CA2088160C - Rotary compressor - Google Patents
Rotary compressorInfo
- Publication number
- CA2088160C CA2088160C CA 2088160 CA2088160A CA2088160C CA 2088160 C CA2088160 C CA 2088160C CA 2088160 CA2088160 CA 2088160 CA 2088160 A CA2088160 A CA 2088160A CA 2088160 C CA2088160 C CA 2088160C
- Authority
- CA
- Canada
- Prior art keywords
- roller
- shaft
- generated
- grooves
- oil 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.)
- Expired - Fee Related
Links
- 230000007423 decrease Effects 0.000 claims abstract description 18
- 230000002093 peripheral effect Effects 0.000 claims abstract description 15
- 239000003921 oil Substances 0.000 abstract description 67
- 239000010687 lubricating oil Substances 0.000 abstract description 30
- 230000003247 decreasing effect Effects 0.000 abstract 1
- 239000003507 refrigerant Substances 0.000 description 13
- 230000006835 compression Effects 0.000 description 12
- 238000007906 compression Methods 0.000 description 12
- 230000000694 effects Effects 0.000 description 10
- 239000000306 component Substances 0.000 description 8
- 230000000717 retained effect Effects 0.000 description 8
- 238000001816 cooling Methods 0.000 description 5
- 208000036366 Sensation of pressure Diseases 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 230000002542 deteriorative effect Effects 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 238000005057 refrigeration Methods 0.000 description 1
Classifications
-
- 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
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0021—Systems for the equilibration of forces acting on the pump
-
- 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
- F04C27/00—Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Abstract
The same number of grooves 20 through 27 are provided in end surfaces 19a and 19b of a roller 19. The grooves 20 through 27 have communicating portions 20a through 27a which communicate with an inner peripheral side of the roller 19 and sealed portions 20b, 20c, 20d, 20e, 20f through 27b, 27c, 27d, 27e and 27f whose cross-sectional area decreases. Accordingly, the cross-sectional area is decreased in a direction in which a lubricating oil flows, and a plurality of oil pressures can thus be obtained. This makes a clearance of the roller 19 fixed.
Description
l Title of the Invention ROTARY COMPRESSOR
Technical Field The present invention relates to a rotary compressor which is for use in the refrigerating cycle of a refrigerator or freezer and which is provided with a compression mechanical portion having an excellent volu-meric efficiency.
Background Art In recent years, there has been an increasing demand for a reduction in the size of a compressor for use in the refrigerating cycle. This is achieved by employing a rotary type compressor in place of a reciprocating type compressor.
However, the rotary compressor has a drawback in that the motion of a roller is unstable because the direction of the rotation thereof on its own axis changes during a single rotation thereof, deteriorating the volumeric efficiency thereof.
A conventional rotary compressor will be described below in detail with reference to Figs. 1 through 4.
Reference numeral 1 denotes a sealed casing and 2 denotes an electric motor portion which is coupled, 20881~0 1 through a shaft 3, to a mechanical portion body 9 including a cylinder 4, a roller 5, a vane 6, a main bearing 7 and a sub bearing 8. The shaft 3 has a main shaft 3a, a sub shaft 3b and a crank 3c which is eccentric from the axis of the main and sub shafts 3a and 3b by E. The shaft 3 has a hole 3e at the center thereof, and the crank 3c has an oil supplying hole 3f and an oil supplying groove 3g. Reference numeral 10 denotes a spring provided on the rear surface of the vane, and lla and llb respectively denote a suction chamber and a compression chamber formed within the cylinder 4 by the roller 5, the vane 6 and the main and sub bearings 7 and 8. The inner peripheral sides of end surfaces 5a and 5b of the roller 5 which respectively face the main and sub bearings 7 and 8 are tapered to form tapered portions 5c and 5d whose cross-sectional area decreases toward the outer peripheral side thereof.
Reference numeral 12 denotes an oil supplying mechanism coupled to the shaft 3. Reference numeral 13 denotes a suction pipe which communicates with the suction chamber lla via a suction passage 14 formed in the sub bearing 8 and the cylinder 4. 15 denotes a discharge hole which communicates with the interior of the sealed casing via a discharge valve 16. 17 denotes a discharge pipe which is opened into the sealed casing 1. 18 denotes a lubricat-ing oil.
In Fig. 4, the arrow of the solid line indi-cates the direction of the motion of the roller 5 which 20~81~0 1 is obtained at a certain time during the operation of the compressor, and the arrow of the broken line indicates the direction in which the lubricating oil 18 flows over the end surfaces 5a and 5b of the roller as a consequence of the operation of the roller 5. Reference numeral 5e denotes a portion of the tapered portion 5c or 5d of the roller 5 whose cross-sectional area gradually decreases in the direction indicated by the arrow of the broken line, and 5f denotes a portion whose cross-sectional area gradually increases in the same direction.
The compression mechanism of the rotary compressor will now be described. A refrigerant gas supplied from a cooling system (not shown) passes through the suction pipe 13 and the suction hole 14, and then reaches the suction chamber lla of the cylinder 4.
Thereafter, the refrigerant gas is gradually compressed by the rotary motion of the shaft 3 which is generated by the rotation of the electric motor portion 2 in the compression chamber llb defined by the roller 5 rotatably supported by the crank 3c of the shaft 3 and the vane 6.
The compressed refrigerant gas is discharged into the interior of the sealed casing 1 through the discharge hole 15 and the discharge valve 16, and then discharged into the cooling system through the discharge pipe 17.
The high-pressure lubricating oil 18 with the refrigerant contained therein and contained in the sealed casing 1 is supplied to the hole 3e of the shaft 3 by means of the oil supplying mechanism 12. Thereafter, the 208~160 1 lubricating oil 18 is supplied to the sliding portion of the main and sub bearings 7 and 8 and to the crank 3c and the inner peripheral side of the roller 5 from the oil supplying hole 3f and the oil supplying groove 3g to lubricate the roller end surfaces 5a and 5b. Subsequ-ently, the lubricating oil 18 passes through the suction chamber lla and the compression chamber llb, is dis-charged into the sealed casing 1 from the discharge hole 15, and then stays at the bottom of the sealed casing 1.
