The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
May. 07, 2024

Filed:

Aug. 18, 2022
Applicant:

Borgwarner Inc., Auburn Hills, MI (US);

Inventors:

Kai Tanaka, Mills River, NC (US);

Tim Weiland, Kirchheimbolanden, DE;

Assignee:

BorgWarner Inc., Auburn Hills, MI (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/02 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F01D 9/026 (2013.01); F01D 25/24 (2013.01); F05D 2220/40 (2013.01); F05D 2240/127 (2013.01); F05D 2250/15 (2013.01); F05D 2260/941 (2013.01);
Abstract

High cycle fatigue (HCF) in a turbine wheel of a sector-divided dual volute turbocharger, particularly a turbocharger where the tongue-to-blade gap is as small as from 1-3% of the wheel diameter, is reduced, by locally increasing the volute cross-sectional area just upstream of the tongues. Thereby, it becomes possible to reduce the force function of the exhaust gas pressure onto the turbine wheel blades. Modifying how the pressure presents itself to the wheel reduces blade excitation and, ultimately, HCF of turbine wheels. In another aspect of the invention, the angle of the tongues are modified to direct the exhaust more directly onto the turbine wheel than conventional tongues. It is surprising that this approach not only accomplishes the desired result, but does this without significant loss of turbine stage efficiency.


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