SAFRAN HELICOPTER ENGINES

METHOD FOR ASSISTING WITH PROPULSION BY DETECTING A FAILURE OF A TURBOSHAFT ENGINE OF AN AIRCRAFT

N° WO2025168907A1

SYSTEM FOR INJECTING HYDROGEN AND AIR

N° WO2025168900A1

PILOT ASSIST METHOD FOR MANAGING AT LEAST ONE CUMULATIVE AGEING PROCESS

N° WO2025168895A1

PILOTING ASSIST METHOD FOR MANAGING AT LEAST ONE CUMULATIVE AGEING PROCESS

N° WO2025168894A1

AIRCRAFT TURBINE ENGINE ASSEMBLY COMPRISING AN EMERGENCY DEVICE FOR THE MECHANICAL COUPLING OF TWO ROTATING PARTS OF THE ASSEMBLY

N° WO2025141269A1

METHOD FOR NITRIDING STEEL PARTS

N° EP4578989A1

PROCESS FOR THREE-DIMENSIONAL PRINTING WITH VARIABLE CROSS-SECTION

N° US2025121562A1

METHOD FOR QUANTIFYING BURNS GENERATED BY GRINDING A PART

N° WO2025133545A1

METHOD FOR CONTROLLING THE FUEL FLOW RATE OF A HELICOPTER TURBINE ENGINE

N° WO2025133516A1

METHOD FOR REALIGNING A PART WITH ITS DIGITAL TWIN USING A VISUAL MARKER

N° WO2025125755A1

RECOVERED-CYCLE AIRCRAFT TURBINE ENGINE

N° WO2025125743A1

STANDARD PART INTENDED TO BE SUBJECTED TO A NON-DESTRUCTIVE TEST

N° WO2025114677A1

TURBINE ENGINE FOR AN AIRCRAFT

N° WO2025120273A1

VENTURI DRAINAGE ASSEMBLY AND METHOD FOR A TURBINE ENGINE

N° WO2025114656A1

METHOD AND DEVICE FOR DYNAMICALLY CHARACTERIZING A BEAM OF RADIATION MOVING BETWEEN VARIOUS POINTS

N° WO2025104408A1

METHOD FOR COMPLETING THE FINISHING OF A COMPONENT PRODUCED BY DEPOSITING AND SOLIDIFYING SUCCESSIVE LAYERS OF A POWDER, AND COMPONENT OBTAINED BY THIS METHOD

N° WO2025099392A1

AIRCRAFT PROPULSION SYSTEM, AIRCRAFT AND HELICOPTER COMPRISING SUCH A PROPULSION SYSTEM AND METHOD FOR CONTROLLING A PROPULSION SYSTEM

N° WO2025074051A1

METHOD FOR MEASURING THE CRYSTAL MISORIENTATION OF A SINGLE-CRYSTAL BLADE

N° WO2025074049A1

VERTICAL AIRCRAFT TURBINE ENGINE DIFFUSER AND METHOD OF USE THEREOF

N° WO2025068046A1

HELICOPTER TURBINE ENGINE SUBASSEMBLY AND HELICOPTER TURBINE ENGINE COMPRISING SUCH A SUBASSEMBLY

N° WO2025062094A1

TRANSMISSION SYSTEM FOR AN AIRCRAFT PROPULSION UNIT HAVING THE CAPABILITY TO UNCOUPLE TWO ROTATING ELEMENTS BY MEANS OF THE FORCE PRODUCED BY HELICAL GEAR MESHING

N° WO2025056845A1

METHOD FOR CHARACTERISING A VIBRATIONAL DAMPING OF A CONTACT BETWEEN TWO PARTS

N° WO2025074047A1

ELECTRIC MACHINE CONTAINING DEVICE FOR COMPULSORY DEMAGNETIZING PERMANENT MAGNET

N° JP2024133183A

Dc-to-dc converter for an electrical aircraft propulsion system

N° IL314145A

CONTROL METHOD FOR DETECTING AT LEAST ONE DEFECT EMERGING FROM THE SURFACE OF A MECHANICAL PART FOR AN AIRCRAFT

N° EP4495585A1

AIRCRAFT PROPULSION ASSEMBLY AND THERMAL MANAGEMENT METHOD

N° WO2025012539A1

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

N° WO2025021441A1

LUBRICATION/COOLING SYSTEM FOR AN AIRCRAFT, AND HYDRAULIC ENCLOSURE

N° WO2025003607A1

TURBOMACHINE WITH PARALLEL ELECTRICAL HYBRIDIZATION

N° WO2024261430A1

METHOD FOR CONTROLLING AN AIRCRAFT PROPULSION SYSTEM HAVING TURBOSHAFT ENGINES OPERATING IN PARALLEL AND CAPABLE OF BEING PLACED ON STANDBY, AND CORRESPONDING AIRCRAFT

N° WO2025011898A1

AIRCRAFT PROPULSION ASSEMBLY COMPRISING A PROPULSION POWER TRANSMISSION SYSTEM WITH THE CAPACITY TO DECOUPLE TWO ROTATING ELEMENTS ACTUATED FROM THE INSIDE OF ONE OF THE ROTATING ELEMENTS

