Rotating machine and turbocharger
11698078 · 2023-07-11
Assignee
Inventors
Cpc classification
F16C27/045
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2360/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C19/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/6659
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/98
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/063
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B39/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/059
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2240/54
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
On an inner circumferential surface (25a) of a housing (25) opposed to an outer circumferential surface (37a, 37b) of an outer ring, toward a front side in a rotation direction (B) of a rotation shaft (21), a first groove (41H, 41I) is formed as a groove portion for guiding an oil (39) in a direction toward a first oil supply hole (41D, 41E).
Claims
1. A rotating machine comprising: a rotating shaft extending along an axis; a bearing which has an inner ring externally fitted onto the rotating shaft, an outer ring provided on an outer peripheral surface side of the inner ring, and rolling bodies disposed between the inner ring and the outer ring, and supports the rotating shaft such that the rotating shaft is rotatable around the axis; and a housing which has an inner peripheral surface that forms a clearance, in which oil is disposed, between the inner peripheral surface and an outer peripheral surface of the outer ring, and a first oil supply hole that supplies the oil to the clearance, wherein a groove portion, which guides the oil in a direction toward the first oil supply hole as the groove portion is directed to a rotation direction front side of the rotating shaft, is formed on at least one of the outer peripheral surface of the outer ring and the inner peripheral surface of the housing facing the outer peripheral surface of the outer ring, an outer side end of the groove portion is formed not to reach an end of the housing, the groove portion includes a first groove, the first groove is inclined with respect to a rotation direction in which the rotating shaft is rotated and an axis direction when viewed in a radial direction of the rotating shaft, the first groove is formed in an outer side region which is between the first oil supply hole and one of both ends of the outer ring which is close to a forming position of the first oil supply hole in the axis direction, the first groove is inclined in a direction toward the first oil supply hole from the end of the outer ring, and an inner side end of the first groove is disposed on an outer side of the first oil supply hole in the axis direction.
2. The rotating machine according to claim 1, wherein a plurality of the first grooves are formed in the axis direction.
3. The rotating machine according to claim 1, wherein the groove portion includes a second groove, the second groove is formed in a central region positioned closer to a central side of the outer ring than the outer side region, and the second groove is inclined in a direction opposite to the first groove or the same direction as the first groove.
4. The rotating machine according to claim 1, wherein the groove portion includes a third groove, the third groove is formed between a forming position of the first groove and the first oil supply hole in the outer side region, and is inclined in a direction opposite to the first groove, and one end of the first groove and one end of the third groove are connected on the rotation direction front side.
5. The rotating machine according to claim 4, wherein a plurality of the groove portions each including the first groove and the third groove are formed at intervals in a circumferential direction of the rotating shaft.
6. The rotating machine according to claim 4, wherein the groove portion has a fourth groove which is formed in the outer side region and is inclined in the same direction as the first groove.
7. The rotating machine according to claim 6, wherein a length of the fourth groove is longer than a length of the first groove, and one end of the fourth groove is connected to the other end of the third groove.
8. The rotating machine according to claim 6, wherein a length of the fourth groove is longer than a length of the first groove, and the fourth groove is separated from the first groove and the third groove.
9. The rotating machine according to claim 1, wherein the outer ring has a recessed portion which is formed in a portion facing the first oil supply hole, a second oil supply hole which is formed to penetrate the portion where the recessed portion is formed in a direction toward the rotating shaft, and supplies the oil to the rolling bodies, and an oil discharge hole which is formed on a side opposite to a side where the second oil supply hole is formed, and discharges the oil.
10. A turbocharger comprising: the rotating machine according to claim 1; a compressor wheel provided to one end portion of the rotating shaft; and a turbine wheel provided to the other end of the rotating shaft.
11. The rotating machine according to claim 2, wherein one first groove of the plurality of the first grooves is inclined in a direction opposite to a direction in which another first groove of the plurality of the first groove is inclined.
