Laurent Soulat

8 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
• US125099952025

  Turbomachine Subassembly Comprising a Gooseneck of Improved Configuration, and Turbomachine Comprising Such a Subassembly

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US123203052025

  Aircraft Turbomachine

  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

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• US120780822024

  Non-axisymmetric Secondary Duct Portion

  SAFRAN AIRCRAFT ENGINES

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• US119058462024

  Turbomachine Polyspherical Hub for Variable Pitch Blades

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US116618602023

  Compressor Module for Turbomachine

  SAFRAN AIRCRAFT ENGINES

  0 cites