AIRBUS OPERATIONS

METHOD AND SYSTEM FOR ESTIMATING AIR FLOW THROUGH AN AIRCRAFT AIR VENT

N° US2025263177A1

REDUCED-MASS FLOATING-NUT SYSTEM AND METHOD FOR ASSEMBLING TWO PARTS USING SAID SYSTEM

N° US2025257751A1

REDUCED MASS FLOATING NUT SYSTEM AND METHOD OF ASSEMBLING TWO PARTS USING SAME

N° EP4600508A1

PROPULSION ASSEMBLY FOR AN AIRCRAFT, HAVING AN EXTRACTION FAN

N° US2025250019A1

AIRCRAFT COMPRISING AT LEAST ONE ENGINE ATTACHMENT SYSTEM WHICH HAS COPLANAR ANCHORING POINTS ON THE ENGINE

N° US2025250018A1

PROPULSION ASSEMBLY FOR AN AIRCRAFT COMPRISING A TURBOJET ENGINE, A PYLON AND MEANS FOR ATTACHING THE TURBOJET ENGINE TO THE PYLON

N° EP4592188A1

FORWARD ENGINE MOUNT FOR A HALF OR FULL WRAPAROUND PYLON

N° US2025242932A1

FORWARD ENGINE MOUNT WITH CONVERGING LINKS

N° US2025242934A1

METHOD AND SYSTEM FOR ASSISTING WITH THE RESTART OF AT LEAST ONE AIRCRAFT ENGINE

N° US2025242935A1

ACOUSTIC ABSORPTION STRUCTURE COMPRISING AT LEAST ONE PARTITION TUBE FOR FORMING TWO TYPES OF RESONATORS, METHOD FOR MANUFACTURING SUCH A STRUCTURE

N° EP4593006A1

A DECOMPRESSION PANEL FOR AN AIRCRAFT AND AN INTERNAL WALL OF AN AIRCRAFT HAVING SUCH A DECOMPRESSION PANEL

N° US2025242905A1

ACOUSTIC ABSORPTION STRUCTURE COMPRISING A CELLULAR STRUCTURE AND AT LEAST ONE PARTITION TUBE WHICH HAS AT LEAST TWO FLAT SIDES WHICH ARE CONNECTED TO THE WALLS OF THE CELLULAR STRUCTURE

N° US2025239247A1

HYDROGEN PROPULSION ASSEMBLY COMPRISING A DEVICE FOR INJECTING INERT GAS, AND AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION ASSEMBLY

N° US2025236410A1

SOUND-ABSORBING STRUCTURE COMPRISING A HONEYCOMB STRUCTURE AND AT LEAST ONE PARTITION TUBE HAVING AT LEAST TWO FLAT SPOTS CONNECTED TO THE WALLS OF THE HONEYCOMB STRUCTURE

N° EP4593005A1

THERMAL ASSEMBLY FOR A PROPULSION SYSTEM OF AN AIRCRAFT

N° US2025229909A1

ASSEMBLY FOR REINFORCING THE FUSELAGE OF AN AIRCRAFT DURING THE REMOVAL OF A REMOVABLE PANEL

N° EP4585507A1

ASSEMBLY FOR REINFORCING THE FUSELAGE OF AN AIRCRAFT WHEN REMOVING A REMOVABLE PANEL

N° US2025229889A1

ENERGY CONVERSION ARRANGEMENT, ENERGY SYSTEM AND AIRCRAFT COMPRISING SAME

N° US2025207538A1

ENERGY CONVERSION ARRANGEMENT, ENERGY SYSTEM AND AIRCRAFT COMPRISING SAME

N° US2025206153A1

ENERGY CONVERSION ARRANGEMENT, ENERGY SYSTEM AND AIRCRAFT COMPRISING SAME

N° US2025206154A1

SUPERCONDUCTING ELECTRICAL SUPPLY LINE, METHOD FOR CONTROLLING A SUPERCONDUCTING ELECTRICAL SUPPLY LINE AND AIRCRAFT COMPRISING SUCH A LINE

