Invention Grant
- Patent Title: Turbine shroud contour exducer relief
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Application No.: US14109883Application Date: 2013-12-17
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Publication No.: US09863275B2Publication Date: 2018-01-09
- Inventor: Brian D. Alexander
- Applicant: HONEYWELL INTERNATIONAL INC.
- Applicant Address: US NJ Morris Plains
- Assignee: Honeywell International, Inc.
- Current Assignee: Honeywell International, Inc.
- Current Assignee Address: US NJ Morris Plains
- Agency: The Law Office of John A. Griecci
- Main IPC: F01D25/24
- IPC: F01D25/24 ; F01D5/04 ; F01D9/04
Abstract:
A turbocharger turbine having a blade-gap zone between the blades and the shroud wall. The blade-gap zone is larger at and near the exducer than at an upstream location where the shroud wall is at its minimum radius. Also disclosed is a method of customizing and manufacturing a turbine by establishing an optimized blade-gap zone at the exducer, and machining it into a turbine housing.
Public/Granted literature
- US20150167496A1 TURBINE SHROUD CONTOUR EXDUCER RELIEF Public/Granted day:2015-06-18
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