AIRBUS SAS

SYSTEM AND METHOD FOR ASSISTING THE LANDING OF AN AIRCRAFT AT AN AIRPORT

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METHOD AND SYSTEM FOR ASSISTING IN THE OPERATIONAL DECISION-MAKING OF AN AIRCRAFT

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SUPERCONDUCTING MOTOR COMPRISING A MOTOR HOUSING WITH SEPARATE COMPARTMENTS FOR INSULATING WINDINGS

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STRUCTURAL PANEL WITH CARBON COMPOSITE PLIES

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Method, Computer Program, Computer-Readable Data Carrier And Computing Device For Deterministic Execution Of An Instruction Set As Well As Apparatus Comprising Same

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FILLING LEVEL MONITORING DEVICE FOR MONITORING THE FILLING LEVEL OF A FLUID CONTAINER, HYDROGEN TANK, AND AIRCRAFT COMPRISING SUCH HYDROGEN TANK

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SYSTEM AND METHOD FOR MANAGING AN ENERGY SOURCE IN A HYBRID ELECTRIC PROPULSION ARCHITECTURE

#8 | 2025-10-30

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METHOD AND SYSTEM FOR PROVIDING COOLING TO THE HOLD OF AN AIRCRAFT

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TAPE STRUCTURE FOR USE IN AN AUTOMATED FIBER PLACEMENT (AFP) METHOD, AUTOMATED FIBER PLACEMENT DEVICE AND AUTOMATED FIBER PLACEMENT (AFP) METHOD

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Human necessities

TRANSPORT OF PASSENGERS WITH REDUCED MOBILITY

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AIRCRAFT CARGO DOOR ACTUATION SYSTEM

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AIRCRAFT CARGO DOOR ACTUATION SYSTEM

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PROPULSION ASSEMBLY FOR AN AIRCRAFT

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PROPULSION ASSEMBLY FOR AN AIRCRAFT

#15 | 2025-03-20 ✅ Patent 12,535,038 granted on 2026-01-27

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POWERPLANT FOR AN AIRCRAFT

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AIRCRAFT FUSELAGE

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VENT SYSTEM

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METHOD AND SYSTEM FOR AUTOMATICALLY GUIDING AN AIRCRAFT TO A LANDING RUNWAY

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AIR MOBILITY SYSTEM WITH ENHANCED SITUATIONAL AWARENESS

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ANTENNA ELEMENT AND ANTENNA ARRAY

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PROPULSION SYSTEM FOR AN AIRCRAFT, SAID PROPULSION SYSTEM COMPRISING A REVERSIBLE FUEL CELL

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COOLING ARCHITECTURE FOR A CRYOGENIC AND SUPERCONDUCTING POWERTRAIN USING LIQUID HYDROGEN ON BOARD AND METHOD FOR MANAGING THE COOLING TEMPERATURE OF THE POWERTRAIN COMPONENTS

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Flat RF tiles for multiple band electrical steerable antennas

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MODULE FOR A DIHYDROGEN SUPPLY SYSTEM FOR AN AIRCRAFT ENGINE

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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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GALLEY FOR AIRCRAFT COMPRISING A TROLLEY LOCKING SYSTEM

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AUTONOMOUS AIR CONDITIONING SYSTEM FOR AIRCRAFT

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Method for Optimizing a Modification of an Ad-Hoc-Edge Network with a Resource-Aware Service Allocation Strategy and a System for Executing Such a Method

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CONTROLLER FOR AN ELECTRICAL POWER SUPPLY CIRCUIT OF A SUPERCONDUCTING MOTOR, SUPERCONDUCTING ELECTRICAL POWER SUPPLY SYSTEM FOR A MOTOR, AND AIRCRAFT COMPRISING SUCH A SYSTEM

#30 | 2024-08-22 ✅ Patent 12,292,349 granted on 2025-05-06

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Pressure measuring rake comprising a patched leading edge, in particular for an engine of an aircraft, and more particularly for a bypass turbojet engine

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AIRCRAFT PROPULSION UNIT COMPRISING AT LEAST ONE PRESSURE RELIEF DEVICE AND AIRCRAFT HAVING AT LEAST ONE SUCH PROPULSION UNIT

#32 | 2024-08-01 ✅ Patent 12,612,180 granted on 2026-04-28

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FLIGHT MANAGEMENT METHOD AND DEVICE IN THE EVENT OF A CHALLENGING CONTEXT IN THE EVENT OF INCAPACITY OF AT LEAST ONE PILOT FLYING

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Electrical propulsion system including a plurality of electric motors coupled to the same input shaft of a transmission system, aircraft including at least one such electrical propulsion assembly

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INKJET PRINTING DEVICE, COMPRISING AT LEAST TWO SERVOCONTROL LOOPS, SUITABLE FOR LARGE COMPLEX SURFACES

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QKD TERMINAL, QKD SYSTEM AND METHOD FOR QUANTUM COMMUNICATION

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METHOD, OPTICAL RECEIVER, QKD PULSE STREAM AND QKD SYSTEM

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METHOD FOR DETERMINING A PROBABILITY OF OCCURRENCE OF A MALFUNCTION CREATING A PERFORMANCE DEFECT IN AN AIRCRAFT

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AIRCRAFT COCKPIT SEAT WITH DISPLAY INTEGRATED INTO THE REAR OF THE SEAT BACK, AND COCKPIT PROVIDED WITH SUCH A SEAT

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METHOD AND AVIONICS COMPUTER FOR ADAPTING AN ANCHOR POINT OF A TERMINAL SEGMENT WITH RESPECT TO A LANDING THRESHOLD POINT, FOR A NON-PRECISION APPROACH

