HERMETIC SCROLL TYPE COMPRESSOR

Abstract: This invention discloses a lubricating mechanism of a hermetically sealed scroll type compressor in which an inner chamber of a housing is kept at suction pressure. The compressor includes a drive shaft (13) supported by bearings in inner blocks. The drive shaft (13) is opera­ tively linked to an orbiting scroll (30) which orbits within a stationary scroll (20). A rotation prevention (34) device prevents rotation of the orbiting scroll (30). The drive shaft (13) includes an axial bore extending from an open end and terminating adjacent a forward bearing. A pin extends from the end of the drive shaft (13) to the orbital scroll (30). A passage links the axial bore to an opening at the end of the pin facing the orbital scroll. Radial bores (82) are provided near the terminal end of the axial bore (81) and at the rearward end of the axial bore near a rearward bearing. The radial bores (82) link the axial bore (81) to a suction chamber (60) of the compressor to allow lubricating oil to lubricate the bearings. The narrow passages (83) allows lubrication of the rotation prevention mechanism. In a second embodiment the suction chamber is divided into two sections by a partition wall. An inclined passage links the two sections to allow the lubricating oil to flow.

Description: This invention relates to a scroll type compressor, and more particularly, to a lubricating mechanism for a hermetically sealed scroll type compressor. A hermetically sealed scroll type compressor is disclosed in Japanese Patent Application Publication No. 61-87994 and is shown in Figure 1. A hermetically sealed housing includes inner chamber 1 which is maintained at discharge pressure. However, the compression mechanism including interfitting scrolls 2 and 3 and the forward end of the drive mechanism are isolated from inner chamber 1 behind partition 4. Channel 5 links intermediate pocket 6 of the interfitting scrolls with chamber 7. Refrigerant gas flows through inlet port 8 and is compressed inwardly by the scrolls towards central pocket 9, and flows to discharge chamber 12 through hole 10 and eventually outlet port 11 to an external element of the refrigeration system. Some of the refrigerant gas also flows to inner chamber 1. The intermediate pressure in pocket 6 is maintained in chamber 7 which contains the forward end of the drive mechanism including bearings 14-16. When the compressor operates, lubricating oil mixed with the refrigerant gas, which settles at the bottom of inner chamber 1, flows through channel 13 to lubricate bearings 14-16 of the drive mechanism due to the pressure difference between inner chamber 1, which is maintained at the discharge pressure, and the intermediate pressure. However, it is difficult to utilize the above type of lubricating mechanism in a hermetically sealed scroll type compressor in which the inner chamber is maintained at the suction pressure. Since the suction pressure is lower than the discharge pressure and the intermediate pressure, the lubricating fluid will not flow to the drive mechanism in this type of compressor. It is a primary object of this invention to provide an effective and simplified lubricating mechanism for use in a hermetically sealed scroll type compressor in which an inner chamber of the hermetically sealed housing is maintained at suction pressure. JP-A-61-87994 discloses a scroll type compressor with a hermetically sealed housing, the compressor comprising a fixed scroll disposed within the housing, and having a first end plate and a first spiral element extending therefrom, the first end plate of the fixed scroll dividing the housing into a discharge chamber and a suction chamber into which the first spiral element extends, an orbiting scroll having a second end plate from which a second spiral element extends, the first and second spiral elements interfitting at an angular and radial offset to form a plurality of line contacts which define at least one pair of sealed off fluid pockets, a drive mechanism operatively connected to the orbiting scroll to effect orbital motion of the orbiting scroll, the drive mechanism including a drive shaft having an axial bore linked with at least one radial bore, and a rotation prevention means for preventing the rotation of the orbiting scroll during orbital motion whereby the volume of the fluid pockets changes to compress fluid in the pockets, and, according to the present invention such a compressor is characterised by the suction chamber extending around the motor up to the adjoining end of the housing the axial bore extending from an opening at one end of the drive shaft to a bottom end nearer to the scrolls at an opposite end of the drive shaft, at least one of the radial bores extending through the drive shaft linking the axial bore near its bottom end to the suction chamber, the housing provided with an for oil-laden inlet port refrigerant gas extending therethrough and terminating in the housing near