APPARATUS FOR INGESTING BOUNDARY LAYER FLOW FOR AN AIRCRAFT

OPTIMIZED SOUND ATTENUATION PANEL FOR AN AIRCRAFT TURBOMACHINE

IMPROVED SURFACE HEAT EXCHANGER FOR AN AIRCRAFT NACELLE

NACELLE FOR AN AIRCRAFT ENGINE

MOUNTING STRUCTURE FOR NACELLE INNER STRUCTURE

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

SURFACE HEAT EXCHANGER FOR A NACELLE OF A TURBINE ENGINE, AND TURBINE ENGINE NACELLE EQUIPPED WITH SUCH A HEAT EXCHANGER

AIRCRAFT PROPULSION ASSEMBLY COMPRISING AN IMPROVED COWLING PANEL

COWL OF AN AIRCRAFT TURBINE ENGINE COMPRISING A CENTRAL GRIPPING INTERFACE

BLOCKER DOOR FOR AN AIRCRAFT THRUST REVERSER

Battery Storage System for an Aircraft

THERMAL MANAGEMENT ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM

THRUST REVERSER COMPRISING A SIMPLIFIED-DEPLOYMENT OBTURATOR MEMBRANE

FAIRING WITH AIR INLET DEVICE FOR AN AIRCRAFT, METHOD OF MAKING SAME, AND AIRCRAFT

COOLING OF GAS FLOWING OVER AIRCRAFT STRUCTURE

ELECTRIC PROPULSION SYSTEMS

ACOUSTICALLY TREATED THRUST REVERSER BULLNOSE FAIRING AND TORQUE BOX

PROPULSION ASSEMBLY FOR AN AIRCRAFT, HAVING AN EXTRACTION FAN

PROPULSION ASSEMBLY FOR AN AIRCRAFT, COMPRISING AN INTERMEDIATE COWL OF THE STATIONARY, REMOVABLE TYPE, MOUNTED ON A HINGE SYSTEM

AIRCRAFT NACELLE PROVIDED WITH AT LEAST ONE THRUST REVERSAL DEVICE COMPRISING AT LEAST ONE LONGITUDINAL DEFLECTOR, AIRCRAFT COMPRISING AT LEAST ONE PROPULSION ASSEMBLY COMPOSED OF SUCH A NACELLE

Ultra-Quiet Aircraft

INTEGRATING AN EXTINGUISHER INTO A "FIRE" ZONE OF A TURBOMACHINE

SEGMENTED NACELLE INLET LIP WITH ELECTRIC ANTI-ICING SYSTEM

LOSS OF LOAD PATH DETECTION SYSTEM FOR AIRCRAFT PROPULSION SYSTEM NACELLE AND METHOD FOR USING SAME

Ram filter purge system

APPARATUS FOR REMOVING MAGNETIC FOREIGN MATTER, BRUSHLESS MOTOR, AND PROPULSION MACHINE

Aircraft duct assembly and sealing structure

METHOD FOR PRODUCING A PERFORATED NACELLE INLET ASSEMBLY

Heat exchanger assembly for an aircraft

INLET AIR MANAGEMENT SYSTEM

HYBRID ELECTRIC ENGINE AND NACELLE SYSTEM

ACOUSTICALLY-TREATED AIR EJECTION NOZZLE FOR A NACELLE

Apparatus for ingesting boundary layer flow for an aircraft

HYBRID AIRCRAFT PROPULSION SYSTEM WITH REMOTELY LOCATED ELECTRIC MACHINE

AIRCRAFT THERMAL ANTI-ICING SYSTEM

HYBRID MANDREL FOR USE IN TOOLING METHODS AND THE MANUFACTURE OF THRUST REVERSER CASCADES AND STRUCTURES SUSCEPTIBLE TO TRAPPED TOOLING

Acoustic attenuation structures

Battery Storage System for an Aircraft

Exhaust nozzle assembly for an aircraft propulsion system

Propulsion system with downstream section having deformable shape-memory material and actuators extending in different consecutive angular sectors

