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US4721441A Expired / Lapsed US ⏱️ 0.0 years remaining

Bearing device for turbocharger

Assignee: IHI Corp
•
Filing: 1987-07-09
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Granted: 1988-01-26
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Expires: 2007-07-09
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Abstract

Abstract A bearing device for a turbocharger wherein a bearing casing is interposed between a turbine casing and a compressor casing; disposed within a bearing housing of the bearing casing are a ball bearing on the side of the turbine and a ball bearing on the side of the compressor both of which is supported by a one-piece oil film damper which is floating; and a pin is loosely fitted into the oil film damper and the bearing housing so as to prevent the rotation of the oil film damper.

Inventors

  • 👤 Kazuya Miyashita
  • 👤 Nobuyuki Ikeya

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 04:24
CPC Classifications
F; F16; F16C; F16C27/00; F16C27/04; F16C27/045; F01; F01D; F01D25/00; F01D25/16; F01D25/162; F01D25/164; F16C19/00; F16C19/54; F16C19/546; F16C19/547; F16C19/548; F16C25/00; F16C25/06; F16C25/08; F16C25/083; F16C35/00; F16C35/04; F16C35/06; F16C35/07; F16C35/077; F05; F05D; F05D2220/00; F05D2220/40; F16C19/02; F16C19/14; F16C19/16; F16C19/163; F16C2360/00; F16C2360/23; F16C2360/24

Claims Analysis

Total Claims: 13
Claim 1
Independent Claim 187 words
A turbocharger comprising: a turbine casing, a compressor casing, a bearing casing interposed between said turbine and compressor casings, a turbine ball bearing unit adjacent to said turbine casing, and a compressor ball bearing unit adjacent to said compressor casing, a turbine shaft supported by said bearing units, a one-piece monolithic oil film damper mounted in said bearing casing to be interposed between said bearing casing and said ball bearing units, said oil film damper being spaced from said bearing casing to define a gap with said bearing casing for essentially the entire length of said oil film damper and engaging both of said ball bearing units, means for injecting oil into said gap for floatingly mounting said oil film damper in said bearing casing, and a pin loosely connecting said oil film damper to said bearing casing to prevent rotation of said oil film damper relative to said bearing casing, said pin being received in a slot defined in said oil film damper and in a slot defined in said bearing casing to allow said oil film damper to float with respect to said bearing casing.
Claim 2
Dependent Claim 187 words
A turbocharger comprising: a turbine casing, a compressor casing, a bearing casing interposed between said turbine and compressor casings, a turbine ball bearing unit adjacent to said turbine casing, and a compressor ball bearing unit adjacent to said compressor casing, a turbine shaft supported by said bearing units, a one-piece monolithic oil film damper mounted in said bearing casing to be interposed between said bearing casing and said ball bearing units, said oil film damper being spaced from said bearing casing to define a gap with said bearing casing for essentially the entire length of said oil film damper and engaging both of said ball bearing units, means for injecting oil into said gap for floatingly mounting said oil film damper in said bearing casing, and a pin loosely connecting said oil film damper to said bearing casing to prevent rotation of said oil film damper relative to said bearing casing, said pin being received in a slot defined in said oil film damper and in a slot defined in said bearing casing to allow said oil film damper to float with respect to said bearing casing.
Claim 3
Dependent Claim 26 words
A turbocharger according to claim 13 wherein said oil injecting means includes an oil discharge port in communication with an oil outlet of said bearing housing.
Claim 4
Dependent Claim 56 words
A turbocharger according to claim 13 wherein said one-piece oil film damper is provided with at least either a small hole formed for effecting jet lubrication of said ball bearing with part of an oil film formed between said oil film damper and said bearing housing or clearances for subjecting said ball bearings to mist lubrication.
Claim 5
Dependent Claim 56 words
A turbocharger according to claim 2 wherein said one-piece oil film damper is provided with at least either a small hole formed for effecting jet lubrication of said ball bearing with part of an oil film formed between said oil film damper and said bearing housing or clearances for subjecting said ball bearings to mist lubrication.
Claim 6
Dependent Claim 112 words
A turbocharger according to claim 1, comprising a spring between the ball bearing adjacent the turbine and the ball bearing adjacent the compressor, said spring being so preloaded that an outer race of at least one of said ball bearings is moved away from an outer race of the other ball bearing in a direction parallel to the longitudinal axis of the turbine shaft; an inner wall surface of said oil film damper having stepped portions, and bearing stoppers engaging said stepped portions, so that when an axial thrust of said turbine shaft in excess of the preload of said spring acts, said ball bearings are prevented from moving toward each other.
Claim 7
Dependent Claim 113 words
A turbocharger according to claim 2, comprising a spring interposed between the ball bearing adjacent the turbine and the ball bearing adjacent the compressor, said spring being so preloaded that an outer race of at least one of said ball bearings is moved away from an outer race of the other ball bearing in a direction parallel to the longitudinal axis of the turbine shaft; an inner wall surface of said oil film damper having stepped portions, and bearing stoppers engaging said stepped portions, so that when an axial thrust of said turbine shaft in excess of the preload of said spring acts, said ball bearings are prevented from moving toward each other.
Claim 8
Dependent Claim 113 words
A turbocharger according to claim 3, comprising a spring interposed between the ball bearings adjacent the turbine and the ball bearing adjacent the compressor, said spring being so preloaded that an outer race of at least one of said ball bearings is moved away from an outer race of the other ball bearing in a direction parallel to the longitudinal axis of the turbine shaft; an inner wall surface of said oil film damper having stepped portions, and bearing stoppers engaging said stepped portions, so that when an axial thrust of said turbine shaft in excess of the preload of said spring acts, said ball bearings are prevented from moving toward each other.
Claim 9
Dependent Claim 113 words
A turbocharger according to claim 4, comprising a spring interposed between the ball bearing adjacent the turbine and the ball bearing adjacent the compressor, said spring being so preloaded that an outer race of at least one of said ball bearings is moved away from an outer race of the other ball bearing in a direction parallel to the longitudinal axis of the turbine shaft; an inner wall surface of said oil film damper having stepped portions, and bearing stoppers engaging said stepped portions, so that when an axial thrust of said turbine shaft in excess of the preload of said spring acts, said ball bearings are prevented from moving toward each other.
Claim 10
Dependent Claim 36 words
a turbocharger according to claim 5 wherein stopper rings are interposed between the stepped portions of said oil film damper on the one hand and the outer races of said ball bearings on the other hand.
Claim 11
Dependent Claim 36 words
A turbocharger according to claim 6 wherein stopper rings are interposed between the stepped portions of said oil film damper on the one hand and the outer races of said ball bearings on the other hand.
Claim 12
Dependent Claim 37 words
A turbocharger according to claim 7 wherein the stopper rings are interposed between the stepped portions of said oil film damper on the one hand and the outer races of said ball bearings on the other hand.
Claim 13
Dependent Claim 36 words
A turbocharger according to claim 8 wherein stopper rings are interposed between the stepped portions of said oil film damper on the one hand and the outer races of said ball bearings on the other hand.

References Cited (Backward Citations)

US2684196A Cited
US2689528A Cited
US2991926A Cited
US2973136A Cited
US3017230A Cited
US3056634A Cited
US4116506A Cited
US4179247A Cited
US4233821A Cited
US4285632A Cited
US4529324A Cited
US4482303A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1991-01-25 1991-07-27 1992-01-26 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1995-01-25 1995-07-27 1996-01-26 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1999-01-25 1999-07-27 2000-01-26 $7700.00 Window Closed / Lapsed

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