Patent · US Active

Inlet swirl control for turbochargers

US8579585B2 · kind B2 · utility

2Cited by
5References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 14, 2012
Grant dateNov 12, 2013
Priority date
Expiry dateMay 14, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T137/2087
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

An inlet duct, an induction system, and a system are disclosed for directing an inlet flow into an inlet compressor for use in an internal combustion engine. An example inlet duct may include one or more relief features disposed on an inner surface of the inlet duct. The one or more relief features may be made integral with the inlet duct. The one or more relief features may be disposed to protrude into the inlet flow to cause the inlet flow to swirl before reaching the inlet compressor.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.