AIRBUS HELICOPTERS

ENGINE FAILURE TRAINING METHOD FOR A SINGLE-ENGINE ROTORCRAFT

ROTORCRAFT WITH A FLIGHT CONTROL SYSTEM FOR IMPROVING ROTORCRAFT CONTROL UPON OCCURRENCE OF AN IN-FLIGHT SHUTDOWN IN AN ASYMMETRIC FLIGHT REGIME MODE

FLIGHT CONTROL SYSTEM HAVING AN ELECTRIC ACTUATOR FOR CONTROLLING A HYDRAULIC SERVO CONTROL

ELECTRICAL FLIGHT CONTROL SYSTEM FOR AIRCRAFT

ELECTRICAL FLIGHT CONTROL SYSTEM FOR CONTROLLING AN AIRCRAFT AND ASSOCIATED AIRCRAFT

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

METHOD AND SYSTEM FOR CONTROLLING AN AIRCRAFT DISPLAY

METHOD FOR THE ANTI-CORROSION TREATMENT OF A MAGNESIUM ALLOY PART, CORRESPONDING ANTI-CORROSION SUBSTANCE AND TREATED PART

METHOD AND ELECTROHYDRAULIC SYSTEM FOR CONTROLLING A RETRACTABLE LANDING GEAR OF AN AIRCRAFT, LANDING GEAR AND AIRCRAFT

MECHANICAL FLIGHT CONTROL SYSTEM OF AN AIRCRAFT WITH MEASUREMENT OF A FORCE IN THE MECHANICAL FLIGHT CONTROL SYSTEM

Rotary Wing Blade of an Aircraft, and Aircraft Provided with such a Blade

AIRCRAFT HAVING A PIVOTING LANDING GEAR PROVIDED WITH A PIVOT LOCKING SYSTEM AND A MONITORING SYSTEM

METHOD FOR REACTIVATING A COMBUSTION ENGINE IN STANDBY MODE DURING AN ASYMMETRIC OPERATING MODE IN A MULTI-ENGINE AIRCRAFT

Rotary-Wing Aircraft Provided with at least one Multi-Plane Pitch Stabilizer

HOLDING TERMINATION FOR A PROTECTIVE SHEATH

METHOD AND AIRCRAFT PROVIDED WITH A SYSTEM FOR DETERMINING A LEVEL OF POLLUTING EMISSION

LANDING GEAR UNIT EQUIPPED WITH A STATIC ELECTRICITY DISSIPATOR SYSTEM AND AIRCRAFT

AIRCRAFT DOOR LOCKING SYSTEM COMPRISING A MONITORING SYSTEM SIGNALING WHETHER THE LOCKING SYSTEM IS IN A LOCKED OR UNLOCKED STATE

DATA TRANSMISSION ARCHITECTURE AND VEHICLE FITTED WITH SUCH ARCHITECTURE

ROTORCRAFT WITH AN UNANTICIPATED YAW PREVENTION SYSTEM

MULTILAYER TEXTILE ASSEMBLY COMPRISING MINERAL REINFORCEMENT FIBERS

AIRCRAFT WITH A TRANSPARENT WALL FIXED TO A STRUCTURE VIA A SHOCK PROTECTION SYSTEM

MECHANICAL SYSTEM HAVING AN OIL SAMPLING DEVICE

SECURE MEASUREMENT SYSTEM AND METHOD FOR DISPLAYING AND TRANSMITTING INTEGRATED DATA

AIRCRAFT PROVIDED WITH A HEATING SYSTEM FOR A TURBOSHAFT ENGINE PLENUM

LINEAR ACTUATING DEVICE AND ASSOCIATED AIRCRAFT ROTOR TEST BENCH

METHOD AND SYSTEM FOR RAPID STARTING OF A COMBUSTION ENGINE IN A MULTI-ENGINE AIRCRAFT

SEAT BEAM FOR A ROTARY-WING AIRCRAFT ADAPTED FOR RECEIVING SEAT POSTS OF A SEAT BENCH DEVICE

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

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

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

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

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

ENGINE FAILURE TRAINING METHOD FOR A HYBRID ROTORCRAFT

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

MEASUREMENT APPARATUS FOR DETERMINING A BENDING MOMENT

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

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

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

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

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

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

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

METHOD OF PROCESSING ENGINE MONITORING PARAMETERS

METHOD AND MULTI-ENGINE ROTORCRAFT FOR SIMULATING AN ENGINE FAILURE

WINDOW WITH A VENT WINDOW ASSEMBLY FOR A VEHICLE

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

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

ROTORCRAFT WITH A NON-RETRACTABLE WHEEL-TYPE LANDING GEAR

METHOD FOR SETTING THE MASS OF A LOAD TO BE TRANSPORTED BY AN AIRCRAFT

DOUBLE-LOCKING HOOKING SYSTEM INTENDED FOR TRANSPORTING A LOAD OUTSIDE AN AIRCRAFT

METHOD FOR TRAINING AT LEAST ONE ARTIFICIAL INTELLIGENCE MODEL FOR ESTIMATING THE WEIGHT OF AN AIRCRAFT DURING FLIGHT BASED ON USE DATA

METHOD AND SYSTEM FOR CONTINUOUS IN-FLIGHT MANAGEMENT OF AN ON-BOARD BEAM GENERATOR

PATH ESTIMATOR FOR DRONE

METHOD AND SYSTEM FOR IDENTIFYING TOOLS