As the shaft 3 is rotated, the roller 5 rotates while turning round about the crank 3c in either of two directions. Consequently, the locus of a certain point on the roller 5 is spiral, and the direction of the movement of the roller 5 changes about 360 while the shaft 3 is rotated. Assuming that the direction of the spiral motion of the roller 5 is that indicated by the arrow in Fig. 4, since the tapered portions 5c and 5d are provided on the end surfaces 5a and 5b of the roller 5 and the cross-section of the portion 5e gradually decreases toward the outer diameter side of the roller, only the lubricating oil 18 which flows into the vicinity of the portion 5e in the tapered portion 5c or 5e gene-rates an oil pressure due to the wedge effect. Consequ-ently, the oil pressure near the tapered portion 5c balances the oil pressure near the tapered portion 5d, and the roller 5 is thus retained such that a clearance ~a between the roller 5 and the main bearing 7 is equal to a clearance ~b between the roller 5 and the sub 2û88160 l bearing 8. The amount of lubricating oil with the refrigerant contained therein which flows into the suction chamber lla and the compression chamber llb from the crank 3c through the roller end surfaces 5a and 5b is proportional to the cube of the clearance. Therefore, where ~a + ~b = constant, the amount of lubricating oil which flows in is at a rinir~lm when ~a = ~b. Thus, the provision of the tapered portions 5c and 5d assures a compressor exhibiting an excellent volumeric efficiency and hence a high efficiency.
Such a compressor is disclosed in, for example, Japanese Utility Model Publication No. 61-20317.
However, in a compressor which has the above-described structure and in which the thickness of the roller, indicated by (outer diameter - inner diameter)/2, is small and the ratio of the high pressure to the low pressure during operation (compression ratio) is high, as in the case of a small compressor for refrigeration having a small cubic capacity, even if the clearance between the end surface of the roller and the main bearing is made equal to the clearance between the end surface of the roller and the sub bearing by the provision of the tapered portions, the clearance of the tapered portion provided over the entire periphery practically increases by a value corresponding to the amount of taper and the sealed distance of the flat surface where no tapered portion is provided decreases over the entire periphery, increasing the amount of 1 lubricating oil with the refrigerant contained therein which flows into the suction chamber and the compression chamber. Thus, the provision of the tapered portion does not ensure reduction in the leakage loss and implo~ell.ent in the volumeric efficiency.
The above-described structure utilizes the wedge effect of the lubricating oil which enters the tapered portion. This wedge effect is generated by the component of the roller rotation in the spiral motion thereof caused by the rotation of the shaft and not generated by the component of the roller rotation about the crank, because the cross-sectional area of the tapered portion r~mA i ns the same in the circumferential direction, and is thus low. Furthermore, the oil pressure is generated by the wedge effect only at the single portion on the end surface of the roller, and no oil pressure is generated at most of the portion of the end surface. Furthermore, since the tapered portion has a shape which continues in the circumferential direction, the pressure generated by the wedge effect may escape in the circumferential direction, reducing the pressure generated by the wedge effect. Therefore, the stability of the roller achieved by the wedge effect is not suffi-cient, and the improvement in the volumeric efficiency is low.
Disclosure of Invention A primary object of the present invention is to 1 stabilize the motion of a roller and thereby improve the volumeric efficiency of the compressing mechanism portion.
A secondary object of the present invention is to minimize the amount of lubricating oil with a refrige-rant contained therein which flows into a suction chamber and a compression chamber.
Practically, a groove, having a communicating portion which communicates with an inner peripheral side of a roller as well as a plurality of sealed portions which extend substantially in a circumferential direction and whose cross-sectional area decreases as a distance to the communicating portion increases, is provided in each of end surfaces of the roller which face a main bearing and a sub bearing.
Furthermore, a plurality of grooves, which communicate with an inner peripheral side of a roller and which face an end surface of the roller at least once during a single rotation of a shaft, are formed in a main bearing and a sub bearing which face the roller.
Brief Description of the Drawings Fig. 1 is a longitudinal cross-sectional view of a conventional rotary compressor;
Fig. 2 is a section taken along the line II -II' of Fig. 1;
Fig. 3 is an enlarged cross-sectional view of a mechanical portion of Fig. l;
l Fig. 4 is a front view of a roller of Fig. 1;
Fig. 5 is a front view of a roller of a rotary compressor showing a first embodiment of the present invention;
Fig. 6 is an enlarged cross-sectional view of a mechanical portion of Fig. 5;
Fig. 7 is a front view of a roller of a rotary compressor showing a second embodiment of the present invention;
Fig. 8 is an enlarged cross-sectional view of a mechanical portion of Fig. 7;
Fig. 9 is a front view of a roller of a rotary compressor showing a third embodiment of the present invention;
Fig. 10 is an enlarged cross-sectional view of a mechanical portion of Fig. 9;
Fig. 11 is a front view of a roller of a rotary compressor showing a fourth embodiment of the present invention;
Fig. 12 is an enlarged cross-sectional view of a mechanical portion of Fig. 11; and Figs. 13 and 14 are cross-sectional views showing the operation of the mechanical portion of Fig.
11 .
Best Mode for Carrying Out the Invention Embodiments of the present invention will now be described with reference to the accompanying drawings 1 in which identical reference numerals to those in Figs. 1 through 4 represent similar or identical elements and description thereof is omitted.
Figs. 5 and 6 illustrates a first embodiment of the present invention.
Reference numeral 19 denotes a roller which is rotatably retained by the crank 3c of the shaft 3, as in the case of the conventional compressor. The same number of grooves 20 through 27 are formed on end surfaces l9a and l9b of the roller 19. The grooves 20 through 27 are respectively formed by communicating portions 20a through 27a which communicate with the inner peripheral portion of the roller 19, and sealing portions 20b through 27b and 20c through 27c which extend from the communicating portions 20a through 27a in the circumferential direction and whose cross-sectional area decreases as a distance to the c~ nicating portions 20a through 27a increases.
In such a structure, the refrigerant gas sucked from the suction pipe 13 is compressed and discharged to the cooling system from the discharge pipe 17 in the same manner as that of the conventional compressor.
The high-pressure lubricating oil 18 with the refrigerant contained therein which is contained in the sealed casing 1 lubricates the mechanical portion body 9 in the same manner as that of the conventional compres-sor. The lubricating oil 18 which flows into the inner peripheral side of the roller 19 lubricates the rollers l9a and l9b, and then returns to the bottom portion of -, ~
1 the sealed casing in the same manner as that of the conventional compressor.
As the shaft 3 is rotated, the roller 19 revolves while turning round about the crank, as in the case of the conventional compressor. As a result, the roller 19 goes on the spiral motion. The direction of the spiral motion which is obtained at a certain instance is indicated by the arrow of the solid line, and the direction in which the lubricating oil 18 flows as a consequence of the motion of the roller 19 is indicated by the arrow of the broken line, as in the case of the conventional compressor.
At that time, in the grooves 20 through 27 formed on the end surface l9a of the roller 19, the sealed portions 20c, 21c, 23b, 24b, 25b, 26b, 26c and 27c in the sealed portions 20b through 27b and 20c through 27c reduce their cross-sectional area in the direction of flow of the lubricating oil 18 which is indicated by the arrow of the broken line, generating a pressure of the lubricating oil 18 which flows in from the communicating portions 20a through 27a.
