—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/08—Rotary pistons
- F01C21/0809—Construction of vanes or vane holders
- F01C21/0818—Vane tracking; control therefor
- F01C21/0854—Vane tracking; control therefor by fluid means
Definitions
- the present invention relates to a vane compressor suitable for a refrigeration cycle using, for example, a working fluid as a refrigerant, more particularly to the structure of a lower end portion in the forward or backward travel direction of the vane of a vane compressor.
- a vane compressor includes a cylinder having both ends closed by side blocks or the like, a rotor, rotatably housed in the cylinder, that has a perfect circular cross section, a vane groove formed radially inward from an outer peripheral surface of the rotor, and a vane housed in the vane groove movably forward and backward.
- the vane compressor has the structure in which the vane is brought into slidable contact with the inner peripheral surface of the cylinder by a centrifugal force caused by the rotation of the rotor or a back pressure from a back pressure chamber provided on the bottom of the vane groove.
- the bottom of the vane groove of the rotor has an arc-shaped cross section and the lower end portion of the vane is arc-shaped so as to match the shape of the bottom of the vane groove. Accordingly, even when the lower end portion of the vane collides with the bottom of the vane groove, impact sound is reduced because arcs make contact with each other.
- the vane can reach the bottom of the vane groove until the centers in the arcs coincide.
- the length of the vane along the vane groove is formed so as not to project from the vane groove even when the vane enters the deepest part of the vane groove. Accordingly, even when the vane moves in the vane groove so as to follow the shape of the inner peripheral surface of the cylinder as the rotor rotates and passes through the radial seal portion on the inner peripheral surface of the cylinder, the vane can enter the cylinder groove without interfering with the bottom of the vane groove.
- the material of the vane compressor can be formed by, for example, forging as described in PTL 2.
- the vane groove including the back pressure chamber, a through hole into which a shaft is inserted, and the like are formed in advance.
- the vane groove of the rotor is polished at high accuracy, but the back pressure chamber provided on the bottom of the vane groove has the shape formed by forging as is. Accordingly, when the vane groove is polished, the position of the vane groove deviates from the position of the back pressure chamber and the center of the vane groove in which the vane slides may deviate from the center of the back pressure chamber.
- the invention addresses the above problems with an object of providing a vane compressor in which the structure of the lower end side in the forward or backward travel direction of a vane is changed so that the shoulder portion of the lower end portion of the vane has difficulty in overriding the arc surface on the side of the concave arc surface of the back pressure chamber and the rotation of the rotor is thereby prevented from being restricted by the vane protruding from the outer peripheral surface of the rotor.
- a vane compressor includes a cylinder having both ends closed by side block members, a rotor rotatably provided in the cylinder, a vane groove formed radially inward from an outer peripheral surface of the rotor, and a vane housed in the vane groove movably forward and backward, one end portion of the vane making slidable contact with an inner peripheral surface of the cylinder as the rotor rotates, in which a back pressure chamber having a concave arc surface is formed on a bottom of the vane groove, the other end portion of the vane has a convex arc surface facing the concave arc surface of the vane groove, and voids are generated between the vane and the bottom of the vane groove on both sides in a thickness direction of the vane when the other end portion of the vane makes contact with the bottom of the vane groove.
- the convex arc surface of the other end portion of the vane has a curvature radius smaller than the concave arc surface on the bottom of the vane groove and the voids are thereby generated on both sides of a contact portion between the other end portion of the vane and the bottom of the vane groove.
- tangential flat surfaces continued to the convex arc surface are formed on both sides in the thickness direction of the other end portion of the vane.
- the radius of the convex arc surface of the other end portion of the vane can be reduced as compared with the case in which the entire surface facing the concave arc surface on the bottom of the vane groove is the convex arc surface, contact can be concentrated on the position at which the other end portion of the vane makes contact with the bottom of the vane groove. Accordingly, even when, for example, fine foreign matter enters the back pressure chamber, the foreign matter is sandwiched between the other end portion of the vane and the bottom of the vane groove, thereby preventing the possibility that the vane cannot enter the deep part of the bottom of the vane groove.
- sliding contact surfaces in slidable contact with the vane groove are formed on both sides in the thickness direction of the vane, chamfering for partially removing the sliding contact surfaces and the convex arc surface is performed between the sliding contact surfaces and the convex arc surface of the other end portion of the vane, and the voids are thereby provided.
- the shoulder portion of the vane it is possible to shave the shoulder portion of the vane or enlarge voids formed between the other end portion of the vane and the bottom of the vane groove on both sides in the thickness direction of the vane when the other end portion of the vane makes contact with the concave arc surface of the vane groove. Accordingly, when the vane enters the deepest part of the vane groove, the shoulder portion of the other end portion of the vane has more difficulty in overriding the arc surface on the side of the concave arc surface of the back pressure chamber.
- the width of the sliding surface of the vane is narrowed.
- the position of the shoulder portion of the vane is prevented from being raised toward the outer peripheral surface of the rotor more than necessary, thereby preventing the width of the sliding surface of the vane from being narrowed.
- the radius of the convex arc surface of the other end portion of the vane can be reduced as compared with the case in which the entire surface facing the concave arc surface on the bottom of the vane groove is the convex arc surface, contact can be concentrated on the position at which the other end portion of the vane makes contact with the bottom of the vane groove. Accordingly, even when, for example, fine foreign matter enters the back pressure chamber, the foreign matter is sandwiched between the other end portion of the vane and the bottom of the vane groove, thereby preventing the possibility that the vane cannot enter the deep part of the bottom of the vane groove.
- the fourth aspect of the invention it is possible to shave the shoulder portion of the vane or enlarge voids formed between the lower end portion of the vane and the bottom of the vane groove on both sides in the thickness direction of the vane when the lower end portion of the vane makes contact with the concave arc surface of the back pressure chamber. Accordingly, when the vane enters the deepest part of the vane groove, the shoulder portion of the lower end portion of the vane has more difficulty in overriding the arc surface on the side of the concave arc surface of the back pressure chamber.
- FIGs. 1 and 2 illustrate an example of a vane compressor used for the refrigeration cycle of, for example, an in-vehicle air conditioner.
- a vane compressor 1 includes a shaft 3, a rotor 4, fixed to the shaft 3, that rotates as the shaft 3 rotates, and first and second housing members 8 and 9 that define a compression space 18 (described later) together with the rotor 4.
- the first housing member 8 and the second housing member 9 constitute a housing 2.
- the first housing member 8 includes a cylinder 8a in which the rotor 4 is housed and a rear side block 8b positioned on the rear side in the shaft direction of the shaft 3 with respect to the cylinder 8a, integrally molded with the cylinder 8a, and closing the rear side of the cylinder 8a.
- the rotor 4 housed in the cylinder 8a is a cylinder having a perfect circular cross section and a center point P1 of the perfect circle is provided with a through hole 4a to which the shaft 3 can be press-fitted, as illustrated in Fig. 2 .
- the rotor 4 has two vanes 6 to be inserted into two vane grooves 5 opened in the outer peripheral surface of the rotor 4.
- any of the vanes 6 includes one end portion having sliding contact surfaces 6a and 6a (described later) in slidable contact with the inner peripheral surface of the vane groove 5 described below on both sides in the thickness direction of the vane 6 and the other end portion having a convex arc surface 611a (described later) and slides on the inner peripheral surface of the cylinder 8a by moving forward or backward from the vane groove 5.
- the vane groove 5 extends radially inward from the outer peripheral surface of the rotor 4.
- a back pressure chamber 10 having a concave arc surface 101, which will be described later, is formed on the bottom of the vane groove 5.
- the vane groove 5 and the back pressure chamber 10 are formed so as to penetrate from front side to the rear side along the shaft direction of the rotor 4.
- the inner peripheral surface of the cylinder 8a has an inner diameter larger than the outer diameter of the rotor 4 and is formed in a perfect circle about a center point P2.