N° US2025210967A1

PROPELLER COMPRISING AT LEAST ONE BLADE HOLDING SYSTEM INCLUDING AT LEAST ONE TRANSVERSE GROOVE

N° US2025196996A1

DEVICE FOR ABSORBING ENERGY BY COMPRESSION, AIRCRAFT COMPRISING AT LEAST ONE SUCH DEVICE

N° EP4570647A1

Device for absorbing energy by compression, aircraft comprising at least one such device

N° CN120156682A

AIRCRAFT COMPRISING AT LEAST ONE REMOVABLE DEVICE FOR ABSORBING ENERGY BY COMPRESSION

N° US2025196989A1

Device for absorbing energy by compression, aircraft comprising at least one such device

N° US2025196988A1

METHOD FOR CONTROLLING THE POSITION OF AN END EFFECTOR OF A MULTI-AXIS ROBOT AND SYSTEM EXECUTING THE METHOD

N° US2025205903A1

Aircraft comprising at least one removable device for absorbing energy by compression

N° CN120156681A

AIRCRAFT PROPULSION ASSEMBLY HAVING AN ENGINE, A PYLON AND MEANS FOR ATTACHING THE ENGINE TO THE PYLON

N° US2025197017A1

AIRCRAFT COMPRISING AT LEAST ONE REMOVABLE DEVICE FOR ABSORBING ENERGY BY COMPRESSION

N° EP4570648A1

Soft-Start Strategy Of A Fuel Cell

N° US2025201879A1

PROPULSION ASSEMBLY FOR AN AIRCRAFT COMPRISING A FLUID-COOLING CIRCUIT WITH QUICK-FIT NACELLE/ENGINE COUPLINGS AND AIRCRAFT PROVIDED WITH SUCH AN ASSEMBLY

N° US2025188851A1

METHOD FOR MONITORING THE COHERENCE OF AN ATMOSPHERIC PRESSURE VALUE USED FOR CONFIGURING FLIGHT INSTRUMENTS OF AN AIRCRAFT

N° US2025189398A1

ASSEMBLY OF AN ENGINE MOUNTING PYLON WITH AN AIRCRAFT ENGINE

N° US2025206452A1

ATTACHMENT SYSTEM FOR LANDING GEAR

N° US2025171136A1

METHOD FOR CONTROLLING THE POSITION OF A TOOL HEAD OF A MULTI-AXIS ROBOT AND SYSTEM FOR CARRYING OUT THE METHOD

N° EP4575686A1

DEVICE FOR MANUFACTURING A STIFFENED PANEL MADE OF COMPOSITE MATERIAL COMPRISING A SYSTEM FOR TEMPORARILY HOLDING MANDRELS ON A MOUNTING SURFACE

N° EP4563333A1

ATTACHMENT SYSTEM FOR LANDING GEAR

N° EP4563468A1

Attachment system, attachment element, receiving element and aircraft

N° CN120057253A

Method for monitoring temperature of brake of landing gear of aircraft

N° CN120024501A

Gaine électrique comprenant au moins un système anti-frottement

N° FR3158193A1

SUPERCONDUCTING MOTOR HAVING A COOLING SYSTEM

N° US2025167657A1

METHOD FOR MONITORING THE TEMPERATURE OF BRAKES OF LANDING GEAR OF AN AIRCRAFT

N° US2025162564A1

METHOD AND DEVICE FOR ANALYZING A REAL FORM OF AN AERODYNAMIC SURFACE OF A PART

N° US2025148156A1

METHOD FOR MONITORING THE TEMPERATURE OF THE BRAKES OF AN AIRCRAFT LANDING GEAR

N° EP4559769A1

METHOD AND SYSTEM FOR OPTIMIZING THE MAINTENANCE OF AN AIRCRAFT STRUCTURE AGAINST CORROSION

N° US2025136295A1

METHOD AND SYSTEM FOR DEFINING A DIGITAL TWIN OF AN AIRCRAFT INTENDED TO IMPROVE A DESIGN OF AN AIRCRAFT STRUCTURE IN ORDER TO CONTRIBUTE TO THE FIGHT AGAINST CORROSION OF THE AIRCRAFT STRUCTURE