That is, in the grooves 20 through 27 except for the groove 22, the oil pressure is generated at either of or both of the sealed portions 20b through 27b and 20c through 27c, and the positions where the oil pressure is generated are thus distributed over the end surface l9a of the roller 19, unlike the conventional compressor in which the oil pressure is generated at only 1 a single position. In addition, generation of the oil pressure occurs in the grooves 20 through 27 formed on the end surface l9b in the same manner as that for the grooves 20 through 27 formed on the end surface l9a: in all the grooves except for the groove 22 located at a position symmetrical with respect to the position of the groove 22 formed on the end surface l9a, the oil pressure is generated at either of or both of the sealed portions 20b through 27b and 20c through 27c, and the positions on the end surface l9b where the oil pressure is generated are symmetrical with respect to the positions on the end surface l9a where the oil pressure is generated.
Regarding the component of the roller rotation about the crank which forms the spiral motion of the roller 19, since the sealed portions 20b through 27b and 20c trough 27c are formed in such a manner that the cross-sectional area thereof decreases substantially in the circumferential direction, the oil pressure due to the wedge effect is generated in the sealed portions whichever direction the roller 19 is rotated about the crank. Furthermore, since the oil pressure is generated near the sealed portions 20b through 27b and 20c through 20c, it cannot escape from the sealed portions, and the oil pressure is thus increased. Therefore, the same amount of oil pressure is generated on the end surfaces l9a and l9b of the roller 19 over the distributed positions, and the generated oil pressures thus balance.
In addition, since the generated oil pressure is higher 1 than the conventionally generated oil pressure because of an increase in the oil pressure generated by the compo-nent of the roller rotation about the crank and the incapability of escape of the generated oil pressure, the roller 19 can be retained at a position which ensures ~a = ~b during one rotation more reliably than the conven-tional roller, and the volumeric efficiency of the compressor can thus be improved.
Furthermore, since the grooves 20 through 27 are not provided over the entire periphery, the sealed distance is longer than that obtained when the tapered portions are provided. Thus, the amount of lubricating oil which flows into the compression chamber and the suction chamber is reduced, and this makes improvement in the volumeric efficiency possible even in the case of a small compressor in which the thickness of the roller is small.
A second embodiment of the present invention will be described below with reference to Figs. 7 and 8.
In the following description, only the differences between the first and second embodiments will be explained.
The same number of grooves 28 through 35 are formed on the end surfaces l9a and l9b of the roller 19.
The grooves 28 through 35 are respectively formed by communicating portions 28a through 35a which communicate with the inner peripheral portion of the roller 19, and sealing portions 28b through 35b, 28c through 35c, 28d l through 35d, 28e through 35e and 28f through 35f which extend from the communicating portions 28a through 35a substantially radially and whose cross-sectional area decreases as a distance to the communicating portions 28a through 35a increases.
In such a structure, the refrigerant gas sucked from the suction pipe 13 is compressed and discharged to the cooling system from the discharge pipe 17 in the same manner as that of the conventional compressor.
The high-pressure lubricating oil 18 with the refrigerant contained therein which is contained in the sealed casing 1 lubricates the mechanical portion body 9 in the same manner as that of the conventional compres-sor. The lubricating oil 18 which flows into the inner peripheral side of the roller 19 lubricates the rollers l9a and l9b, and then returns to the bottom portion of the sealed casing in the same manner as that of the conventional compressor.
As the shaft 3 is rotated, the roller 19 revolves while rotating about the crank, as in the case of the conventional compressor. As a result, the roller 19 performs the spiral motion. The direction of the spiral motion which is obtained at a certain instance is indicated by the arrow of the solid line, and the direc-tion in which the lubricating oil 18 flows as a consequ-ence of the motion of the roller 19 is indicated by the arrow of the broken line, as in the case of the conventional compressor.
~ - 14 -l At that time, in the grooves 28 through 35 formed on the end surface l9a of the roller l9, a pressure of the lubricating oil 18 which flows in from the communicating portions 28a through 35a is generated at the sealed portions whose cross-sectional area decreases in the direction of flow of the lubricating oil 18 which is indicated by the arrow of the broken line in the sealed portions 28b through 35b, 28c through 35c, 28d through 35d, 28e through 35e and 28f through 35f. In the groove 28, for example, an oil pressure is generated at the sealed portions 28e and 28f. In the groove 32, an oil pressure is generated at the sealed portions 32c and 32d. That is, in all the grooves 28 through 35, the oil pressure is generated at two portions, and the positions where the oil pressure is generated are thus distributed over the end surface l9a of the roller 19, unlike the conventional compressor in which the oil pressure is generated at only a single position. In addition, gener-ation of the oil pressure occurs on the end surface l9b in the same manner as that for the end surface l9a.
Therefore, the positions on the end surface l9b where the oil pressure is generated are symmetrical with respect to the positions on the end surface l9a where the oil pres-sure is generated, and the oil pressure generated on the end surfaces l9a and l9b thus balance with each other.
Regarding the component of the roller rotation about the crank which forms the spiral motion of the roller 19, since the sealed portions 28c through 35c, 28d 1 through 35d, 28e through 3Se and 28f through 35f are formed in such a manner that the cross-sectional area thereof decreases substantially in the circumferential direction, the oil pressure due to the wedge effect is generated in these sealed portions whichever direction the roller 19 is rotated about the crank. Furthermore, since the oil pressure is generated near the sealed portions 28b through 35b, 28c through 35c, 28d through 35d, 28e through 35e and 28f through 35f, it cannot escape from the sealed portions, and the oil pressure is retained high. Therefore, the same amount of oil pres-sure is generated on the end surfaces l9a and l9b of the roller 19 over the distributed positions, and the gene-rated oil pressures thus balance. In addition, since the generated oil pressure is higher than the conventionally generated oil pressure because of an increase in the number of positions where the oil pressure is generated, an increase in the amount of oil pressure generated by the component of the roller rotation about the crank and the incapability of escape of the generated oil pressure, the roller 19 can be retained at a position which ensures ~a = ~b during one rotation more reliably than the conventional roller, and the volumeric efficiency of the compressor can thus be improved while the leakage loss can be reduced.
Furthermore, since the grooves 28 through 35 are not provided over the entire periphery, the sealed distance is longer than that obtained when the tapered 1 portions are provided. Thus, the amount of lubricating oil which flows into the compression chamber and the suction chamber is reduced, and this makes an improvement in the volumeric efficiency possible even in the case of a small compressor in which the thickness of the roller is small.
A third embodiment of the present invention will be described below with reference to Figs. 9 and 10.