- the rotor 4 is housed in the cylinder 8a so that the outer peripheral surface of the rotor 4 and the inner peripheral surface of the cylinder 8a form a fine clearance (radial seal portion P3 at which the cylinder 8a is closest to the rotor 4) at one position in the peripheral direction. Since the rotor 4 about the center point P1 is housed in the cylinder 8a as described above, a compression space 18 is defined between the inner peripheral surface of the cylinder 8a and the outer peripheral surface of the rotor 4. This compression space 18 is partitioned by the two vanes 6 housed in the two vane grooves 5 formed in the rotor 4 into two compression chambers 19 and the volumes of the compression chambers 19 are changed as the rotor 4 rotates.
- the second housing member 9 is configured by integrating a front side block 9a in contact with the front side end surface of the cylinder 8a with a shell 9b, extending in the shaft direction of the shaft 3 from the front side block 9a, that surrounds the outer peripheral surfaces of the cylinder 8a and the rear side block 8b.
- the second housing member 9 is coupled to the first housing member 8 via a coupling tool 7 such as a bolt.
- a pulley 20 to which rotational power is transmitted from the power source (not illustrated) of a vehicle via a belt (not illustrated) is rotatably mounted onto a boss section 9c integrated with the front side block 9a and the rotational power is transmitted from the pulley 20 to the shaft 3 via an electromagnetic clutch 21.
- the second housing member 9 is provided with an intake port 11 and a discharge port 12 of the working fluid (refrigerant gas) and the intake port 11 communicates with an intake space 14 including a space 14a formed in the second housing member 9 and a concavity 14b formed in the cylinder 8a.
- the shaft 3 is rotatably supported via plain bearings 23 and 24 that are bearing portions held and formed by the front side block 9a of the second housing member 9 and the rear side block 8b of the first housing member 8.
- a seal member 13 is present between the shaft 3 and the inner side surface of the second housing member 9 in the part close to the base end of the boss section 9C of the second housing member 9 to prevent the working fluid from leaking externally from the opening of the boss section 9c.
- the peripheral surface of the cylinder 8a is provided with an intake port 25 communicating with the intake space 14 so as to correspond to the compression space 18 and a discharge port 26 communicating with a discharge space 15. Accordingly, when the cylinder 8a is fitted to the shell 9b, the intake space 14 communicates with the compression chambers 19 via the intake port 25, the discharge space 15 having both ends separated by flange sections 8c and 8d is formed between the outer peripheral surface of the cylinder 8a and the inner side surface of the shell 9b, and the discharge space 15 can communicate with the compression chambers 19 via the discharge port 26.
- the discharge port 26 is opened or closed by a discharge valve 27 housed in the discharge space 15.
- the discharge space 15 communicates with an oil separator 16 via a passing hole 28 formed in the flange section 8d.
- the oil separator 16 communicates with the discharge port 12.
- the rotational power from the power source (not illustrated) is transmitted to the shaft 3 via the pulley 20 and the electromagnetic clutch 21 and, when the rotor 4 rotates, the working fluid having flowed to the intake space 14 from the intake port 11 is sucked by the compression space 18 via the intake port 25. Since the volumes of the compression chambers 19 partitioned by the vanes 6 in the compression space 18 are changed as the rotor 4 rotates, the working fluid between the vanes 6 is compressed and discharged from the discharge port 26 to the discharge space 15 via the discharge valve 27.
- the working fluid discharged to the discharge space 15 moves in the peripheral direction along the outer peripheral surface (inner side surface of the shell 9b) of the cylinder 8a and is introduced to the oil separating chamber of the oil separator 16 formed in the rear side block 8b via the passing hole 28 formed in the flange section 8d. After that, oil is separated from the working fluid during rotation in the oil separating chamber of the oil separator 16 and then the working fluid is discharged to an external circuit through the discharge port 12.
- FIG. 3 illustrates embodiment 1 of the invention
- Fig. 4 illustrates the other example of embodiment 1 of the invention
- Figs. 5 and 6 illustrate embodiment 2 of the invention
- Fig. 7 illustrates embodiment 3 of the invention
- Fig. 8 illustrates a comparative example to be compared with embodiment 1, the other example of embodiment 1, embodiment 2, and embodiment 3.
- Embodiment 1, the other example of embodiment 1, embodiment 2, and embodiment 3 will be described while being compared with the comparative example.
- the vane groove 5 in embodiment 1 extends radially inward from the outer peripheral surface of the rotor 4 as described above and has the inner side surfaces in contact with the sliding contact surfaces 6a and 6a of the vane 6 on both sides in the thickness direction of the vane 6.
- Fig. 3 (a) illustrates a center line C passing through the center in the thickness direction of the vane 6.
- the back pressure chamber 10 in embodiment 1 includes two side arc surfaces 101a and 101b and one bottom side arc surface 101c positioned between the two side arc surfaces 101a and 101b.
- the side arc surface 101a, the bottom side arc surface 101c, and the side arc surface 101b that form the back pressure chamber 10 are disposed along an arc S1 assumed about a center point P5 of the back pressure chamber 10 and constitute the concave arc surface 101 of the back pressure chamber 10.
- a diameter L1 of the back pressure chamber 10 is larger than a dimension L2 (illustrated in Fig. 3(b) ) of the vane groove 5 in the thickness direction of the vane 6.
- Reference numeral 103 in Fig. 3 indicates the center in the arc of the arc S1 that forms the concave arc surface 101 of the back pressure chamber 10.
- the back pressure chamber 10 has the concave arc surface 101
- reference numeral 103 indicates the center in the arc of the arc S1 that forms the concave arc surface 101 of the back pressure chamber 10
- the center line C passing through the center in the thickness direction of the vane 6 is illustrated.
- the vane 6 in embodiment 1 has a lower end portion 61 close to the lower end in the forward or backward travel direction of the vane 6 as the other end portion described above.
- the lower end portion 61 has the convex arc surface 611a in which an entire contact surface 611 facing a bottom side arc surface 102c of the back pressure chamber 10 is along an arc S2. Accordingly, shoulder portions K1 and K2 of the lower end portion 61 coincide with the start end and the terminal end of the arc S2 about the center point P5.
- a curvature radius L4 of the arc S2 forming the convex arc surface 611a of the lower end portion 61 is smaller than a curvature radius L3 of the arc S1 forming the concave arc surface 101 of the back pressure chamber 10.
- Reference numeral 63 in Fig. 3 indicates the center in the arc of the arc S2 forming the convex arc surface 611a of the lower end portion 61.
- the curvature radius L4 of the arc S2 forming the convex arc surface 611a is substantially half the dimension L2 in the thickness direction of the vane 6.
- the convex arc surface 611a of the lower end portion 61 is a half peripheral surface and the center point P5 of the arc S2 and the shoulder portions K1 and K2 of the lower end portion 61 are positioned in a single line.
- a center point P4 of the arc S1 does not deviate from the center point P5 of the arc S2 as illustrated in Fig.
- the curvature radius L4 of the arc S2 forming the convex arc surface 611a of the lower end portion 61 is the same as the curvature radius L3 of the arc S1 forming the concave arc surface 101 of the back pressure chamber 10. Also in this case, when the position of the vane groove 5 does not deviate from the position of the back pressure chamber 10, the center point P4 of the arc S1 does not deviate from the center point P5 of the arc S2 as illustrated in Fig.
- the position of the vane groove 5 deviates from the position of the back pressure chamber 10
- the center line C of the vane groove 5 in the thickness direction of the vane 6 and the center point P5 of the back pressure chamber 10 may deviate by approximately a predetermined dimension X1 along the thickness direction of the vane 6 from a set position, as illustrated in Figs. 3 (b) and 8 (b) .
- center 63 in the arc of the convex arc surface 611a of the contact surface 611 and the center 103 in the arc of the concave arc surface 101 of the back pressure chamber 10 also deviate by the predetermined dimension X1 along the thickness direction of the vane 6, as illustrated in Figs. 3(b) and 8(b) .
