Invention Grant
- Patent Title: Turbine de-swirl elements
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Application No.: US15467933Application Date: 2017-03-23
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Publication No.: US10280832B2Publication Date: 2019-05-07
- Inventor: Martin Babak
- Applicant: Honeywell International Inc.
- Applicant Address: US CA Torrance
- Assignee: GARRETT TRANSPORTATION I INC.
- Current Assignee: GARRETT TRANSPORTATION I INC.
- Current Assignee Address: US CA Torrance
- Agency: The Law Office of John A. Griecci
- Main IPC: F02B33/44
- IPC: F02B33/44 ; F02B37/00 ; F01D9/04 ; F01D5/04

Abstract:
A turbocharger including a turbocharger housing, a rotor and a heat shroud. The turbocharger housing includes a turbine housing affixed to a bearing housing. The rotor includes an axial turbine wheel with a hub, and a shaft extending through the bearing housing. The hub defines a back-disk surface that faces the bearing housing, and the bearing-housing defines an outer surface facing the turbine hub. The turbine housing forms a radial scroll, and the heat shroud forms a curved portion turning that radial scroll direction to an axial direction. The heat shroud establishes a back-disk cavity between a bearing-housing turbine-end-wall outer surface, the turbine-wheel back-disk surface, the curved portion of the heat shroud, and a cylindrical outer surface of a turbine-end portion of the shaft. The heat shroud includes flat ribs within the back-disk cavity to impede the circumferential flow of exhaust gas within the back-disk cavity.
Public/Granted literature
- US20180274435A1 TURBINE DE-SWIRL ELEMENTS Public/Granted day:2018-09-27
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