Patent · US Active

Hybrid propulsive engine including at least one independently rotatable compressor stator

US8549833B2 · kind B2 · utility

68Cited by
27References
46Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 30, 2009
Grant dateOct 8, 2013
Priority date
Expiry dateJun 23, 2032

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T70/50
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A hybrid propulsive technique, comprising providing a flow of a working fluid through at least a portion of an at least one jet engine. The hybrid propulsive technique comprises extracting energy from the working fluid that is at least partially converted into electrical power, and converting at least a portion of the electrical power to a torque. The hybrid propulsive technique also comprises rotating an at least one independently rotatable compressor stator at least partially responsive to the converting the at least a portion of the electrical power to the torque.

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