Turbocharger bearing assembly and lubrication thereof
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F02B-033/44
F01D-025/16
F01D-025/18
출원번호
US-0697678
(2010-02-01)
등록번호
US-8353158
(2013-01-15)
우선권정보
GB-0714929.7 (2007-08-01)
발명자
/ 주소
Purdey, Matthew J
Khan, Mohammed Hanif
출원인 / 주소
Cummins Turbo Technologies Limited
인용정보
피인용 횟수 :
3인용 특허 :
7
초록▼
A turbocharger bearing housing defines a bore in which the turbocharger shaft is mounted for rotation in journal bearings. Lubricating oil is delivered to the journal bearings and a residue is retained in reservoirs in which the journal bearings are located. Two fluid retaining members are disposed
A turbocharger bearing housing defines a bore in which the turbocharger shaft is mounted for rotation in journal bearings. Lubricating oil is delivered to the journal bearings and a residue is retained in reservoirs in which the journal bearings are located. Two fluid retaining members are disposed around the shaft, each forming a wall of the reservoir and being sealed to the bearing housing. The lubricating fluid reservoir is provided between the fluid retaining members to a depth that at least partially immerses the journal bearings even when the oil supply is interrupted. This ensures that there is sufficient oil to lubricate the bearings at engine start-up, thereby reducing the risk of wear.
대표청구항▼
1. A turbocharger comprising: a turbocharger shaft for rotation about an axis and for supporting a compressor wheel at first end and a turbine wheel at a second end;a bearing housing having a wall defining a bore in which the turbocharger shaft is received with a substantially annular clearance, the
1. A turbocharger comprising: a turbocharger shaft for rotation about an axis and for supporting a compressor wheel at first end and a turbine wheel at a second end;a bearing housing having a wall defining a bore in which the turbocharger shaft is received with a substantially annular clearance, the turbocharger shaft being supported for rotation in the bore by at least two journal bearings housed within the annular clearance;a first gas seal between the turbocharger and the bearing housing proximate the first end of the turbocharger shaft;a second gas seal between the turbocharger shaft and the bearing housing proximate the second end of the turbocharger shaft;at least one fluid passage for delivering lubricating fluid from a fluid source to the at least two journal bearings;at least three fluid retaining members, including a first, a second, and a third fluid retaining member, disposed around the turbocharger shaft and each having an outer portion that is sealed to the wall, and each disposed between the first and second gas seals; andthe at least two journal bearings being disposed at an axial position between the first fluid retaining member and the second fluid retaining member and the third fluid retaining member being disposed between a first journal bearing and second journal bearing of the at least two journal bearings so that, in use when the turbocharger shaft is not rotating, a volume of lubricating fluid is retained in a first lubricating fluid reservoir defined between the first and third fluid retaining members and the wall to a depth that at least partially immerses the first journal bearing, and in a second lubricating fluid reservoir defined between the second and third fluid retaining members and the wall to a depth that at least partially immerses the second journal bearing. 2. A turbocharger according to claim 1, wherein the at least three fluid retaining members are disposed between the second gas seal and the compressor wheel. 3. A turbocharger according to claim 1, wherein at least one of the at least three fluid retaining members is substantially annular. 4. A turbocharger according to claim 1, wherein a first of the at least three fluid retaining members is an axial thrust bearing acting between the turbocharger shaft and the bearing housing so as to resist axial thrust forces of the turbocharger shaft. 5. A turbocharger according to claim 4, wherein the axial thrust bearing comprises a sealing element disposed in an interface between a surface of the axial thrust bearing and a surface of the bearing housing. 6. A turbocharger according to claim 4, wherein the thrust bearing bears against a bearing surface of the bearing housing that has a fluid relief passage offset by a predetermined distance from the turbocharger shaft axis, whereby fluid above a certain level in the reservoir is able to egress via the fluid relief passage. 7. A turbocharger according to claim 6, wherein the fluid relief passage is in the form of an opening in the bearing surface of the bearing housing. 8. A turbocharger according to claim 1, wherein at least one of the three fluid retaining members is integrally formed with the bearing housing. 9. A turbocharger according to claim 8, wherein at least one of the three fluid retaining members is in the form of a substantially annular rib integrally formed with the bearing housing. 10. A turbocharger according to claim 1, wherein at least one of the at least three fluid retaining members is seated in a groove defined in the bearing housing. 11. A turbocharger according to claim 10, wherein the outer portion of the at least three fluid retaining member seated in the groove is resiliently flexible such that it expands or deforms radially into said groove. 12. A turbocharger according to claim 1, wherein the outer portion of at least one of the at least three fluid retaining members comprises an elastomeric element for sealing against a surface of the bearing housing. 