12. The rotating machine according to claim 2, wherein the outer side region includes a first outer side region and a second outer side region, the first outer side region is a region between the first oil supply hole and one end of both ends of the outer ring, the second outer side region is a region between the first oil supply hole and the other end of the both ends of the outer ring that is different from the one end of the outer ring, one first groove of the plurality of the first grooves is formed in the first outer side region, and another first groove of the plurality of the first groove is formed in the second outer side region.
13. The rotating machine according to claim 12, wherein the first oil supply hole includes one first oil supply hole and another first oil supply hole, the one end of the outer ring is an end to which a forming position of the one first oil supply hole is closer than a forming position of the other first oil supply hole in the axis direction, the other end of the outer ring is an end to which the forming position of the other first oil supply hole is closer than the forming position of the one first oil supply hole in the axis direction, the first outer side region is a region between the one first oil supply hole and the one end of the outer ring, and the second outer side region is a region between the other first oil supply hole and the other end of the outer ring.
Description
BRIEF DESCRIPTION OF DRAWINGS
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DESCRIPTION OF EMBODIMENTS
(13) Hereinafter, embodiments in which the present invention is applied will be described in detail with reference to the drawings.
First Embodiment
(14) A turbocharger 10 according to an embodiment of the present invention will be described with reference to
(15) In
(16) Further, in
(17) In
(18) In the following description, a front side of the direction in which the rotating shaft 21 is rotated is referred to as a “rotation direction B front side”. In
(19) In
(20) The turbocharger 10 has a rotating machine 11, a thrust sleeve 12, an annular member 14, a compressor wheel 16, and a turbine wheel 18.
(21) The rotating machine 11 has the rotating shaft 21, a bearing 23 as a radial bearing, and a housing 25.
(22) A portion of the rotating shaft 21 protrudes to the outside of the housing 25, and the remaining portion of the rotating shaft 21 is housed in the housing 25. A seal member is disposed between the other end portion of the housing 25 and the rotating shaft 21 on a side where the turbine wheel 18 is disposed.
(23) The bearing 23 has an inner ring 31, the outer ring 32, and rolling bodies 34. The inner ring 31 is a cylindrical member, and is externally fitted onto the rotating shaft 21.
(24) The outer ring 32 has an outer ring main body 37, a first recessed portion 37A, second recessed portions 37B.sub.1 and 37B.sub.2, outer peripheral surfaces 37a and 37b, second oil supply holes 37C.sub.1 and 37C.sub.2, and oil discharge hole 37D.
(25) The outer ring main body 37 is a cylindrical member. The outer ring main body 37 is fixed to an inner side of the housing 25 to face an outer peripheral surface 31a of the inner ring 31 in a state where a clearance C is formed between the outer ring main body 37 and the inner peripheral surface 25a of the housing 25.
(26) The first recessed portion 37A is formed at a central portion of the outer ring main body 37. The first recessed portion 37A extends in the circumferential direction of the outer ring main body 37. The first recessed portion 37A is a ring-shaped groove.
(27) The second recessed portions 37B.sub.1 and 37B.sub.2 are formed on the outer ring main body 37 so as to interpose the first recessed portion 37A therebetween from both sides in the axis direction Da. The second recessed portion 37B.sub.1 is formed on one side of the outer ring 32. The second recessed portion 37B.sub.2 is formed on the other side of the outer ring 32.
(28) Each of the second recessed portions 37B.sub.1 and 37B.sub.2 extends in the circumferential direction of the outer ring main body 37. The second recessed portions 37B.sub.1 and 37B.sub.2 are ring-shaped grooves.
(29) The outer peripheral surfaces 37a are surfaces disposed between the first recessed portion 37A and the second recessed portions 37B.sub.1 and 37B.sub.2. The outer peripheral surface 37a faces an inner peripheral surface 25a of the housing 25 in the radial direction Dr. The outer peripheral surfaces 37a are disposed on both side of the first recessed portion 37A in the axis direction Da.
(30) The outer peripheral surfaces 37b are surfaces disposed on the outer sides of the second recessed portions 37B.sub.1 and 37B.sub.2. Two outer peripheral surfaces 37b are provided in the axis direction Da. The outer peripheral surface 37b faces the inner peripheral surface 25a of the housing 25 in the radial direction Dr.
