Eva Julie Lebeault

10 Patents

• US125704042026

  Propulsion Assembly for an Aircraft Comprising a Stator Vane Integrated Into an Upstream Part of a Mounting Pylon of Reduced Height

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US124804522025

  Aircraft Dual-flow Turbine Engine Assembly, the Assembly Being Equipped with Incidence-controlled Air Discharge Fins

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US123711522025

  Aeronautical Thruster

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US122919782025

  Bypass Turbomachine for an Aircraft

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US122156072025

  Unducted Turbine Engine Comprising Stator Blades Having Different Chords

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US121349832024

  Process for Using an Air Input of a Turboreactor Nacelle Comprising an Air Input Lip Which Comprises a Portion Which Can Be Moved to Promote a Thrust Inversion Phase

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US121108422024

  Air Outlet for a Nacelle for an Aircraft Bypass Turbojet Engine Comprising a Guiding Device to Favor a Reverse Thrust Phase

  SAFRAN AIRCRAFT ENGINES

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• US119332462024

  Turbojet Engine Comprising a Nacelle with an Air Intake to Promote a Reversed Thrust Phase

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US119058462024

  Turbomachine Polyspherical Hub for Variable Pitch Blades

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US116618602023

  Compressor Module for Turbomachine

  SAFRAN AIRCRAFT ENGINES

  0 cites