Patent · US Active

Exhaust gas turbocharger for a reciprocating internal combustion engine and corresponding reciprocating internal combustion engine

US7513114B2 · kind B2 · utility

6Cited by
3References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 22, 2006
Grant dateApr 7, 2009
Priority date
Expiry dateMay 11, 2027

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T10/12
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

In an exhaust gas turbocharger for a reciprocating internal combustion engine comprising an exhaust gas turbine in the exhaust line and a compressor in the inlet line of the engine, the exhaust gas turbine has two exhaust gas flow passages, by way of which exhaust gas is fed to the turbine rotor, the ratio of the turbine rotor diameter to the compressor wheel diameter being set by a function, which is dependent on the displacement volume of the internal combustion engine.

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