FLUIDIC PROPULSIVE SYSTEM

PROPULSION ENGINE ASSEMBLIES PROVIDING ACCESS TO COMPONENTS WITHIN PROPULSOR CAVITIES

AIRCRAFT COMPRISING AT LEAST ONE DEFLECTOR CONFIGURED TO DIVERT A GAS EXHAUST CONE EXITING A PROPULSION ASSEMBLY AWAY FROM A TRAILING EDGE OF A WING

AERODYNAMIC DIVERTER

FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES

CONFIGURATION FOR VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES

AIRCRAFT COMPRISING AT LEAST ONE COWL HAVING TWO PARTS MOVABLE RELATIVE TO EACH OTHER

Engine pylon rear secondary structure

ASSEMBLY FOR AN AIRCRAFT, SAID ASSEMBLY HAVING A PYLON AND A RESERVOIR CONTAINING AN EXTINGUISHING AGENT

INTERNAL FIXED STRUCTURE FOR AN AIRCRAFT NACELLE

Aircraft propulsive assembly comprising a nacelle with a t-shaped frame

ELECTRICAL POWER SYSTEM FOR A VEHICLE

Dissassembly for dual engine vertical take off and landing collapsible fixed wing aircraft

ASSEMBLY FOR DUAL ENGINE VERTICAL TAKE OFF AND LANDING COLLAPSIBLE FIXED WING AIRCRAFT

CONNECTORS AND JOINTS FOR DUAL ENGINE VERTICAL TAKE OFF AND LANDING COLLAPSIBLE FIXED WING AIRCRAFT

Aircraft Electric Motor Cooling System

Dual engine vertical take off and landing collapsible fixed wing aircraft

FLUIDIC PROPULSIVE SYSTEM

OPEN ROTOR PYLON FAIRING

Open rotor pylon fairing

OPEN ROTOR PYLON FAIRING

OPEN ROTOR PYLON FAIRING

Fluidic propulsive system and thrust and lift generator for aerial vehicles

AIRCRAFT HAVING AN ENGINE PYLON WITH A MOBILE COWL

EJECTOR AND AIRFOIL CONFIGURATIONS

PROPULSION SYSTEM OF AN AIRCRAFT, HAVING AN ASYMMETRICAL NACELLE

NACELLE APPARATUS WITH AIR-CONDUCTING DEVICE AND VERTICAL TAKE-OFF AND LANDING AIRCRAFT

Configuration for vertical take-off and landing system for aerial vehicles

Assembly Comprising a Nacelle Panel and a Housing

Bypass turbofan including a system for blocking the secondary flow including veils

Propulsive assembly for aircraft

Exhaust nozzle assembly, propulsion system employing the exhaust nozzle assembly, and aircraft employing the propulsion system

AIRCRAFT EQUIPPED WITH FUEL CELL SYSTEM AND THRUST CONTROL METHOD

ELECTRIC TILTROTOR AIRCRAFT WITH TILTING COAXIAL MOTORS AND GEARBOX

ASSEMBLY FOR MOUNTING AN UNDERWING PYLON TO A RIB OF AN AIRCRAFT WING

STRUT ASSEMBLY AND METHOD FOR COUPLING AN ENGINE TO A WING OF AN AIRCRAFT

Systems and methods for aircraft wing plug

Electrical power system for a vehicle

Electrical power system for a vehicle

FLIGHT STABILIZATION SYSTEM WITHOUT CROSS SHAFTS FOR VTOL TILTROTOR AIRCRAFT

COMPACT AERIAL MISSION MODULAR MATERIAL HANDLING SYSTEM

Cooling system for aircraft components including ram chute body and relatively rotatable air conduit

FAIRING FOR WING-MOUNTED ENGINES

Aircraft engine attachment assembly

Aircraft propulsor and method for using said propulsor

Aircraft propulsion assembly comprising a plate heat exchanger, of hexagonal longitudinal section, positioned in a bifurcation

Control system for an aircraft and a method of operating the control system

Heat shield assembly for use with an aircraft engine

Vertical Takeoff and Landing Aeronautical Apparatus with a Folding Wing

Multicopter with boom-mounted rotors

VORTEX CONTROL ON ENGINE NACELLE STRAKE AND OTHER VORTEX GENERATORS

Aircraft and direct drive engine under wing installation

Aircraft nacelle comprising a seal system with a spring for a cap of said nacelle

