SANDWICH STRUCTURES INCLUDING HYBRID ADHESIVES AND METHODS THEREOF

Leading-Edge Ducted Fan Thrust Reduction System

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

PROPULSION ASSEMBLY FOR AN AIRCRAFT

Low Drag Nacelle and Pylon Fairing

Rotor deployment mechanism for vertical take-off and landing aircraft

AIRCRAFT FAIRING HAVING A REMOVABLE PANEL AND A COMPRESSIBLE SEAL, AIRCRAFT HAVING AT LEAST ONE SUCH FAIRING

NOZZLE ASSEMBLY FOR USE WITH A PROPULSION SYSTEM AND SLEEVE ASSEMBLY FOR USE WITH THE NOZZLE ASSEMBLY

Propulsion system

Lift nacelle

AIR GUIDANCE DEVICE OF A VERTICAL TAKE-OFF AND LANDING AIRCRAFT, AND VERTICAL TAKE-OFF AND LANDING AIRCRAFT

NACELLE DEVICE AND VTOL AIRCRAFT

CURVED STIFFENER FOR A TURBINE ENGINE NACELLE AND METHOD FOR PRODUCING SUCH A STIFFENER

Nozzle assembly for use with a propulsion system

TELESCOPIC ASSEMBLY WITH LOCKING DEVICE IN RETRACTED CONFIGURATION

METHOD FOR MOUNTING A VORTEX GENERATOR ON A CURVED AERODYNAMIC PANEL OF AN AIRCRAFT AND AIRCRAFT COMPRISING AT LEAST ONE VORTEX GENERATOR MOUNTED IN THIS WAY

Aviation turbofan engine and fan duct nozzle

PROPULSION ASSEMBLY FOR AN AIRCRAFT COMPRISING A STATOR VANE INTEGRATED INTO AN UPSTREAM PART OF A MOUNTING PYLON OF REDUCED HEIGHT

SELF-CLEANING EXTERNAL LAYER COMPRISING A SELF-CLEANING AERODYNAMIC SURFACE, AND VEHICLE COMPRISING SAID EXTERNAL LAYER

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

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

SYSTEMS AND METHODS FOR MODULAR AIRCRAFT

METHOD FOR MANUFACTURING AN AEROSPACE AND/OR AERONAUTIC TUBULAR COMPOSITE PART AND SUCH A COMPOSITE PART

Rotary wing aircraft

PROPULSION ASSEMBLY FOR AN AIRCRAFT, COMPRISING A LOAD BEARER

AIRCRAFT PROPULSION ASSEMBLY COMPRISING AT LEAST ONE DEVICE FOR CLEANING A NACELLE AIR INTAKE BY SPRAYING A CLEANING LIQUID

Articulated electric propulsion system and lightweight vertical take-off and landing aircraft using same

Systems and methods for modular aircraft

Lift nacelle

Winged tiltrotor aircraft

Method for manufacturing an acoustic absorption structure, and acoustic absorption structure obtained in this way

Nacelle inlet with horizontal droop (NIHD)

System with locking indicator for a nacelle element, comprising a removable key for locking and controlling the indicator

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

Adaptive ducted fan propulsion system

De-icing device for an air intake of an aircraft turbojet engine nacelle

Gas turbine engine mounted above wing and with camber

GAS TURBINE ENGINE MOUNTED ABOVE WING AND WITH CAMBER

Propulsion system for an aircraft

System and method for supplying passively filtered ram air to a hydrogen fuel cell of a UAV

Expandable cellular system for a sandwich panel

System for verifying turbojet engine parts using radio frequency identification, comprising an integrated antenna

Aircraft engine nacelle with an aft end major axis substantially parallel to the leading edge of a wing

Aircraft with electrical energy storage in nacelles

Articulated Electric Propulsion System With Fully Stowing Blades And Lightweight Vertical Take-Off And Landing Aircraft Using Same

Method for manufacturing a composite preform for the manufacture of a composite panel with double curvature geometry