- the shoulder portions K1 and K2 of the lower end portion 61 override the side arc surfaces 101a and 101b of the back pressure chamber 10 as illustrated in Fig. 8(b) when the vane 6 enters the deepest part of the vane groove 5.
- a clearance G1 is generated between the center 63 in the arc of the convex arc surface 611a of the lower end portion 61 and the center 103 in the arc of the concave arc surface 101 of the back pressure chamber 10 along the forward or backward travel direction of the vane 6. Since this clearance G1 is large, the upper end portion of the vane 6 projects from the outer peripheral surface of the rotor 4, the vane 6 interferes with the inner peripheral surface of the cylinder 8a, possibly disabling the rotation of the rotor 4.
- the shoulder portions K1 and K2 of the lower end portion 61 have difficulty in overriding the arc surface on the side arc surfaces 101a and 101b of the back pressure chamber 10 as illustrated in Fig. 3(b) .
- a clearance G2 is generated along the forward or backward travel direction of the vane 6 between the center 63 of the arc surface of the lower end portion 61 and the center 103 of the arc surface of the concave arc surface 101 of the back pressure chamber 10, as illustrated in Fig. 3(b) .
- this clearance G2 is small, the upper end portion of the vane 6 does not project from the outer peripheral surface of the rotor 4 in embodiment 1, the vane 6 does not interfere with the inner peripheral surface of the cylinder 8a, thereby preventing the rotation of the rotor 4 from being disabled.
- Fig. 4 illustrates the other example of embodiment 1 illustrated in Fig. 3 .
- the other example of embodiment 1 will be described below with reference to Fig. 3 .
- the same components as in embodiment 1 are given the same reference numerals in principle and descriptions are omitted.
- the lower end portion 61 of the vane 6 in the other example of embodiment 1 is the same as the lower end portion 61 illustrated in Fig. 3 in that the entire contact surface 611 facing the bottom side arc surface 101c of the back pressure chamber 10 is the convex arc surface 611a along the arc S2.
- the curvature radius L4 of the arc S2 forming the convex arc surface 611a is larger than substantially the half of the dimension L2 in the thickness direction of the vane 6 and smaller than the curvature radius L3 of the arc S1 forming the concave arc surface 101 of the back pressure chamber 10.
- the convex arc surface 611a of the lower end portion 61 is smaller than a half peripheral surface and the center point P5 of the arc S2 is disposed closer to the sliding contact surface 6a of the vane 6 than the shoulder portions K1 and K2 of the lower end portion 61.
- the shoulder portions K1 and K2 of the lower end portion 61 have difficulty in overriding the side arc surfaces 101a and 101b of the back pressure chamber 10 as illustrated in Fig. 4(b) .
- the clearance G2 in Fig. 4(b) generated because the convex arc surface 611a of the lower end portion 61 is raised along the arc of the concave arc surface 101 of the back pressure chamber 10 is small as in embodiment 1 in Fig.
- the vane 6 does not project from the outer peripheral surface of the rotor 4 also in the other example of embodiment 1, the vane 6 does not interfere with the inner peripheral surface of the cylinder 8a, thereby preventing the rotation of the rotor 4 from being disabled.
- FIGs. 5 and 6 illustrate embodiment 2 as described above. Embodiment 2 will be described below with reference to Figs. 5 and 6 . However, the same components as in embodiment 1 and the other example of embodiment 1 are given the same reference numerals in principle and descriptions are omitted.
- the contact surface 611 includes the convex arc surface 611a and two tangential flat surfaces 611b continued to the convex arc surface 611a.
- the convex arc surface 611a is formed along an arc S3a of a circle S3, centered at P6, that has a radius L5 smaller than the radius L3 of the arc S1 forming the concave arc surface 101 of the back pressure chamber 10, the arc S3a facing the bottom side arc surface 101c.
- the tangential flat surfaces 611b are formed so as to make contact with the arc S3a forming the convex arc surface 611a in embodiment 2 and the contact flat surfaces 611b are flat surfaces extending from both ends of the arc S3 toward the shoulder portions K1 and K2 while being inclined toward the sliding contact surfaces 6a of the vane 6.
- the shape of the lower end portion 61 of the vane 6 in embodiment 2 can also be formed by, for example, providing the flat surfaces 611b on both sides in the thickness direction of the lower end portion 61 at the same angle as the oblique angle of the tangential flat surface of the arc surface (arc S1) passing through a point P7 at which the arc S1 forming the concave arc surface 101 of the back pressure chamber 10 and a virtual line V extending from the inner side surface of the vane groove 5 intersect and by connecting the intersection of the flat surface 611b and the flat surface 611b via the arc S3a of the contact circle S3 having the curvature radius L5 smaller than the curvature radius L3 of the arc S1 forming the concave arc surface of the back pressure chamber 10.
- the flat surface 611b may be slightly inclined toward the shaft line of the vane groove 5 from the same angle as the oblique angle of the tangential flat surface of the arc surface (arc S1) passing through the point P7, which is not illustrated.
- Fig. 7 illustrate embodiment 3 as described above. Embodiment 3 will be described below with reference to Fig. 7 . However, the same components as in the embodiments described above are given the same reference numerals in principle and descriptions are omitted.
- the lower end portion 61 of the vane 6 in embodiment 3 is tapered by partially removing the sliding contact surface 6a and a part of the convex arc surface 611a of the vane 6 and forming the chamfered oblique surface 101c with respect to the convex arc surface 611a (the curvature radius L4 of the arc S2 is the same as the curvature radius L3 of the arc S1 forming the concave arc surface 101 of the back pressure chamber 10) having the entire contact surface 611 facing the bottom side arc surface 101c of the back pressure chamber 10 disposed along the arc S2 about the center point P5.
- the curvature radius L4 of the arc S2 may be smaller than the curvature radius L3 of the arc S1 forming the concave arc surface 101 of the back pressure chamber 10.
- the chamfered oblique surface 101c may be formed by partially removing the sliding contact surface 6a of the vane 6 or the convex arc surface 611a.
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Abstract
Description
- The present invention relates to a vane compressor suitable for a refrigeration cycle using, for example, a working fluid as a refrigerant, more particularly to the structure of a lower end portion in the forward or backward travel direction of the vane of a vane compressor.
- As described in, for example,
PTL 1,PTL 2, and the like, a vane compressor includes a cylinder having both ends closed by side blocks or the like, a rotor, rotatably housed in the cylinder, that has a perfect circular cross section, a vane groove formed radially inward from an outer peripheral surface of the rotor, and a vane housed in the vane groove movably forward and backward. In addition, the vane compressor has the structure in which the vane is brought into slidable contact with the inner peripheral surface of the cylinder by a centrifugal force caused by the rotation of the rotor or a back pressure from a back pressure chamber provided on the bottom of the vane groove. - In the vane compressor proposed in
PTL 1, the bottom of the vane groove of the rotor has an arc-shaped cross section and the lower end portion of the vane is arc-shaped so as to match the shape of the bottom of the vane groove. Accordingly, even when the lower end portion of the vane collides with the bottom of the vane groove, impact sound is reduced because arcs make contact with each other. - In addition, since the bottom of the vane groove and the lower end portion of the vane are arc-shaped so as to become close to each other, the vane can reach the bottom of the vane groove until the centers in the arcs coincide. In consideration of this, the length of the vane along the vane groove is formed so as not to project from the vane groove even when the vane enters the deepest part of the vane groove. Accordingly, even when the vane moves in the vane groove so as to follow the shape of the inner peripheral surface of the cylinder as the rotor rotates and passes through the radial seal portion on the inner peripheral surface of the cylinder, the vane can enter the cylinder groove without interfering with the bottom of the vane groove.
