Philippe Gérard Chanez

5 Patents

• US124804522025

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

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US123443762025

  Nacelle Air Intake for an Aircraft Propulsion Assembly to Promote a Thrust Reversal Phase

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US119133782024

  Assembly for a Turbomachine

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US119134042024

  Nacelle Air Outlet for Aircraft Turbojet Engine Comprising a Straightening Device for Facilitating a Reverse Thrust Phase

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US117727792023

  Propulsion Unit with Improved Boundary Layer Ingestion

  SAFRAN AIRCRAFT ENGINES

  0 cites