AIRBUS OPERATIONS LTD · BAE SYSTEMS AIRBUS SA

METHOD FOR DETERMINING AT LEAST ONE CHARACTERISTIC OF A MOVEMENT OF A MOBILE STRUCTURE OF AN AIRCRAFT AND AIRCRAFT COMPRISING A DEVICE FOR ITS IMPLEMENTATION

N° US2025242940A1

ATTACHMENT SYSTEM FOR LANDING GEAR

N° US2025171136A1

Attachment system, attachment element, receiving element and aircraft

N° CN120057253A

ATTACHMENT SYSTEM FOR LANDING GEAR

N° EP4563468A1

SEAT RAIL AND A SEAT MOUNTING SYSTEM FOR AN AIRCRAFT

N° US2025074600A1

Ventilation system, fueling system, method of discharging tank fluid, and non-transitory computer-readable storage medium

N° CN119508070A

VENT SYSTEM

N° JP2025031663A

VENT SYSTEM

N° EP4512723A1

VENT SYSTEM

N° US2025066034A1

Seat track and seat mounting system for aircraft, and aircraft

N° CN119527553A

DOUBLE-WALL PIPE FOR AN AIRCRAFT FUEL SYSTEM

N° EP4497985A1

DOUBLE-WALL PIPE FOR AIRCRAFT FUEL SYSTEM

N° JP2025017354A

Double-walled tube for aircraft fuel system, aircraft fuel system and aircraft

N° CN119348839A

DOUBLE-WALL PIPE FOR AN AIRCRAFT FUEL SYSTEM

N° US2025033788A1

METHOD OF BRAKING AIRCRAFT

N° EP4497679A1

SYSTEM FOR ASSISTING WITH OPERATIONS TO BE EFFECTED IN AN AIRCRAFT DURING A PHASE OF MOVING OVER THE GROUND IN AN AIRPORT

N° US2025006067A1

Method and system for assisting operation to be performed in aircraft during movement phase on ground in airport

N° CN119229692A

AIRCRAFT WING

N° US2024417066A1

AILE POUR UN AÉRONEF ET COMPORTANT UN SYSTÈME DE DÉGIVRAGE

N° FR3152492A1

Antenna element and antenna array

N° CN118920077A

ANTENNA ELEMENT AND ANTENNA ARRAY

N° US2024380119A1

Procédé de détermination d’au moins une caractéristique d’un mouvement d’une structure mobile d’un aéronef et aéronef comprenant un dispositif pour sa mise en œuvre

N° FR3158790A1

AIRCRAFT FUEL STORAGE SYSTEM

N° US2024239510A1

METHOD OF MANUFACTURING AN AIRCRAFT ASSEMBLY

N° US2024239515A1

Attachment system for landing gear

N° GB202318161D0

A SEAT RAIL AND A SEAT MOUNTING SYSTEM FOR AN AIRCRAFT

N° EP4516667A1

Vent system

N° GB202312885D0

Method of braking aircraft

N° GB202311673D0

Double-wall pipe for an aircraft fuel system

N° GB202311353D0

SYSTEME D’ASSISTANCE A DES OPERATIONS A REALISER DANS UN AERONEF LORS D’UNE PHASE DE DEPLACEMENT AU SOL DANS UN AEROPORT

N° FR3150624A1

AN AIRCRAFT WING

N° EP4477532A1

ANTENNA ELEMENT AND ANTENNA ARRAY

N° EP4462591A1

Aircraft fuselage intended to receive two storage tanks designed to contain liquid hydrogen

N° CN116902196A

AIRCRAFT FUSELAGE FOR RECEIVING TWO TANKS INTENDED TO CONTAIN LIQUID HYDROGEN

N° EP4265525A1

METHOD OF CONFIGURING A NETWORK OF TIRE MONITORING DEVICES

N° US2023311593A1

METHOD OF EXCHANGING CRYPTOGRAPHIC PARAMETERS IN A NETWORK OF TIRE MONITORING DEVICES

N° US2025214384A1

Tire pressure monitoring devices

N° US2023311592A1

A METHOD OF CONFIGURING A NETWORK OF TIRE MONITORING DEVICES

N° EP4253101A1

Aircraft fuselage intended to receive two tanks designed to contain liquid hydrogen

N° US2023339593A1

MONITORING FRICTION ASSOCIATED WITH A PLURALITY OF AIRCRAFT WHEELS

N° EP4249332A1

Monitoring friction associated with a plurality of aircraft wheels

N° US2023322413A1

MANAGING MICROBIAL CONTAMINATION OF FUEL TANK

N° US2025178750A1

METHOD AND APPARATUS FOR MANUFACTURING AT LEAST A PORTION OF A BOX STRUCTURE OF AN AIRCRAFT COMPRISING A FORMING STEP AND CENTRAL WING BOX OBTAINED THEREBY

N° EP4230394A1

Method for manufacturing at least one portion of a box structure of an aircraft comprising a forming step, and a central wingbox thus obtained