VEHICLE COMPONENT WITH INTEGRATED ENGINE SUPPORT STRUCTURE AND BODY SECTION

ICE PROTECTION SYSTEMS FOR AIRCRAFT FUELED BY HYDROGEN

Nacelle of an aircraft engine, comprising an improved heat exchanger

Method for producing a perforated nacelle inlet assembly

Aircraft fluid ice protection system

Ultra-quiet aircraft

NACELLE AIR INTAKE FOR AN AIRCRAFT PROPULSION ASSEMBLY TO PROMOTE A THRUST REVERSAL PHASE

AIRCRAFT POWERPLANT WITH BOOSTED GAS TURBINE ENGINE

Adjusting aircraft powerplant power split to control powerplant vibrations

Aircraft equipped with at least one pressure-relief device including a mobile wall retained in a closed position

THERMAL MANAGEMENT SYSTEM FOR AN AIRCRAFT INCLUDING AN ELECTRIC PROPULSION ENGINE

Assembly for a turbomachine

Nacelle inlet structure fitting with locator clip and hoist bracket

SYSTEM FOR A VERTICAL TAKEOFF AND LANDING AIRCRAFT WITH AN IN-BOOM LIFT PROPULSOR

Ice protection systems for aircraft

Thrust reverser having three gates

Combustion engine including turbomachine

Propulsion unit with foldable propeller blades and method for folding the blades

Electric motor nacelle for a vertical take-off and landing aircraft and aircraft comprising such a nacelle

PROPULSION UNIT WITH FOLDABLE PROPELLER BLADES AND METHOD FOR FOLDING THE BLADES

FIREWALL ASSEMBLIES FOR HYBRID ELECTRIC AIRCRAFT POWERPLANTS

Aircraft nacelle inlet

System for a vertical takeoff and landing aircraft with an in-boom lift propulsor

AIRCRAFT NOISE CONTROL

Propulsion system for an aircraft

Aircraft nacelle comprising a connection between ducts comprising flanges which are oriented towards the interior, and aircraft comprising at least one nacelle of this type

Methods involving and apparatuses for a turbine engine fairing

INTEGRATED ELECTRIC MOTOR AND THERMAL MANAGEMENT SYSTEM

Jam detection and jam tolerant motion control

FILLING AN AIRCRAFT TURBINE ENGINE LUBRICANT TANK

Thermal management system for gas turbine engine

Nacelle air outlet for aircraft turbojet engine comprising a straightening device for facilitating a reverse thrust phase

Convertiplane

Convertiplane

Electric connection of an electric machine in an aircraft turbomachine

Microwave thermal anti-icing system for aircraft acoustic structure

Integrated microwave thermal anti-icing system

Aircraft energy storage mounting system

Means for handling gaseous fuel

Method for manufacturing a cellular structure obtained from bent strips of material, and cellular structure thus obtained

Vertical take-off and landing cocoon-type flying vehicle

Noise attenuation in an engine nacelle

Electric propulsion system of an aircraft

Aircraft pylon comprising a tubular primary structure including at least one twin-walled pipe, and aircraft comprising at least one such pylon

Fiber-reinforced aircraft component and aircraft comprising same

AIR INTAKE LIP OF AN AIRCRAFT ENGINE NACELLE, COMPRISING AT LEAST ONE INFRARED EMISSION SOURCE

AIR INTAKE LIP OF A TURBOMACHINE NACELLE COMPRISING AN ACOUSTIC DEVICE AND METHOD FOR PRODUCING SUCH A LIP

Attachable acoustic panels and method of making same

AIRCRAFT ENGINE PYLON AFT AERODYNAMIC FAIRING

Resistive skin shell incorporating perforated metal bands, and acoustic inner wall of an aircraft air intake formed from such resistive skin shells

Assembly for an aircraft having a pylon and a nacelle comprising a visor fitted with tensioning systems and centering systems

