Michel Slusarz

5 Patents

• US121580842024

  Wall Provided with a Cooling Hole Having a Diffusion Portion with a Triangular Section

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US121464202024

  Aircraft Turbomachine Blade and Method for Manufacturing Same Using Lost-wax Casting

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US120919892024

  Turbomachine Blade with Improved Cooling

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US119133542024

  Turbomachine Moving Blade with Cooling Circuit Having a Double Row of Discharge Slots

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US117191022023

  Blade Provided with a Cooling Circuit

  SAFRAN AIRCRAFT ENGINES

  0 cites