Electric aircraft propulsion system

Nacelle for an aircraft aft fan

Acoustic attenuation panel for an aircraft jet engine nacelle

Movable cover for a proprotor nacelle

Redundant propulsion device and electric aircraft

Inlet bulkheads for large diameter aircraft engines

Bypass propulsion unit, comprising a thrust reverser with movable cascades

Profiled structure and associated turbomachine

Axial flow ducted fan with a movable section

MACHINABLE MOLDED FRETTING BUFFER

Propulsion unit including lifting points disposed on thrust reverser cylinder supports

Aircraft nacelles having adjustable chines

Aircraft nacelles having adjustable chines

Aircraft nacelles having adjustable chines

Aircraft nacelles having adjustable chines

Aircraft nacelles having adjustable chines

Aircraft nacelles having adjustable chines

Acoustic treatment structure for an aircraft propulsion unit nacelle

Aircraft nacelle having electric motor and thrust reversing air exhaust flaps

Propulsion system for an aircraft

Air inflow lip for turbojet nacelle

Lift nacelle

Modulated fire extinguishing vent for a gas turbine engine

ACOUSTIC PANEL FOR AN AIRCRAFT TURBOJET NACELLE, AND METHOD FOR MANUFACTURING AN ELEMENT OF A NACELLE

Fastening device for a heat-shield panel

Propulsion unit for aircraft

Aircraft wing assemblies

Propulsive assembly of an aircraft comprising a junction fairing between a nacelle and a pylon of the aircraft equipped with a removable cowl and aircraft equipped with said propulsive assembly

Wing-nacelle splice assemblies for tiltrotor aircraft

Cell structure and acoustic attenuation device for a nacelle of an aircraft propulsion assembly

Aerodynamic nacelle strakes as axial locator

Method for manufacturing a preform for composite materials

Boundary layer ingestion fan system

Boundary layer ingestion fan system

Fireproof pressure relief assembly

NACELLE INTAKE

Articulated electric propulsion system with fully stowing blades and lightweight vertical take-off and landing aircraft using same

AIRCRAFT JET ENGINE COMPRISING MEANS FOR VARYING ITS OUTPUT SURFACE AREA

Aircraft propulsion unit and process for reducing a ventilation air flow in the aircraft propulsion unit

Air intake, nacelle and propulsion unit for monobloc sector aircraft

Nacelle of an aircraft propulsion assembly comprising a plurality of damper elements between a front section and a main section, and associated aircraft propulsion assembly

Articulated electric propulsion system with fully stowing blades and lightweight vertical take-off and landing aircraft using same

Movable cover for a proprotor nacelle

Aircraft nacelle with rotary fan cowling incorporating an access hatch

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

Front fairing of an aircraft pylon comprising a mobile shroud and aircraft equipped with said front fairing

Air inlet with integrated fluid diverter

THREE-DIMENSIONAL METAL INSULATING PART

VERTICAL TAKE-OFF AND LANDING AIRCRAFT

Engine nacelle for an aircraft

Nacelle forward part of a propulsion assembly comprising an inclined stiffening frame

Method for manufacturing a preform for composite materials

Aircraft comprising at least one engine assembly linked to the fuselage of the aircraft by two connecting rods positioned at least partially in an air inlet of the engine assembly

