Invention Grant
- Patent Title: Turbocharger shroud with cross-wise grooves and turbocharger incorporating the same
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Application No.: US14395281Application Date: 2013-04-11
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Publication No.: US09683442B2Publication Date: 2017-06-20
- Inventor: Stephanie Dextraze , David G. Grabowska
- Applicant: BorgWarner Inc.
- Applicant Address: US MI Auburn Hills
- Assignee: BorgWarner Inc.
- Current Assignee: BorgWarner Inc.
- Current Assignee Address: US MI Auburn Hills
- Agency: Perkins Coie LLP
- International Application: PCT/US2013/036089 WO 20130411
- International Announcement: WO2013/162896 WO 20131031
- Main IPC: F04D25/04
- IPC: F04D25/04 ; F01D5/14 ; F01D5/20 ; F01D11/02 ; F04D29/16 ; F04D29/42 ; F04D29/68 ; F01D5/04 ; F04D17/10 ; F04D29/28 ; F04D29/52

Abstract:
A turbocharger (5) comprising a housing (10) including a compressor shroud (14) and a turbine shroud (12). A compressor wheel (18) is disposed in the compressor shroud (14) and includes a plurality of compressor blades (45, 46). Each compressor blade (45, 46) includes a leading edge (50, 51) and a compressor shroud contour edge (54, 55), wherein each compressor shroud contour edge (54, 55) is in close confronting relation to the compressor shroud (14). A turbine wheel (16) is disposed in the turbine shroud (12) and includes a plurality of turbine blades (26). Each turbine blade (26) includes a leading edge (30) and a turbine shroud contour edge (34), wherein each turbine shroud contour edge (34) is in close confronting relation to the turbine shroud (12). At least one of the compressor shroud (14) and turbine shroud (12) includes a plurality of grooves (70, 72) extending cross-wise with respect to the corresponding compressor or turbine shroud contour edges (34, 54, 55).
Public/Granted literature
- US20150118079A1 TURBOCHARGER SHROUD WITH CROSS-WISE GROOVES AND TURBOCHARGER INCORPORATING THE SAME Public/Granted day:2015-04-30
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