Grooves 37 through 44 are formed in each of the end surfaces 36a and 36b of the roller 36. In the grooves 37 through 44, co~llnicating portions 37a through 44a are formed in such a manner that they pass the inner peripheral portion of the roller 36 and the grooves 37 through 44, and sealed portions 37b through 44b, 37c through 44c, 37d through 44d, 37e through 44e and 37f through 44f are formed radially from portions of the communicating portion 37a through 44a which open into the grooves 37 through 44. In this embodiment, an oil pressure is generated due to the spiral motion of the roller at the sealed portions 37b through 44f, as in the cases of the previously described embodiments. At that time, since the communicating portions 37a through 44a are opened into the central portions of the grooves 37 through 44 and the distance from the communicating portions 37a through 44a to all the sealed portions 37b through 44f is hence the same, an oil pressure is gener-ated under the same conditions. Therefore, a higher oil pressure than that generated in the second embodiment can 1 be generated, and the lubricating oil can be supplied smoothly.
A fourth embodiment of the present invention will be described below with reference to Figs. 11 through 14.
Reference numerals 45 and 46 respectively denote a main bearing and a sub bearing which rotatably support the shaft 3 in the same manner as that of the conventional compressor. Reference numeral 47 designates a roller which is rotatably retained on the crank 3c of the shaft 3. The same number of grooves 48 through 55 are formed in the main and sub bearings 45 and 46. Each of the grooves 48 through 55 has a shape in which the cross-sectional area thereof is the largest at the center thereof and decreases in the circumferential and radial directions.
In Fig. 11, dot-dot-dashed lines indicate the inner peripheral surface of the cylinder 4, the vane 6 and the roller 47. Fig. 11 shows the positions relation between the grooves 48 through 55 and the roller 47 which is obtained at a certain rotational position.
Figs. 13 and 14 show the positional relation between the grooves 48 through 55 and the roller 47. In these figures, although the grooves 48 through 55 should have a hidden outline, they are indicated by the solid line for the ease of understanding.
In such a structure, the refrigerant gas sucked from the suction pipe 13 is compressed and discharged to - 18 - '~U88160 l the cooling system from the discharge pipe 17 in the same manner as that of the conventional compressor.
The high-pressure lubricating oil 18 with the refrigerant contained therein which is contained in the sealed casing 1 lubricates the mechanical portion body 9 in the same manner as that of the conventional compres-sor. The lubricating oil 18 which flows into the inner peripheral side of the roller 19 lubricates the rollers l9a and l9b, and then returns to the bottom portion of the sealed casing in the same manner as that of the conventional compressor.
As the shaft 3 is rotated, the roller 47 revolves while rotating about the crank, as in the case of the conventional compressor. The direction of the spiral motion which is obtained at a certain rotational _ angle is indicated by the arrow of the solid line in Fig.
13, as in the case of the conventional compressor.
At that time, the grooves 50, 51, 52 and 53 in the grooves 48 through 55 of the main bearing 45 are sealed by the end surface of the roller 47. The grooves 48 through 55 of the sub bearing 46 are also sealed similarly. Since the grooves 48 through 55 have a shape in which the cross-sectional area thereof is the largest at the central portion thereof and decreases in the radial and circumferential directions, when the lubricat-ing oil moves within the sealed grooves 50 through 53 in the direction indicated by the solid line, an oil pressure is generated in the grooves 50 through 53. In l addition, the positions where the oil pressure is generated in the grooves S0 through 53 are symmetrical.
That is, in this embodiment, the oil pressure is gener-ated on each of the two end surfaces of the roller 47 at four positions, and the oil pressure generated on one of the end surfaces balances the oil pressure generated on the other end surface.
Regarding the component of the roller rotation about the crank which forms the spiral motion thereof, since the grooves 48 and 55 are formed in such a manner that the cross-sectional area thereof decreases in the circumferential direction, the oil pressure is generated in the sealed grooves 50 through 53 due the wedge effect whichever direction the roller rotates about the crank.
In addition, since the grooves 48 through 55 are formed separately, the oil pressure generated in the sealed grooves 50 through 53 cannot escape from the sealed grooves, and the oil pressure is thus retained high.
Furthermore, as shown in Fig. 14, when the shaft 3 is rotated to another rotational position, the grooves 48, 49, 50 and 51 are now sealed by the end surface of the roller 47, and an oil pressure is gene-rated in each of these grooves. Thus, whichever of the rotational positions the shaft 3 is rotated, some grooves in the grooves 48 through 55 are sealed.
Therefore, the same amount of oil pressure is generated on the end surfaces of the roller 47 over the distributed positions, and the generated oil pressures 1 thus balance. In addition, since the generated oil pressure is higher than the conventionally generated oil pressure because of an increase in the amount of oil pressure generated by the component of the roller rotation about the crank and the incapability of escape of the generated oil pressure, the roller 47 can be retained at a position which ensures ~a = ~b during one rotation more reliably than the conventional roller, and the volumeric efficiency of the compressor can thus be improved while the power loss due to leakage can be reduced.
Furthermore, since the roller 47 faces only part of the grooves 48 through 55, the sealed distance is longer than that obtained when the tapered portion is provided. Consequently, the amount of lubricating oil which flows into the compression chamber is reduced, and this makes an improvement in the volumeric efficiency possible even in the case of a compressor in which the thickness of the roller is small.
Industrial Applicability As will be understood from the foregoing description, since the sealed portions of the lubricating oil and the communicating portions which communicate with the inner peripheral surface of the roller are formed in the contact surfaces between the roller and the main and sub bearings, the same amount of oil pressure can be generated over the distributed positions and the 1 generated oil pressures thus balance. Thus, if the rotary compressor is employed in a refrigerating cycle which is for use in, for example, a refrigerator or a freezer, the performance of the refrigerating cycle can be improved because the motion of the roller is stabi-lized and the volumeric efficiency is thus improved.
Technical Field The present invention relates to a rotary compressor which is for use in the refrigerating cycle of a refrigerator or freezer and which is provided with a compression mechanical portion having an excellent volu-meric efficiency.
Background Art In recent years, there has been an increasing demand for a reduction in the size of a compressor for use in the refrigerating cycle. This is achieved by employing a rotary type compressor in place of a reciprocating type compressor.
However, the rotary compressor has a drawback in that the motion of a roller is unstable because the direction of the rotation thereof on its own axis changes during a single rotation thereof, deteriorating the volumeric efficiency thereof.
A conventional rotary compressor will be described below in detail with reference to Figs. 1 through 4.
