SAFRAN NACELLES

AIRFLOW EJECTOR NOZZLE HAVING A CONSTANT OUTLET CROSS-SECTION PROVIDED WITH A STREAM ADJUSTMENT DEVICE, AND TURBINE ENGINE PROVIDED WITH SUCH A NOZZLE

N° WO2025172658A1

ENSEMBLE DE GUIDAGE POUR UN ENSEMBLE PROPULSIF D’AERONEF

N° FR3158708A1

THRUST-REVERSAL SYSTEM FOR AN AIRCRAFT TURBOJET ENGINE, NACELLE AND PROPULSION UNIT COMPRISING SUCH A SYSTEM

N° WO2025133543A1

THRUST-REVERSAL SYSTEM FOR AN AIRCRAFT TURBOJET ENGINE, NACELLE AND PROPULSION ASSEMBLY INCLUDING SUCH A SYSTEM

N° WO2025133542A1

METHOD FOR MANUFACTURING A COMPOSITE PANEL

N° WO2025133540A1

ASSEMBLY COMPRISING A STATIONARY SURFACE AND A MOVABLE SURFACE OF AN AIRCRAFT

N° US2025236405A1

OPENING COWL FOR A TURBINE ENGINE

N° WO2025125757A1

METHOD FOR MANUFACTURING A MULTI-PERFORATED COMPOSITE ACOUSTIC SKIN WITHOUT MECHANICAL PIERCING

N° US2025178293A1

PROPULSION UNIT FOR AN AIRCRAFT

N° WO2025114660A1

SURFACE HEAT EXCHANGER COMPRISING A PRESSURE LOSS REDUCER AND AIRCRAFT NACELLE PROVIDED WITH SUCH A HEAT EXCHANGER

N° WO2025114662A1

HYDRAULIC CONTROL DEVICE FOR A THRUST REVERSER

N° WO2025109261A1

HYDRAULIC CONTROL DEVICE FOR A THRUST REVERSER

N° WO2025109262A1

AIR INTAKE FOR AN AIRCRAFT TURBOPROP AND METHOD FOR USING SAME WHEN THE AIRCRAFT IS ON THE GROUND

N° WO2025103988A1

THRUST REVERSER WITH SEALING MEMBRANE AND RETENTION SYSTEM

N° WO2025099398A1

ACOUSTIC PANEL FOR AN AIRCRAFT TURBINE ENGINE

N° WO2025104390A1

THRUST REVERSER COMPRISING AT LEAST ONE DEPLOYABLE MEMBRANE, AND A MEMBRANE-DEPLOYMENT MEMBER ARRANGED IN A CAVITY OF A MOBILE REVERSER COWL

