Invention Grant
US08763393B2 Sealing arrangement between a variable-nozzle assembly and a turbine housing of a turbocharger
有权
可变喷嘴组件与涡轮增压器的涡轮壳体之间的密封布置
- Patent Title: Sealing arrangement between a variable-nozzle assembly and a turbine housing of a turbocharger
- Patent Title (中): 可变喷嘴组件与涡轮增压器的涡轮壳体之间的密封布置
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Application No.: US13205330Application Date: 2011-08-08
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Publication No.: US08763393B2Publication Date: 2014-07-01
- Inventor: Emmanuel Severin , Pierre Barthelet , Lionel Toussaint , Olivier Millotte
- Applicant: Emmanuel Severin , Pierre Barthelet , Lionel Toussaint , Olivier Millotte
- Applicant Address: US NJ Morristown
- Assignee: Honeywell International Inc.
- Current Assignee: Honeywell International Inc.
- Current Assignee Address: US NJ Morristown
- Agency: Alston & Bird LLP
- Main IPC: F02B33/44
- IPC: F02B33/44 ; F02B37/24 ; F02C6/12 ; F01D17/16 ; F02B37/22 ; F02D41/00 ; F01D9/04 ; B23P15/00

Abstract:
A turbocharger includes a variable-nozzle assembly that includes an insert having a tubular portion received into a stepped bore of a turbine housing and having a nozzle portion extending radially out from one end of the tubular portion, and a generally annular nozzle ring axially spaced from the nozzle portion and an array of vanes rotatably mounted to the nozzle ring. Sealing of the interface between the tubular portion of the insert and the turbine housing is provided by a sealing ring formed as a generally annular body having a U- or V-shaped cross-section oriented such that an open side of the U- or V-shaped cross-section faces in a radial direction. The U- or V-shaped cross-section defines two opposing legs, one of the legs being engaged against an end face of the tubular portion of the insert and the other leg being engaged against an upstream-facing step surface of the turbine housing bore.
Public/Granted literature
- US20130036733A1 Sealing Arrangement Between a Variable-Nozzle Assembly and a Turbine Housing of a Turbocharger Public/Granted day:2013-02-14
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