Aircraft engine pylon having a movable assembly of cowls

Aircraft engine pylon having a mobile cowl

Wing assembly for an aircraft

REMOTE MOUNT OF ENGINE ACCESSORIES

Electric tiltrotor aircraft with tilting coaxial motors and gearbox

Compact aerial mission modular material handling system

Compound helicopter with braced wings in joined-wing configuration

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

Ducted fan case attachment structure

Pylon mounted tilt rotor

Air cooling

Fire resistance device designed to be placed between one end of a mounting strut for an aircraft turbomachine and a cowling of the turbomachine delimiting an inter-flow compartment

Aircraft wing

Nacelle

Aircraft engine nacelle with asymmetric fan cowls

Propulsion engine assemblies providing access to components within propulsor cavities

FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES

Synergistic hybrid propulsion

PROPULSION SYSTEM, AIRCRAFT HAVING A PROPULSION SYSTEM, AND METHOD OF MANUFACTURING AN AIRCRAFT

Aeronautical apparatus

Flush fluid inlet designs for aero-acoustic tone mitigation of aircraft

Aircraft pylon comprising at least one seal interposed between a fixed structure and a removable panel of a fairing

Pylon mounted tilt rotor

Nacelle for gas turbine engine and aircraft comprising the same

Systems and methods for aircraft wing plug

Rotatable nacelle for centrifugal fan on aircraft

Exhaust nozzle assembly, propulsion system employing the exhaust nozzle assembly, and aircraft employing the propulsion system

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

Aircraft nacelle having a fan ramp with articulated flaps

DISTRIBUTED ELECTRIC ENERGY PODS NETWORK AND ASSOCIATED ELECTRICALLY POWERED VEHICLE

Turbofan comprising a system comprising a screen for closing off the bypass duct

Assembly for an aircraft, the assembly including a pylon and a tank containing an extinguisher fluid

Aircraft having an engine wing assembly

Stowed blade active restraint

Autonomous propeller propulsion system for an aircraft, said autonomous propeller propulsion system comprising a fuel cell

Methods and apparatus for mitigating aerodynamic flutter of aircraft wing flaps

Flap actuation systems for aircraft

Propulsion assembly for an aircraft, comprising a nacelle load support fastened to a pylon

FLUIDIC PROPULSIVE SYSTEM

Joining components

Winglet ejector configurations

Configuration for vertical take-off and landing system for aerial vehicles

Aircraft nacelle having electric motor and thrust reversing air exhaust flaps

Aircraft nacelle comprising at least one heat exchanger

AIRCRAFT NACELLE

AIRCRAFT PYLON FAIRING

AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM WITH ELECTRIC STORAGE LOCATED IN WINGS

Aircraft having hybrid-electric propulsion system with electric storage located in fuselage

Primary structure of an aircraft pylon having at least one transverse reinforcer equipped with two diagonally disposed link rods, and aircraft comprising such a primary structure

Propulsion unit for aircraft

Aircraft propulsion system including a heat exchanger system

Method for assembling at least two parts by transparent welding, method for assembling a primary structure of an aircraft pylon by transparent welding, primary structure of an aircraft pylon thus obtained and aircraft comprising said primary structure

HIGH-SPEED HYBRID PROPULSION FOR AIRCRAFT

Aircraft nacelle comprising a cowl with two articulated doors

High visibility panel latch

Slat-thrust reverser clearance

Aircraft turbomachine assembly comprising an articulated cowl

STRUCTURE, SUSPENSION SYSTEM, ENGINE ASSEMBLY AND AIRCRAFT

Aircraft Pylon Central Fairing Comprising At Least One Articulated Panel, And Aircraft Equipped With Said Central Fairing

Heat shield assembly and method

Roll load bearing aircraft propulsor moveable panel systems and methods

Geared turbofan gas turbine engine mounting arrangement

Nacelle system and methods of operation

Air supply system for an aircraft

Fluidic propulsive system and thrust and lift generator for aerial vehicles

VERTICAL TAKE-OFF AND LANDING AIRCRAFT

Rear fairing for a turbojet engine pylon made of composite materials

Nacelle

Gas turbine engine

Aircraft comprising at least one cowling equipped with an improved hinge system

Multicopter with boom-mounted rotors

Multicopter with angled rotors

Turbojet engine comprising a nacelle equipped with a fan case and with a fixed structure

