Patents/Assignees

Airbus Operations SAS

314 patents in portfolio

US12565321utility2026
Front Engine Attachment System Intended for an Aircraft Engine and Having a Compact Structure
0 cites
US12565322utility2026
Propulsion System for an Aircraft Comprising a Turbojet, a Pylon and Engine Attachment
0 cites
US12565326utility2026
Air Intake Lip of an Aircraft Engine Nacelle Provided with a Passive Shut-off Device for an Exhaust Device
0 cites
US12567551utility2026
Electrical Protection Device of Circuit-breaker Type Which Can Be Positioned on a Continuous Electrical Cable
0 cites
US12559244utility2026
Aircraft Propulsion Assembly Having a Jet Engine, a Pylon and Means for Attaching the Jet Engine to the Pylon
0 cites
US12560281utility2026
Reservoir Tank Comprising a Shell and at Least One End Wall That Are Joined Together So as to Limit the Deformations of Said End Wall
0 cites
US12546257utility2026
System for Recovering Gaseous Dihydrogen Produced in a Liquid Dihydrogen Distribution Duct of an Aircraft
0 cites
US12539974utility2026
Front Engine Attachment System for an Aircraft Engine, Which Has a Compact Structure
0 cites
US12540772utility2026
System for Generating an Inert Gas for an Aircraft Using Liquid Hydrogen
0 cites
US12535038utility2026
Powerplant for an Aircraft
0 cites
US12535042utility2026
Aircraft Nacelle Equipped with at Least One Thrust Reversal Device Comprising at Least One Longitudinal Deflector, Aircraft Comprising at Least One Propulsion Unit Having Such a Nacelle
0 cites
US12534180utility2026
Device for Sealing a Joint Between a Wing Box and a Central Fuselage of an Aircraft, Corresponding Sealing Processes and Corresponding Aircraft
0 cites
US12534213utility2026
Propulsion Assembly for an Aircraft, Having an Extraction Fan
0 cites
US12534215utility2026
Propulsion Unit Comprising at Least One Electric Motor and a Coupling System Positioned on Either Side of a Transmission System
0 cites
US12535032utility2026
Aircraft Nacelle Comprising a Sealed Box Structure and a Door Which Opens the Box Structure to the Outside
0 cites
US12535187utility2026
Double-skin Cryogenic Tank Equipped with at Least One Inspection Device
0 cites
US12536915utility2026
Method and System for Assisting the Avoidance of an Excursion by an Aircraft from a Runway or Taxiway of an Aerodrome
0 cites
US12529681utility2026
Probe for Checking the Presence of Paramagnetic Particles in a Tank
0 cites
US12509209utility2025
Assembly for Reinforcing the Fuselage of an Aircraft When Removing a Removable Panel
0 cites
US12509235utility2025
Electric Propulsion Assembly Comprising at Least One Electric Motor Positioned in Front of a Transmission System, Aircraft Comprising at Least One Such Propulsion Assembly
0 cites

← PreviousPage 2 of 16Next →