AIRBUS HELICOPTERS

METHOD FOR CONTROLLING A HYBRID DRIVE SYSTEM FOR A VEHICLE AND ARCHITECTURE FOR CONTROLLING SUCH A HYBRID DRIVE SYSTEM

N° EP4585441A1

METHOD FOR CONTROLLING A HYBRID POWER PLANT FOR A VEHICLE AND CONTROL ARCHITECTURE FOR SUCH A HYBRID POWER PLANT

N° US2025223049A1

MECHANICAL SYSTEM WITH MOVABLE MECHANICAL ELEMENTS, A MAGNETIC PLUG AND A LUBRICATION SYSTEM PROVIDED WITH MECHANICAL AND MAGNETIC FILTERS

N° EP4603684A1

METHOD FOR MONITORING AN ENERGY LEVEL OF AN ELECTRICAL ENERGY SOURCE OF A HYBRID DRIVE SYSTEM FOR AN AIRCRAFT

N° EP4583358A1

METHOD FOR MONITORING AN ENERGY LEVEL OF AN ELECTRICAL ENERGY SOURCE OF A HYBRID POWER PLANT FOR AN AIRCRAFT

N° US2025225883A1

MECHANICAL SYSTEM PROVIDED WITH MOVING MECHANICAL ELEMENTS, A MAGNETIC PLUG AND A LUBRICATION SYSTEM PROVIDED WITH MECHANICAL AND MAGNETIC FILTERS

N° US2025257796A1

STRUCTURAL ARRANGEMENT FOR AN ELONGATED NOSE REGION OF A ROTARY-WING AIRCRAFT

N° US2025229887A1

METHOD FOR MONITORING THE OPERATION OF A ROTORCRAFT POWER PLANT AND ASSOCIATED ROTORCRAFT

N° US2025223052A1

METHOD FOR MONITORING AN OPERATION OF A ROTORCRAFT POWER PLANT AND ASSOCIATED ROTORCRAFT

N° EP4582344A1

ENGINE FAILURE TRAINING METHOD FOR A HYBRID ROTORCRAFT

N° US2025182646A1

METHOD FOR TRAINING THE FAILURE OF AN ENGINE ON A HYBRID MOTOR-DRIVEN ROTORCRAFT

N° EP4563470A1

AIRCRAFT PROVIDED WITH A HEATING SYSTEM FOR A TURBINE ENGINE PLENUM

N° EP4571075A1

Power plant having turboshaft engine and adaptive starting circuit, and adaptive starting method for turboshaft engine

N° CN120100590A

POWER PLANT PROVIDED WITH A TURBINE ENGINE AND AN ADAPTIVE START CIRCUIT AND METHOD FOR ADAPTIVELY STARTING A TURBINE ENGINE

N° EP4567266A1

POWER PLANT PROVIDED WITH A TURBOSHAFT ENGINE AND AN ADAPTIVE STARTING CIRCUIT AND ADAPTIVE STARTING METHOD FOR A TURBOSHAFT ENGINE

N° US2025179962A1

Monitoring system for monitoring hybrid power plant of rotorcraft, related rotorcraft and method

N° CN120057277A

MONITORING SYSTEM FOR MONITORING A HYBRID POWER PLANT OF A ROTORCRAFT, ASSOCIATED ROTORCRAFT AND METHOD

N° US2025171157A1

MONITORING SYSTEM FOR MONITORING A HYBRID POWER PLANT OF A ROTORCRAFT, ASSOCIATED ROTORCRAFT AND METHOD

N° EP4559807A1

System having mechanical connection with two mechanical torque transmission paths

N° CN119737397A

SYSTEM HAVING A MECHANICAL CONNECTION DEVICE WITH TWO MECHANICAL TORQUE TRANSMISSION PATHS

N° US2025108930A1

MEASUREMENT APPARATUS FOR DETERMINING A BENDING MOMENT

N° US2025155315A1

MEASUREMENT SYSTEM COMPRISING AN OPTICAL FIBER PROVIDED WITH AT LEAST ONE BRAGG GRATING FOR MEASURING DYNAMIC DEFORMATION, AIRCRAFT AND METHOD

N° US2025137858A1

MEASURING SYSTEM COMPRISING AN OPTICAL FIBRE PROVIDED WITH AT LEAST ONE BRAGG GRATING FOR MEASURING A DYNAMIC DEFORMATION, AIRCRAFT AND METHOD