(31) Oil 39 supplied from the housing 25 is disposed in the clearance C formed between the outer peripheral surfaces 37a and 37b and the inner peripheral surface 25a of the housing 25 in a state where the rotating shaft 21 is rotated.
(32) In a state where the rotating shaft 21 is rotated, a structure including the outer peripheral surfaces 37a and 37b, the inner peripheral surface 25a of the housing 25 facing the outer peripheral surfaces 37a and 37b, and the oil 39 disposed between the outer peripheral surfaces 37a and 37b and the inner peripheral surface 25a functions as oil film damper.
(33) The second oil supply hole 37C.sub.1 is formed to penetrate a portion of the outer ring main body 37 in the radial direction Dr, which is positioned on an upper end portion and in which the second recessed portion 37B.sub.1 is formed.
(34) The second oil supply hole 37C.sub.2 is formed to penetrate a portion of the outer ring main body 37 in the radial direction Dr, which is positioned on an upper end portion and in which the second recessed portion 37B.sub.2 is formed.
(35) The second oil supply holes 37C.sub.1 and 37C.sub.2 configured as described above supply the oil 39, which is supplied from the housing 25, to a portion (specifically, a plurality of rolling bodies 34) between the inner ring 31 and the outer ring 32.
(36) The oil discharge hole 37D is formed to penetrate a lower end portion of the outer ring main body 37 in the radial direction Dr. The oil discharge hole 37D is formed in the outer ring main body 37 to be positioned on a side opposite to the forming regions of the second oil supply holes 37C.sub.1 and 37C.sub.2.
(37) The oil discharge hole 37D is a hole for discharging the oil, which is supplied from the housing 25 and passes through the inside of the bearing 23, to the outside of the bearing 23.
(38) The housing 25 has a main housing body 41, oil supply pipe connection port 41B, oil distribution portion 41C, the first oil supply holes 41D and 41E, a first oil discharge port 41F, a second oil discharge port 41G, and first grooves 41H and 41I as groove portions.
(39) The main housing body 41 extends in the axis direction Da. A housing space 41A which extends in the axis direction Da and houses the thrust sleeve 12, the annular member 14, the remaining portion of the rotating shaft 21, and the bearing 23 is formed inside the main housing body 41.
(40) The main housing body 41 has an inner peripheral surface 41a which faces the outer peripheral surfaces 37a and 37b of the outer ring main body 37. The inner peripheral surface 41a of the main housing body 41 is a surface corresponding to the inner peripheral surface 25a of the housing 25.
(41) The oil supply pipe connection port 41B is formed on an outer circumferential portion of the main housing body 41, which is positioned on an upper portions side. One end of the oil supply pipe connection port 41B is exposed from the outer peripheral surface of the main housing body 41. The oil supply pipe connection port 41B extends in a direction toward the bearing 23 from the outer peripheral surface of the main housing body 41.
(42) An end portion of oil supply pipe (not illustrated) for supplying the oil 39 is connected to the oil supply pipe connection port 41B.
(43) The oil distribution portion 41C is formed in a portion of the main housing body 41, which is positioned on an inner side of the oil supply pipe connection port 41B.
(44) The oil distribution portion 41C is a space communicating with the oil supply pipe connection port 41B. The oil distribution portion 41C extends in a direction toward the bearing 23 from the oil supply pipe connection port 41B.
(45) The first oil supply hole 41D is formed to penetrate the main housing body 41 positioned between the oil distribution portion 41C and the second recessed portion 37B.sub.1. One end of the first oil supply hole 41D communicates with the oil distribution portion 41C, and the other end of the first oil supply hole 41D is exposed from the inner peripheral surface 41a.
(46) The other end of the first oil supply hole 41D faces the second recessed portion 37B.sub.1 in the radial direction Dr. The first oil supply hole 41D supplies the oil 39 supplied from the oil distribution portion 41C to the second recessed portion 37B.sub.1.