the opening at the one end of the axial bore. In operation, the refrigeration gas includes a lubricating fluid which flows from the axial bore towards the radial bores and the offset channel. The fluid lubricates the bearings supporting the drive shaft as well as a rotation prevention mechanism located at the forward end of the drive shaft. In one construction; which forms the subject of divisional application no. 90125436.7 the suction chamber is divided into first and second suction chamber sections by a partition wall. The partition wall completely isolates the two chamber sections with the exception of an inclined bore located below and near the forward end of the drive shaft. Lubricant fluid settles at the bottom of the first section. The forward end of the drive shaft including the projecting pin, and the scrolls, are located in the second of the suction chamber. In operation, the first section of the suction chamber is maintained at a higher pressure than the second section causing the fluid to flow upwardly through the inclined bore to lubricate the rotation prevention device and the forward bearing of the drive shaft. In the accompanying drawings: Figure 1 is a vertical longitudinal section of a scroll type compressor in accordance with the prior art; Figure 2 is a vertical longitudinal section of a hermetically sealed scroll type compressor in accordance with a first example of the invention; and, Figure 3 is a vertical longitudinal section of a hermetically sealed scroll type compressor in accordance with a second example of the invention. Referring to Figure 2, a hermetically sealed scroll type compressor in accordance with one embodiment of the present invention is shown. For purposes of explanation only, the left side of the Figure will be referenced as the forward end or front and the right side of the Figure will be referenced as the rearward end. The compressor includes hermetically sealed casing 10, fixed and orbiting scrolls 20, 30 and motor 40. Fixed scroll 20 includes circular end plate 21 and spiral element or wrap 22 extending from one end (rearward) surface thereof. Fixed scroll 20 is fixedly disposed within a front end portion of casing 10 by a plurality of screws 26. Circular end plate 21 of fixed scroll 20 partitions an inner chamber of casing 10 into two chambers, for example, discharge chamber 50 and suction chamber 60. O-ring seal 23 is disposed between an inner peripheral surface of casing 10 and an outer peripheral surface of circular end plate 21 to seal the mating surfaces of casing 10 and circular end plate 21. Orbiting scroll 30 disposed within suction chamber 60 includes circular end plate 31 and spiral element or wrap 32 extending from one end (forward) surface of circular end plate 31. Spiral element 22 of fixed scroll 20 and spiral element 32 of orbiting scroll 30 interfit at an angular and radial offset to form a plurality of linear contacts which define at least one pair of sealed off fluid pockets 70. Annular projection 33 is formed at the rearward end surface of circular end plate 31 opposite spiral element 32. Rotation prevention device 34 is disposed on the outer circumferential surface of annular projection 33 to prevent rotation of orbiting scroll 30 during orbital motion. Inner blocks 11, 12 secure stator 41 of motor 40 and are fixedly disposed near opposite ends within suction chamber 60. Drive shaft 13 axially penetrates the centers of inner blocks 11, 12. Both ends of drive shaft 13 are rotatably supported by inner blocks 11, 12 through bearings 14, 15 respectively. Motor 40 includes stator 41 and rotor 42 fixedly secured to an outer peripheral surface of drive shaft 13. Pin member 16 is integral with and axially projects from the forward end surface of drive shaft 13 and is radially offset from the axis of drive shaft 13. Bushing 17 is rotatably disposed within annular projection 33 and is supported by bearing 18. Pin member 16 is rotatably inserted in hole 19 of bushing 17 which is offset from the center of bushing 17. Drive shaft 13 is provided with axial bore 81 and a plurality of radial bores 82. Axial bore 81 extends from an opening at a first (rearward) end of drive shaft 13, that is, the end opposite pin member 16, to a closed end rearward of pin member 16. Narrow passage 83 links the forward closed end of axial bore 81 to an open end surface of pin member 16 adjacent orbiting scroll 30. The plurality of radial bores 82 link axial bore 81 near its closed end to first cavity 61 located between motor 40 and bearing 14. A plurality of further radial bores 84 are located near the opening of axial bore 81 adjacent bearing 15. Suction gas inlet pipe 85 is inserted through the rear end of casing 10 and faces the opening of axial bore 81. Discharge gas outlet pipe 86 is attached to a side wall of casing 10 and links discharge member 50 to an external element. In operation, stator 41 generates a magnetic field causing rotation of rotor 42, thereby rotating drive shaft 