N° WO2024246450A1

IMPROVED PROPULSION ASSEMBLY FOR A MULTI-ENGINE HYBRID AIRCRAFT

N° WO2024236253A1

Fuel supply circuit of an aircraft engine

N° US2024295192A1

METAL POWDER FOR ADDITIVE MANUFACTURING METHOD

N° WO2024194589A1

METAL POWDER FOR ADDITIVE MANUFACTURING PROCESS

N° WO2024194588A1

METHOD AND SYSTEM FOR STARTING AN AERONAUTICAL TURBINE ENGINE HAVING A FREE TURBINE AND A SINGLE-SPOOL GAS GENERATOR

N° WO2024170855A1

METHOD AND SYSTEM FOR DUAL-VOLTAGE START OF AN AERONAUTICAL TURBINE ENGINE HAVING A FREE TURBINE AND A SINGLE-SPOOL GAS GENERATOR

N° WO2024170853A1

Procédé d’assistance à la propulsion par détection d’une défaillance d’un turbomoteur d’un aéronef

N° FR3159150A1

Système d’injection d’hydrogène et d’air

N° FR3158983A1

Procédé d’aide au pilotage pour la gestion d’au moins un vieillissement cumulatif

N° FR3158954A1

Procédé d’aide au pilotage pour la gestion d’au moins un vieillissement cumulatif

N° FR3159020A1

DEVICE FOR CENTRING AND ROTATIONALLY GUIDING A SHAFT LINE OF A TURBOMACHINE, AND TURBOMACHINE

N° WO2024165810A1

METHOD FOR ASSISTING THE PILOTING OF A ROTARY WING AIRCRAFT IN A FUEL-ECONOMY MODE

N° WO2024161091A1

METHOD AND SYSTEM FOR ASSISTING WITH THE PILOTING OF A ROTARY WING AIRCRAFT IN A FUEL ECONOMY MODE

N° WO2024161092A1

Vis à rupture détectable et procédés de détection et de fabrication associés

N° FR3158767A1

ASSEMBLY FOR AN AIRCRAFT PROPULSION ASSEMBLY WITH DISENGAGEABLE COUPLING OF TWO SHAFTS BY A COUPLING SLEEVE WITH PRESSURIZED-FLUID ACTUATION

N° WO2024161082A1

Dispositif de transmission amélioré pour aéronef hybridé et procédé de désengagement utilisant un tel dispositif

N° FR3158273A1

Procede de nitruration de pièces EN ACIER

N° FR3157873A1

ASSEMBLAGE POUR TURBOMACHINE D’AERONEF, COMPRENANT UN DISPOSITIF DE SECOURS DE COUPLAGE MECANIQUE DE DEUX PIECES TOURNANTES DE L’ASSEMBLAGE

N° FR3157891A1

ASSEMBLAGE POUR TURBOMACHINE D’AERONEF, COMPRENANT UN DISPOSITIF DE SECOURS DE COUPLAGE MECANIQUE DE DEUX PIECES TOURNANTES DE L’ASSEMBLAGE

N° FR3157893A1

ASSEMBLAGE POUR TURBOMACHINE D’AERONEF, COMPRENANT UN DISPOSITIF DE SECOURS DE COUPLAGE MECANIQUE DE DEUX PIECES TOURNANTES DE L’ASSEMBLAGE

N° FR3157892A1

ENSEMBLE PROPULSEUR HYBRIDE ELECTRIQUE POUR AERONEF

N° FR3157353A1

Procédé de contrôle du débit carburant d’une turbomachine d’hélicoptère

N° FR3157471A1

PROCÉDÉ DE QUANTIFICATION DES BRÛLURES GÉNÉRÉES PAR RECTIFICATION D’UNE PIÈCE

N° FR3157631A1

METHOD FOR MEASURING THE THERMAL HISTORY OF A PART

N° WO2024134103A1

ELECTRICAL SUPPLY CIRCUIT FOR A TURBINE ENGINE, TURBINE ENGINE AND AIRCRAFT COMPRISING SUCH A TURBINE ENGINE

N° WO2024134088A1

AUTOMATED CONTROL OF TURBINE ENGINES OF A ROTARY-WING AIRCRAFT DURING A FAILURE ON A TURBINE ENGINE

N° WO2024134086A1

Procédé de recalage d’une pièce avec son jumeau numérique à l’aide d’un marqueur visuel

N° FR3156905A1

TURBOMACHINE D’AERONEF A CYCLE RECUPERE

N° FR3156834A1

AIRCRAFT ELECTRIC OR HYBRID PROPULSION ARCHITECTURE

N° WO2024126944A1

TRANSFER OF POWER BETWEEN A HIGH-PRESSURE BODY AND A LOW-PRESSURE BODY OF AN AIRCRAFT TURBINE ENGINE

N° WO2024126933A1

METHOD AND SYSTEM FOR CONTROLLING THE PERMEABILITY OF A LUBRICATION CIRCUIT OF AN AIRCRAFT TURBOMACHINE

N° WO2024121289A1

Procédé d’estimation de durée de vie d’une pièce aéronautique de fabrication additive et un ensemble comprenant la pièce et une éprouvette

