Fernando Gea Aguilera

10 Patents

• US125092152025

  Acoustic Attenuation Device for an Aircraft Propulsion Unit

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US123711522025

  Aeronautical Thruster

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US123379862025

  Reduced Bulk Acoustic Treatment Panel for a Turbojet Engine

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US119134052024

  Turbine Engine with a Flow Splitter Having a Profile with Inclined Serrations

  Safran Aircraft Engines

  0 cites
• US118737632024

  Optimised Discharge Line Grid and Optimized Discharge Valve

  UNIVERSITE CLAUDE BERNARD LYON I

  0 cites
• US118595342024

  Profiled Structure and Associated Turbomachine

  Safran Aircraft Engines

  0 cites
• US117325882023

  Profiled Structure for an Aircraft or Turbomachine for an Aircraft

  OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES

  0 cites
• US116681962023

  Profiled Structure for an Aircraft or Turbomachine

  OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES

  0 cites
• US116296642023

  Turbine Engine with a Flow Splitter Having a Profile with Inclined Serrations

  Safran Aircraft Engines

  0 cites
• US115607962023

  Profiled Structure for an Aircraft or Turbomachine for an Aircraft

  OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES

  0 cites