Patents/Assignees

Airbus Operations SAS

314 patents in portfolio

US12111004utility2024
Bulkhead Fitting Device Enabling Slight Relative Movements and the Absorption of Forces Between a Conduit and a Wall, and Installation Including at Least One Such Bulkhead Fitting Device
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US12103139utility2024
Vacuum Tool Including at Least One Improved Sealing Gasket
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US12106744utility2024
Method for Manufacturing an Acoustic Absorption Structure, and Acoustic Absorption Structure Obtained in This Way
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US12104554utility2024
Aircraft Propulsion Assembly Equipped with a Thrust-reversing Device Comprising at Least One Inflatable Barrier, and Aircraft Comprising at Least One Such Propulsion Assembly
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US12097967utility2024
Fastening System for an Aircraft Configured to Fasten at Least One Tank Intended to Contain Liquid Hydrogen
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US12083778utility2024
Soundproofing Coating Comprising a Cellular Structure
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US12077274utility2024
Aircraft Comprising at Least One Systems Cabinet Connected to a Landing Gear Compartment by at Least One Sliding Connection Sliding in a Longitudinal Direction
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US12077275utility2024
Aircraft Comprising at Least One System Rack Connected to a Floor Rail by at Least One Connecting System
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US12077312utility2024
Aircraft Having a Dihydrogen Transport Pipe and an Embedding Channel for Said Transport Pipe
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US12078293utility2024
Tank Comprising Inner and Outer Chambers and at Least One Link System with Flexible Radial Blades Linking Said Chambers
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US12078428utility2024
Heat Exchanger Limiting the Risk of Contamination Between Two Fluids and Aircraft Comprising at Least One Such Heat Exchanger
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US12065239utility2024
Aircraft Comprising a Fuselage and Wings Each Having an Outer Part and a Widened Inner Part Between the Fuselage and the Outer Part
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US12065260utility2024
Aircraft Comprising at Least One Hydrogen Supply Device and at Least One Sealed Container, in Which at Least One Item of Equipment of Said Hydrogen Supply Device Is Positioned
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US12060851utility2024
Bypass Turbofan Including a System for Blocking the Secondary Flow Including Veils
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US12060965utility2024
Optimized Connection Assembly Between Two Portions of a Supply Line for a Cryogenic Fluid, Including an Additional Thermal Insulation Chamber and a Fluid Expansion Chamber
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US12053915utility2024
Method for Manufacturing a Door of a Thrust Reversal System
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US12054271utility2024
Method for Assembling an Aircraft Pylon and Aircraft Pylon Obtained by This Method
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US12054272utility2024
Assembly of a Pylon with an Engine of an Aircraft
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US12054273utility2024
Aircraft Comprising an Engine Pylon with a Movable Cover Assembly and a Specific Locking System
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US12054275utility2024
Resistive Skin Shell Incorporating Perforated Metal Bands, and Acoustic Inner Wall of an Aircraft Air Intake Formed from Such Resistive Skin Shells
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