-
- PTL 1:
JP-A-10-18984 - PTL 2:
JP-A-11-230068 - The material of the vane compressor can be formed by, for example, forging as described in
PTL 2. In the material of the rotor formed by forging, the vane groove including the back pressure chamber, a through hole into which a shaft is inserted, and the like are formed in advance. When the completed product of the rotor is created from such rotor materials formed as described above by forging or molding, the vane groove in which the vane slides and which requires dimensional accuracy is polished, but the back pressure chamber in which no member slides or to which no member is fitted is not machined. - When the rotor of the vane compressor described in
PTL 1 is made from materials formed by forging or molding, the vane groove of the rotor is polished at high accuracy, but the back pressure chamber provided on the bottom of the vane groove has the shape formed by forging as is. Accordingly, when the vane groove is polished, the position of the vane groove deviates from the position of the back pressure chamber and the center of the vane groove in which the vane slides may deviate from the center of the back pressure chamber. - When the center of the vane groove in which the vane slides deviates from the center of the back pressure chamber, as illustrated in
Fig. 8 , even if the vane enters the deepest part of the vane groove, the center of the arc surface of the lower end portion of the vane does not coincide with the center of the arc surface of the vane groove, and the shoulder portion of the lower end portion of the vane overrides the arc surface on the side of the bottom of the vane groove. Accordingly, the lower end portion of the vane cannot enter the deepest part of the vane groove, the upper end portion projects from the outer peripheral surface of the rotor and the vane interferes with the inner peripheral surface of the cylinder, possibly disabling the rotation of the rotor. - The invention addresses the above problems with an object of providing a vane compressor in which the structure of the lower end side in the forward or backward travel direction of a vane is changed so that the shoulder portion of the lower end portion of the vane has difficulty in overriding the arc surface on the side of the concave arc surface of the back pressure chamber and the rotation of the rotor is thereby prevented from being restricted by the vane protruding from the outer peripheral surface of the rotor.
- A vane compressor according to the invention includes a cylinder having both ends closed by side block members, a rotor rotatably provided in the cylinder, a vane groove formed radially inward from an outer peripheral surface of the rotor, and a vane housed in the vane groove movably forward and backward, one end portion of the vane making slidable contact with an inner peripheral surface of the cylinder as the rotor rotates, in which a back pressure chamber having a concave arc surface is formed on a bottom of the vane groove, the other end portion of the vane has a convex arc surface facing the concave arc surface of the vane groove, and voids are generated between the vane and the bottom of the vane groove on both sides in a thickness direction of the vane when the other end portion of the vane makes contact with the bottom of the vane groove. In a vane compressor according to the second aspect, the convex arc surface of the other end portion of the vane has a curvature radius smaller than the concave arc surface on the bottom of the vane groove and the voids are thereby generated on both sides of a contact portion between the other end portion of the vane and the bottom of the vane groove.
- Accordingly, if the center of the vane groove in the thickness direction of the vane deviates from the center of the back pressure chamber in the thickness direction of the vane, voids are formed between the lower end portion of the vane and the bottom of the vane groove on both sides in the thickness direction of the vane when the lower end portion of the vane makes contact with the concave arc surface of the back pressure chamber. Accordingly, when the vane enters the deepest part of the vane groove, the shoulder portion of the lower end portion of the vane has difficulty in overriding the arc surface on the side of the back pressure chamber of the concave arc surface on the bottom of the vane groove. Accordingly, it is possible to prevent a defect that causes the upper end portion of the vane to project from the outer peripheral surface of the rotor, interfere with the inner peripheral surface of the cylinder, and inhibit the rotation of the rotor.
- In a vane compressor according to the third aspect, tangential flat surfaces continued to the convex arc surface are formed on both sides in the thickness direction of the other end portion of the vane.
- Accordingly, when the entire surface of the other end of vane facing the concave arc surface on the bottom of the vane groove is the convex arc surface, since the position of the shoulder portion of the vane is raised toward the outer peripheral surface of the rotor, the width of the sliding surface of the vane is narrowed. However, since the tangential flat surfaces are present, the position of the shoulder portion of the vane is prevented from being raised toward the outer peripheral surface of the rotor more than necessary, thereby preventing the width of the sliding surface of the vane from being narrowed.
- In addition, since the radius of the convex arc surface of the other end portion of the vane can be reduced as compared with the case in which the entire surface facing the concave arc surface on the bottom of the vane groove is the convex arc surface, contact can be concentrated on the position at which the other end portion of the vane makes contact with the bottom of the vane groove. Accordingly, even when, for example, fine foreign matter enters the back pressure chamber, the foreign matter is sandwiched between the other end portion of the vane and the bottom of the vane groove, thereby preventing the possibility that the vane cannot enter the deep part of the bottom of the vane groove.
- In a vane compressor according to the fourth aspect, sliding contact surfaces in slidable contact with the vane groove are formed on both sides in the thickness direction of the vane, chamfering for partially removing the sliding contact surfaces and the convex arc surface is performed between the sliding contact surfaces and the convex arc surface of the other end portion of the vane, and the voids are thereby provided.
- Accordingly, it is possible to shave the shoulder portion of the vane or enlarge voids formed between the other end portion of the vane and the bottom of the vane groove on both sides in the thickness direction of the vane when the other end portion of the vane makes contact with the concave arc surface of the vane groove. Accordingly, when the vane enters the deepest part of the vane groove, the shoulder portion of the other end portion of the vane has more difficulty in overriding the arc surface on the side of the concave arc surface of the back pressure chamber.
- As described above, in the invention, even if the center of the vane groove in the thickness direction of the vane deviates from the center of the back pressure chamber in the thickness direction of the vane, voids are formed between the lower end portion of the vane and the concave arc surface of the back pressure chamber on both sides in the thickness direction of the vane when the lower end portion of the vane makes contact with the concave arc surface of the back pressure chamber. Accordingly, when the vane enters the deepest part of the vane groove, it is possible to prevent the shoulder portion of the lower end portion of the vane from overriding the arc surface on the side of the concave arc surface of the back pressure chamber. Accordingly, it is possible to prevent a defect that causes the upper end portion of the vane to project from the outer peripheral surface of the rotor, interfere with the inner peripheral surface of the cylinder, and inhibit the rotation of the rotor.
- According to particularly the third aspect of the invention, when the entire surface of the other end portion of the vane facing the concave arc surface on the bottom of the vane groove is the convex arc surface, since the position of the shoulder portion of the vane is raised toward the outer peripheral surface of the rotor, the width of the sliding surface of the vane is narrowed. However, since the tangential flat surfaces are present, the position of the shoulder portion of the vane is prevented from being raised toward the outer peripheral surface of the rotor more than necessary, thereby preventing the width of the sliding surface of the vane from being narrowed.
- In addition, according to particularly the third aspect of the invention, since the radius of the convex arc surface of the other end portion of the vane can be reduced as compared with the case in which the entire surface facing the concave arc surface on the bottom of the vane groove is the convex arc surface, contact can be concentrated on the position at which the other end portion of the vane makes contact with the bottom of the vane groove. Accordingly, even when, for example, fine foreign matter enters the back pressure chamber, the foreign matter is sandwiched between the other end portion of the vane and the bottom of the vane groove, thereby preventing the possibility that the vane cannot enter the deep part of the bottom of the vane groove.
- According to particularly the fourth aspect of the invention, it is possible to shave the shoulder portion of the vane or enlarge voids formed between the lower end portion of the vane and the bottom of the vane groove on both sides in the thickness direction of the vane when the lower end portion of the vane makes contact with the concave arc surface of the back pressure chamber. Accordingly, when the vane enters the deepest part of the vane groove, the shoulder portion of the lower end portion of the vane has more difficulty in overriding the arc surface on the side of the concave arc surface of the back pressure chamber.
