Patents/Assignees

Airbus Operations SAS

314 patents in portfolio

US12441454utility2025
Heat Shield Provided with Protective Layers, in Particular for a Part of an Aircraft
0 cites
US12441482utility2025
Fuel Tank for an Aircraft
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US12428127utility2025
Aircraft Central Wing Box Comprising Beams Pressed Respectively Against Outer Faces of the Top and Bottom Panels of Said Box, Each Provided with at Least One Attachment Passing Through the Top or Bottom Panel
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US12428136utility2025
Device and Method for Generating Flutter on at Least a Part of an Aircraft
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US12428163utility2025
Connecting Assembly for Connecting Two Aircraft Structures, Aircraft Part Comprising Such Assembly, and Aircraft
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US12429014utility2025
Propulsion Assembly Comprising a Fuel Conditioning System Positioned Behind a Debris Ejection Zone, Aircraft Comprising at Least One Such Propulsion Assembly
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US12429512utility2025
Method for Detecting a Malfunction Suffered by an Integrated Drive Generator, in an Aircraft
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US12429885utility2025
Method for Adjusting Aircraft Controls
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US12432885utility2025
Enhanced Avionics Rack Module
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US12420944utility2025
Module for a Dihydrogen Supply System for an Aircraft Engine
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US12424114utility2025
Method and Apparatus for Operating an Aircraft Having Two Engines
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US12412978utility2025
Method for Manufacturing an Aircraft Radome by Assembling Small-sized Pieces of Skin, Aircraft Radome and Aircraft
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US12404001utility2025
Method for Managing the Configuration of an Aircraft Alternately Comprising Tail Cones Incorporating or Not at Least One Auxiliary Power Unit or Not, Aircraft and Device Making It Possible to Implement Said Method
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US12404032utility2025
Aircraft Comprising at Least One Engine Attachment System That Has Reduced Vertical Bulk
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US12404035utility2025
Aircraft Comprising a Dihydrogen Transport Line, a Channel for Embedding Said Transport Line and a System for Evacuating Air and Water Present in Said Embedded Channel
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US12404820utility2025
Aircraft Nacelle Equipped with at Least One Thrust Reversal Device Comprising at Least One Longitudinal Deflector Configured to House a Longitudinal Actuator
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US12397520utility2025
Honeycomb Structure Having Improved Thermal Conductivity
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US12397899utility2025
Assembly for an Aircraft Comprising a Wing and an Engine Pylon for Coupling a Propulsion System to Said Wing
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US12397919utility2025
Assembly for Fixing Beams, Including a Support Plate and Two Fixings on Respective Opposite Sides of the Support Plate
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US12397920utility2025
Device for Coupling a Propulsion System to an Engine Pylon of an Aircraft, and Corresponding Aircraft
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