Invention Grant
- Patent Title: Variable nozzle turbocharger
- Patent Title (中): 可变喷嘴涡轮增压器
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Application No.: US11667799Application Date: 2004-11-16
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Publication No.: US08109715B2Publication Date: 2012-02-07
- Inventor: Philippe Renaud , Denis Tisserant
- Applicant: Philippe Renaud , Denis Tisserant
- Applicant Address: US NJ Morristown
- Assignee: Honeywell International, Inc.
- Current Assignee: Honeywell International, Inc.
- Current Assignee Address: US NJ Morristown
- International Application: PCT/EP2004/012992 WO 20041116
- International Announcement: WO2006/053579 WO 20060526
- Main IPC: F01D9/02
- IPC: F01D9/02

Abstract:
There is provided a turbocharger with a variable nozzle assembly having a plurality of cambered vanes positioned annularly around a turbine wheel, each vane (20) being pivotable around a pivot point (Pp) and being configured to have a leading edge (Ple) and a trailing edge (Pte) connected by an outer airfoil surface (2) and an inner airfoil surface (4), said outer airfoil surface (2) being substantially convex and said inner airfoil surface (4) having a convex section at the leading edge (Ple) which has a local extreme (Pex) of curvature and transitions into a concave section towards the trailing edge (Pte). The positions of the pivot point (Pp) and the local extreme (Pex) are set such that, even when the vanes are placed in a closed position, the exhaust gas stream exercises a positive torque on the vanes which tends to open the nozzle.
Public/Granted literature
- US20080131267A1 Variable Nozzle Turbocharger Public/Granted day:2008-06-05
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