Reference numeral 1 denotes a sealed casing and 2 denotes an electric motor portion which is coupled, 20881~0 1 through a shaft 3, to a mechanical portion body 9 including a cylinder 4, a roller 5, a vane 6, a main bearing 7 and a sub bearing 8. The shaft 3 has a main shaft 3a, a sub shaft 3b and a crank 3c which is eccentric from the axis of the main and sub shafts 3a and 3b by E. The shaft 3 has a hole 3e at the center thereof, and the crank 3c has an oil supplying hole 3f and an oil supplying groove 3g. Reference numeral 10 denotes a spring provided on the rear surface of the vane, and lla and llb respectively denote a suction chamber and a compression chamber formed within the cylinder 4 by the roller 5, the vane 6 and the main and sub bearings 7 and 8. The inner peripheral sides of end surfaces 5a and 5b of the roller 5 which respectively face the main and sub bearings 7 and 8 are tapered to form tapered portions 5c and 5d whose cross-sectional area decreases toward the outer peripheral side thereof.
Reference numeral 12 denotes an oil supplying mechanism coupled to the shaft 3. Reference numeral 13 denotes a suction pipe which communicates with the suction chamber lla via a suction passage 14 formed in the sub bearing 8 and the cylinder 4. 15 denotes a discharge hole which communicates with the interior of the sealed casing via a discharge valve 16. 17 denotes a discharge pipe which is opened into the sealed casing 1. 18 denotes a lubricat-ing oil.
In Fig. 4, the arrow of the solid line indi-cates the direction of the motion of the roller 5 which 20~81~0 1 is obtained at a certain time during the operation of the compressor, and the arrow of the broken line indicates the direction in which the lubricating oil 18 flows over the end surfaces 5a and 5b of the roller as a consequence of the operation of the roller 5. Reference numeral 5e denotes a portion of the tapered portion 5c or 5d of the roller 5 whose cross-sectional area gradually decreases in the direction indicated by the arrow of the broken line, and 5f denotes a portion whose cross-sectional area gradually increases in the same direction.
The compression mechanism of the rotary compressor will now be described. A refrigerant gas supplied from a cooling system (not shown) passes through the suction pipe 13 and the suction hole 14, and then reaches the suction chamber lla of the cylinder 4.
Thereafter, the refrigerant gas is gradually compressed by the rotary motion of the shaft 3 which is generated by the rotation of the electric motor portion 2 in the compression chamber llb defined by the roller 5 rotatably supported by the crank 3c of the shaft 3 and the vane 6.
The compressed refrigerant gas is discharged into the interior of the sealed casing 1 through the discharge hole 15 and the discharge valve 16, and then discharged into the cooling system through the discharge pipe 17.
The high-pressure lubricating oil 18 with the refrigerant contained therein and contained in the sealed casing 1 is supplied to the hole 3e of the shaft 3 by means of the oil supplying mechanism 12. Thereafter, the 208~160 1 lubricating oil 18 is supplied to the sliding portion of the main and sub bearings 7 and 8 and to the crank 3c and the inner peripheral side of the roller 5 from the oil supplying hole 3f and the oil supplying groove 3g to lubricate the roller end surfaces 5a and 5b. Subsequ-ently, the lubricating oil 18 passes through the suction chamber lla and the compression chamber llb, is dis-charged into the sealed casing 1 from the discharge hole 15, and then stays at the bottom of the sealed casing 1.
As the shaft 3 is rotated, the roller 5 rotates while turning round about the crank 3c in either of two directions. Consequently, the locus of a certain point on the roller 5 is spiral, and the direction of the movement of the roller 5 changes about 360 while the shaft 3 is rotated. Assuming that the direction of the spiral motion of the roller 5 is that indicated by the arrow in Fig. 4, since the tapered portions 5c and 5d are provided on the end surfaces 5a and 5b of the roller 5 and the cross-section of the portion 5e gradually decreases toward the outer diameter side of the roller, only the lubricating oil 18 which flows into the vicinity of the portion 5e in the tapered portion 5c or 5e gene-rates an oil pressure due to the wedge effect. Consequ-ently, the oil pressure near the tapered portion 5c balances the oil pressure near the tapered portion 5d, and the roller 5 is thus retained such that a clearance ~a between the roller 5 and the main bearing 7 is equal to a clearance ~b between the roller 5 and the sub 2û88160 l bearing 8. The amount of lubricating oil with the refrigerant contained therein which flows into the suction chamber lla and the compression chamber llb from the crank 3c through the roller end surfaces 5a and 5b is proportional to the cube of the clearance. Therefore, where ~a + ~b = constant, the amount of lubricating oil which flows in is at a rinir~lm when ~a = ~b. Thus, the provision of the tapered portions 5c and 5d assures a compressor exhibiting an excellent volumeric efficiency and hence a high efficiency.
Such a compressor is disclosed in, for example, Japanese Utility Model Publication No. 61-20317.
However, in a compressor which has the above-described structure and in which the thickness of the roller, indicated by (outer diameter - inner diameter)/2, is small and the ratio of the high pressure to the low pressure during operation (compression ratio) is high, as in the case of a small compressor for refrigeration having a small cubic capacity, even if the clearance between the end surface of the roller and the main bearing is made equal to the clearance between the end surface of the roller and the sub bearing by the provision of the tapered portions, the clearance of the tapered portion provided over the entire periphery practically increases by a value corresponding to the amount of taper and the sealed distance of the flat surface where no tapered portion is provided decreases over the entire periphery, increasing the amount of 1 lubricating oil with the refrigerant contained therein which flows into the suction chamber and the compression chamber. Thus, the provision of the tapered portion does not ensure reduction in the leakage loss and implo~ell.ent in the volumeric efficiency.
The above-described structure utilizes the wedge effect of the lubricating oil which enters the tapered portion. This wedge effect is generated by the component of the roller rotation in the spiral motion thereof caused by the rotation of the shaft and not generated by the component of the roller rotation about the crank, because the cross-sectional area of the tapered portion r~mA i ns the same in the circumferential direction, and is thus low. Furthermore, the oil pressure is generated by the wedge effect only at the single portion on the end surface of the roller, and no oil pressure is generated at most of the portion of the end surface. Furthermore, since the tapered portion has a shape which continues in the circumferential direction, the pressure generated by the wedge effect may escape in the circumferential direction, reducing the pressure generated by the wedge effect. Therefore, the stability of the roller achieved by the wedge effect is not suffi-cient, and the improvement in the volumeric efficiency is low.
Disclosure of Invention A primary object of the present invention is to 1 stabilize the motion of a roller and thereby improve the volumeric efficiency of the compressing mechanism portion.
A secondary object of the present invention is to minimize the amount of lubricating oil with a refrige-rant contained therein which flows into a suction chamber and a compression chamber.
