Patent · US Active

Compressor for an internal combustion engine

US8307648B2 · kind B2 · utility

4Cited by
1References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 15, 2008
Grant dateNov 13, 2012
Priority date
Expiry dateApr 20, 2031

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2270/101
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

In a compressor of a turbocharger of an internal combustion engine comprising a housing with an inflow channel; a compressor impeller arranged in the inflow channel; and a bypass channel which has a first flow opening upstream of the compressor impeller inlet, a second flow opening downstream of the compressor impeller inlet and an axial annular chamber which connects the first and the second flow openings. An axial vane structure is provided in the axial annular chamber of the bypass channel, which imparts a swirl direction corresponding to that of the air mass flow in the inflow channel to the air mass flowing through the bypass channel from the second to the first flow opening.

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