N° FR3156529A1

TURBOMACHINE POUR UN AERONEF

N° FR3156489A1

TURBINE ENGINE COMPRISING AN IMMOBILISING MAGNETIC COUPLING DEVICE

N° WO2024121495A1

Ensemble de drainage par effet Venturi pour turbomachine

N° FR3156162A1

Pièce étalon destinée à faire l’objet d’un contrôle non destructif

N° FR3156199A1

Procédé de vérification de pièces

N° FR3156200A1

Procédé de gestion de l’énergie d’un système propulsif hybride d’aéronef

N° FR3155813A1

IMPROVED HYBRID TURBOPROP ENGINE FOR AIRCRAFT

N° WO2024115842A1

METHOD FOR PROVIDING INFORMATION TO AN OPERATOR FOR MANAGING AT LEAST ONE CUMULATIVE AGEING PROCESS

N° WO2024110733A1

PROCEDE ET DISPOSITIF DE CARACTERISATION DYNAMIQUE D’UN FAISCEAU DE RAYONNEMENT SE DEPLAÇANT ENTRE DIFFERENTS POINTS

N° FR3155579A1

WIRELESS DATA COLLECTION SYSTEM

N° WO2024104853A1

WIRELESS DATA COLLECTION SYSTEM

N° WO2024104852A1

PROCÉDÉ DE PARACHEVEMENT D’UNE PIÈCE REALISEE PAR DÉPÔT ET SOLIDIFICATION DE COUCHES SUCCESSIVES D’UNE POUDRE ET PIECE OBTENUE PAR CE PROCEDE

N° FR3154935A1

DEVICE FOR SUSPENDING AN EQUIPMENT ITEM FOR A TURBOMACHINE ON A TURBOMACHINE ENGINE STRUCTURE

N° WO2024089345A1

Device for suspending turbine equipment item from turbine engine structure

N° CN120077192A

Turbine equipped with heat exchanger and having recovery cycle

N° CN120077194A

TURBOMACHINE WITH RECUPERATION CYCLE EQUIPPED WITH A HEAT EXCHANGER

N° WO2024084150A1

Éprouvette d’essai et dispositif pour la caractérisation d’un amortissement vibratoire d’un contact entre deux pièces

N° FR3153891A1

Procédé de mesure de désorientation cristalline d’une aube monocristalline

N° FR3153892A1

SYSTÈME DE PROPULSION D’UN AÉRONEF, AERONEF ET HELICOPTERE COMPORTANT UN TEL SYSTÈME DE PROPULSION ET PROCEDE DE COMMANDE D’UN SYSTÈME DE PROPULSION

N° FR3153598A1

Diffuseur de turbomachine d’aéronef verticale et son procédé d’utilisation

N° FR3153637A1

DEVICE FOR MEASURING THE ROTATIONAL SPEED OF AN AIRCRAFT PROPELLER

N° EP4594760A1

DEVICE FOR MEASURING THE ROTATIONAL SPEED OF AN AIRCRAFT PROPELLER

N° WO2024069095A1

Device for measuring rotational speed of propeller of aircraft

N° CN120035764A

Sous-ensemble de turbomachine d’hélicoptère et turbomachine d’hélicoptère comprenant un tel sous-ensemble

N° FR3153109A1

Système de transmission pour ensemble propulsif d’aéronef à capacité de découplage de deux éléments tournants au moyen de l’effort produit par un engrènement hélicoïdal

N° FR3153117A1

METHOD FOR CALIBRATING A MODEL FOR ESTIMATING A TORQUE SUPPLIED BY AN ELECTRIC MACHINE

N° EP4587805A1

Chambre de combustion

N° FR3152863A1

METHOD FOR CALIBRATING A MODEL FOR ESTIMATING A TORQUE SUPPLIED BY AN ELECTRIC MACHINE

N° WO2024056971A1

Method for calibrating model for estimating torque provided by electric machine

N° CN120035751A

METHOD FOR MANAGING THE OUTPUT OF A SPECIFIC-CONSUMPTION MODE OF AN AIRCRAFT TURBINE ENGINE

N° EP4569210A1

Method for assisting propulsion by detecting failure of aircraft turboshaft engine

N° CN119654476A

Method for managing exit of specific consumption mode of aircraft turbine engine

N° CN119677937A

METHOD FOR MANAGING THE OUTPUT OF A SPECIFIC-CONSUMPTION MODE OF AN AIRCRAFT TURBINE ENGINE

N° WO2024033593A1

METHOD FOR ASSISTING WITH PROPULSION BY DETECTING A FAILURE OF A TURBOSHAFT ENGINE OF AN AIRCRAFT

N° EP4569208A1

METHOD FOR ASSISTING WITH PROPULSION BY DETECTING A FAILURE OF A TURBOSHAFT ENGINE OF AN AIRCRAFT

N° WO2024033594A1

RECOVERED-CYCLE AIRCRAFT TURBINE ENGINE

N° WO2024033588A1

RECOVERED-CYCLE AIRCRAFT TURBINE ENGINE

N° EP4569213A1