Wolfgang Brochard

7 Patents

• US124866982025

  Locking Mechanism for at Least One Movable Element Situated in a First Zone and Comprising a Component That Can Be Adjusted from a Second Zone, and Aircraft Comprising at Least One Such Locking Mechanism

  Airbus Operations SAS

  0 cites
• US123379822025

  Aircraft Air Inlet Comprising at Least Two Walls Connected End to End by Welding, Method for the Assembly of Such an Air Inlet, and Aircraft Comprising at Least One Such Air Inlet

  AIRBUS OPERATIONS SAS

  0 cites
• US121045572024

  Output Cone of an Aircraft Propulsive Assembly Forming an Acoustic Treatment System with at Least Two Degrees of Freedom

  Airbus Operations (S.A.S.)

  0 cites
• US120539152024

  Method for Manufacturing a Door of a Thrust Reversal System

  Airbus Operations SAS

  0 cites
• US119814462024

  Assembly for a Nacelle of an Aircraft Engine, Said Assembly Comprising a Fixed Cowl and a Cowl Mounted So as to Be Able to Move on the Fixed Cowl

  Airbus Operations SAS

  0 cites
• US117467052023

  Method for Manufacturing an Acoustic Element of a Sound Absorption Structure from at Least One Sheet of Material

  Airbus Operations S.A.S.

  0 cites
• US116798892023

  Nacelle of an Aircraft Propulsion Assembly Comprising a Plurality of Damper Elements Between a Front Section and a Main Section, and Associated Aircraft Propulsion Assembly

  Airbus Operations S.A.S.

  0 cites