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- [
Fig. 1 (a) ] Fig. 1(a) is a cross sectional view illustrating an example of a vane compressor according to the invention, and a cross sectional view cut so that a discharge port can be seen. - [
Fig. 1(b)] Fig. 1(b) is a cross sectional view illustrating an example of a vane compressor according to the invention, and a cross sectional view cut so that an intake port can be seen. - [
Fig. 2] Fig. 2 is a cross sectional view taken along line A-A inFig. 1(b) . - [
Fig. 3(a)] Fig. 3(a) is a schematic view illustrating the structures of a vane, a vane groove, and a back pressure chamber according toembodiment 1 of the invention, and an enlarged view illustrating the vane and the back pressure chamber when the vane groove does not deviate from the back pressure chamber in the thickness direction of the vane. - [
Fig. 3(b)] Fig. 3(b) is a schematic view illustrating the structures of a vane, a vane groove, and a back pressure chamber according toembodiment 1 of the invention, and an overall view illustrating the vane, the vane groove, and the back pressure chamber when the vane groove deviates from the back pressure chamber in the thickness direction of the vane. - [
Fig. 4(a)] Fig. 4(a) is a schematic view illustrating the structures of a vane, a vane groove, and a back pressure chamber according to the other example ofembodiment 1 of the invention, and an enlarged view illustrating the vane and the back pressure chamber when the vane groove does not deviate from the back pressure chamber in the thickness direction of the vane. - [
Fig. 4(b)] Fig. 4(b) is a schematic view illustrating the structures of a vane, a vane groove, and a back pressure chamber according to the other example ofembodiment 1 of the invention, and an overall view illustrating the vane, the vane groove, and the back pressure chamber when the vane groove deviates from the back pressure chamber in the thickness direction of the vane. - [
Fig. 5(a)] Fig. 5(a) is a schematic view illustrating the structures of a vane, a vane groove, and a back pressure chamber according toembodiment 2 of the invention, and an enlarged view illustrating the vane and the back pressure chamber when the vane groove does not deviate from the back pressure chamber in the thickness direction of the vane. - [
Fig. 5(b)] Fig. 5(b) is a schematic view illustrating the structures of a vane, a vane groove, and a back pressure chamber according toembodiment 2 of the invention, and an overall view illustrating the vane, the vane groove, and the back pressure chamber when the vane groove deviates from the back pressure chamber in the thickness direction of the vane. - [
Fig. 6] Fig. 6 is an explanatory diagram illustrating an example of setting the angle of the tangential flat surfaces of the other end portion of the vane according toembodiment 2 of the invention illustrated inFig. 5(a) and Fig. 5(b) . - [
Fig. 7(a)] Fig. 7(a) is a schematic view illustrating the structures of a vane, a vane groove, and a back pressure chamber according toembodiment 3 of the invention, and an enlarged view illustrating the vane and the back pressure chamber when the vane groove does not deviate from the back pressure chamber in the thickness direction of the vane. - [
Fig. 7(b)] Fig. 7(b) is a schematic view illustrating the structures of a vane, a vane groove, and a back pressure chamber according toembodiment 3 of the invention, and an overall view illustrating the vane, the vane groove, and the back pressure chamber when the vane groove deviates from the back pressure chamber in the thickness direction of the vane. - [
Fig. 8(a)] Fig. 8(a) is a schematic view illustrating the structures of a vane, a vane groove, and a back pressure chamber according to a comparative example (to be compared with theembodiment 1, the other example ofembodiment 1,embodiment 2, andembodiment 3 of the invention) having a problem in the lower end portion of the vane, and an enlarged view illustrating the vane and the back pressure chamber when the vane groove does not deviate from the back pressure chamber in the thickness direction of the vane. - [
Fig. 8(b)] Fig. 8(b) is a schematic view illustrating the structures of a vane, a vane groove, and a back pressure chamber according to a comparative example (to be compared with theembodiment 1, the other example ofembodiment 1,embodiment 2, andembodiment 3 of the invention) having a problem in the lower end portion of the vane, and an overall view illustrating the vane, the vane groove, and the back pressure chamber when the vane groove deviates from the back pressure chamber in the thickness direction of the vane. - Embodiments of the invention will be described below with reference to the attached drawings.
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Figs. 1 and2 illustrate an example of a vane compressor used for the refrigeration cycle of, for example, an in-vehicle air conditioner. Avane compressor 1 includes ashaft 3, arotor 4, fixed to theshaft 3, that rotates as theshaft 3 rotates, and first and 8 and 9 that define a compression space 18 (described later) together with thesecond housing members rotor 4. Thefirst housing member 8 and thesecond housing member 9 constitute ahousing 2. - In the embodiment, the
first housing member 8 includes acylinder 8a in which therotor 4 is housed and arear side block 8b positioned on the rear side in the shaft direction of theshaft 3 with respect to thecylinder 8a, integrally molded with thecylinder 8a, and closing the rear side of thecylinder 8a. - The
rotor 4 housed in thecylinder 8a is a cylinder having a perfect circular cross section and a center point P1 of the perfect circle is provided with a throughhole 4a to which theshaft 3 can be press-fitted, as illustrated inFig. 2 . In addition, therotor 4 has twovanes 6 to be inserted into twovane grooves 5 opened in the outer peripheral surface of therotor 4. - Although the structures of the
vanes 6 in the examples illustrated inFigs. 3 to 8 will be described later, any of thevanes 6 includes one end portion having sliding 6a and 6a (described later) in slidable contact with the inner peripheral surface of thecontact surfaces vane groove 5 described below on both sides in the thickness direction of thevane 6 and the other end portion having aconvex arc surface 611a (described later) and slides on the inner peripheral surface of thecylinder 8a by moving forward or backward from thevane groove 5. - In any of the examples illustrated in
Figs. 3 to 8 , thevane groove 5 extends radially inward from the outer peripheral surface of therotor 4. In addition, aback pressure chamber 10 having aconcave arc surface 101, which will be described later, is formed on the bottom of thevane groove 5. Thevane groove 5 and theback pressure chamber 10 are formed so as to penetrate from front side to the rear side along the shaft direction of therotor 4. - As illustrated in
Fig. 2 , in the embodiment, the inner peripheral surface of thecylinder 8a has an inner diameter larger than the outer diameter of therotor 4 and is formed in a perfect circle about a center point P2. Therotor 4 is housed in thecylinder 8a so that the outer peripheral surface of therotor 4 and the inner peripheral surface of thecylinder 8a form a fine clearance (radial seal portion P3 at which thecylinder 8a is closest to the rotor 4) at one position in the peripheral direction. Since therotor 4 about the center point P1 is housed in thecylinder 8a as described above, acompression space 18 is defined between the inner peripheral surface of thecylinder 8a and the outer peripheral surface of therotor 4. Thiscompression space 18 is partitioned by the twovanes 6 housed in the twovane grooves 5 formed in therotor 4 into twocompression chambers 19 and the volumes of thecompression chambers 19 are changed as therotor 4 rotates. - The
second housing member 9 is configured by integrating afront side block 9a in contact with the front side end surface of thecylinder 8a with ashell 9b, extending in the shaft direction of theshaft 3 from thefront side block 9a, that surrounds the outer peripheral surfaces of thecylinder 8a and therear side block 8b. In addition, thesecond housing member 9 is coupled to thefirst housing member 8 via acoupling tool 7 such as a bolt. By inserting thefirst housing member 8 from arear side opening 9d of theshell 9b and fitting thefirst housing member 8 to theshell 9b, the front side of thecylinder 8a is closed by thefront side block 9a and therear side opening 9d of theshell 9b is closed by therear side block 8b. - In addition, in the
