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US4652219A Expired / Lapsed US ⏱️ 0.0 years remaining

Turbocharger having a preloaded bearing assembly

Assignee: Teledyne Technologies Inc
•
Filing: 1986-08-08
•
Granted: 1987-03-24
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Expires: 2006-08-08
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Abstract

Abstract A turbocharger having a main housing with a throughbore through which a tubular bearing carrier is coaxially positioned. A shaft extends through the bearing carrier and is rotatably secured to the bearing carrier by a pair of axially spaced bearing assemblies, each having an inner race, an outer race and bearing elements entrapped therebetween. A pair of spacers are coaxially positioned around the shaft in between the bearing assemblies so that an outer axial end of each spacer abuts against the outer race of each bearing assembly. A helical compression spring in a state of compression urges the spacers axially away from each other to equalize the axial compressive load on each bearing assembly and thereby minimize bearing skidding and uneven wear.

Inventors

  • 👤 J. Albert McEachern, Jr.
  • 👤 J. William Brogdon

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 15:49
CPC Classifications
F; F01; F01D; F01D25/00; F01D25/16; F16; F16C; F16C19/00; F16C19/54; F16C19/546; F16C19/547; F16C19/548; F16C25/00; F16C25/06; F16C25/08; F16C25/083; F16C27/00; F16C27/04; F16C27/045; F05; F05D; F05D2220/00; F05D2220/40; F16C19/02; F16C19/14; F16C19/16; F16C19/163; F16C2360/00; F16C2360/23; F16C2360/24

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 264 words
A turbocharger comprising: a main housing having a throughbore, a tubular bearing carrier coaxially positioned within said throughbore, means for securing said bearing carrier to said housing against axial movement, a shaft extending through said bearing carrier, said shaft having a turbine at one end and a compressor at its other end, a pair of bearing assemblies for rotatably mounting said shaft to said bearing carrier, each bearing assembly comprising an inner race, an outer race, and bearing elements entrapped between said races, said bearing assemblies being axially spaced from each other and contained between said turbine and said compressor, means for securing said inner races against axial movement to said shaft, means contained between said bearing assemblies for urging the outer races of said bearing assemblies axially away from each other, wherein said bearing carrier includes a radially inwardly extending flange and wherein said urging means comprises: a first annular spacer positioned around said shaft and having an outer end in abutment with an inner axial end of the outer race of one bearing assembly, a second annular spacer positioned around said shaft and having an outer end in abutment with an inner axial end of the outer race of the other bearing assembly, said second spacer having an inner axial end in abutment with one axial end of said flange, and means for resiliently urging said first annular spacer and the other axial end of said flange away from each other whereby said resilient urging means automatically positions each said bearing assembly at a predetermined axial position with respect to said flange.
Claim 2
Dependent Claim 264 words
A turbocharger comprising: a main housing having a throughbore, a tubular bearing carrier coaxially positioned within said throughbore, means for securing said bearing carrier to said housing against axial movement, a shaft extending through said bearing carrier, said shaft having a turbine at one end and a compressor at its other end, a pair of bearing assemblies for rotatably mounting said shaft to said bearing carrier, each bearing assembly comprising an inner race, an outer race, and bearing elements entrapped between said races, said bearing assemblies being axially spaced from each other and contained between said turbine and said compressor, means for securing said inner races against axial movement to said shaft, means contained between said bearing assemblies for urging the outer races of said bearing assemblies axially away from each other, wherein said bearing carrier includes a radially inwardly extending flange and wherein said urging means comprises: a first annular spacer positioned around said shaft and having an outer end in abutment with an inner axial end of the outer race of one bearing assembly, a second annular spacer positioned around said shaft and having an outer end in abutment with an inner axial end of the outer race of the other bearing assembly, said second spacer having an inner axial end in abutment with one axial end of said flange, and means for resiliently urging said first annular spacer and the other axial end of said flange away from each other whereby said resilient urging means automatically positions each said bearing assembly at a predetermined axial position with respect to said flange.
Claim 3
Dependent Claim 21 words
The invention as defined in claim 1 wherein said resilient urging means comprises a compression spring in a state of compression.
Claim 4
Dependent Claim 50 words
The invention as defined in claim 1 and comprising a spacer tube positioned around said shaft so that opposite ends of said tube abut against the inner axial ends of said inner races, and means secured to said shaft which abut against the outer axial ends of said inner races.
Claim 5
Dependent Claim 39 words
The invention as defined in claim 3 wherein said last mentioned means comprises a pair of annular slingers, said slingers being secured to said shaft so that each slinger abuts against an outer axial end of each inner race.

References Cited (Backward Citations)

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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1990-03-23 1990-09-22 1991-03-24 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1994-03-23 1994-09-22 1995-03-24 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1998-03-23 1998-09-22 1999-03-24 $7700.00 Window Closed / Lapsed

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