(47) The first oil supply hole 41E is formed to penetrate the main housing body 41 positioned between the oil distribution portion 41C and the second recessed portion 37B.sub.2. One end of the first oil supply hole 41E communicates with the oil distribution portion 41C, and the other end of the first oil supply hole 41E is exposed from the inner peripheral surface 41a.
(48) The other end of the first oil supply hole 41E faces the second recessed portion 37B2 in the radial direction Dr. The first oil supply hole 41E supplies the oil 39 supplied from the oil distribution portion 41C to the second recessed portion 37B.sub.2.
(49) The first oil discharge port 41F is formed to penetrate the main housing body 41 positioned directly below the outer ring 32, in the radial direction Dr. The first oil discharge port 41F is disposed to face the oil discharge hole 37D in the radial direction Dr. The first oil discharge port 41F guides the oil 39 discharged from the bearing 23 toward the second oil discharge port 41G.
(50) The second oil discharge port 41G is formed to penetrate the main housing body 41 positioned below the first oil discharge port 41F, in the radial direction Dr. The second oil discharge port 41G discharges the oil 39 passing through the first oil discharge port 41F to the outside of the main housing body 41.
(51) One first groove 41H is formed in the outer side region E.sub.1.
(52) The first groove 41H is inclined in a direction toward the first oil supply hole 41D from one end of the outer ring 32. The first groove 41H is a spiral groove inclined in a direction toward the first oil supply hole 41D from one end of the outer ring 32.
(53) The first groove 41H guides the oil 39 in a direction toward the first oil supply hole 41D as the first groove 41H is directed to the rotation direction B front side of the rotating shaft 21.
(54) The outer side end of the first groove 41H is formed not to reach the one end of the housing 25. The inner side end of the first groove 41H is disposed on the outer side of the second recessed portion 37B.sub.1.
(55) The number of first grooves 41H is preferably one or more, and is not limited to the number (one) illustrated in
(56) One first groove 41I is formed in the outer side region E.sub.2.
(57) The first groove 41I is inclined in a direction toward the first oil supply hole 41E from the other end of the outer ring 32. The first groove 41I is a spiral groove inclined in a direction opposite to the first groove 41H.
(58) The first groove 41I guides the oil 39 in a direction toward the first oil supply hole 41E as the first groove 41I is directed to the rotation direction B front side of the rotating shaft 21.
(59) The outer side end of the first groove 41I is formed not to reach the other end of the housing 25. The inner side end of the first groove 41I is disposed on the outer side of the second recessed portion 37B.sub.2.
(60) The number of first grooves 41I is preferably one or more, and is not limited to the number (one) illustrated in
(61) By forming the first grooves 41H and 41I configured as described above on the inner peripheral surface 41a of the main housing body 41 facing the outer ring 32, the oil 39 which is moved in the direction toward the end of the outer ring 32 can be guided in a direction toward the first oil supply holes 41D and 41E along the first grooves 41H and 41I.
(62) As a result, it is possible to suppress that the oil 39 supplied between the housing 25 and the outer ring 32 leaks from the end of the outer ring 32 to the outside of the outer ring 32.
(63) The thrust sleeve 12 is provided on the outer peripheral surface of the rotating shaft 21 positioned between the inner ring 31 and the compressor wheel 16. The thrust sleeve 12 has a thrust collar 12A protruding to the outer side of the radial direction Dr.
(64) The annular member 14 is a member extending to the outer side of the radial direction Dr from the thrust sleeve 12 positioned between the thrust collar 12A and the compressor wheel 16.
(65) The annular member 14 is in contact with the thrust sleeve 12 via a seal member on the inner side of the radial direction Dr, and is in contact with the main housing body 41 via a seal member on the outer side of the radial direction Dr.
(66) Further, the inner side portion of the annular member 14 abuts on the thrust collar 12A in the axis direction Da. This portion functions as a thrust bearing.
(67) The compressor wheel 16 is provided to the portion (portion including one end portion) of the rotating shaft 21 protruding from the housing 25. A compressor housing (not illustrated) is provided on the outer side of the compressor wheel 16.