second housing member 9, apulley 20 to which rotational power is transmitted from the power source (not illustrated) of a vehicle via a belt (not illustrated) is rotatably mounted onto aboss section 9c integrated with thefront side block 9a and the rotational power is transmitted from thepulley 20 to theshaft 3 via anelectromagnetic clutch 21. In addition, thesecond housing member 9 is provided with anintake port 11 and adischarge port 12 of the working fluid (refrigerant gas) and theintake port 11 communicates with anintake space 14 including a space 14a formed in thesecond housing member 9 and a concavity 14b formed in thecylinder 8a. - The
shaft 3 is rotatably supported via 23 and 24 that are bearing portions held and formed by theplain bearings front side block 9a of thesecond housing member 9 and therear side block 8b of thefirst housing member 8. In addition, aseal member 13 is present between theshaft 3 and the inner side surface of thesecond housing member 9 in the part close to the base end of the boss section 9C of thesecond housing member 9 to prevent the working fluid from leaking externally from the opening of theboss section 9c. - The peripheral surface of the
cylinder 8a is provided with anintake port 25 communicating with theintake space 14 so as to correspond to thecompression space 18 and adischarge port 26 communicating with adischarge space 15. Accordingly, when thecylinder 8a is fitted to theshell 9b, theintake space 14 communicates with thecompression chambers 19 via theintake port 25, thedischarge space 15 having both ends separated by flange sections 8c and 8d is formed between the outer peripheral surface of thecylinder 8a and the inner side surface of theshell 9b, and thedischarge space 15 can communicate with thecompression chambers 19 via thedischarge port 26. Thedischarge port 26 is opened or closed by adischarge valve 27 housed in thedischarge space 15. In addition, thedischarge space 15 communicates with anoil separator 16 via a passinghole 28 formed in the flange section 8d. In addition, theoil separator 16 communicates with thedischarge port 12. - In the structure described above, in the
vane compressor 1, the rotational power from the power source (not illustrated) is transmitted to theshaft 3 via thepulley 20 and theelectromagnetic clutch 21 and, when therotor 4 rotates, the working fluid having flowed to theintake space 14 from theintake port 11 is sucked by thecompression space 18 via theintake port 25. Since the volumes of thecompression chambers 19 partitioned by thevanes 6 in thecompression space 18 are changed as therotor 4 rotates, the working fluid between thevanes 6 is compressed and discharged from thedischarge port 26 to thedischarge space 15 via thedischarge valve 27. The working fluid discharged to thedischarge space 15 moves in the peripheral direction along the outer peripheral surface (inner side surface of theshell 9b) of thecylinder 8a and is introduced to the oil separating chamber of theoil separator 16 formed in therear side block 8b via the passinghole 28 formed in the flange section 8d. After that, oil is separated from the working fluid during rotation in the oil separating chamber of theoil separator 16 and then the working fluid is discharged to an external circuit through thedischarge port 12. - By the way,
Fig. 3 illustratesembodiment 1 of the invention,Fig. 4 illustrates the other example ofembodiment 1 of the invention,Figs. 5 and6 illustrateembodiment 2 of the invention,Fig. 7 illustratesembodiment 3 of the invention, andFig. 8 illustrates a comparative example to be compared withembodiment 1, the other example ofembodiment 1,embodiment 2, andembodiment 3.Embodiment 1, the other example ofembodiment 1,embodiment 2, andembodiment 3 will be described while being compared with the comparative example. - The
vane groove 5 inembodiment 1 extends radially inward from the outer peripheral surface of therotor 4 as described above and has the inner side surfaces in contact with the sliding 6a and 6a of thecontact surfaces vane 6 on both sides in the thickness direction of thevane 6.Fig. 3 (a) illustrates a center line C passing through the center in the thickness direction of thevane 6. - As illustrated in
Fig. 3 , theback pressure chamber 10 inembodiment 1 includes two 101a and 101b and one bottomside arc surfaces side arc surface 101c positioned between the two 101a and 101b.side arc surfaces - The
side arc surface 101a, the bottomside arc surface 101c, and theside arc surface 101b that form theback pressure chamber 10 are disposed along an arc S1 assumed about a center point P5 of theback pressure chamber 10 and constitute theconcave arc surface 101 of theback pressure chamber 10. A diameter L1 of theback pressure chamber 10 is larger than a dimension L2 (illustrated inFig. 3(b) ) of thevane groove 5 in the thickness direction of thevane 6.Reference numeral 103 inFig. 3 indicates the center in the arc of the arc S1 that forms theconcave arc surface 101 of theback pressure chamber 10. - Also in the comparative example illustrated in
Fig. 8 , theback pressure chamber 10 has theconcave arc surface 101,reference numeral 103 indicates the center in the arc of the arc S1 that forms theconcave arc surface 101 of theback pressure chamber 10, and the center line C passing through the center in the thickness direction of thevane 6 is illustrated. - The
vane 6 inembodiment 1 has alower end portion 61 close to the lower end in the forward or backward travel direction of thevane 6 as the other end portion described above. Thelower end portion 61 has theconvex arc surface 611a in which anentire contact surface 611 facing a bottom side arc surface 102c of theback pressure chamber 10 is along an arc S2. Accordingly, shoulder portions K1 and K2 of thelower end portion 61 coincide with the start end and the terminal end of the arc S2 about the center point P5. A curvature radius L4 of the arc S2 forming theconvex arc surface 611a of thelower end portion 61 is smaller than a curvature radius L3 of the arc S1 forming theconcave arc surface 101 of theback pressure chamber 10.Reference numeral 63 inFig. 3 indicates the center in the arc of the arc S2 forming theconvex arc surface 611a of thelower end portion 61. InFig. 3 , for example, the curvature radius L4 of the arc S2 forming theconvex arc surface 611a is substantially half the dimension L2 in the thickness direction of thevane 6. Accordingly, theconvex arc surface 611a of thelower end portion 61 is a half peripheral surface and the center point P5 of the arc S2 and the shoulder portions K1 and K2 of thelower end portion 61 are positioned in a single line. When the position of thevane groove 5 does not deviate from the position of theback pressure chamber 10, a center point P4 of the arc S1 does not deviate from the center point P5 of the arc S2 as illustrated inFig. 3(a) , these points are present in the center line C of thesame vane groove 5, and thecenter 63 in the arc of theconvex arc surface 611a of thelower end portion 61 can coincide with thecenter 103 in the arc of theconcave arc surface 101 of theback pressure chamber 10. - Although the
entire contact surface 611 facing a bottom side arc surface 102 of theback pressure chamber 10 is theconvex arc surface 611a along the arc S2 in thelower end portion 61 of thevane 6 in the comparative example, the curvature radius L4 of the arc S2 forming theconvex arc surface 611a of thelower end portion 61 is the same as the curvature radius L3 of the arc S1 forming theconcave arc surface 101 of theback pressure chamber 10. Also in this case, when the position of thevane groove 5 does not deviate from the position of theback pressure chamber 10, the center point P4 of the arc S1 does not deviate from the center point P5 of the arc S2 as illustrated inFig. 8 (a) , these points are present in the center line C of thesame vane groove 5, and thecenter 63 in the arc of theconvex arc surface 611a of thelower end portion 61 can coincide with thecenter 103 in the arc of theconcave arc surface 101 of theback pressure chamber 10. - However, in the comparative example, even when the
convex arc surface 611a of thelower end portion 61 is brought into contact with the bottomside arc surface 101c of theback pressure chamber 10 so that thecenter 63 in the arc of theconvex arc surface 611a of thelower end portion 61 coincides with thecenter 103 in the arc of theconcave arc surface 101 of theback pressure chamber 10, voids D are not formed between thevane 6 and theconcave arc surface 101 of theback pressure chamber 10, as illustrated inFig. 8(a) . In contrast, inembodiment 1, when theconvex arc surface 611a of thelower end portion 61 is brought into contact with the bottomside arc surface 101c of theback pressure chamber 10 so that thecenter 63 in the arc of theconvex arc surface 611a of thelower end portion 61 coincides with thecenter 103 in the arc of theconcave arc surface 101 of theback pressure chamber 10, the voids D are formed between thevane 6 and theconcave arc surface 101 of theback pressure chamber 10 on both sides in the thickness direction of the vane, as illustrated inFig. 3(a) . - On the other hand, in manufacturing the