N° WO2025099388A1

THRUST REVERSER COMPRISING AN IMPROVED SAFETY SYSTEM FOR DEPLOYING A MEMBRANE FOR SEALING OFF THE SECONDARY FLOW PATH

N° WO2025088267A1

AIRFLOW EJECTION NOZZLE WITH CONSTANT OUTLET SECTION AND TURBINE ENGINE EQUIPPED WITH SUCH A NOZZLE

N° WO2025078774A1

AIR FLOW EJECTOR NOZZLE WITH DETACHABLE INTERNAL STRUCTURE AND TURBINE ENGINE PROVIDED WITH SUCH A NOZZLE

N° WO2025078775A1

THRUST REVERSER COMPRISING AT LEAST ONE DEPLOYABLE MEMBRANE, HAVING LOW-MASS DEPLOYMENT MEANS

N° WO2025074063A1

DEVICE FOR HANDLING AN ELEMENT OF AN AIRCRAFT AND HANDLING ASSEMBLY PROVIDED WITH SUCH A DEVICE

N° WO2025068663A1

THRUST REVERSER COMPRISING AT LEAST ONE DEPLOYABLE DEFLECTION MEMBRANE WITH IMPROVED ATTACHMENT

N° WO2025068657A1

METHOD FOR MANUFACTURING AN OPEN PART WITH REINFORCED RIBS

N° WO2025052080A1

METHOD FOR PRODUCING A PART MADE OF COMPOSITE MATERIAL AND HAVING RAISED ELEMENTS, AND CORRESPONDING PART

N° WO2025052081A1

PROPULSION ASSEMBLY WITH LONGITUDINAL LOCKING OF AT LEAST ONE NACELLE COVER

N° WO2025052084A1

THRUST REVERSER COMPRISING AT LEAST ONE DEPLOYABLE DEFLECTION MEMBRANE HAVING A DESIGN THAT FACILITATES MAINTENANCE

N° WO2025052068A1

STRUCTURAL AND/OR ACOUSTIC PANEL OF A NACELLE OF AN AIRCRAFT PROPULSION ASSEMBLY AND RELATED MANUFACTURING METHOD

N° US2024391206A1

THRUST REVERSER GRILLE FOR AN AIRCRAFT NACELLE AND METHOD FOR PRODUCING SUCH A GRILLE

N° WO2025032298A1

CELLULAR STRUCTURE FOR AN ACOUSTIC PANEL

N° WO2025032296A1

machining device equipped with guiding means and method for producing an orifice with such a device

