Patent · US Active

Rotary screw compressor rotor having work extraction mechanism

US11359632B2 · kind B2 · utility

0Cited by
8References
8Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 31, 2014
Grant dateJun 14, 2022
Priority date
Expiry dateSep 29, 2037

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF04C29/0014
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas compressor is disclosed that includes a first rotor having a first rotor body, the first rotor body including a plurality of helical lobes, an infernal volume within the first rotor body defined by a wall, and a turbine disposed within the internal volume, the turbine including a turbine body and a plurality of airfoils extending substantially radially from the turbine body to the wall, where the internal volume is structured to enable a cooling fluid to flow therethrough. The gas compressor further includes a second rotor body including a plurality of helical flutes, an inlet manifold and an outlet manifold, both disposed within the second rotor body, and a body channel within at least one flute extending from and in fluid communication with the inlet manifold to the outlet manifold, where the body channel is structured to enable a cooling fluid to flow therethrough.

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