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US3969804A Expired / Lapsed US ⏱️ 0.0 years remaining

Bearing housing assembly method for high speed rotating shafts

Assignee: Roto Master Inc
•
Filing: 1975-04-14
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Granted: 1976-07-20
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Expires: 1995-04-14
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Abstract

Abstract A bearing housing for high speed rotating shafts wherein the bearing housing is constructed in two parts with the bearing being of the semi-floating type. One part of the bearing housing presses against the bearing to resist any axial thrust that may be exerted on the bearing during high speed operation. The bearing is floating on a lubricant around its outer diameter in the other portion of the two part bearing housing. With the bearing being stationary in the housing, the only critical surface becomes the internal surface between the bearing and the shaft itself. By varying the position of the two parts of the bearing housing, the passage for the lubricant to enter the bearing housing can be located at a near vertical position while permitting desired orientation of the end of the bearing housing.

Inventors

  • 👤 Hugh MacInnes
  • 👤 Paul M. Uitti

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 09:22
CPC Classifications
F; F01; F01D; F01D25/00; F01D25/24; F01D25/16; F01D25/166; F16; F16C; F16C17/00; F16C17/10; F16C33/00; F16C33/02; F16C33/04; F16C33/06; F16C33/10; F16C2360/00; F16C2360/23; F16C2360/24; Y; Y02; Y02T; Y02T50/00; Y02T50/60; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49229; Y10T29/49236; Y10T29/49245; Y10T29/49826; Y10T29/49904

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 262 words
A method of assembling a turbocharger for use on any given design of internal combustion engine, said turbocharger having a two part bearing housing for enclosing a semi-floating axial thrust type bearing, a first part of said bearing housing having a hole for receiving said bearing and a shaft therein, said first part having passages therethrough substantially perpendicular to said hole for allowing gravity flow of lubricant to said bearing and shaft, a second part of said two part bearing housing also having a hole to receive said bearing and said shaft and having a surface for counteracting axial thrust of said bearing, said method consisting of; a. positioning an exhaust turbine portion of said turbocharger in proper relationship for connection to an exhaust system of said engine; b. rotating said first part of said bearing housing in relation to said exhaust turbine portion to provide essentially vertical alignment of said lubricant passages for gravity flow of lubricant therethrough; c. positioning a compressor portion of said turbocharger in proper relationship for connection to the fuel intake of said engine; d. rotating said second part of said bearing housing for proper alignment with said compressor portion; e. rotationally adjusting said first part of said bearing housing for alignment with said second part of said bearing housing while maintaining gravity flow of lubricant through said lubricant passages; f. connecting said first part of said bearing housing to said second part of said bearing housing; g. connecting said first part to said exhaust turbine portion; and h. connecting said second part to said compressor portion.
Claim 2
Independent Claim 262 words
A method of assembling a turbocharger for use on any given design of internal combustion engine, said turbocharger having a two part bearing housing for enclosing a semi-floating axial thrust type bearing, a first part of said bearing housing having a hole for receiving said bearing and a shaft therein, said first part having passages therethrough substantially perpendicular to said hole for allowing gravity flow of lubricant to said bearing and shaft, a second part of said two part bearing housing also having a hole to receive said bearing and said shaft and having a surface for counteracting axial thrust of said bearing, said method consisting of; a. positioning an exhaust turbine portion of said turbocharger in proper relationship for connection to an exhaust system of said engine; b. rotating said first part of said bearing housing in relation to said exhaust turbine portion to provide essentially vertical alignment of said lubricant passages for gravity flow of lubricant therethrough; c. positioning a compressor portion of said turbocharger in proper relationship for connection to the fuel intake of said engine; d. rotating said second part of said bearing housing for proper alignment with said compressor portion; e. rotationally adjusting said first part of said bearing housing for alignment with said second part of said bearing housing while maintaining gravity flow of lubricant through said lubricant passages; f. connecting said first part of said bearing housing to said second part of said bearing housing; g. connecting said first part to said exhaust turbine portion; and h. connecting said second part to said compressor portion.
Claim 3
Dependent Claim 62 words
The method of assembling a turbocharger as recited in claim 1 includes after the step of positioning of said exhaust turbine position the additional step of mounting said exhaust turbine portion in said exhaust system, and after the step of connecting said second part to said compressor portion the additional step of mounting said compressor portion in said intake of said engine.
Claim 4
Dependent Claim 30 words
The method of assembling as recited in claim 2 includes after the last aforementioned step the additional step of connecting said lubricant passages to a lubricating system of said engine.
Claim 5
Dependent Claim 34 words
The method of assembling a turbocharger as recited in claim 1 includes after the positioning of said exhaust turbine portion the additional step of loosely connecting said first part to said exhaust turbine portion.

References Cited (Backward Citations)

US1717817A Cited
US2646210A Cited
US3058787A Cited
US3056634A Cited
US3043636A Cited
US3176620A Cited
US3411706A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-07-20 1980-01-19 1980-07-20 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-07-20 1984-01-19 1984-07-20 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-07-20 1988-01-19 1988-07-20 $7700.00 Window Closed / Lapsed

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