N° US2025001508A1

INSTALLATION FOR ASSEMBLING A CORE OF A PANEL, AND ASSOCIATED METHOD

N° WO2025003614A1

INSTALLATION FOR ASSEMBLING THE CORE OF A PANEL AND ASSOCIATED METHOD

N° WO2025003615A1

LOST-MOTION ACTUATING DEVICE FOR A THRUST REVERSER

N° WO2025003603A1

MULTIAXIAL FIBRE SHEET COMPRISING METAL ELEMENTS FOR PRODUCING A COMPOSITE MATERIAL PART

N° WO2024261428A1

AIR INTAKE MODULE FOR AN AIRCRAFT TURBOMACHINE AND METHOD FOR DE-ICING THEREOF

N° US2024425191A1

METHOD AND DEVICE FOR MACHINING AN AERONAUTICAL WORKPIECE

N° WO2024246473A1

AIR INLET OF AN AIRCRAFT TURBOMACHINE NACELLE, AND ASSOCIATED METHOD

N° WO2024245975A1

METHOD FOR MANUFACTURING AN AERODYNAMIC PANEL FOR AN AIRCRAFT PROPULSION ASSEMBLY

N° WO2024246452A1

METHOD FOR DEPOSITING A METAL COATING BY THERMAL SPRAYING AND MIXTURE FOR IMPLEMENTING SUCH A METHOD

N° WO2024241015A1

THRUST REVERSER COMPRISING AT LEAST ONE DEPLOYABLE DEFLECTING MEMBRANE

N° WO2024241010A1

THRUST REVERSER COMPRISING AT LEAST ONE DEPLOYABLE DEFLECTING MEMBRANE

N° WO2024241011A1

ACOUSTIC ATTENUATION STRUCTURE PROVIDED WITH S-SHAPED CELLS HAVING DRAINED BARRIERS AND METHOD FOR MANUFACTURING SAME

N° WO2024236244A1

PROPELLER OF AN AEROPLANE TURBINE ENGINE AND METHOD FOR DE-ICING SAME

N° WO2024231261A2

DEVICE FOR ATTACHING A HEAT SHIELD TO AN AIRCRAFT PANEL AND ASSOCIATED METHOD

N° WO2024236240A1

THRUST REVERSAL SYSTEM FOR AN AIRCRAFT, AND ASSOCIATED INSTALLATION AND AIRCRAFT

N° WO2024224025A1

IMPROVED SURFACE HEAT EXCHANGER FOR AN AIRCRAFT NACELLE

N° WO2024224023A1

ACOUSTIC PANEL FOR AN AIRCRAFT TURBOMACHINE

N° US2024351699A1

ACOUSTICALLY-TREATED AIR EJECTION NOZZLE FOR A NACELLE

N° US2024253804A1

ACOUSTIC PANEL FOR AN AIRCRAFT PROPULSION ASSEMBLY AND METHOD FOR PRODUCING SAME

N° WO2024200965A1

THRUST REVERSER RING FOR AN AIRCRAFT NACELLE THRUST REVERSER AND AIRCRAFT NACELLE

N° WO2024180302A1

THRUST REVERSER MODULE OF A THRUST REVERSER RING FOR AN AIRCRAFT NACELLE THRUST REVERSER

N° WO2024180303A1

CASCADE FOR A THRUST REVERSER COMPRISING BLADED STAGES CONNECTED BY THEIR CELLULAR STRUCTURES

N° WO2024175862A1

TUYERE D’EJECTION DE FLUX D’AIR A SECTION DE SORTIE CONSTANTE EQUIPEE D’UN DISPOSITIF DE REGLAGE DE VEINE ET TURBOMACHINE EQUIPEE D’UNE TELLE TUYERE.

N° FR3159200A1

THRUST REVERSER FOR AN AIRCRAFT TURBINE ENGINE COMPRISING MEANS FOR DEPLOYING AND RETRACTING, BY MEANS OF A CABLE, A DIAPHRAGM FOR CLOSING THE SECONDARY DUCT

N° WO2024165824A1

SYSTEME AMELIORE DE COMMANDE D’UN ENSEMBLE PROPULSIF POUR AERONEF

N° FR3158952A1

Injecteur pour dispositif de dégivrage d’une entrée d'air d'une nacelle de turbomachine d'aéronef et procédé associé

N° FR3158704A1

DEVICE FOR COUNTING A NUMBER OF MECHANICAL CYCLES PRODUCED BY A CYCLICALLY MOVING PART, AND ASSOCIATED METHODS AND AIRCRAFT

N° WO2024161081A1

DEVICE FOR DETECTING THE POSITION OF A MOBILE PART, AND ASSOCIATED METHOD AND AIRCRAFT

N° WO2024161080A1

TOOLING AND METHOD FOR MANUFACTURING APERTURED ELEMENTS SUCH AS THRUST REVERSER CASCADES FOR AN AIRCRAFT NACELLE

N° US2024367355A1

JET DEFLECTION MODULE FOR A THRUST REVERSER OF AN AIRCRAFT TURBINE ENGINE

N° WO2024153877A1

JET DEFLECTION MODULE FOR A THRUST REVERSER OF AN AIRCRAFT TURBINE ENGINE

N° WO2024153873A1

METHOD FOR MANUFACTURING AN AIRCRAFT ENGINE THRUST REVERSER CASCADE, AND CASCADE MANUFACTURED IN THIS WAY

N° WO2024141747A1

THRUST REVERSER CASCADE FOR AN AIRCRAFT ENGINE

N° WO2024141748A1

Système d’inversion de poussée pour turboréacteur d’aéronef, nacelle et ensemble propulsif comportant un tel système

N° FR3157475A1

Système d’inversion de poussée pour turboréacteur d’aéronef, nacelle et ensemble propulsif comportant une tel système

N° FR3157474A1

Procédé de fabrication d’un panneau composite

N° FR3157257A1

Ensemble comprenant une surface fixe et une surface mobile d’un aéronef.

N° FR3156758A1

Capot ouvrant pour turbomachine

N° FR3156757A1

MACHINING DEVICE AND METHOD FOR REPAIRING AN ANNULAR WORKPIECE

N° WO2024126947A2

THRUST REVERSER COMPRISING AN IMPROVED SYSTEM FOR DEPLOYING A MEMBRANE FOR SEALING OFF THE SECONDARY FLOW PATH

N° WO2024126934A1

OPTIMISED HONEYCOMB CORE AND ACOUSTIC ATTENUATION PANEL COMPRISING IT FOR AN AIRCRAFT TURBOMACHINE

N° US2024191655A1

TOOL FOR HANDLING AN INLET COWL OF AN AIRCRAFT TURBINE ENGINE

N° WO2024126921A1

COWL OF AN AIRCRAFT TURBINE ENGINE COMPRISING A CENTRAL GRIPPING INTERFACE

N° WO2024126920A1

Procédé de fabrication d’une peau acoustique composite multi-perforée sans perçage mécanique