N° EP4545904A1

SYSTEM HAVING A MECHANICAL CONNECTION DEVICE WITH TWO MECHANICAL TORQUE TRANSMISSION PATHS

N° EP4530490A1

METHOD FOR ANTICORROSION TREATMENT OF A MAGNESIUM ALLOY PART, ASSOCIATED ANTICORROSION AQUEOUS SOLUTION AND PART

N° WO2025021441A1

MECHANICAL POWER TRANSMISSION SYSTEM GEARBOX AND AIRCRAFT

N° KR20250047109A

ACTUATOR PROVIDED WITH TWO PRESSURE SENSORS AND A VIRTUAL PRESSURE SENSOR; A BRAKING SYSTEM AND AN AIRCRAFT PROVIDED WITH SUCH AN ACTUATOR, AND THE APPLIED METHOD

N° EP4556325A1

METHOD FOR CONTROLLING A ROTORCRAFT ASSOCIATED ROTORCRAFT AND COMPUTER PROGRAM

N° KR20250060800A

Method for controlling rotorcraft, associated rotorcraft and computer program

N° CN119898481A

MECHANICAL POWER TRANSMISSION SYSTEM, GEARBOX AND AIRCRAFT

N° US2025100702A1

MECHANICAL POWER TRANSMISSION SYSTEM, POWER TRANSMISSION GEARBOX AND AIRCRAFT

N° EP4530498A1

ACTUATOR PROVIDED WITH TWO PRESSURE SENSORS AND A VIRTUAL PRESSURE SENSING DEVICE; A BRAKING SYSTEM AND AN AIRCRAFT PROVIDED WITH SUCH AN ACTUATOR, AND THE METHOD APPLIED

N° US2025162550A1

METHOD FOR CONTROLLING A ROTORCRAFT, ASSOCIATED ROTORCRAFT AND COMPUTER PROGRAM

N° US2025136273A1

GROUND SERVICE DEVICE FOR SECURING ROTOR BLADES OF A ROTARY-WING AIRCRAFT

N° US2025121956A1

METHOD FOR CONTROLLING A ROTORCRAFT, ASSOCIATED ROTORCRAFT AND COMPUTER PROGRAM

N° EP4545406A1

METHOD AND DEVICE FOR DETERMINING THE ABSOLUTE POSE OF A CAMERA LOCATED ON BOARD AN AIRCRAFT OR SPACECRAFT

N° WO2024241017A1

PARTITION FOR A VEHICLE COMPRISING A DEVICE FOR ASSISTING THE EVACUATION OF PERSONS BY AN EMERGENCY EXIT FROM THE PARTITION

N° EP4530191A1

METHOD AND DEVICE FOR DETERMINING THE ABSOLUTE POSE OF A CAMERA LOCATED ON BOARD AN AIRCRAFT OR SPACECRAFT

N° EP4526843A1

METHOD FOR ASSISTING THE PILOTING OF A ROTORCRAFT AND ROTORCRAFT THUS EQUIPPED

N° KR20250015814A

PIVOTING LANDING GEAR PROVIDED WITH AN IMMOBILIZATION SYSTEM

N° KR20250009340A

METHOD FOR ASSISTING THE PILOTING OF A ROTORCRAFT AND ROTORCRAFT THUS EQUIPPED

N° US2025187741A1

METHOD FOR ASSISTING THE PILOTING OF A ROTORCRAFT AND ROTORCRAFT THUS EQUIPPED

N° EP4495009A1

PIVOTING LANDING GEAR PROVIDED WITH AN IMMOBILIZATION SYSTEM

N° US2025019068A1

PIVOTING LANDING GEAR PROVIDED WITH AN IMMOBILISATION SYSTEM

N° EP4491512A1

A Method Of Processing Engine Monitoring Parameters

N° KR20240161764A

METHOD OF PROCESSING ENGINE MONITORING PARAMETERS

N° US2024367813A1

ROTORCRAFT FLIGHT TRAINING METHOD ASSOCIATED SYSTEM AND ROTORCRAFT

N° KR20240172030A

METHOD AND DEVICE FOR MONITORING THE HEALTH OF A MECHANICAL SYSTEM OF A VEHICLE BY USING THRESHOLDS THAT VARY DEPENDING ON OPERATING PARAMETERS OF THE SYSTEM