Aircraft seal

Combustion engine including turbomachine

Combustion engine including turbomachine

Gas turbine engine nacelle and method of designing same

Method for manufacturing a soundproofing assembly having two superposed panels

Aircraft turbofan having a cowl articulated in rotation and a system for deploying said cowl

Method for manufacturing an acoustic panel having a capsular skin, and acoustic panel incorporating such a skin

Acoustic attenuation structures

Nacelle

UNIVERSAL VEHICLE WITH IMPROVED STABILITY FOR SAFE OPERATION IN AIR, WATER AND TERRAIN ENVIRONMENTS

Strip-form acoustic material having an integrated flange, and internal wall of an aircraft air intake made with this material

Electric aircraft propulsion system

Cellular sound insulation structure including a diaphragm provided with a tube configured to treat different acoustic frequencies, method for manufacturing such a cellular sound insulation structure, and associated tool

Method for producing an alveolar soundproofing structure including a diaphragm, and alveolar soundproofing structure obtained

Apparatus and method for configuring control message in broadcasting system

Inlet air management system

EXTERNAL AUXILIARY POWER UNIT

Transpirationally cooled exhaust center body for an aircraft propulsion system

Aircraft anti-icing system

HYBRID MANDREL FOR USE IN TOOLING METHODS AND THE MANUFACTURE OF THRUST REVERSER CASCADES AND STRUCTURES SUSCEPTIBLE TO TRAPPED TOOLING

Locking linear actuator

Multifrequency absorption acoustic panel for an aircraft nacelle

Variable seal for an engine nacelle

Composite structural panels and methods of forming thereof

Sealing arrangement between two ring-shaped walls of an aircraft engine

AFT ENGINE PYLON FAIRING OF AN AIRCRAFT WITH MULTILAYER HEAT SHIELD

Firewall assemblies for hybrid electric aircraft powerplants

Aircraft part anti-icing treatment method

THERMAL ANTI-ICING SYSTEM WITH MICROWAVE SYSTEM

Blade fragment barrier for aircraft engine inlet cowl

Aircraft with linear thruster arrangement

Anterior part of the nacelle of an aircraft propulsion assembly whose air intake lip is linked to the outer panel by nesting

Dual hybrid propulsion system for an aircraft having a cross-connecting clutch

Passive internal compartment exhaust for an aircraft propulsion system

Nacelle cowl deflection limiter

Three actuator cascade type thrust reverser actuation system

Fire seal assembly for nacelle doors

Electrical generation from turbine engines

Acoustic damper

Anterior part of a nacelle of an aircraft propulsion system having a shield in front of its rigidifying frame

Fiber-reinforced aircraft component and aircraft comprising same

Nacelle

Nacelle with a translatable inlet for an aircraft propulsion system

Aircraft nacelles having adjustable chines

Aircraft nacelles having adjustable chines

AIRCRAFT NACELLES HAVING ADJUSTABLE CHINES

Pressure relief latch

Propulsion system for an aircraft

Method and apparatus for aircraft anti-icing

Anti-ice pulsed jet hiller reactor

Method and apparatus for aircraft anti-icing

Modular arrangement of a converter and aircraft having a modular arrangement

Aircraft engine nacelle

Method for manufacturing a structural and/or acoustic panel for a nacelle of an aircraft propulsion unit, and corresponding device

Deployable noise shield panels

Fastening device for a heat-shield panel

Torque ripple control for an aircraft power train

Engine layouts and associated compartmentalization for aircraft having hybrid-electric propulsion system

Method and apparatus for forming a nacelle leading edge

System of harness and engine case for aircraft engine

Gas turbine engine and method to cool a gas turbine engine case assembly

Stretch forming method for a sheet metal skin with convex and concave curvatures

Thermal Management System for an Aircraft Including an Electric Propulsion Engine

Method for manufacturing a preform for composite materials

Thermal management system for gas turbine engine

Method for manufacturing an acoustic element of a sound absorption structure from at least one sheet of material