Practically, a groove, having a communicating portion which communicates with an inner peripheral side of a roller as well as a plurality of sealed portions which extend substantially in a circumferential direction and whose cross-sectional area decreases as a distance to the communicating portion increases, is provided in each of end surfaces of the roller which face a main bearing and a sub bearing.
Furthermore, a plurality of grooves, which communicate with an inner peripheral side of a roller and which face an end surface of the roller at least once during a single rotation of a shaft, are formed in a main bearing and a sub bearing which face the roller.
Brief Description of the Drawings Fig. 1 is a longitudinal cross-sectional view of a conventional rotary compressor;
Fig. 2 is a section taken along the line II -II' of Fig. 1;
Fig. 3 is an enlarged cross-sectional view of a mechanical portion of Fig. l;
l Fig. 4 is a front view of a roller of Fig. 1;
Fig. 5 is a front view of a roller of a rotary compressor showing a first embodiment of the present invention;
Fig. 6 is an enlarged cross-sectional view of a mechanical portion of Fig. 5;
Fig. 7 is a front view of a roller of a rotary compressor showing a second embodiment of the present invention;
Fig. 8 is an enlarged cross-sectional view of a mechanical portion of Fig. 7;
Fig. 9 is a front view of a roller of a rotary compressor showing a third embodiment of the present invention;
Fig. 10 is an enlarged cross-sectional view of a mechanical portion of Fig. 9;
Fig. 11 is a front view of a roller of a rotary compressor showing a fourth embodiment of the present invention;
Fig. 12 is an enlarged cross-sectional view of a mechanical portion of Fig. 11; and Figs. 13 and 14 are cross-sectional views showing the operation of the mechanical portion of Fig.
11 .
Best Mode for Carrying Out the Invention Embodiments of the present invention will now be described with reference to the accompanying drawings 1 in which identical reference numerals to those in Figs. 1 through 4 represent similar or identical elements and description thereof is omitted.
Figs. 5 and 6 illustrates a first embodiment of the present invention.
Reference numeral 19 denotes a roller which is rotatably retained by the crank 3c of the shaft 3, as in the case of the conventional compressor. The same number of grooves 20 through 27 are formed on end surfaces l9a and l9b of the roller 19. The grooves 20 through 27 are respectively formed by communicating portions 20a through 27a which communicate with the inner peripheral portion of the roller 19, and sealing portions 20b through 27b and 20c through 27c which extend from the communicating portions 20a through 27a in the circumferential direction and whose cross-sectional area decreases as a distance to the c~ nicating portions 20a through 27a increases.
In such a structure, the refrigerant gas sucked from the suction pipe 13 is compressed and discharged to the cooling system from the discharge pipe 17 in the same manner as that of the conventional compressor.
The high-pressure lubricating oil 18 with the refrigerant contained therein which is contained in the sealed casing 1 lubricates the mechanical portion body 9 in the same manner as that of the conventional compres-sor. The lubricating oil 18 which flows into the inner peripheral side of the roller 19 lubricates the rollers l9a and l9b, and then returns to the bottom portion of -, ~
1 the sealed casing in the same manner as that of the conventional compressor.
As the shaft 3 is rotated, the roller 19 revolves while turning round about the crank, as in the case of the conventional compressor. As a result, the roller 19 goes on the spiral motion. The direction of the spiral motion which is obtained at a certain instance is indicated by the arrow of the solid line, and the direction in which the lubricating oil 18 flows as a consequence of the motion of the roller 19 is indicated by the arrow of the broken line, as in the case of the conventional compressor.
At that time, in the grooves 20 through 27 formed on the end surface l9a of the roller 19, the sealed portions 20c, 21c, 23b, 24b, 25b, 26b, 26c and 27c in the sealed portions 20b through 27b and 20c through 27c reduce their cross-sectional area in the direction of flow of the lubricating oil 18 which is indicated by the arrow of the broken line, generating a pressure of the lubricating oil 18 which flows in from the communicating portions 20a through 27a.
That is, in the grooves 20 through 27 except for the groove 22, the oil pressure is generated at either of or both of the sealed portions 20b through 27b and 20c through 27c, and the positions where the oil pressure is generated are thus distributed over the end surface l9a of the roller 19, unlike the conventional compressor in which the oil pressure is generated at only 1 a single position. In addition, generation of the oil pressure occurs in the grooves 20 through 27 formed on the end surface l9b in the same manner as that for the grooves 20 through 27 formed on the end surface l9a: in all the grooves except for the groove 22 located at a position symmetrical with respect to the position of the groove 22 formed on the end surface l9a, the oil pressure is generated at either of or both of the sealed portions 20b through 27b and 20c through 27c, and the positions on the end surface l9b where the oil pressure is generated are symmetrical with respect to the positions on the end surface l9a where the oil pressure is generated.
Regarding the component of the roller rotation about the crank which forms the spiral motion of the roller 19, since the sealed portions 20b through 27b and 20c trough 27c are formed in such a manner that the cross-sectional area thereof decreases substantially in the circumferential direction, the oil pressure due to the wedge effect is generated in the sealed portions whichever direction the roller 19 is rotated about the crank. Furthermore, since the oil pressure is generated near the sealed portions 20b through 27b and 20c through 20c, it cannot escape from the sealed portions, and the oil pressure is thus increased. Therefore, the same amount of oil pressure is generated on the end surfaces l9a and l9b of the roller 19 over the distributed positions, and the generated oil pressures thus balance.
In addition, since the generated oil pressure is higher 1 than the conventionally generated oil pressure because of an increase in the oil pressure generated by the compo-nent of the roller rotation about the crank and the incapability of escape of the generated oil pressure, the roller 19 can be retained at a position which ensures ~a = ~b during one rotation more reliably than the conven-tional roller, and the volumeric efficiency of the compressor can thus be improved.
Furthermore, since the grooves 20 through 27 are not provided over the entire periphery, the sealed distance is longer than that obtained when the tapered portions are provided. Thus, the amount of lubricating oil which flows into the compression chamber and the suction chamber is reduced, and this makes improvement in the volumeric efficiency possible even in the case of a small compressor in which the thickness of the roller is small.
A second embodiment of the present invention will be described below with reference to Figs. 7 and 8.
In the following description, only the differences between the first and second embodiments will be explained.
The same number of grooves 28 through 35 are formed on the end surfaces l9a and l9b of the roller 19.
The grooves 28 through 35 are respectively formed by communicating portions 28a through 35a which communicate with the inner peripheral portion of the roller 19, and sealing portions 28b through 35b, 28c through 35c, 28d l through 35d, 28e through 35e and 28f through 35f which extend from the communicating portions 28a through 35a substantially radially and whose cross-sectional area decreases as a distance to the communicating portions 28a through 35a increases.