N° KR20240165260A

METHOD AND DEVICE FOR MONITORING THE HEALTH OF A MECHANICAL SYSTEM OF A VEHICLE BY USING A THRESHOLD VARIABLE FROM AN OPERATING PARAMETER OF

N° CN118960824A

METHOD AND DEVICE FOR MONITORING THE HEALTH OF A MECHANICAL SYSTEM OF A VEHICLE BY USING THRESHOLDS THAT VARY DEPENDING ON OPERATING PARAMETERS OF THE SYSTEM

N° US2024383617A1

ROUTING METHOD AND DEVICE FOR A TWO-ENGINE AIRCRAFT HAVING AN ECONOMICAL OPERATING MODE

N° EP4462219A1

ROTORCRAFT FLIGHT TRAINING METHOD, ASSOCIATED SYSTEM AND ROTORCRAFT

N° US2024404424A1

METHOD AND SYSTEM FOR ASSISTING THE PILOTING OF AN AIRCRAFT WITH A HEAD-UP DISPLAY

N° KR20240153915A

METHOD AND SYSTEM FOR ASSISTING THE PILOTING OF AN AIRCRAFT WITH A HEAD-UP DISPLAY

N° US2025011003A1

AIRCRAFT PROVIDED WITH A RAIN-REPELLENT VENTILATION SYSTEM FOR AN ELECTRIC MACHINE

N° US2024409229A1

METHOD AND DEVICE FOR MONITORING THE HEALTH OF A MECHANICAL SYSTEM OF A VEHICLE BY USING THRESHOLDS THAT VARY DEPENDING ON OPERATING PARAMETERS OF THE SYSTEM

N° EP4464997A1

AIRCRAFT PROVIDED WITH A RAIN-REPELLENT VENTILATION SYSTEM FOR AN ELECTRIC MACHINE

N° KR20240174815A

METHOD AND DEVICE FOR ASSISTING THE PILOTING OF AN AIRCRAFT WITH A HEAD-UP DISPLAY

N° EP4450926A1

AIRCRAFT WITH ANTIRAIN VENTILATION SYSTEM FOR AN ELECTRIC MACHINE

N° EP4474288A1

METHOD FOR DETERMINING A FUEL CONSUMPTION MARGIN OF AN ENGINE IN RELATION TO A THEORETICAL CONSUMPTION

N° KR20240176421A

Method and device for entering and exiting economical mode of operation of dual-engine aircraft

N° CN118934251A

METHOD FOR DETERMINING A FUEL CONSUMPTION MARGIN OF AN ENGINE IN RELATION TO A THEORETICAL CONSUMPTION

N° US2024418102A1

METHOD AND DEVICE FOR ENTERING AND EXITING AN ECONOMY OPERATING MODE FOR A TWIN-ENGINE AIRCRAFT

N° US2024377838A1

METHOD AND MULTI-ENGINE ROTORCRAFT FOR SIMULATING AN ENGINE FAILURE

N° US2024354461A1

METHOD FOR CONTROLLING A MULTI-ENGINE ROTARY-WING AIRCRAFT WITH REDUCED FUEL CONSUMPTION ON THE GROUND

N° US2024343404A1

WINDOW WITH A VENT WINDOW ASSEMBLY FOR A VEHICLE

N° US2024308641A1

Système mécanique muni d’éléments mécaniques mobiles, d’un bouchon magnétique ainsi que d’un système de lubrification muni de filtres mécanique et magnétique.

N° FR3159215A1

METHOD FOR DETERMINING A FUEL CONSUMPTION MARGIN OF AN ENGINE WITH RESPECT TO A THEORETICAL CONSUMPTION

N° EP4477865A1

METHOD AND DEVICE FOR ENTERING AND EXITING AN ECONOMICAL OPERATING MODE FOR A TWIN-ENGINE AIRCRAFT

N° EP4461641A1

METHOD AND MULTI-ENGINE ROTORCRAFT FOR SIMULATING AN ENGINE FAILURE

N° EP4450399A1

METHOD AND AIRCRAFT PROVIDED WITH AT LEAST ONE ACOUSTIC REFLECTOR FOR A FREE STANDING ROTOR SYSTEM

N° EP4455002A1

METHOD FOR CONTROLLING A MULTI-ENGINE ROTARY WING AIRCRAFT WITH REDUCED FUEL CONSUMPTION ON THE GROUND

N° EP4446232A1

ROTORCRAFT PROVIDED WITH A CELL SUPPORTED BY A LANDING GEAR WITH SKIDS WITH VARIABLE STRESS-RELIEVING ZONES

N° EP4438473A1

METHOD AND SYSTEM FOR DETECTING HARD LANDING

N° EP4438471A1

A STRUCTURAL ARRANGEMENT FOR AN ELONGATED NOSE REGION OF A ROTARY-WING AIRCRAFT

N° EP4585506A1

Procédé de surveillance d’un niveau d’énergie d’une source d’énergie électrique d’une installation motrice hybride pour aéronef