NACELLE INLET AND SYSTEM AND METHOD FOR MAKING SAME

Surface trim for acoustic absorption

Method of manufacturing composite laminate panel sub-elements for a modular assembly structure, a method of assembling the sub-elements, and a structure assembled of the panel sub-elements

COLD NOZZLE OPTIMISATION

Aircraft engine nacelle comprising a system of ice protection

Aircraft engine nacelle comprising an anti-icing protection system

Active laminar flow control plenum panel arrangements and installation methods

Active laminar flow control plenum panel arrangement

Active laminar flow control structural plenums fastened

Inlet deep cavity flutter liner

Composite part with smooth outer face and manufacturing method thereof

Air intake structure of an aircraft nacelle

NACELLE FOR AN AIRCRAFT ENGINE INCLUDING MEANS PREVENTING THE DEFORMATION OF THE ARTICULATED FAN COVERS

Method for separated flow detection

Sound-absorbing panel with a cellular core and a de-icing system

Multi-degree of freedom acoustic panel

Method of manufacturing a panel for an aircraft propulsion unit nacelle

Additive manufacturing process of a part for an aircraft propulsion unit nacelle

Turbine engine assembly and method of manufacturing thereof

Aircraft propulsion assembly comprising air-liquid heat exchangers

Systems and methods of optimizing cooling and providing useful heating from single phase and two phase heat management in propulsion systems

Nacelle inlet lip fuse structure

Jet engine comprising a nacelle equipped with reverser flaps provided with vortex-generating means

Nacelle system and methods of operation

Engine enclosure air inlet section

Active laminar flow control system with composite panel

Acoustic panel for thrust reversers

AERODYNAMIC AIRCRAFT WALL COMPRISING AT LEAST ONE VORTEX GENERATOR, AND AIRCRAFT COMPRISING THE SAID AERODYNAMIC WALL

Machine vision acoustic panel repair with retention of acoustic properties

ADJUSTMENT FEATURES FOR ENGINE COWL DOOR

Aircraft jet engine nacelle, propulsion assembly and aircraft comprising such a nacelle

Cooling system for heat generating components in a fairing

Aircraft engine nacelle provided with an icing protection system and associated protection method

Structured panel with structural reinforcement(s)

HYBRID MANDREL

Tooling for forming nacelle components

Aircraft propulsion assembly comprising two adjacent engines, of which the outlet nozzles have a straight portion in the vicinity of a median plane of the propulsion assembly

ACTIVE COOLING SYSTEM

Integrated drain mast structure

Metal and composite leading edge assemblies

Inlet assembly for an aircraft aft fan

Thermoplastic particle-toughened prepreg for use in making composite parts which tolerate hot and wet conditions

Prepreg for use in making composite parts which tolerate hot and wet conditions

Air intake systems and methods of assembly thereof

Anterior part of a nacelle of an aircraft propulsion unit having a shock absorbing element

Method for spin forming lipskins

Fairings for power generation machines

Method for manufacturing a preform for composite materials

Acoustic attenuation panel for an aircraft propulsion unit and propulsion unit including such a panel

Actuator assembly having self-lubricating components

Hydraulic piston actuator for a door

Seal system for variable geometry gaps in aircraft systems

System for monitoring an aircraft device

Integrated heat management for hybrid propulsion

Frost protection system for an aircraft engine nacelle

Aircraft anti-icing system

Locating an aperture based on a signature of an embedded conductive element

Non-metallic engine case inlet compression seal for a gas turbine engine

MANUFACTURING A SHAPED STRUCTURAL PANEL WITH A MANDREL AND A PRESSURE VESSEL

Acoustic device manufacturing system

Acoustic liner having internal structure

Active system generating destructive acoustic interference for an aircraft engine with multiple fan spools