13. A turbocharger according to claim 12, wherein the at least one of the at least three fluid retaining members further comprises a circlip bonded to the elastomeric member. 14. A turbocharger according to claim 13, wherein the at least one of the at least three fluid retaining member further comprises an annular member with an outer surface for supporting the elastomeric element. 15. A turbocharger according to claim 1, wherein at least one of the at least three fluid retaining members comprises an annular body with a central aperture in which said turbocharger shaft is received, the body having a substantially radially extending portion and a substantially axially extending portion that forms said outer portion, an outer surface of the axially extending portion being arranged to seal against a surface of the bearing housing. 16. A turbocharger according to claim 1, wherein at least one of the at least three fluid retaining members is disposed immediately adjacent to the at least one journal bearing so as to retain the bearing in an axial direction. 17. A turbocharger according to claim 1, wherein there is provided at least one fluid drain outside of at least one of the first lubricating fluid reservoir and the second lubricating fluid reservoir for allowing lubricating fluid to drain from the bore. 18. A turbocharger comprising: a turbocharger shaft for rotation about an axis and for supporting a compressor wheel at first end and a turbine wheel at a second end;a bearing housing having a wall defining a bore in which the turbocharger shaft is received with a substantially annular clearance, the turbocharger shaft being supported for rotation in the bore by at least one journal bearing housed within the annular clearance;a first gas seal between the turbocharger shaft and the bearing housing proximate the first end of the turbocharger shaft;a second gas seal between the turbocharger shaft and the bearing housing proximate the second end of the turbocharger shaft;at least one fluid passage for delivering lubricating fluid from a fluid source to the at least one journal bearing;at least two fluid retaining members disposed around the turbocharger shaft and each having an outer portion that is sealed to the wall; andthe at least one journal bearing being disposed at an axial position between the at least two fluid retaining members so that, in use when the turbocharger shaft is not rotating, a volume of lubricating fluid is retained in at least one lubricating fluid reservoir defined between the at least two fluid retaining members and the wall to a depth that at least partially immerses the at least one journal bearing;wherein: a first of the at least two fluid retaining members is an axial thrust bearing acting between the turbocharger shaft and the bearing housing so as to resist axial thrust forces of the turbocharger shaft; andthe thrust bearing bears against a bearing surface of the bearing housing that has a fluid relief passage offset by a predetermined distance from the turbocharger shaft axis, whereby fluid above a certain level in the reservoir is able to egress via the fluid relief passage. 19. A turbocharger according to claim 18, wherein the fluid relief passage is in the form of an opening in the bearing surface of the bearing housing. 20. A turbocharger comprising: a turbocharger shaft for rotation about an axis and for supporting a compressor wheel at first end and a turbine wheel at a second end;a bearing housing having a wall defining a bore in which the turbocharger shaft is received with a substantially annular clearance, the turbocharger shaft being supported for rotation in the bore by at least one journal bearing housed within the annular clearance;a first gas seal between the turbocharger shaft and the bearing housing proximate the first end of the turbocharger shaft;a second gas seal between the turbocharger shaft and the bearing housing proximate the second end of the turbocharger shaft;at least one fluid passage for delivering lubricating fluid from a fluid source to the at least one journal bearing;at least two fluid retaining members disposed around the turbocharger shaft and each having an outer portion that is sealed to the wall; andthe at least one journal bearing being disposed at an axial position between the at least two fluid retaining members so that, in use when the turbocharger shaft is not rotating, a volume of lubricating fluid is retained in at least one lubricating fluid reservoir defined between the at least two fluid retaining members and the wall to a depth that at least partially immerses the at least one journal bearing;wherein: the outer portion of at least one of the at least two fluid retaining members comprises an elastomeric element for sealing against a surface of the bearing housing; andthe at least one of the at least two fluid retaining members further comprises a circlip bonded to the elastomeric member. 21. A turbocharger according to claim 20, wherein the at least one of the at least two fluid retaining members further comprises an annular member with an outer surface for supporting the elastomeric element.
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이 특허에 인용된 특허 (7)
Baker Glenn L. (Columbus IN) Engle David R. (Paris Crossing IN) Williams Roger (North Vernon IN), Bearing system for turbocharger.
Fleury Jean-Luc P. (Manhattan Beach) LaRue Gerald D. (Torrance) Silva Kusumal J. (Gardena) Gutknecht Daniel A. (Torrance) Garcia Martin D. (San Pedro CA), Compressor wheel and shaft assembly for turbocharger.
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