13. This rotation is converted to orbital motion of orbiting scroll 30 through bushing 17; rotational motion is prevented by rotation prevention drive 34. Refrigerant gas introduced into suction chamber 60 through suction gas inlet pipe 85 is taken into the outer sealed fluid pockets 70 between fixed scroll 20 and orbiting scroll 30, and moves inwardly towards the center of spiral elements 22, 32 due to the orbital motion of orbiting scroll 30. As the refrigerant moves towards the central pocket, it undergoes a resultant volume reduction and compression, and is discharged to discharge chamber 50 through discharge port 24 and one-way valve 25. Discharge gas in discharge chamber 50 then flows to an external fluid circuit (not shown) through discharge gas outlet pipe 86. The lubricating mechanism of this embodiment operates as follows. Refrigerant gas including lubricating oil (jointly denoted refrigerant gas, hereinafter) is introduced into suction chamber 60 from suction gas inlet pipe 85, and is largely taken into axial bore 81. A large part of the refrigerant gas flow out of axial bore 81, and into first cavity 61 through radial bores 82, and then flows through a gap in bearing 14 into second cavity 62 on the opposite side of bearing 14, rearward of rotation prevention device 34. The remainder of the refrigerant gas in axial bore 81 flows through narrow passage 83 and into the gap between bushing 17 and annular projection 33. The gas then flows through a gap in bearing 18, and into second cavity 62. Subsequently, refrigerant gas in second cavity 62 flows through rotation prevention device 34, before being taken into sealed fluid pockets 70. Thus, refrigerant gas effectively flows to lubricate bearing 14, bearing 18 and rotation prevention device 34. Additionally, some lubricant oil is partly separated from the refrigerant gas and remains beneath orbiting scroll 30, while some of the lubricant is taken into sealed fluid pockets 70 as a mist due to orbital motion of orbiting scroll 30. Finally, some of the refrigerant gas flows through the plurality of radial bores 84 to further lubricate bearing 15. Referring to Figure 3, a hermetically sealed scroll type compressor in accordance with a second embodiment of the present invention is shown. The same construction is accorded like numerals as shown with respect to Figure 2 and the description of some of the identical elements is substantially omitted. Inner blocks 110 and 120 securing stator 41 of motor 40 are fixedly disposed within suction chamber 60. Drive shaft 13 axially penetrates the center of inner blocks 110 and 120. Inner block 110 may be disposed perpendicularly to the axis of rotation of drive shaft 13. Both ends of drive shaft 13 are rotatably supported by inner blocks 110 and 120 through bearings 14 and 15. The axis of rotation of the drive shaft is disposed parallel to a level surface on which the compressor is mounted. Inner block 110 divides suction chamber 60 into first suction chamber section 63 rearward of inner block 110 in which motor 40 is located and second suction chamber section 64 forward of inner block 110 in which orbiting scroll 30 and rotation prevention mechanism 34 are located. Inclined passage 111 links first and second suction chamber sections 63, 64 and is formed at a lower part of inner block 110. Inclined hole 111 extends upwardly from first suction chamber 63 towards second suction chamber section 64. The lubricating mechanism of this embodiment operates as follows. Refrigerant gas including lubricating oil is introduced into first suction chamber section 63 and is mostly taken into axial bore 81. However, a large part of the refrigerant gas flows into first suction chamber section 63 from axial bore 81 through a plurality of radial bores 82 and 84 so that lubricating oil is separated from the refrigerant gas due to centrifugal forces and particle interactions and settles at the bottom of first suction chamber section 63. Subsequently, refrigerant gas flows into second suction chamber section 64 through the gap of bearing 14 so that a small pressure difference is created between first and second suction chambers sections 63 and 64. The pressure of second suction chamber section 64 is lower than the pressure of first suction chamber section 63. Accordingly, lubricating oil 130 settled at the bottom of first suction chamber section 63 flows to second suction chamber section 64 through inclined passage 111 to lubricate rotation preventing mechanism 34 and a contact portion between fixed and orbiting scrolls 20, 30. Furthermore, the open end of inclined passage 111 formed at the second suction chamber section side is located at a position which is higher than the uppermost level of lubricating oil 130 in the bottom of first suction chamber section 63 to prevent an overflow of settled lubricating oil 130 to the scrolls when the compressor is re-started after not operating for a long period of time. Therefore, damage to the scrolls is prevented.