(68) The turbine wheel 18 is provided to the other end portion of the rotating shaft 21. A turbine housing (not illustrated) is provided on the outer side of the turbine wheel 18.
(69) With the rotating machine 11 of the first embodiment, by forming the first grooves 41H and 41I inclined in the direction toward the first oil supply holes 41D and 41E from the end of the outer ring 32, in the outer side regions E.sub.1 and E.sub.2, which are positioned between the first oil supply holes 41D and 41E and the ends of the outer ring 32 close to the forming positions of the first oil supply holes 41D and 41E in the axis direction Da, the oil 39 which is moved toward the end of the outer ring 32 can be moved in a direction toward the first oil supply holes 41D and 41E from the end of the outer ring 32 along the first grooves 41H and 41I.
(70) As a result, it is possible to suppress that the oil 39 supplied between the housing 25 and the outer ring 32 leaks from the end of the outer ring to the outside of the outer ring.
(71) The turbocharger 10 including the above-described rotating machine 11 can obtain the function of the stable oil film damper, and therefore can be driven in a stable state.
(72) Next, a rotating machine 45 of a first modification example of the first embodiment will be described with reference to
(73) The rotating machine 45 is configured in the same manner as the rotating machine 11 except that the rotating machine 45 has a housing 46 instead of the housing 25 constituting the rotating machine 11 of the first embodiment.
(74) The housing 46 is configured in the same manner as the housing 25 except that second grooves 46A and 46B are formed on the housing 25 described in the first embodiment.
(75) That is, in the rotating machine 45 of the first modification example of the first embodiment, the groove portion includes the first grooves 41H and 41I, and the second grooves 46A and 46B.
(76) The second grooves 46A and 46B are formed in the central region E.sub.3 which is positioned closer to the central side of the outer ring 32 than the outer side regions E.sub.1 and E.sub.2.
(77) The second grooves 46A and 46B are formed on the inner peripheral surface 41a of the main housing body 41 so as to avoid the second oil supply holes 37C.sub.1 and 37C.sub.2 and the first oil discharge port 41F.
(78) The second groove 46A is disposed between the first oil discharge port 41F and the second oil supply hole 37C.sub.1. The second groove 46A is inclined in a direction opposite to the first groove 41H.
(79) The second groove 46B is disposed between the first oil discharge port 41F and the second oil supply hole 37C.sub.2. The second groove 46B is inclined in a direction opposite to the first groove 41I.
(80) With the rotating machine 45 of the first modification example of the first embodiment, by forming the second grooves 46A and 46B, which are inclined in the directions opposite to the first grooves 41H and 41I, in the central region E.sub.3 positioned closer to the central side of the outer ring 32 than the outer side regions E.sub.1 and E.sub.2, the oil 39 supplied from the first oil supply holes 41D and 41E can be moved in a direction toward the first oil supply holes 41D and 41E.
(81) For example, in
(82) Further, the position where the second grooves 46A and 46B are formed is preferably the central region E.sub.3, but is not limited to the forming position of the second grooves 46A and 46B illustrated in
(83) Next, a rotating machine 50 of a second modification example of the first embodiment will be described with reference to
(84) The rotating machine 50 is configured in the same manner as the rotating machine 11 except that the rotating machine 50 has a housing 51 instead of the housing 25 constituting the rotating machine 11 of the first embodiment.
(85) The housing 51 is configured in the same manner as the housing 25 except that second grooves 51A and 51B are formed on the housing 25 described in the first embodiment.
(86) That is, in the second modification example of the first embodiment, the groove portion includes the first grooves 41H and 41I, and the second grooves 51A and 51B.
(87) The second grooves 51A and 51B are formed in the central region E.sub.3. The second grooves 51A and 51B are formed on the inner peripheral surface 41a of the main housing body 41 so as to avoid the second oil supply holes 37C.sub.1 and 37C.sub.2 and the first oil discharge port 41F.