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Chemistry; metallurgy

METHODS FOR ANODIZING A PART SURFACE AND SUBSEQUENTLY COATING THE ANODIZED PART SURFACE FOR CORROSION PROTECTION PURPOSES

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Apparatus comprising a device for regulating a concentration of dihydrogen

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PHOTON SOURCE AND METHOD FOR QUANTUM COMMUNICATION

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Structural cooling system for an aircraft

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FREE SPACE OPTICAL COMMUNICATIONS TERMINAL

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Propulsive assembly for aircraft

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THERMAL AND ACOUSTIC INSULATION SYSTEM FOR AN AIRCRAFT

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POWER FUSE AND AIRCRAFT COMPRISING SUCH A POWER FUSE

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ELECTRONIC COMPONENT COMPRISING A TWO-PHASE FLUID FOR EVACUATING THE HEAT ENERGY FROM THE SEMICONDUCTORS OF SAID ELECTRONIC COMPONENT

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PROPULSION UNIT COMPRISING A TRANSMISSION SYSTEM, SEVERAL ELECTRIC MOTORS AND AT LEAST ONE REMOTE COUPLING SYSTEM, AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION UNIT

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MODULAR SYSTEM FOR STORING AND JETTISONING FLUID AND AIRCRAFT PROVIDED WITH SUCH A SYSTEM

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Electrical-energy transfer device comprising a centering system

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Reputation-Based Trust Determination Method

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METHOD FOR POLARIZATION COMPENSATION AND FREE-SPACE OPTICAL COMMUNICATION SYSTEM FOR AIRCRAFT

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VEHICLE OPERATOR MONITORING METHOD AND SYSTEM

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ELECTRICAL ARRANGEMENT FOR DIRECT CURRENT ELECTRIC SYSTEMS

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METHOD AND SYSTEM FOR GENERATING A LATERAL TRAJECTORY OF AN AIRCRAFT

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ELECTRIC PROPULSION ASSEMBLY COMPRISING AT LEAST ONE ELECTRIC MOTOR POSITIONED IN FRONT OF A TRANSMISSION SYSTEM, AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION ASSEMBLY

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ELECTRIC MACHINE WITH DIRECTLY COOLED WINDINGS

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INDUCTIVE COMPONENT FOR ELECTRIC OR HYBRID AIRCRAFT

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Semi-Active Noise Control System for an Aircraft

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Pump Arrangement for Providing a Saturated Liquid

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Tank system with a valve in the form of a pendulum system

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METHOD FOR MANAGING THE LONGITUDINAL POSITION OF A FOLLOWER AIRCRAFT WITH RESPECT TO A LEADER AIRCRAFT

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PITOT TUBE SENSING APPARATUS

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SYSTEM AND METHOD FOR SYNCHRONIZED DATA PLAYBACK AND AIRCRAFT

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POWER ELECTRONICS SYSTEM, ELECTRICAL SYSTEM, AND PROPULSION SYSTEM FOR A VEHICLE SUCH AS AN AIRCRAFT

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Fluid Transport Device And Method For Manufacturing A Fluid Transport Device

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Filling level monitoring device for a fluid gas container, hydrogen tank and aircraft comprising such hydrogen tank

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Aircraft Fuselage Intended to Receive Two Tanks Designed to Contain Liquid Hydrogen

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Joining method and assembly for an aircraft

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METHOD OF RECYCLING A STRUCTURE OR AT LEAST A PORTION THEREOF, AND COMPONENT FOR AN AIRCRAFT OR SPACECRAFT

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METHOD AND SYSTEM FOR DETERMINING FLOW PROPERTIES OF A FLUID FLOWING ALONG A SURFACE

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Propulsion system for an aircraft and method for protecting the propulsion system

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METHOD AND APPARATUS FOR OPERATING AN AIRCRAFT HAVING TWO ENGINES

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Device for connection of two double-wall pipes and hydrogen line including said connection device

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Permanent Magnet Material

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Flight formation assistance system for aircraft

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CIRCUIT BREAKER WITH PRE-CHARGING AND CURRENT LIMITING FUNCTIONS, METHOD OF OPERATING SAME, POWER SUPPLY CIRCUIT AND AIRCRAFT

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PROCESSING DEVICE AND METHOD FOR DISTRIBUTING DATA TO A PLURALITY OF PROCESSING UNITS

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Device for generating power, comprising an air-towed vessel towing at least one water current turbine

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Electrical energy storage system and a vehicle comprising such an electrical energy storage system

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SYSTEM AND METHOD FOR COGNITIVE ASSISTANCE IN AT LEAST PARTIALLY MANUAL AIRCRAFT ASSEMBLY

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METHOD FOR OPERATING ONE OR MORE NODES IN A COMMUNICATIONS NETWORK FOR COORDINATING TRANSMISSIONS OF DIFFERENT NODES IN THE NETWORK USING DATA VALIDITY AS DECISION METRIC

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Hydrogen tank assembly for a vehicle, such as an aircraft

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SYSTEM FOR LOCALIZING OBJECTS IN AN INDOOR ENVIRONMENT USING A WIRELESS COMMUNICATION NETWORK

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Propulsion assembly for an aircraft

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Shielding arrangement for aircraft wiring

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System for combined dihydrogen heating and fluid cooling for an aircraft, and aircraft comprising such a system

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OPTICAL LEVEL GAUGE APPARATUS AND METHOD, LIQUID TANK ASSEMBLY AND VEHICLE EMPLOYING THE SAME

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AIRCRAFT AND ELECTRICAL CONNECTOR FOR CONNECTING ELECTRICAL CONDUCTORS IN AN AIRCRAFT

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Auxiliary power unit for an aircraft

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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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