N° US2023264804A1

AIRCRAFT FUEL STORAGE SYSTEM

N° EP4403472A1

METHOD OF MANUFACTURING AN AIRCRAFT ASSEMBLY

N° EP4400429A1

METHOD OF MONITORING A STATE OF A MACHINE LEARNING CLASSIFIER

N° US2023368009A1

Optimized connection assembly between two portions of a cryogenic line, comprising a double sealing barrier, a fluid expansion chamber and a detector for detecting the presence of the fluid in said chamber

N° US2023135912A1

OPTIMIZED CONNECTION ASSEMBLY BETWEEN TWO PORTIONS OF A CRYOGENIC PIPELINE, COMPRISING A DOUBLE SEALING BARRIER, A FLUID EXPANSION CHAMBER AND A DETECTOR FOR DETECTING THE PRESENCE OF FLUID IN SAID CHAMBER

N° EP4174355A1

Fuselage d’aéronef destiné à recevoir deux réservoirs prévus pour contenir de l’hydrogène liquide.

N° FR3134799A1

TIRE PRESSURE MONITORING DEVICES

N° EP4253100A1

A METHOD OF EXCHANGING CRYPTOGRAPHIC PARAMETERS IN A NETWORK OF TIRE MONITORING DEVICES

N° EP4253099A1

Monitoring friction associated with a plurality of aircraft wheels

N° GB202204263D0

PROCEDE D’ESTIMATION D’UNE VITESSE DE CORROSION D’AU MOINS UN ELEMENT D’UN AERONEF

N° FR3133840A1

Procédé de fabrication d’au moins une partie d’une structure en caisson d’un aéronef comportant une étape de formage, caisson central de voilure ainsi obtenu

N° FR3132863A1

ENSEMBLE DE CONNEXION OPTIMISE ENTRE DEUX PORTIONS D’UNE CANALISATION CRYOGENIQUE, COMPRENANT UNE DOUBLE BARRIERE D’ETANCHEITE, UNE CHAMBRE D’EXPANSION DE FLUIDE ET UN DETECTEUR DE PRESENCE DU FLUIDE DANS LADITE CHAMBRE.

N° FR3128759A1

Hinge assembly for aircraft component, aircraft component, wing and aircraft

N° CN114623147A

Hinge assembly for aircraft component, aircraft component, wing and aircraft

N° CN114623146A

BRAKE CONTROL

N° US2021402973A1

METHOD AND DEVICE FOR ESTIMATING THE STATE OR THE PRESSURE OF THE TYRES OF AN AIRCRAFT

N° EP3929006A1

PROCEDE ET DISPOSITIF D'ESTIMATION DE L'ÉTAT OU DE LA PRESSION DES PNEUS D’UN AERONEF

N° FR3111846A1

METHOD FOR JOINING TWO PIECES

N° EP3922567A1

Landing gear assembly

N° US2022009620A1

LANDING GEAR ASSEMBLY

N° EP3870508A1

LANDING GEAR ASSEMBLY

N° CN113165734A

LANDING GEAR ASSEMBLY

N° WO2020234314A1

Method For Assembling An Aircraft Pylon

N° US2020231294A1

Overheat detection systems for aircrafts

N° CN111562071A

Overheat detection systems for aircraft

N° US2020191680A1

OVERHEAT DETECTION SYSTEMS FOR AIRCRAFTS

N° CA3064918A1

Joint and aircraft

N° CN110963054A

Landing gear assembly

N° GB201907114D0

Landing gear temperature characteristic

N° CN110282149A

AIRCRAFT BRAKING

N° EP3530533A2

AIRCRAFT BRAKING

N° CN110194262A

VEHICLE BRAKING

N° EP3530529A1

AIRCRAFT BRAKING

N° EP3957528A1

Vehicle brake

N° CN110194281A

Brake control

N° CN110194280A

BRAKE CONTROL

N° EP3530532A1

AIRCRAFT BRAKING

N° EP4324709A2

BRAKE MONITORING

N° US2019263373A1

BRAKE CONTROL

N° US2019263374A1

Apparatus and method for determining aircraft brake future use cycles

N° US2019263375A1

Aircraft braking

N° US2019263510A1

Brake monitoring

N° CN110194279A

BRAKE MONITORING

N° EP3530531A1

Tool and method for installing a seal by allowing a precompression to join two tubular parts

N° US2019184532A1

TOOL AND METHOD FOR INSTALLING SEAL

N° CN110014391A

OVERHEAT DETECTION SYSTEMS FOR AIRCRAFTS

N° EP3667276A1

Sistemas de detección de sobrecalentamiento para aeronaves

N° ES2895496T3

Method and a control unit for controlling actuation of a foldable wing tip section of a wing of an aircraft

N° US2020023938A1

Vehicle braking

N° GB201817600D0

Method for assembling a primary structure of an aircraft pylon

N° US2019112074A1

Aircraft braking

N° GB201811179D0

Brake control

N° GB201811178D0

System for moving an aircraft door

N° GB201803303D0

Brake monitoring

N° GB201803203D0

Braking control system for an aircraft

N° US2017008503A1

Aircraft Steering System Controller

N° CN106335634A