(88) The second groove 51A is disposed between the first oil discharge port 41F and the second oil supply hole 37C.sub.1. The second groove 51A is inclined in the same direction as the first groove 41H.
(89) The second groove 51B is disposed between the first oil discharge port 41F and the second oil supply hole 37C.sub.2. The second groove 51B is inclined in the same direction as the first groove 41I.
(90) With the rotating machine 50 of the second modification example of the first embodiment, by forming the second grooves 51A and 51B, which are inclined in the same directions as the first grooves 41H and 41I, in the central region E.sub.3 positioned closer to the central side of the outer ring 32 than the outer side regions E.sub.1 and E.sub.2, the oil 39 supplied from the first oil supply holes 41D and 41E can be moved in a direction toward the first oil supply holes 41D and 41E.
(91) For example, in
(92) Further, the position where the second grooves 51A and 51B are formed is preferably the central region E.sub.3, but is not limited to the forming position of the second grooves 51A and 51B illustrated in
Second Embodiment
(93) A rotating machine 60 of a second embodiment of the present invention will be described with reference to
(94) The rotating machine 60 is configured in the same manner as the rotating machine 11 except that the rotating machine 60 has a housing 61 and a bearing 62 instead of the housing 25 and the bearing 23 constituting the rotating machine 11 of the first embodiment.
(95) The housing 61 is configured in the same manner as the housing 25 except that the first oil supply holes 41D and 41E are not formed.
(96) The bearing 62 is configured in the same manner as the bearing 23 except that the bearing 62 has an outer ring 64 instead of the outer ring 32.
(97) The outer ring 64 is configured in the same manner as the outer ring 32 except that the first grooves 41H and 41I are formed on the outer peripheral surfaces 37b corresponding to the outer side regions E.sub.1 and E.sub.2.
(98) With the rotating machine 60 of the second embodiment, by forming the first grooves 41H and 41I on the outer peripheral surfaces 37b of the outer ring 64 corresponding to the outer side regions E.sub.1 and E.sub.2, the same effect as the rotating machine 11 described in the first embodiment can be obtained.
(99) In the second embodiment, the second grooves 46A and 46B illustrated in
Third Embodiment
(100) A rotating machine 70 of a third embodiment of the present invention will be described with reference to
(101) The rotating machine 70 is configured in the same manner as the rotating machine 11 except that the rotating machine 70 has the bearing 62 described in the second embodiment instead of the bearing 23 constituting the rotating machine 11 of the first embodiment.
(102) That is, in the rotating machine of the third embodiment, the first grooves 41H and 41I are formed on each of the housing 25 and the outer ring 64.
(103) In a case where the first grooves 41H and 41I are formed on each of the housing 25 and the outer ring 64 as in the rotating machine 70 of the third embodiment, the same effect as the rotating machine 11 of the first embodiment can be obtained.
(104) In the third embodiment, the second grooves 46A and 46B illustrated in
Fourth Embodiment
(105) A rotating machine 80 of a fourth embodiment of the present invention will be described with reference to
(106) The rotating machine 80 is configured in the same manner as the rotating machine 11 except that the rotating machine 80 has a housing 81 instead of the housing 25 constituting the rotating machine 11 of the first embodiment.
(107) The housing 81 is configured in the same manner as the housing 25 except that groove portions 81A and 81B are formed on the inner peripheral surface 41a of the main housing body 41 instead of the first grooves 41H and 41I formed on the housing 25 of the first embodiment.
(108) The groove portion 81A has a first groove 82A and a third groove 82B.
(109) The first groove 82A is formed on the inner peripheral surface 41a positioned on one end side of the outer ring 32, in the outer side region E.sub.1. The first groove 82A is inclined in a direction toward the first oil supply hole 41D from one end of the outer ring 32.
(110) The first groove 82A is a groove shorter than the first groove 41H described in the first embodiment. A plurality of first grooves 82A are formed at intervals in the circumferential direction Dc.
(111) The third groove 82B is formed at a position adjacent to the first groove 82A in the axis direction Da, in the outer side region E.sub.1. A plurality of third grooves 82B are formed at intervals in the circumferential direction Dc.