Claims: 1. A scroll type compressor with a hermetically sealed housing (10), the compressor comprising a fixed scroll (20) disposed within the housing (10), and having a first end plate (21) and a first spiral element (22) extending therefrom, the first end plate (21) of the fixed scroll (20) dividing the housing (10) into a discharge chamber (50) and a suction chamber (60) into which the first spiral element (22) extends, an orbiting scroll (30) having a second end plate (31) from which a second spiral element (32) extends, the first and second spiral elements (22, 32) interfitting at an angular and radial offset to form a plurality of line contacts which define at least one pair of sealed off fluid pockets (70), a drive mechanism operatively connected to the orbiting scroll (30) to effect orbital motion of the orbiting scroll (30), the drive mechanism including a drive shaft (13) having an axial bore (81) linked with at least one radial bore (82), and a rotation prevention means (34) for preventing the rotation of the orbiting scroll during orbital motion whereby the volume of the fluid pockets (70) changes to compress fluid in the pockets; characterised by the suction chamber extending around the motor up to the adjoining end of the housing, the axial bore (81) extending from an opening at one end of the drive shaft (13) to a bottom end nearer to the scrolls (20, 30) at an opposite end of the drive shaft (13), at least one of the radial bores (82) extending through the drive shaft (13) linking the axial bore (81) near its bottom end to the suction chamber (60), the housing (10) provided with an for oil-laden inlet port refrigerant gas (85) extending therethrough and terminating in the housing near the opening at the one end of the axial bore (81). 2. A compressor according to claim 1, wherein the drive shaft (13) further includes an integral pin member (16) disposed at the opposite end of the drive shaft (13), the pin member (16) being radially offset with respect to the axis of the drive shaft (13) and operatively connected to the orbiting scroll (30) through a bushing (17). 3. A compressor according to claim 2, further comprising a narrow passage (83), formed from the bottom end of the axial bore (81) to an end surface of the pin member (16) facing the orbiting scroll (30). 4. A compressor according to any one of the preceding claims, wherein the drive mechanism includes a motor (40) supported in the housing (10), the motor (40) including a rotor (42) secured to the drive shaft (13). 5. A compressor according to claim 4, wherein at least one radial bore (82) is located at a position which is closer to the orbital scroll (30) than the rotor (42). 6. A compressor according to any one of the preceding claims, further comprising a second radial bore (84) located near the opening at the one end of the axial bore (81) and linking the axial bore (81) to the suction chamber. 7. A compressor according to claim 6, further comprising a bearing (15) supporting the drive shaft (13) near the second radial bore (84), the bearing (15) being lubricated, in use, by fluid flowing through the second radial bore (84). 8. A compressor according to any one of the preceding claims, further including a bearing (14) supporting the drive shaft (15) at the opposite end and the one radial bore (82), the bearing (14) being lubricated, in use, by fluid flowing through the radial bore (82). 9. A compressor according to any one of the preceding claims, wherein the axis of rotation of the drive mechanism is disposed substantially horizontally when the compressor is in its normal attitude for use, the suction chamber (60) being divided into first and second suction chamber sections (63, 64) by a partition wall (110), the fixed and orbiting scrolls (20, 30) and the rotation prevention means (34) being disposed within the second suction chamber section (64), the drive mechanism being disposed within the first suction chamber section (63) the refrigerant gas inlet port (85) being disposed at the first suction chamber section (63), an inclined passage (111) linking the first and second suction chamber sections (63, 64) formed in a lower part of the partition wall (110), the inclined passage (111) inclined upwardly from the first suction chamber section (63) to the second suction chamber section (64), wherein lubricating oil separated from refrigerant gas settles at the bottom of the first suction chamber section (63). 10. A compressor according to claim 9, wherein a drive shaft (13) of the drive mechanism is rotatably supported through the partition wall (110) by a bearing. 11. A compressor according to claim 9 or claim 10, wherein one open end of the inclined passage (111) formed at the second suction chamber section side (64) is located at a higher level, in use, than the uppermost limit level of the surface of the lubricating oil. 12. A compressor according to any one of claims 9 to 11, wherein the partition wall (110) is disposed perpendicularly to the axis of rotation of the drive mechanism.

Inventors: KIKUCHI, KAZUTO, SHIMIZU, SHIGEMI
Applicants: SANDEN CORPORATION
Application year: 1988
Main classification: F04C18
IPC codes: F04C29, F04C23