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US4654941A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of assembling a variable nozzle turbocharger

Assignee: Garrett Corp
•
Filing: 1985-12-13
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Granted: 1987-04-07
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Expires: 2005-12-13
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Abstract

Abstract A turbocharger having a variable nozzle vane assembly to be used in association with an engine. A nozzle ring having a plurality of rotatable vanes mounted thereto defining an annular passageway within the turbine housing through which exhaust gas passes upstream of a turbine. Included is a means for rotating the plurality of vanes and a means for preventing binding of the components during thermal cycling.

Inventors

  • 👤 Fred E. Burdette
  • 👤 Jean-Luc Fleury
  • 👤 Manfred Roessler

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 10:48
CPC Classifications
F; F02; F02B; F02B37/00; F02B37/12; F02B37/24; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/16; F01D17/165; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49316; Y10T29/4932; Y10T29/49323

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 166 words
In a turbocharger having an exhaust gas driven turbine rotatably mounted to a shaft having a compressor impeller thereon, a compressor housing enclosing said compressor impeller, a center housing including bearing means for rotatably supporting the shaft, and a turbine housing enclosing said turbine and forming a volute therein, a method of assembling the turbocharger with a spring loaded nozzle ring comprising the steps of: mounting a flange member having a central opening to said center housing; pivotably mounting a plurality of vanes to said nozzle ring; sliding a tube member having a tab at each end within said central opening; indexing one of said tabs within a slot in said flange member; sliding said nozzle ring onto the tube member; indexing the other tab within a slot in said nozzle ring; simultaneously mounting said turbine housing to said flange member and biasing said nozzle ring toward said turbine housing such that said plurality of vanes are spring loaded against a portion of said turbine housing.
Claim 2
Dependent Claim 166 words
In a turbocharger having an exhaust gas driven turbine rotatably mounted to a shaft having a compressor impeller thereon, a compressor housing enclosing said compressor impeller, a center housing including bearing means for rotatably supporting the shaft, and a turbine housing enclosing said turbine and forming a volute therein, a method of assembling the turbocharger with a spring loaded nozzle ring comprising the steps of: mounting a flange member having a central opening to said center housing; pivotably mounting a plurality of vanes to said nozzle ring; sliding a tube member having a tab at each end within said central opening; indexing one of said tabs within a slot in said flange member; sliding said nozzle ring onto the tube member; indexing the other tab within a slot in said nozzle ring; simultaneously mounting said turbine housing to said flange member and biasing said nozzle ring toward said turbine housing such that said plurality of vanes are spring loaded against a portion of said turbine housing.
Claim 3
Dependent Claim 26 words
The method according to claim 1 further including the step of mounting spacer pins to said nozzle ring between said turbine housing and said nozzle ring.
Claim 4
Dependent Claim 32 words
The method according to claim 2 further including the steps of forming a spacer tip extension integral with the spacer and inserting the tip extension within a bore in said turbine housing.
Claim 5
Dependent Claim 33 words
The method according to claim 2 further including the steps of forming an extension integral with the spacer and inserting the extension through said nozzle ring into a slot in said flange member.

References Cited (Backward Citations)

US2976013A Cited
GB861630A Cited
GB880903A Cited
US3033519A Cited
SU715812A1 Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1990-04-06 1990-10-06 1991-04-07 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1994-04-06 1994-10-06 1995-04-07 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1998-04-06 1998-10-06 1999-04-07 $7700.00 Window Closed / Lapsed

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