TRI-ROTOR TAILSITTER AIRCRAFT

Mechanisms, systems and methods to allow step-ajdustment of aerodynamic surfaces

Wing-nacelle splice assemblies for tiltrotor aircraft

Dual-flow jet engine for an aircraft with an improved aperture

LAMINAR FLOW COATING FOR AERODYNAMIC SURFACES

High-mounted aircraft nacelle

Baseless vortex generator

Fairing integrating with outer mold line and protective portions

Two position cowling assembly for single person operation

Stall recovery chine spoiler system

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

Tiltrotor aircraft having rotatable wing extensions

Tiltrotor aircraft rotating proprotor assembly

METHOD FOR OBTAINING A POROUS ACOUSTIC LAYER AND POROUS ACOUSTIC LAYER THUS OBTAINED

Sealing cooling inner fixed structure

Aircraft seal structure and aircraft

Aircraft fire seal structure and aircraft

High temperature seals for blanketless inner fixed structure

Composite fan cowl having core with varying thickness

Self-locking alignment at a nacelle interface

Aircraft

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

Translating nacelle wall for an aircraft tail mounted fan section

Locking device for pivoting cowls of a thrust reverser

Storage models for tiltrotor aircraft

Storage modes for tiltrotor aircraft

Storage modes for tiltrotor aircraft

Tiltrotor aircraft having rotatable wing extensions

Tiltrotor aircraft having active wing extensions

Inlet duct selector for tiltrotor barrier filter

NACELLE AND METHOD FOR INFLUENCING FLUID FLOWS IN A NACELLE

Wireless aircraft engine communication system

Wireless aircraft engine monitoring system

Stabilizer assembly for an aircraft AFT engine

Delta fuselage for vertical take-off and landing (VTOL) aircraft

Nacelle deflection measurement assembly

Aircraft, aircraft engine, and aircraft engine nacelle

Flow drag mitigation device

Air intake turboprop assemblies

Cylindrical case and jet engine

Variable-geometry ducted fan

Methods and systems for applying aerodynamically functional coatings to a surface

Aircraft propulsion system having at least one anti-fire tank

Gas turbine engine cover

Synergetic noise absorption and anti-icing for aircrafts

Pressure relief door assembly

Krueger flap assembly systems and methods

Aircraft external part with inflatable panels

Aircraft propulsion assembly with fire extinguishing system

Pylon with noise attenuating fairing

USE OF A CODE FOR MARKING A NACELLE

Aircraft nacelle comprising at least one fan cowl door which is mounted so as to be able to rotate about the longitudinal axis of the nacelle

Gas turbine engine accessory architecture

Optimized nacelle profile and plenum shape for boundary layer ingestion active laminar flow control

Articulated electric propulsion system with fully stowing blades and lightweight vertical take-off and landing aircraft using same

NOSE CONE STRUCTURE FOR PYLON OF AIRCRAFT WITH WING-HUNG LAYOUT

Nacelle for an aircraft engine assembly comprising at least one jointed nacelle cowling at its front end

INNER FIXED STRUCTURE ACOUSTIC PANEL WITH DIRECTIONAL PERFORATIONS

Airplane suspension cowling structure with wing-mounted arrangement

Aircraft battery containment pods

Perforated surface for suction-type laminar flow control

Methods and apparatus for supporting engines and nacelles relative to aircraft wings

Aircraft with a nacelle-housed main landing gear

Foldable guiding ventilator cover for an aircraft engine assembly

AFT pylon fairing for aircraft

Cowl with pressure driven latch

Methods and apparatus for passive thrust vectoring and plume deflection

Aircraft nacelle comprising an improved air intake

Aerodynamic fairing

Nacelle-To-Pylon Fairing

Lipskin for a nacelle and methods of making the same

Turbomachine comprising a device for the cooling of a pylon

Bilaterally asymmetric design for minimizing wave drag

Nacelle inner flow structure leading edge latching system

Engine pylon having a drain

Active aircraft pylon noise control system

Airframe stabilization mechanism for vertical takeoff and landing transport plane

Aircraft turbojet engine nacelle comprise an increased-rigidity air intake

Aerodynamic fairing divided into sub-portions

Aircraft propulsion unit comprising a nacelle provided with a fan cowl locking and closing mechanism

Propulsion system nacelle with reduced number of external split lines

Gas ejection cone for aircraft turbojet engines

System and method for cooling an aircraft wing

Flame resistant shield

Composite panel having a built-in duct

Assembly formed by a turbine engine and a system for attaching it to an aircraft structure