rotor 4 of the invention using the manufacturing method described above, when thevane groove 5 is polished, the position of thevane groove 5 deviates from the position of theback pressure chamber 10, the center line C of thevane groove 5 in the thickness direction of thevane 6 and the center point P5 of theback pressure chamber 10 may deviate by approximately a predetermined dimension X1 along the thickness direction of thevane 6 from a set position, as illustrated inFigs. 3 (b) and8 (b) . In addition, thecenter 63 in the arc of theconvex arc surface 611a of thecontact surface 611 and thecenter 103 in the arc of theconcave arc surface 101 of theback pressure chamber 10 also deviate by the predetermined dimension X1 along the thickness direction of thevane 6, as illustrated inFigs. 3(b) and8(b) . - Since the voids D are not formed between the
vane 6 and the concave arc surface of theback pressure chamber 10 on both sides in the thickness direction of the vane in the comparative example inFig. 8 , the shoulder portions K1 and K2 of thelower end portion 61 override the 101a and 101b of theside arc surfaces back pressure chamber 10 as illustrated inFig. 8(b) when thevane 6 enters the deepest part of thevane groove 5. A clearance G1 is generated between thecenter 63 in the arc of theconvex arc surface 611a of thelower end portion 61 and thecenter 103 in the arc of theconcave arc surface 101 of theback pressure chamber 10 along the forward or backward travel direction of thevane 6. Since this clearance G1 is large, the upper end portion of thevane 6 projects from the outer peripheral surface of therotor 4, thevane 6 interferes with the inner peripheral surface of thecylinder 8a, possibly disabling the rotation of therotor 4. - In contrast, since the voids D are formed between the
vane 6 and theconcave arc surface 101 of theback pressure chamber 10 on both sides in the thickness direction of the vane inembodiment 1, the shoulder portions K1 and K2 of thelower end portion 61 have difficulty in overriding the arc surface on the 101a and 101b of theside arc surfaces back pressure chamber 10 as illustrated inFig. 3(b) . Since theconvex arc surface 611a of thelower end portion 61 is raised along the arc of theconcave arc surface 101 of theback pressure chamber 10, a clearance G2 is generated along the forward or backward travel direction of thevane 6 between thecenter 63 of the arc surface of thelower end portion 61 and thecenter 103 of the arc surface of theconcave arc surface 101 of theback pressure chamber 10, as illustrated inFig. 3(b) . However, since this clearance G2 is small, the upper end portion of thevane 6 does not project from the outer peripheral surface of therotor 4 inembodiment 1, thevane 6 does not interfere with the inner peripheral surface of thecylinder 8a, thereby preventing the rotation of therotor 4 from being disabled. -
Fig. 4 illustrates the other example ofembodiment 1 illustrated inFig. 3 . The other example ofembodiment 1 will be described below with reference toFig. 3 . However, the same components as inembodiment 1 are given the same reference numerals in principle and descriptions are omitted. - The
lower end portion 61 of thevane 6 in the other example ofembodiment 1 is the same as thelower end portion 61 illustrated inFig. 3 in that theentire contact surface 611 facing the bottomside arc surface 101c of theback pressure chamber 10 is theconvex arc surface 611a along the arc S2. In contrast, in thelower end portion 61 of thevane 6 in the other example ofembodiment 1, the curvature radius L4 of the arc S2 forming theconvex arc surface 611a is larger than substantially the half of the dimension L2 in the thickness direction of thevane 6 and smaller than the curvature radius L3 of the arc S1 forming theconcave arc surface 101 of theback pressure chamber 10. Accordingly, theconvex arc surface 611a of thelower end portion 61 is smaller than a half peripheral surface and the center point P5 of the arc S2 is disposed closer to the slidingcontact surface 6a of thevane 6 than the shoulder portions K1 and K2 of thelower end portion 61. - Also in the other example of
embodiment 1, when the position of thevane grooves 5 does not deviate from the position of theback pressure chamber 10, as illustrated inFig. 4(a) , the center point P4 of the arc S1 does not deviate from the center point P5 of the arc S2, these center points are present in the center line C of thesame vane groove 5, and thecenter 63 in the arc of theconvex arc surface 611a of thelower end portion 61 can coincide with thecenter 103 in the arc of theconcave arc surface 101 of theback pressure chamber 10. - In addition, also in the other example of
embodiment 1, when theconvex arc surface 611a of thelower end portion 61 is brought into contact with the bottomside arc surface 101c of theback pressure chamber 10 so that thecenter 63 in the arc of theconvex arc surface 611a of thelower end portion 61 coincides with thecenter 103 in the arc of theconcave arc surface 101 of theback pressure chamber 10 as illustrated inFig. 4(a) , the voids D are formed between thevane 6 and the concave arc surface of theback pressure chamber 10 on both sides in the thickness direction of vane, unlike the comparative example inFig. 8 . - Accordingly, even when the
vane groove 5 deviates from theback pressure chamber 10 along the thickness direction of the vane, since the voids D are generated between thevane 6 and theconcave arc surface 101 of theback pressure chamber 10 on both sides in the thickness direction of the vane, the shoulder portions K1 and K2 of thelower end portion 61 have difficulty in overriding the 101a and 101b of theside arc surfaces back pressure chamber 10 as illustrated inFig. 4(b) . In addition, the clearance G2 inFig. 4(b) generated because theconvex arc surface 611a of thelower end portion 61 is raised along the arc of theconcave arc surface 101 of theback pressure chamber 10 is small as inembodiment 1 inFig. 3 , so the upper end portion of thevane 6 does not project from the outer peripheral surface of therotor 4 also in the other example ofembodiment 1, thevane 6 does not interfere with the inner peripheral surface of thecylinder 8a, thereby preventing the rotation of therotor 4 from being disabled. -
Figs. 5 and6 illustrateembodiment 2 as described above.Embodiment 2 will be described below with reference toFigs. 5 and6 . However, the same components as inembodiment 1 and the other example ofembodiment 1 are given the same reference numerals in principle and descriptions are omitted. - In the
lower end portion 61 of thevane 6 inembodiment 2, thecontact surface 611 includes theconvex arc surface 611a and two tangentialflat surfaces 611b continued to theconvex arc surface 611a. - As illustrated in
Fig. 5 , theconvex arc surface 611a is formed along an arc S3a of a circle S3, centered at P6, that has a radius L5 smaller than the radius L3 of the arc S1 forming theconcave arc surface 101 of theback pressure chamber 10, the arc S3a facing the bottomside arc surface 101c. The tangentialflat surfaces 611b are formed so as to make contact with the arc S3a forming theconvex arc surface 611a inembodiment 2 and the contactflat surfaces 611b are flat surfaces extending from both ends of the arc S3 toward the shoulder portions K1 and K2 while being inclined toward the slidingcontact surfaces 6a of thevane 6. - As illustrated in
Fig. 6 , the shape of thelower end portion 61 of thevane 6 inembodiment 2 can also be formed by, for example, providing theflat surfaces 611b on both sides in the thickness direction of thelower end portion 61 at the same angle as the oblique angle of the tangential flat surface of the arc surface (arc S1) passing through a point P7 at which the arc S1 forming theconcave arc surface 101 of theback pressure chamber 10 and a virtual line V extending from the inner side surface of thevane groove 5 intersect and by connecting the intersection of theflat surface 611b and theflat surface 611b via the arc S3a of the contact circle S3 having the curvature radius L5 smaller than the curvature radius L3 of the arc S1 forming the concave arc surface of theback pressure chamber 10. It should be noted that theflat surface 611b may be slightly inclined toward the shaft line of thevane groove 5 from the same angle as the oblique angle of the tangential flat surface of the arc surface (arc S1) passing through the point P7, which is not illustrated. - Also in
embodiment 2, when the position of thevane grooves 5 does not deviate from the position of theback pressure chamber 10, the center point P4 of the arc S1 does not deviate from the center point P6 of the circle S3 (arc S3a) as illustratedFig. 5(a) , these center points are present in the center line C in thesame vane groove 5, and thecenter 63 in the arc of theconvex arc surface 611a of thelower end portion 61 can coincide with thecenter 103 in the arc of theconcave arc surface 101 of theback pressure chamber 10. - In addition, also in