In such a structure, the refrigerant gas sucked from the suction pipe 13 is compressed and discharged to the cooling system from the discharge pipe 17 in the same manner as that of the conventional compressor.
The high-pressure lubricating oil 18 with the refrigerant contained therein which is contained in the sealed casing 1 lubricates the mechanical portion body 9 in the same manner as that of the conventional compres-sor. The lubricating oil 18 which flows into the inner peripheral side of the roller 19 lubricates the rollers l9a and l9b, and then returns to the bottom portion of the sealed casing in the same manner as that of the conventional compressor.
As the shaft 3 is rotated, the roller 19 revolves while rotating about the crank, as in the case of the conventional compressor. As a result, the roller 19 performs the spiral motion. The direction of the spiral motion which is obtained at a certain instance is indicated by the arrow of the solid line, and the direc-tion in which the lubricating oil 18 flows as a consequ-ence of the motion of the roller 19 is indicated by the arrow of the broken line, as in the case of the conventional compressor.
~ - 14 -l At that time, in the grooves 28 through 35 formed on the end surface l9a of the roller l9, a pressure of the lubricating oil 18 which flows in from the communicating portions 28a through 35a is generated at the sealed portions whose cross-sectional area decreases in the direction of flow of the lubricating oil 18 which is indicated by the arrow of the broken line in the sealed portions 28b through 35b, 28c through 35c, 28d through 35d, 28e through 35e and 28f through 35f. In the groove 28, for example, an oil pressure is generated at the sealed portions 28e and 28f. In the groove 32, an oil pressure is generated at the sealed portions 32c and 32d. That is, in all the grooves 28 through 35, the oil pressure is generated at two portions, and the positions where the oil pressure is generated are thus distributed over the end surface l9a of the roller 19, unlike the conventional compressor in which the oil pressure is generated at only a single position. In addition, gener-ation of the oil pressure occurs on the end surface l9b in the same manner as that for the end surface l9a.
Therefore, the positions on the end surface l9b where the oil pressure is generated are symmetrical with respect to the positions on the end surface l9a where the oil pres-sure is generated, and the oil pressure generated on the end surfaces l9a and l9b thus balance with each other.
Regarding the component of the roller rotation about the crank which forms the spiral motion of the roller 19, since the sealed portions 28c through 35c, 28d 1 through 35d, 28e through 3Se and 28f through 35f are formed in such a manner that the cross-sectional area thereof decreases substantially in the circumferential direction, the oil pressure due to the wedge effect is generated in these sealed portions whichever direction the roller 19 is rotated about the crank. Furthermore, since the oil pressure is generated near the sealed portions 28b through 35b, 28c through 35c, 28d through 35d, 28e through 35e and 28f through 35f, it cannot escape from the sealed portions, and the oil pressure is retained high. Therefore, the same amount of oil pres-sure is generated on the end surfaces l9a and l9b of the roller 19 over the distributed positions, and the gene-rated oil pressures thus balance. In addition, since the generated oil pressure is higher than the conventionally generated oil pressure because of an increase in the number of positions where the oil pressure is generated, an increase in the amount of oil pressure generated by the component of the roller rotation about the crank and the incapability of escape of the generated oil pressure, the roller 19 can be retained at a position which ensures ~a = ~b during one rotation more reliably than the conventional roller, and the volumeric efficiency of the compressor can thus be improved while the leakage loss can be reduced.
Furthermore, since the grooves 28 through 35 are not provided over the entire periphery, the sealed distance is longer than that obtained when the tapered 1 portions are provided. Thus, the amount of lubricating oil which flows into the compression chamber and the suction chamber is reduced, and this makes an improvement in the volumeric efficiency possible even in the case of a small compressor in which the thickness of the roller is small.
A third embodiment of the present invention will be described below with reference to Figs. 9 and 10.
Grooves 37 through 44 are formed in each of the end surfaces 36a and 36b of the roller 36. In the grooves 37 through 44, co~llnicating portions 37a through 44a are formed in such a manner that they pass the inner peripheral portion of the roller 36 and the grooves 37 through 44, and sealed portions 37b through 44b, 37c through 44c, 37d through 44d, 37e through 44e and 37f through 44f are formed radially from portions of the communicating portion 37a through 44a which open into the grooves 37 through 44. In this embodiment, an oil pressure is generated due to the spiral motion of the roller at the sealed portions 37b through 44f, as in the cases of the previously described embodiments. At that time, since the communicating portions 37a through 44a are opened into the central portions of the grooves 37 through 44 and the distance from the communicating portions 37a through 44a to all the sealed portions 37b through 44f is hence the same, an oil pressure is gener-ated under the same conditions. Therefore, a higher oil pressure than that generated in the second embodiment can 1 be generated, and the lubricating oil can be supplied smoothly.
A fourth embodiment of the present invention will be described below with reference to Figs. 11 through 14.
Reference numerals 45 and 46 respectively denote a main bearing and a sub bearing which rotatably support the shaft 3 in the same manner as that of the conventional compressor. Reference numeral 47 designates a roller which is rotatably retained on the crank 3c of the shaft 3. The same number of grooves 48 through 55 are formed in the main and sub bearings 45 and 46. Each of the grooves 48 through 55 has a shape in which the cross-sectional area thereof is the largest at the center thereof and decreases in the circumferential and radial directions.
In Fig. 11, dot-dot-dashed lines indicate the inner peripheral surface of the cylinder 4, the vane 6 and the roller 47. Fig. 11 shows the positions relation between the grooves 48 through 55 and the roller 47 which is obtained at a certain rotational position.
Figs. 13 and 14 show the positional relation between the grooves 48 through 55 and the roller 47. In these figures, although the grooves 48 through 55 should have a hidden outline, they are indicated by the solid line for the ease of understanding.
In such a structure, the refrigerant gas sucked from the suction pipe 13 is compressed and discharged to - 18 - '~U88160 l the cooling system from the discharge pipe 17 in the same manner as that of the conventional compressor.
The high-pressure lubricating oil 18 with the refrigerant contained therein which is contained in the sealed casing 1 lubricates the mechanical portion body 9 in the same manner as that of the conventional compres-sor. The lubricating oil 18 which flows into the inner peripheral side of the roller 19 lubricates the rollers l9a and l9b, and then returns to the bottom portion of the sealed casing in the same manner as that of the conventional compressor.
As the shaft 3 is rotated, the roller 47 revolves while rotating about the crank, as in the case of the conventional compressor. The direction of the spiral motion which is obtained at a certain rotational _ angle is indicated by the arrow of the solid line in Fig.
13, as in the case of the conventional compressor.