N° US2025139321A1

Actuation system for cargo door of aircraft, aircraft and method for opening cargo door of aircraft using actuation system

N° CN119898465A

AIRCRAFT CARGO DOOR ACTUATION SYSTEM

N° US2025136265A1

PRINTING METHOD FOR PRODUCING A PAINTED SUPPORT

N° US2025144949A1

Aircraft, actuation system for cargo door of aircraft, and method of opening cargo door of aircraft

N° CN119898464A

AIRCRAFT CARGO DOOR ACTUATION SYSTEM

N° US2025136264A1

Printing method

N° CN119898133A

DEVICE AND METHOD FOR GENERATING FLUTTER ON AT LEAST A PART OF AN AIRCRAFT

N° US2025136271A1

PRINTING METHOD FOR PRODUCING A PAINTED SUBSTRATE

N° EP4545309A1

Fixing device, assembly comprising fixing device and dismounting method of fixing device

N° CN119844474A

METHOD AND SYSTEM FOR AUTOMATICALLY ESTIMATING THE REMAINING USEFUL LIFETIME OF AT LEAST ONE OXYGEN BOTTLE IN THE COCKPIT OF AN AIRCRAFT

N° US2025130135A1

METHOD AND SYSTEM FOR MONITORING MEASUREMENTS OF STATIC-PRESSURE PROBES OF AN AIRCRAFT

N° US2025137864A1

BLIND TYPE REMOVABLE FIXING DEVICE, ASSEMBLY COMPRISING AT LEAST ONE SUCH FIXING DEVICE AND METHOD OF DISMANTLING SUCH A FIXING DEVICE

N° US2025129812A1

Propulsion assembly for aircraft and aircraft

N° CN119825573A

Procédé de fabrication d’une pièce tridimensionnelle à partir d’au moins une feuille métallique comprenant un réseau de pré-plis, pièce tridimensionnelle obtenue à partir dudit procédé

N° FR3154025A1

PROPULSION ASSEMBLY INTENDED FOR AN AIRCRAFT AND HAVING A HEAT EXCHANGE SYSTEM IN THE EXHAUST NOZZLE

N° US2025122829A1

MOUNTING OF A PYLON WITH AN AIRCRAFT ENGINE

N° EP4574669A1

PROPULSION ASSEMBLY FOR AN AIRCRAFT COMPRISING A SYSTEM FOR HEAT EXCHANGE IN THE EXHAUST NOZZLE

N° EP4538515A1

DISMOUNTABLE FASTENING DEVICE OF THE BLIND TYPE, ASSEMBLY COMPRISING AT LEAST ONE SUCH FASTENING DEVICE AND METHOD FOR DISASSEMBLING SUCH A FASTENING DEVICE

N° EP4542063A1

PROPULSION ASSEMBLY FOR AN AIRCRAFT

N° US2025121929A1

PROPULSION ASSEMBLY FOR AN AIRCRAFT

N° US2025121927A1

AIRCRAFT CARGO DOOR ACTUATION SYSTEM

N° EP4545405A1

AIRCRAFT CARGO DOOR ACTUATION SYSTEM

N° EP4545404A1

SYSTEME DE PILE A COMBUSTIBLE ET PROCEDE DE DEMARRAGE CORRESPONDANT

N° FR3158834A1

PROPULSION ASSEMBLY FOR AIRCRAFT

N° EP4538514A1

METHOD AND SYSTEM USING A NEURAL NETWORK TO PREDICT A TIME OF OCCUPANCY OF A RUNWAY BY AN AIRCRAFT

N° US2025131835A1

AIRCRAFT COMPRISING AT LEAST ONE ENGINE ATTACHMENT SYSTEM THAT HAS REDUCED VERTICAL BULK

N° US2025115365A1

METHOD FOR CONSTRUCTING A SIMPLIFIED REPRESENTATION OF OBSTACLES IN THE VICINITY OF AN AIRPORT

N° US2025118217A1

Aircraft comprising at least one engine attachment system with reduced vertical volume