embodiment 2, as illustrated inFig. 5 (a) , when theconvex arc surface 611a of thelower end portion 61 makes contact with the bottomside arc surface 101c of theback pressure chamber 10 so that thecenter 63 in the arc of theconvex arc surface 611a of thelower end portion 61 coincides with thecenter 103 in the arc of theconcave arc surface 101 of theback pressure chamber 10, the voids D are formed between thevane 6 and the concave arc surface of theback pressure chamber 10 on both sides in the thickness direction of the vane, unlike the comparative example inFig. 8 . - Accordingly, even when the
vane groove 5 deviates from theback pressure chamber 10 along the thickness direction of the vane, since the voids D are generated between thevane 6 and theconcave arc surface 101 of theback pressure chamber 10 on both sides in the thickness direction of the vane, the shoulder portions K1 and K2 of thelower end portion 61 have difficulty in overriding the 101a and 101b of theside arc surfaces back pressure chamber 10 as illustrated inFig. 5(b) . In addition, the clearance G2 inFig. 5(b) generated because theconvex arc surface 611a of thelower end portion 61 is raised along the arc of theconcave arc surface 101 of theback pressure chamber 10 is small as in the above embodiments, so the upper end portion of thevane 6 does not project from the outer peripheral surface of therotor 4 also inembodiment 2, thevane 6 does not interfere with the inner peripheral surface of thecylinder 8a, thereby preventing the rotation of therotor 4 from being disabled. -
Fig. 7 illustrateembodiment 3 as described above.Embodiment 3 will be described below with reference toFig. 7 . However, the same components as in the embodiments described above are given the same reference numerals in principle and descriptions are omitted. - The
lower end portion 61 of thevane 6 inembodiment 3 is tapered by partially removing the slidingcontact surface 6a and a part of theconvex arc surface 611a of thevane 6 and forming the chamferedoblique surface 101c with respect to theconvex arc surface 611a (the curvature radius L4 of the arc S2 is the same as the curvature radius L3 of the arc S1 forming theconcave arc surface 101 of the back pressure chamber 10) having theentire contact surface 611 facing the bottomside arc surface 101c of theback pressure chamber 10 disposed along the arc S2 about the center point P5. However, although not illustrated, the curvature radius L4 of the arc S2 may be smaller than the curvature radius L3 of the arc S1 forming theconcave arc surface 101 of theback pressure chamber 10. In addition, the chamferedoblique surface 101c may be formed by partially removing the slidingcontact surface 6a of thevane 6 or theconvex arc surface 611a. - When the position of the
vane grooves 5 does not deviate from the position of theback pressure chamber 10, the center point P4 of the arc S1 does not deviate from the center point P5 of the circle S2 as illustrated inFig. 7(a) , these center points are present in the center line C in thesame vane groove 5, and thecenter 63 in the arc of theconvex arc surface 611a of thelower end portion 61 can coincide with thecenter 103 in the arc of theconcave arc surface 101 of theback pressure chamber 10. - In addition, also in
embodiment 3, as illustrated inFig. 7 (a) , when theconvex arc surface 611a of thelower end portion 61 makes contact with the bottomside arc surface 101c of theback pressure chamber 10 so that thecenter 63 in the arc of theconvex arc surface 611a of thelower end portion 61 coincides with thecenter 103 in the arc of theconcave arc surface 101 of theback pressure chamber 10, the voids D are formed between thevane 6 and the concave arc surface of theback pressure chamber 10 on both sides in the thickness direction of the vane, unlike the comparative example inFig. 8 . - Accordingly, even when the
vane groove 5 deviates from theback pressure chamber 10 along the thickness direction of the vane, since the voids D are generated between thevane 6 and theconcave arc surface 101 of theback pressure chamber 10 on both sides in the thickness direction of the vane, the shoulder portions K1 and K2 of thelower end portion 61 have difficulty in overriding the 101a and 101b of theside arc surfaces back pressure chamber 10 as illustrated inFig. 7(b) . In addition, the clearance G2 inFig. 7(b) generated because theconvex arc surface 611a of thelower end portion 61 is raised along the arc of theconcave arc surface 101 of theback pressure chamber 10 is small as in the above embodiments, so the upper end portion of thevane 6 does not project from the outer peripheral surface of therotor 4 also inembodiment 3, thevane 6 does not interfere with the inner peripheral surface of thecylinder 8a, thereby preventing the rotation of therotor 4 from being disabled. -
- 1:
- vane compressor
- 4:
- rotor
- 5:
- vane groove
- 6:
- vane
- 6a:
- sliding contact surface
- 61:
- lower end portion (other end portion)
- 611:
- contact surface
- 611a:
- convex arc surface
- 611b:
- tangential flat surface, flat surface
- 611c:
- chamfered oblique surface
- 63:
- center in arc of convex arc surface
- 8a:
- cylinder
- 10:
- back pressure chamber
- 101:
- concave arc surface
- 101a, 101b:
- side arc surface
- 101c:
- bottom side arc surface
- 103:
- center in arc of concave arc surface
- K1, K2:
- shoulder portion of vane
- D:
- void
Claims (4)
- A vane compressor comprising:a cylinder having both ends closed by side block members;a rotor rotatably provided in the cylinder;a vane groove formed radially inward from an outer peripheral surface of the rotor; anda vane housed in the vane groove movably forward and backward, one end portion of the vane making slidable contact with an inner peripheral surface of the cylinder as the rotor rotates,wherein a back pressure chamber having a concave arc surface is formed on a bottom of the vane groove, the other end portion of the vane has a convex arc surface facing the concave arc surface of the vane groove, and voids are generated between the other end portion of the vane and the bottom of the vane groove on both sides in a thickness direction of the vane when the other end portion of the vane makes contact with the bottom of the vane groove.
- The vane compressor according to claim 1,
wherein the convex arc surface of the other end portion of the vane has a curvature radius smaller than the concave arc surface on the bottom of the vane groove and
the voids are thereby generated on both sides of a contact portion between the other end portion of the vane and the bottom of the vane groove. - The vane compressor according to claim 2,
wherein tangential flat surfaces continued to the convex arc surface are formed on both sides in the thickness direction of the other end portion of the vane. - The vane compressor according to claim 1 or 2,
wherein sliding contact surfaces in slidable contact with the vane groove are formed on both sides in the thickness direction of the vane,
chamfering for partially removing the sliding contact surfaces and the convex arc surface is performed between the sliding contact surfaces and the convex arc surface of the other end portion of the vane, and
the voids are thereby provided.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2015130554 | 2015-06-30 | ||
| PCT/JP2016/069083 WO2017002785A1 (en) | 2015-06-30 | 2016-06-28 | Vane compressor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP3318760A1 true EP3318760A1 (en) | 2018-05-09 |
| EP3318760A4 EP3318760A4 (en) | 2019-02-27 |
Family
ID=57608765
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP16817893.7A Withdrawn EP3318760A4 (en) | 2015-06-30 | 2016-06-28 | Vane compressor |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP3318760A4 (en) |
| JP (1) | JPWO2017002785A1 (en) |
| WO (1) | WO2017002785A1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN119609701B (en) * | 2025-01-02 | 2025-10-24 | 中国航发北京航空材料研究院 | Positioning device and method for single set triple turbine guide vane |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3869231A (en) * | 1973-10-03 | 1975-03-04 | Abex Corp | Vane type fluid energy translating device |
| JPH0538379U (en) * | 1991-10-29 | 1993-05-25 | カルソニツク株式会社 | Rotary compressor |
| JP3108018B2 (en) * | 1996-07-03 | 2000-11-13 | カルソニックカンセイ株式会社 | Rotary compressor |
-
2016
- 2016-06-28 WO PCT/JP2016/069083 patent/WO2017002785A1/en not_active Ceased
- 2016-06-28 JP JP2017526357A patent/JPWO2017002785A1/en active Pending
- 2016-06-28 EP EP16817893.7A patent/EP3318760A4/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| JPWO2017002785A1 (en) | 2018-04-12 |
| EP3318760A4 (en) | 2019-02-27 |
| WO2017002785A1 (en) | 2017-01-05 |
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