Patent · US Active

Compressor, exhaust gas turbocharger and internal combustion machine

US10655642B2 · kind B2 · utility

1Cited by
2References
22Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 22, 2017
Grant dateMay 19, 2020
Priority date
Expiry dateNov 27, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2260/96
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A compressor for an internal combustion machine includes a compressor impeller rotatably mounted in a compressor casing. A circumferential step is integrated into a wall which delimits an intake section disposed upstream of the compressor impeller in an operating flow direction of a gas to be compressed. The circumferential step is a mouth-free circumferential step which faces the compressor impeller and delimits a flow cross section. A ratio of a shortest distance between the compressor impeller and the circumferential step to a largest cross-sectional dimension in the flow cross section delimited by the circumferential step is at least 0.5. An exhaust gas turbocharger and an internal combustion machine are also provided.

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