(112) The third groove 82B is inclined in a direction opposite to the inclination direction of the first groove 82A. In the rotation direction B front side, one end of the third groove 82B and one end of the first groove 82A are connected.
(113) A plurality of groove portions 81A configured as described above are formed at intervals in the circumferential direction Dc.
(114) In a state where the rotating shaft 21 is rotated, in oil reservoir portion 81Aa which is a portion where one end of the third groove 82B and one end of the first groove 82A are connected (a part of the first and third grooves 82A and 82B), the oil 39 guided by the first groove 82A and the third groove 82B is likely to accumulate. The oil 39 accumulated in the oil reservoir portion 81Aa functions as a part of the oil film damper.
(115) As the shape of the groove portion 81A configured as described above, for example, a V shape illustrated in
(116) The groove portion 81B has a first groove 82C and a third groove 82D.
(117) The first groove 82C is formed on the inner peripheral surface 41a positioned on the other end side of the outer ring 32, in the outer side region E.sub.2. The first groove 82C is inclined in a direction toward the first oil supply hole 41E from the other end of the outer ring 32.
(118) The first groove 82C is a groove shorter than the first groove 41I described in the first embodiment. A plurality of first grooves 82C are formed at intervals in the circumferential direction Dc.
(119) The third groove 82D is formed at a position adjacent to the first groove 82C in the axis direction Da, in the outer side region E.sub.2. A plurality of third grooves 82D are formed at intervals in the circumferential direction Dc.
(120) The third groove 82D is inclined in a direction opposite to the inclination direction of the first groove 82C. In the rotation direction B front side, one end of the third groove 82D and one end of the first groove 82C are connected.
(121) A plurality of groove portions 81B configured as described above are formed at intervals in the circumferential direction Dc.
(122) In a state where the rotating shaft 21 is rotated, in oil reservoir portion 81Ba which is a portion where one end of the third groove 82D and one end of the first groove 82C are connected (a part of the first and third grooves 82C and 82D), the oil 39 guided by the first groove 82C and the third groove 82D is likely to accumulate. The oil 39 accumulated in the oil reservoir portion 81Ba functions as a part of the oil film damper.
(123) As the shape of the groove portion 81B configured as described above, for example, a V shape illustrated in
(124) With the rotating machine 80 of the fourth embodiment, by forming the third groove 82B, which is inclined in the direction opposite to the first groove 82A and of which one end is connected to one end of the first groove 82A on the rotation direction B front side, and the third groove 82D, which is inclined in the direction opposite to the first groove 82C and of which one end is connected to one end of the first groove 82C on the rotation direction B front side, the oil can be likely to accumulate in the oil reservoir portions 81Aa and 81Ba where one ends of the first grooves 82A and 82C and one ends of the third grooves 82B and 82D are connected, and therefore, it is possible to suppress that oil leaks from both ends of the outer ring 32.
(125) In the fourth embodiment, the second grooves 46A and 46B illustrated in
(126) A rotating machine 90 of a first modification example of the fourth embodiment of the present invention will be described with reference to
(127) The rotating machine 90 is configured in the same manner as the rotating machine 80 except that the rotating machine 90 has a housing 91 instead of the housing 81 constituting the rotating machine 80 of the fourth embodiment.
(128) The housing 91 is configured in the same manner as the housing 25 except that groove portions 92A and 92B are formed on the inner peripheral surface 41a of the main housing body 41 instead of the groove portions 81A and 81B formed on the housing 81 of the fourth embodiment.
(129) The groove portion 92A is configured in the same manner as the groove portion 81A except that the groove portion 92A has a fourth groove 93A in addition to the configuration of the groove portion 81A described in the fourth embodiment.
(130) The fourth groove 93A is formed in the outer side region E.sub.1 positioned between the third groove 82B and the central region E.sub.3. The fourth groove 93A is a groove inclined in the same direction as the first groove 82A. The fourth groove 93A is a groove longer than the first groove 82A. A plurality of fourth grooves 93A are formed in the circumferential direction Dc. One end of the fourth groove 93A is connected to the other end of the third groove 82B.