At that time, the grooves 50, 51, 52 and 53 in the grooves 48 through 55 of the main bearing 45 are sealed by the end surface of the roller 47. The grooves 48 through 55 of the sub bearing 46 are also sealed similarly. Since the grooves 48 through 55 have a shape in which the cross-sectional area thereof is the largest at the central portion thereof and decreases in the radial and circumferential directions, when the lubricat-ing oil moves within the sealed grooves 50 through 53 in the direction indicated by the solid line, an oil pressure is generated in the grooves 50 through 53. In l addition, the positions where the oil pressure is generated in the grooves S0 through 53 are symmetrical.
That is, in this embodiment, the oil pressure is gener-ated on each of the two end surfaces of the roller 47 at four positions, and the oil pressure generated on one of the end surfaces balances the oil pressure generated on the other end surface.
Regarding the component of the roller rotation about the crank which forms the spiral motion thereof, since the grooves 48 and 55 are formed in such a manner that the cross-sectional area thereof decreases in the circumferential direction, the oil pressure is generated in the sealed grooves 50 through 53 due the wedge effect whichever direction the roller rotates about the crank.
In addition, since the grooves 48 through 55 are formed separately, the oil pressure generated in the sealed grooves 50 through 53 cannot escape from the sealed grooves, and the oil pressure is thus retained high.
Furthermore, as shown in Fig. 14, when the shaft 3 is rotated to another rotational position, the grooves 48, 49, 50 and 51 are now sealed by the end surface of the roller 47, and an oil pressure is gene-rated in each of these grooves. Thus, whichever of the rotational positions the shaft 3 is rotated, some grooves in the grooves 48 through 55 are sealed.
Therefore, the same amount of oil pressure is generated on the end surfaces of the roller 47 over the distributed positions, and the generated oil pressures 1 thus balance. In addition, since the generated oil pressure is higher than the conventionally generated oil pressure because of an increase in the amount of oil pressure generated by the component of the roller rotation about the crank and the incapability of escape of the generated oil pressure, the roller 47 can be retained at a position which ensures ~a = ~b during one rotation more reliably than the conventional roller, and the volumeric efficiency of the compressor can thus be improved while the power loss due to leakage can be reduced.
Furthermore, since the roller 47 faces only part of the grooves 48 through 55, the sealed distance is longer than that obtained when the tapered portion is provided. Consequently, the amount of lubricating oil which flows into the compression chamber is reduced, and this makes an improvement in the volumeric efficiency possible even in the case of a compressor in which the thickness of the roller is small.
Industrial Applicability As will be understood from the foregoing description, since the sealed portions of the lubricating oil and the communicating portions which communicate with the inner peripheral surface of the roller are formed in the contact surfaces between the roller and the main and sub bearings, the same amount of oil pressure can be generated over the distributed positions and the 1 generated oil pressures thus balance. Thus, if the rotary compressor is employed in a refrigerating cycle which is for use in, for example, a refrigerator or a freezer, the performance of the refrigerating cycle can be improved because the motion of the roller is stabi-lized and the volumeric efficiency is thus improved.
Claims (4)
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A rotary compressor comprising: a cylinder; a main shaft and a sub bearing which are fixed to end surfaces of said cylinder; a shaft which is rotatable within said main bearing and said sub bearing and has a crank; a roller rotatably accommodated on said crank of said shaft; a vane which makes contact with said roller and reciprocatively slides within a groove provided in said cylinder; and a groove provided in each of end surfaces of said roller which respectively face said main bearing and said sub bearing, said groove having a communicating portion for communicating with an inner peripheral side of said roller and a plurality of sealed portions which continue from said communicating portion and whose cross-sectional area decreases as a distance to said communicating portion increases.
2. A rotary compressor according to claim 1, wherein said sealed portions extend substantially in a circumferential direction and have the cross-sectional area which decreases as the distance to said communicat-ing portion increases.
3. A rotary compressor according to claim 1, wherein said sealed portions extend substantially in a radial direction and have the cross-sectional area which decreases as the distance to said communicating portion increases.
4. A rotary compressor comprising: a cylinder; a main bearing and a sub bearing which are fixed to end surfaces of said cylinder; a shaft which is rotatable within said main bearing and said sub bearing and has a crank; a roller rotatably accommodated on said crank of said shaft; a vane which makes contact with said roller and reciprocatively slides within a groove provided in said cylinder; and a plurality of grooves separately provided in an end surface of each of said main bearing and said sub bearing in such a manner that a cross-sectional area thereof decreases in radial and circum-ferential directions and that they face an end surface of said roller at least once during a single rotation of said shaft.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/JP1991/000725 WO1992021881A1 (en) | 1991-05-30 | 1991-05-30 | Rotary compressor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2088160A1 CA2088160A1 (en) | 1992-12-01 |
| CA2088160C true CA2088160C (en) | 1995-04-04 |
Family
ID=14014435
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA 2088160 Expired - Fee Related CA2088160C (en) | 1991-05-30 | 1991-05-30 | Rotary compressor |
Country Status (5)
| Country | Link |
|---|---|
| EP (1) | EP0541801B1 (en) |
| BR (1) | BR9106801A (en) |
| CA (1) | CA2088160C (en) |
| DE (1) | DE69125008T2 (en) |
| WO (1) | WO1992021881A1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108105094B (en) * | 2017-12-07 | 2023-10-03 | 珠海格力节能环保制冷技术研究中心有限公司 | Compressor and heat exchange equipment with same |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5470809A (en) * | 1977-11-16 | 1979-06-07 | Nippon Denso Co Ltd | Emergency sound information reader |
| JPS56106088A (en) * | 1980-01-29 | 1981-08-24 | Matsushita Electric Ind Co Ltd | Rotary type fluid equipment |
| JPS56135780A (en) * | 1980-03-27 | 1981-10-23 | Matsushita Electric Ind Co Ltd | Compressor |
-
1991
- 1991-05-30 CA CA 2088160 patent/CA2088160C/en not_active Expired - Fee Related
- 1991-05-30 DE DE69125008T patent/DE69125008T2/en not_active Expired - Fee Related
- 1991-05-30 WO PCT/JP1991/000725 patent/WO1992021881A1/en active IP Right Grant
- 1991-05-30 BR BR919106801A patent/BR9106801A/en not_active IP Right Cessation
- 1991-05-30 EP EP91910170A patent/EP0541801B1/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| DE69125008D1 (en) | 1997-04-10 |
| DE69125008T2 (en) | 1997-08-28 |
| EP0541801B1 (en) | 1997-03-05 |
| BR9106801A (en) | 1994-01-25 |
| WO1992021881A1 (en) | 1992-12-10 |
| EP0541801A1 (en) | 1993-05-19 |
| EP0541801A4 (en) | 1995-04-19 |
| CA2088160A1 (en) | 1992-12-01 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKLA | Lapsed |