Jean Charles Marie Coussirou

2 Patents

• US123720042025

  Turbine Blade for an Aircraft Turbomachine, Provided with a Channel for Ejecting a Primary Flow Towards an Inter-lip Cavity

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US120185822024

  Turbine Blade for an Aircraft Turbine Engine, Comprising a Platform Provided with a Channel for Primary Flow Rejection Towards a Purge Cavity

  SAFRAN AIRCRAFT ENGINES

  0 cites