N° FR3156059A1

ENSEMBLE PROPULSIF POUR UN AERONEF

N° FR3156169A1

METHOD FOR DETECTING AN ELECTRICAL FAULT IN A CABLE NETWORK OF A HARNESS AND ASSOCIATED DEVICE

N° WO2024115857A1

Procédé de montage de deux pièces l’une sur l’autre par matage sacrificiel et assemblage ainsi réalisé

N° FR3155869A1

Echangeur de chaleur surfacique comprenant un réducteur de pertes de charge et nacelle d’aéronef équipée d’un tel échangeur de chaleur

N° FR3155863A1

DISPOSITIF DE COMMANDE HYDRAULIQUE D’UN INVERSEUR DE POUSSEE

N° FR3155864A1

DISPOSITIF DE COMMANDE HYDRAULIQUE D’UN INVERSEUR DE POUSSEE

N° FR3155865A1

AIR INLET INTENDED TO BE CONNECTED TO A FAN CASING OF A TURBINE ENGINE BY A FLANGE-TYPE ASSEMBLY AND PROPULSION ASSEMBLY COMPRISING A TURBINE ENGINE EQUIPPED WITH SUCH AN AIR INLET

N° WO2024115839A1

PANNEAU ACOUSTIQUE POUR UNE TURBOMACHINE D’AERONEF

N° FR3155460A1

PROPULSION UNIT FOR AN AIRCRAFT

N° WO2024110720A1

PROPULSION UNIT FOR AN AIRCRAFT

N° WO2024110718A1

PROPULSION UNIT FOR AN AIRCRAFT

N° WO2024110719A1

Entrée d’air d’un turbopropulseur d’aéronef et son procédé d’utilisation lorsque l’aéronef est au sol

N° FR3155212A1

PROPULSION UNIT FOR AN AIRCRAFT

N° WO2024110717A1

THRUST REVERSER COMPRISING A SEALING MEMBRANE PROVIDED WITH A SEAL

N° WO2024105332A1

METHOD FOR DE-ICING A PART OF AN AIRCRAFT, COMPUTER PROGRAM AND CORRESPONDING SYSTEM, AIRCRAFT COMPRISING SUCH A SYSTEM

N° WO2024105334A1

Thrust reverser comprising sealing membrane provided with seal

N° CN120153168A

INVERSEUR DE POUSSEE COMPRENANT AU MOINS UNE MEMBRANE DEPLOYABLE, AINSI QU’UN ORGANE DE DEPLOIEMENT DE MEMBRANE AGENCE DANS UNE CAVITE D’UN CAPOT MOBILE D’INVERSEUR

N° FR3155266A1

INVERSEUR DE POUSSEE COMPRENANT UNE MEMBRANE D’OBTURATION DEPLOYABLE DANS UNE VEINE DE FLUX MELANGE

N° FR3155265A1

INVERSEUR DE POUSSEE A BIELLE DE DEPLOIEMENT DE MEMBRANE D’OBTURATION, INTEGREE AU CAPOT MOBILE DE L’INVERSEUR

N° FR3155264A1

Inverseur de poussée avec membrane d’obturation et système de retenue

N° FR3155267A1

STRUCTURE AERONAUTIQUE ANTI-FOUDRE

N° FR3154983A1

GEODESIC DRAPING METHOD

N° WO2024094946A1

THRUST REVERSER WITH IMPROVED RELIABILITY

N° WO2024094947A1

Reverse thrust device with improved reliability

N° CN120129784A

Geodesic line laying method

N° CN120152842A

TURBINE ENGINE GUIDE VANE INCORPORATING AN ELECTRICAL DISTRIBUTION DEVICE

N° WO2024089373A1