13 Patents
- US121349822024Strip-form Acoustic Material Having an Integrated Flange, and Internal Wall of an Aircraft Air Intake Made with This Material
AIRBUS OPERATIONS SAS
0 cites - US120542752024Resistive Skin Shell Incorporating Perforated Metal Bands, and Acoustic Inner Wall of an Aircraft Air Intake Formed from Such Resistive Skin Shells
AIRBUS OPERATIONS SAS
0 cites - US120306592024Anterior Part of a Nacelle for an Aircraft Propulsion Assembly, Whose Front Frame Is Connected to an Outer Wall Without Penetrating It
Airbus Operations SAS
0 cites - US120238792024Method for Manufacturing Deicing Acoustic Skin for an Aircraft Acoustic Panel, Using a Fiber Spacing Device
AIRBUS OPERATIONS SAS
0 cites - US119521362024Method for Manufacturing an Acoustic Panel Having a Capsular Skin, and Acoustic Panel Incorporating Such a Skin
Airbus Operations SAS
0 cites - US119455962024Method for Producing an Alveolar Soundproofing Structure Including a Diaphragm, and Alveolar Soundproofing Structure Obtained
Airbus Operations SAS
0 cites - US117458872023Multifrequency Absorption Acoustic Panel for an Aircraft Nacelle
Airbus Operations (S.A.S.)
0 cites - US117313812023Method for Manufacturing Two Soundproof Panels in the Same Mold Using Two Mold Cavities
AIRBUS OPERATIONS SAS
0 cites - US116855072023Sound-absorbing Panel with a Cellular Core and a De-icing System
Airbus Operations S.A.S.
0 cites - US116550452023Anterior Part of the Nacelle of an Aircraft Propulsion Assembly Whose Air Intake Lip Is Linked to the Outer Panel by Nesting
AIRBUS OPERATIONS SAS
0 cites - US116490622023Forward Part of an Aircraft Propulsion Unit Nacelle Comprising a Main Propagation Path for Forces Between an Air Intake Lip and a Back Skin of an Acoustic Panel
AIRBUS OPERATIONS SAS
0 cites - US116490632023Acoustic Panel for an Aircraft Nacelle Air Inlet with Castellated Resistive Skin, Propulsion Unit and Aircraft Fitted with Such Acoustic Panels
AIRBUS OPERATIONS SAS
0 cites