N° CN119773977A

METHOD FOR MANUFACTURING AN INTERMEDIATE RESISTIVE MEMBRANE OF AN ACOUSTIC COATING

N° US2025108551A1

METHOD FOR MANUFACTURING AN INTERMEDIATE RESISTIVE MEMBRANE OF AN ACOUSTIC LINER

N° US2025108544A1

Deformable sealing plug and method of plugging cavity using such sealing plug

N° CN119712844A

DEFORMABLE SEALING PLUG AND PROCESS FOR PLUGGING A CAVITY USING SUCH A SEALING PLUG

N° US2025100714A1

TEMPERATURE MEASURING DEVICE WITH AN OPTICAL FIBER INSULATED FROM A FIXING WALL BY A PART COMPRISING CORK

N° US2025102372A1

PROPULSION ASSEMBLY FOR AIRCRAFT

N° EP4538513A1

Temperature measuring device with optical fiber insulated from fixed wall by part comprising cork

N° CN119714591A

TEMPERATURE MEASURING DEVICE WITH OPTICAL FIBRE ISOLATED FROM A FIXING WALL BY A PART COMPRISING CORK

N° EP4530589A1

AIRCRAFT NACELLE PROVIDED WITH AT LEAST ONE THRUST REVERSAL DEVICE COMPRISING AT LEAST ONE LONGITUDINAL DEFLECTOR, AIRCRAFT COMPRISING AT LEAST ONE PROPULSION ASSEMBLY COMPOSED OF SUCH A NACELLE

N° US2025092847A1

AIRPORT INSTALLATION INCLUDING A PLURALITY OF DIHYDROGEN STORAGE TANKS

N° US2025102113A1

Aircraft pod equipped with thrust reverser comprising longitudinal deflector, and aircraft

N° CN119659961A

POWERPLANT FOR AN AIRCRAFT

N° US2025092829A1

AIRCRAFT COMPRISING A DIHYDROGEN SUPPLY SYSTEM AND A DIHYDROGEN HEAT TREATMENT SYSTEM

N° US2025091724A1

SET OF PIPES COMPRISING AN IMPROVED RETAINING SYSTEM

N° US2025092971A1

Set of tubes comprising improved retention system

N° CN119617203A

Power device for aircraft and aircraft comprising such power device

N° CN119641483A

METHOD AND SYSTEM FOR MONITORING A SAFETY LEVEL OF A TRAJECTORY OF AN AIRCRAFT AND FOR GENERATING A CORRESPONDING ALERT

N° US2025095498A1

Method and system for monitoring aircraft trajectory security levels and generating corresponding alarms

N° CN119673003A

AIRCRAFT NACELLE PROVIDED WITH AT LEAST ONE THRUST REVERSER DEVICE COMPRISING AT LEAST ONE LONGITUDINAL DEFLECTOR, AIRCRAFT COMPRISING AT LEAST ONE PROPULSION ASSEMBLY COMPRISING SUCH A NACELLE

N° EP4528093A1

DEFORMABLE SEALING PLUG AND METHOD FOR SEALING A CAVITY USING SUCH A SEALING PLUG

N° EP4530503A1

ASSEMBLY FOR AN AIRCRAFT COMPRISING A WING AND A REACTOR MASS FOR COUPLING A PROPULSION SYSTEM TO THE WING

N° CN119527558A

AIRCRAFT COMPRISING AT LEAST ONE ENGINE MOUNTING SYSTEM HAVING WING MOUNTS POSITIONED APPROXIMATELY IN A MEDIAN LONGITUDINAL PLANE

N° US2025074612A1

ASSEMBLY FOR AN AIRCRAFT COMPRISING A WING AND A REACTOR MAST FOR COUPLING A PROPULSION SYSTEM TO SAID WING

N° US2025074610A1

AIRCRAFT FUSELAGE

N° US2025074574A1

ASSEMBLY OF A LONGITUDINAL MEMBER OF A WING AND AN ENGINE PYLON WHICH ARE HORIZONTALLY ALIGNED RELATIVE TO ONE ANOTHER

N° US2025074611A1