A turbocharger includes a rotating shaft which extends along an axial line thereof, a turbine rotor which is provided on one end side of the rotating shaft, a compressor rotor which is provided on the other end side of the rotating shaft, a roller bearing which rotatably supports the rotating shaft around the axis line between the turbine rotor and the compressor rotor, a housing which covers the roller bearing from an outer peripheral side of the roller bearing, and a tubular sleeve which is provided inside the housing, which is disposed on an outer peripheral side of an outer ring of the roller bearing with a gap for holding a lubricant between the sleeve and the outer ring, and at least part of which is formed of a damping material.
1. A turbocharger comprising:
a rotating shaft which extends along an axial line thereof;
a turbine rotor which is provided on one end side of the rotating shaft;
a compressor rotor which is provided on the other end side of the rotating shaft;
a roller bearing which rotatably supports the rotating shaft around the axis line between the turbine rotor and the compressor rotor;
a housing which covers the roller bearing from an outer peripheral side of the roller bearing; and
a sleeve which is provided inside the housing, which is disposed on an outer peripheral side of an outer ring of the roller bearing with a gap for holding a lubricant between an inner surface of the sleeve and the outer ring, and at least part of which is formed of a damping material,
wherein an outer surface of the sleeve includes a shape having a plurality of protrusions continuous in a direction of a central axis of the rotating shaft,
wherein recessed portions corresponding to the protrusions of the sleeve are formed on an inner surface of an accommodation portion which is formed inside the housing and in which the roller bearing is accommodated,
wherein the plurality of protrusions are fitted into the recessed portions of the accommodation portion thereby positioning the sleeve in a circumferential direction with respect to the accommodation portion.
2. The turbocharger according to claim 1 , wherein the sleeve includes a first sleeve disposed on an inner peripheral side and a second sleeve disposed on an outer peripheral side of the first sleeve.
3. The turbocharger according to claim 2 , wherein the first sleeve and the second sleeve are formed of different damping materials from each other.
4. The turbocharger according to claim 3 , wherein one of the first sleeve and the second sleeve is formed of a metal material and the other of the first sleeve and the second sleeve is formed of a damping material.
5. The turbocharger according to claim 4 , wherein the first sleeve is formed of a material having higher rigidity than that of the second sleeve.
6. The turbocharger according to claim 3 , wherein the first sleeve is formed of a material having higher rigidity than that of the second sleeve.
7. The turbocharger according to claim 2 , wherein one of the first sleeve and the second sleeve is formed of a metal material and the other of the first sleeve and the second sleeve is formed of a damping material.
8. The turbocharger according to claim 7 , wherein the first sleeve is formed of a material having higher rigidity than that of the second sleeve.
9. The turbocharger according to claim 2 , wherein the first sleeve is formed of a material having higher rigidity than that of the second sleeve.
10. The turbocharger according to claim 1 , wherein a lowest end portion of each of the outer ring, the sleeve, and the accommodation portion has a discharge flow path penetrating each of the outer ring, the sleeve, and the accommodation portion toward a lower side.
11. A turbocharger comprising:
a rotating shaft which extends along an axial line thereof;
a turbine rotor which is provided on one end side of the rotating shaft;
a compressor rotor which is provided on the other end side of the rotating shaft;
a roller bearing which rotatably supports the rotating shaft around the axis line between the turbine rotor and the compressor rotor;
a housing which covers the roller bearing from an outer peripheral side of the roller bearing; and
a sleeve which is provided inside the housing, which is disposed on an outer peripheral side of an outer ring of the roller bearing with a gap for holding a lubricant between the sleeve and the outer ring, and at least part of which is formed of a damping material,
wherein an accommodation portion that accommodates the roller bearing is provided inside the housing,
wherein an outer peripheral surface of the sleeve on the accommodation portion side is formed in a bellows shape in which irregularities continuous in a circumferential direction around a central axis of the rotating shaft are formed to be continued in a direction of the central axis, and
wherein the outer peripheral surface of the sleeve contacts with the inner peripheral surface of the accommodation portion.
12. The turbocharger according to claim 11 , wherein the sleeve includes a first sleeve disposed on an inner peripheral side and a second sleeve disposed on an outer peripheral side of the first sleeve.
13. The turbocharger according to claim 12 , wherein the first sleeve and the second sleeve are formed of different damping materials from each other.
14. The turbocharger according to claim 13 , wherein one of the first sleeve and the second sleeve is formed of a metal material and the other of the first sleeve and the second sleeve is formed of a damping material.
15. The turbocharger according to claim 14 , wherein the first sleeve is formed of a material having higher rigidity than that of the second sleeve.
16. The turbocharger according to claim 13 , wherein the first sleeve is formed of a material having higher rigidity than that of the second sleeve.
17. The turbocharger according to claim 12 , wherein one of the first sleeve and the second sleeve is formed of a metal material and the other of the first sleeve and the second sleeve is formed of a damping material.
18. The turbocharger according to claim 17 , wherein the first sleeve is formed of a material having higher rigidity than that of the second sleeve.
19. The turbocharger according to claim 12 , wherein the first sleeve is formed of a material having higher rigidity than that of the second sleeve.