Rémi Lansiaux

6 Patents

• US125653212026

  Front Engine Attachment System Intended for an Aircraft Engine and Having a Compact Structure

  AIRBUS OPERATIONS SAS

  0 cites
• US125399742026

  Front Engine Attachment System for an Aircraft Engine, Which Has a Compact Structure

  AIRBUS OPERATIONS SAS

  0 cites
• US124040322025

  Aircraft Comprising at Least One Engine Attachment System That Has Reduced Vertical Bulk

  Airbus Operations SAS

  0 cites
• US119758562024

  Front Engine Attachment System for an Aircraft Engine, Comprising a More a Lightweight Structure

  AIRBUS OPERATIONS SAS

  0 cites
• US116798862023

  Device for Connecting an Aircraft Engine and a Primary Structure of an Aircraft Pylon Comprising a Rudder and a System for Limiting the Displacement of the Rudder Incorporating a Double Stop, Aircraft Comprising Such a Device

  Airbus Operations SAS

  0 cites
• US115721842023

  Front Engine Attachment System for an Aircraft Engine, Having Rod Systems with Two Rods

  Airbus Operations SAS

  0 cites