Patents Assigned to SONIC BLUE AEROSPACE
  • Publication number: 20080175703
    Abstract: An electric turbine compressor fan for hybrid propulsion wherein the compressor contains one or more rotor stages (compressor and diffuser), each being driven by one or more electric ring motors, such that the compressor rotor stages are designed and tuned more precisely to the compression ratio to be attained within the turbine design operating characeristics, thrust requirements and flight envelope.
    Type: Application
    Filed: July 25, 2007
    Publication date: July 24, 2008
    Applicant: SONIC BLUE AEROSPACE
    Inventor: Richard H. Lugg