Aircraft propulsion system comprising an AFT pylon fairing with lateral walls that are profiled for injecting cool air along a thermal protection floor

Nacelle inner flow structure leading edge latching system

Thermal insulation support

Aircraft engine pylon AFT aerodynamic fairing

Internal locking mechanism for a hold open rod

Method for cooling a thermal protection floor of an aft aerodynamic fairing of a structure for mounting an aircraft propulsion system

Airfoil combination for aircraft turbofan

Method of processing acoustic waves emitted at the outlet of a turbo engine of an aircraft with a dielectric-barrier discharge device and aircraft comprising such a device

Device for reducing noise from jet-pylon interactions on jet engines

Apparatus for facilitating access to a nacelle interior

Engine pylon comprising a vortex generator, and method for the production thereof

Modular externally accessible batteries for an aircraft

Nacelle incorporating an element for connecting a lip and an acoustic attenuation panel together

FLOW-MODIFYING FORMATION FOR AIRCRAFT WING

ATTENUATION OF OPEN ROTOR NOISE

Morphing structure and method

Spring loaded pressure relief door

Composite material hollow axisymmetric body

Variable geometry aircraft pylon structure and related operation techniques

Twelve-hour structure for thrust reverser, in particular with grids

Active aircraft pylon noise control system

Aircraft nacelle comprising a reinforced outer wall

Pylon for attaching a gas turbine engine

Nacelle comprising an air entrance in a cap

Method of manufacture by superplastic forming and by fishplating of a rib for an aerodynamic fairing of an aircraft engine mounting pylon

Gas turbine engine with ejector

Fairing of aircraft elevator

Airplane having engines partially encased in the fuselage

Breather duct shielding

Leading edge flap method

Noise reducing device and jet propulsion system

Breather duct shielding

Gas turbine engine having a nacelle and a breather duct

Nacelle for aircraft engine having a nozzle with a variable section

Engine nacelle of an aircraft comprising a vortex generator arrangement

GAS TURBINE ENGINE WITH EJECTOR

Gas turbine engine with ejector

Modular externally accessible batteries for an aircraft

Aircraft comprising a device for reducing the induced drag

Engine pylon for the suspension of a turbo engine under an aircraft wing

Retractable nacelle chine

Leading edge flap apparatuses and associated methods

Gas turbine engine nacelle having a symmetric flowpath

Morphing structure and method

Devices and methods to improve wing aerodynamics at low airspeeds

Engine pod for an aircraft with a vortex generator arrangement

Aircraft engine assembly comprising a junction aerodynamic fairing mounted on two separate elements

Nacelle with a displacement device for aircraft jet engine and aircraft including such nacelle

Airplane engine pylon comprising at least one protruding element to generate a vortex of the airflow

High bypass-ratio turbofan jet engine

Composite heat shield

Aircraft comprising a central fairing that adjusts the pressure on the wing structures by means of local geometric deformations

Device for controlling a vortex trail generated by the oblong element of an aircraft bearing surface

Aircraft wing arrangement comprising an engine attachment pylon defining, in the forward region, a lateral airflow channel

MAST FOR AN AIRCRAFT NACELLE INCORPORATING MEANS FOR LIMITING THE APPEARANCE OF VIBRATIONS, IN PARTICULAR IN CERTAIN FLIGHT REGIMES, AT A HIGH MACH NUMBER AND LOW LIFT

Morphing structure

Vortex generator at hot gas output

Aeroengine ventilation system

Leading edge flap apparatuses and associated methods

Morphing structure

Aircraft braking method and ducted fan jet engine for implementing the method

Methods and apparatuses for controlling airflow proximate to engine/airfoil systems

Nacelle chine installation for drag reduction

Hydrogen fuel system for an aircraft

Passive, low-drag device for pylon-nacelle juncture flow separation mitigation

Engine controller for a gas turbine engine

Ducted fan having aerodynamic features

Collapsible ducted fan unmanned aerial system