Nicolas Joseph Sirvin

6 Patents

• US121349832024

  Process for Using an Air Input of a Turboreactor Nacelle Comprising an Air Input Lip Which Comprises a Portion Which Can Be Moved to Promote a Thrust Inversion Phase

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US121297952024

  Air Inlet Duct for a Nacelle of an Aircraft Propulsion Assembly

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US119332462024

  Turbojet Engine Comprising a Nacelle with an Air Intake to Promote a Reversed Thrust Phase

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US119133782024

  Assembly for a Turbomachine

  SAFRAN AIRCRAFT ENGINES

  0 cites
• US117396882023

  Turbojet Comprising a Nacelle with an Air Intake for Promoting a Reverse Thrust Phase

  Safran Aircraft Engines

  0 cites
• US116497652023

  Method for Operating an Air Intake of a Turbojet Engine Nacelle During a Thrust Phase and During a Reverse Thrust Phase

  SAFRAN AIRCRAFT ENGINES

  0 cites