Baseless vortex generator

Three actuator cascade type thrust reverser actuation system

Structural panel with splice joint between adjacent core structures

Fairing integrating with outer mold line and protective portions

Nacelle

Nacelle

Cooling system for rotor blade actuators

Convergent divergent exit nozzle for a gas turbine engine

STRUCTURAL ELEMENT OF AN AIRCRAFT PART AND METHOD FOR MANUFACTURING A STRUCTURAL ELEMENT

Jet engine with deflector

AIRCRAFT ENGINE HAVING AT LEAST ONE REVERSE THRUST SYSTEM ACTUATOR ARRANGED IN A GAS EXHAUST CONE

Single-piece extended laminar flow inlet lipskin

Strake for aircraft propulsion system nacelle

Kevlar wrap removal from fan casing

Bird-strike energy absorbing net

Method of manufacturing a composite sandwich panel for an aircraft propulsion unit

Metal fire seals system for aircraft engine mount

Aerodynamic drainage device

Gas turbine engine

Turbomachine cowling with screen

Composite material part

Hybrid propulsion drive train system for tiltrotor aircraft

Acoustic liner and method of forming an acoustic liner

Universal vehicle with improved stability for safe operation in air, water and terrain environments

Heat exchanger assembly for a gas turbine engine propulsion system

AIR INTAKE STRUCTURE FOR AN AIRCRAFT NACELLE

Method for forming a structural panel

FILAMENT WINDING PROCESS FOR FILLETS

SUPERSONIC TURBOFAN ENGINE

Flexible band electrical component mounts and methods

Aircraft drive device and aircraft provided with a drive device

VTOL aircraft with jet engine coupled to downward thrust nozzles

Aircraft fire seal structure and aircraft

Liner assembly, engine housing, and methods of assembling the same

Aircraft nacelle anti-ice systems and methods

Aircraft seal structure and aircraft

Aircraft fire seal structure and aircraft

Acoustic attenuation structure with a plurality of attenuation degrees for a propulsion assembly of an aircraft

Monolithic lipskin and method of fabrication

Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system

Aircraft nacelle including a link between a conduit of an air inlet and a conduit of an engine

Accessory gearbox for a gas turbine engine

Embedded aircraft heater repair

Locking device for pivoting cowls of a thrust reverser

Method for manufacturing of at least one part of an engine component by means of a blank of intumescent material

Supplemental cooling air for turbine exhaust components and surfaces

Drone with magnet fluid sealed bearing unit and drive motor having the bearing unit

Compression molding assembly and methods for molding a thermoplastic blocker door

Thermal management system for an electric propulsion engine

Inlet guide vane assembly for reducing airflow swirl distortion of an aircraft aft fan

Inlet assembly for an aircraft aft fan

Inlet assembly for an aircraft aft fan

Systems and methods for restraining exhaust gas ducts

DRAG REDUCING LINER ASSEMBLY AND METHODS OF ASSEMBLING THE SAME

Sliding fastener systems to accommodate differential thermal growth

Sandwich panel disbond repair

NACELLE AND METHOD FOR INFLUENCING FLUID FLOWS IN A NACELLE

Laser Projected Engine Hazard Zone Systems And Methods

Runback control

Antenna diagnostics for wireless communication unit for communicating engine data

Wireless aircraft engine communication system

Wireless aircraft engine monitoring system

Gas turbine engine and method to cool a gas turbine engine case assembly

Thermal insulation blanket and thermal insulation blanket assembly

Aircraft with injection cooling system and injection cooling system

Fence for duct tone mitigation

Electrical assist for aircraft

Kinetic energy absorption device and aircraft comprising such a device

Panel and insert for corner radii

Acoustic attenuation panel for a turbojet engine nacelle

Bulb seal and spring

Automatic deflection limiting latches for a thrust reverser

Engine bleed system with multi-tap bleed array

THERMAL MANAGEMENT SYSTEM FOR DEICING AIRCRAFT WITH TEMPERATURE BASED FLOW RESTRICTOR

High offset hook latch

Tandem thrust reverser with sliding rails

Structural, cellular core with corrugated support walls

Thrust reverser compression rod with spring biased engagement

Pawl latch

Nozzle and vane system for nacelle anti-icing