(131) The groove portion 92B is configured in the same manner as the groove portion 81B except that the groove portion 92B has a fourth groove 93B in addition to the configuration of the groove portion 81B described in the fourth embodiment.
(132) The fourth groove 93B is formed in the outer side region E.sub.2 positioned between the third groove 82D and the central region E.sub.3. The fourth groove 93B is a groove inclined in the same direction as the first groove 82C. The fourth groove 93B is a groove longer than the first groove 82C. A plurality of fourth grooves 93B are formed in the circumferential direction Dc. One end of the fourth groove 93B is connected to the other end of the third groove 82D.
(133) With the rotating machine 90 according to the first modification example of the fourth embodiment, by providing the above-described groove portions 92A and 92B, the oil can be guided in a direction toward the first oil supply holes 41D and 41E from both ends of the outer ring along the fourth grooves 93A and 93B. As a result, it is possible to further suppress that oil leaks from both ends of the outer ring.
(134) In the first modification example of the fourth embodiment, the second grooves 46A and 46B illustrated in
(135) A rotating machine 100 of a second modification example of the fourth embodiment will be described with reference to
(136) The rotating machine 100 is configured in the same manner as the rotating machine 90 except that the forming positions of the fourth grooves 93A and 93B constituting the rotating machine 90 of the first modification example of the fourth embodiment are different.
(137) The fourth groove 93A is separated from the groove portions 81A, and a part of the fourth groove 93A is disposed between the groove portions 81A which are disposed adjacent to each other in the circumferential direction Dc.
(138) The fourth groove 93B is separated from the groove portion 81B, and a part of the fourth groove 93B is disposed between the groove portion 81B Which are disposed adjacent to each other in the circumferential direction. Dc.
(139) In the rotating machine 100 according to the second modification example of the fourth embodiment, the same effect as the rotating machine 90 according to the first modification example of fourth embodiment described above can be obtained.
(140) The preferred embodiments of the present invention have been described above, but the present invention is not limited to a specific embodiment, and can be variously modified and changed within the scope of the present invention described in the claims.
(141) For example, the first grooves 41H, 41I, 82A, and 82C, the second grooves 46A, 46B, 51A, and 51B, the third grooves 82B and 82D, and the fourth grooves 93A and 93B described in the first to fourth embodiments may be appropriately combined.
(142) Further, the rotating machines 11, 45, 50, 60, 70, 80, 90, and 100 described in the first to fourth embodiments can be applied to devices other than the turbocharger.
INDUSTRIAL APPLICABILITY
(143) The present invention can be applied to a rotating machine and a turbocharger.
REFERENCE SIGNS LIST
(144) 10: turbocharger 11, 45, 50, 60, 70, 80, 90, 100: rotating machine 12: thrust sleeve 12A: thrust collar 14: annular member 16: compressor wheel 18: turbine wheel 21: rotating shaft 23, 62: bearing 46, 51, 61, 81, 91: housing 25a, 41a: inner peripheral surface 31: inner ring 31a, 37a, 37h: outer peripheral surface 32, 64: outer ring 34: rolling body 37: outer ring main body 37A: first recessed portion 37B.sub.1, 37B.sub.2: second recessed portion 37C.sub.1, 37C.sub.2: second oil supply hole 37D: oil discharge hole 39: oil 41: main housing body 41B: oil supply pipe connection port 41C: oil distribution portion 411D, 41E: first oil supply hole 41F: first oil discharge port 41G: second oil discharge port 41H, 41I, 82A, 82C: first groove 46A, 46B, 51A, 51B: second groove 81A, 81B, 92A, 92B: cootie portion 81Aa, 81Ba: oil reservoir portion 82B, 82D: third groove 93A, 93B: fourth groove B: rotation direction C: clearance Da: axis direction Dc: circumferential direction Dr: radial direction E.sub.1, E.sub.2: outer side region E.sub.3: central region O: axis