N° FR3158157A1

Procédé de surveillance d’un fonctionnement d’une installation motrice de giravion et giravion associé

N° FR3158098A1

Procédé de pilotage d’une installation motrice hybride pour véhicule et une architecture de pilotage d’une telle installation motrice hybride

N° FR3158094A1

METHODS FOR DETERMINING THE CYCLOSTATIONNARITY OF A VIBRATION SIGNAL RELATING TO A MECHANICAL SYSTEM, FOR ARRANGING VIBRATION SENSORS FOR MONITORING SUCH A SYSTEM, AND FOR MONITORING IT

N° US2024255380A1

Rotorcraft, fuselage of which is carried by skid landing gear having region that is subject to variable forces

N° CN118723069A

Method and system for detecting a hard landing

N° US2024327028A1

Method for testing a hybrid drive system on an aircraft, associated computer program and aircraft

N° US2024343415A1

METHOD AND DEVICE FOR DETECTING A FAULT IN A MECHANICAL SYSTEM COMPRISING AT LEAST ONE ROTATING MEMBER

N° US2024253811A1

Rotorcraft provided with an airframe carried by a skid landing gear with zones for taking up variable forces

N° US2024326991A1

METHODS FOR DETERMINING CYCLOSTATIONARYITY OF A VIBRATION SIGNAL RELATIVE TO A MECHANICAL SYSTEM, FOR ARRANGING VIBRATORY SENSORS FOR MONITORING SUCH A SYSTEM AND FOR MONITORING

N° EP4407282A1

METHOD FOR TESTING A HYBRID POWER PLANT PROVIDED ON AN AIRCRAFT, ASSOCIATED COMPUTER PROGRAM AND AIRCRAFT

N° EP4414269A1

Aéronef muni d’un système de chauffage pour un plenum de turbomoteur

N° FR3156759A1

METHOD AND DEVICE FOR DETECTING A DEFECT ON A MECHANICAL SYSTEM COMPRISING AT LEAST ONE ROTATING MEMBER

N° EP4407290A1

Installation motrice munie d’un turbomoteur et d’un circuit de démarrage adaptatif et procédé de démarrage adaptatif d’un turbomoteur

N° FR3156170A1

procédé d’entraînement à la panne moteur sur un giravion à motorisation hybride

N° FR3156119A1

Système de surveillance pour surveiller une installation motrice hybride de giravion, giravion et procédé associés

N° FR3155811A1

Actionneur muni de deux capteurs de pression et d’un senseur de pression virtuel ; un système de freinage et un aéronef munis d’un tel actionneur, et le procédé appliqué

N° FR3155482A1

METHOD AND SYSTEM FOR DETECTING OBSTACLES WITH AN OBSTACLE SENSOR FOR A ROTARY-WING AIRCRAFT

N° US2024201390A1

METHOD OF OPTIMIZING THE NOISE GENERATED IN FLIGHT BY A ROTORCRAFT

N° US2024084748A1

A MEASUREMENT APPARATUS FOR DETERMINING A BENDING MOMENT

N° EP4556873A1

METHOD AND SYSTEM FOR DETECTING OBSTACLES WITH AN OBSTACLE SENSOR FOR A ROTARY-WING AIRCRAFT

N° EP4390439A1

procédé de contrôle d’un giravion, programme d’ordinateur et giravion associés

N° FR3154709A1

Système de mesure comprenant une fibre optique munie d’au moins un réseau de Bragg pour mesurer une déformation dynamique, aéronef et procédé.

N° FR3154800A1

Outil abrasif morphologique et son procédé de fabrication, et procédé de retouche d’au moins une dent d’une pièce de transmission mécanique avec un tel outil

N° FR3154338A1

A GROUND SERVICE DEVICE FOR SECURING ROTOR BLADES OF A ROTARY-WING AIRCRAFT

N° EP4541713A1