Aircraft pylon comprising a coaxial heat exchanger

Fluidic propulsive system and thrust and lift generator for aerial vehicles

Fluidic propulsive system and thrust and lift generator for aerial vehicles

Fluidic propulsive system and thrust and lift generator for aerial vehicles

High-mounted aircraft nacelle

Baseless vortex generator

Ejector and airfoil configurations

Nacelle

Convergent divergent exit nozzle for a gas turbine engine

Device and method for parts assembly for a nacelle of an aircraft turbojet engine

Aircraft incorporating a low-temperature bleed system

Hinge assembly

Method and system for mounting an aircraft engine

Tiltrotor aircraft with outboard fixed engines

Aircraft and direct drive engine under wing installation

EJECTOR AND AIRFOIL CONFIGURATIONS

LANDING GEAR FAIRING WITH AERODYNAMIC SURFACES FOR TAIL SITTER AIRCRAFT

Nacelle

Stall recovery chine spoiler system

Aircraft propulsion assembly provided with steps allowing an operator to reach the top of same

Aircraft hydraulic systems having shared components

Bogie mechanism for a tiltrotor proprotor door

Roller track assembly for a tiltrotor proprotor door

Tiltrotor aircraft rotating proprotor assembly

VARIABLE INCIDENT NACELLE APPARATUS AND METHODS

Airplane with angled-mounted turboprop engine

Integrated strut support fittings with underwing longerons

Multicopter with boom-mounted rotors

Multicopter with angled rotors

Heat shield flange sliding joint

SELF-MOVING APPARATUS AND COMPONENTS THEREOF

Sliding joint kits, systems containing the same, and related methods

Nacelle

System for installing and removing a propulsion unit on a pylon of an aircraft

Bulb seal and spring

Acoustic panel for aircraft nacelle, and method of manufacturing the acoustic panel

WINGLET EJECTOR CONFIGURATIONS

Aircraft including a wing with improved acoustic treatment

Heat shield assembly and method

Configuration for vertical take-off and landing system for aerial vehicles

Tapered sockets for aircraft engine mount assemblies

Beam springs for aircraft engine mount assemblies

Clamped splines for aircraft engine mount assemblies

Sleeved bolt assemblies for aircraft engine mount assemblies

Thrust reverser cascade systems and methods

Hybrid propulsion vertical take-off and landing aircraft

Compliant engine nacelle for aircraft

Distributed electric ducted fan wing

Vertical take-off and landing (VTOL) aircraft with exhaust deflector

Aircraft brace housing a fluid transfer line

Optimized aircraft pylon fairing

Propulsion assembly for an aircraft, comprising a gas generator, two offset fans and an air inlet sleeve

Aircraft with a strut-braced foldable wing

Aircraft propulsion system having at least one anti-fire tank

Aircraft engine mounting system

Ejector and airfoil configurations

Fluidic propulsive system

Fluidic propulsive system and thrust and lift generator for aerial vehicles

Sound attenuation apparatus and method

CONTROL SYSTEM AND STRATEGY FOR TAIL SITTER

Latch beam deflection support

Pylon with noise attenuating fairing

Extremely quiet short take-off and landing (STOL) aircraft

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

Modular nacelles to provide vertical takeoff and landing (VTOL) capabilities to fixed wing aerial vehicles, and associated systems and methods

Engine cowling of an aircraft gas turbine

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

Method of attaching nacelle structure to minimize fatigue loading

Slat-thrust reverser clearance

Convertible tiltrotor aircraft

Pusher fan engine with in wing configuration

Thrust reverser sliding door assembly

Convergent divergent exit nozzle for a gas turbine engine

REMOVABLE AUXILIARY POWER DEVICE FOR AIRCRAFT AND AIRCRAFT ADAPTED TO USE AT LEAST ONE SUCH DEVICE

Integrated pusher turbofan for aircraft

Electric propulsion assembly for an aircraft

Assembly for an aircraft comprising an attachment pylon primary structure formed with three independent elements

Bifurcation honeycomb sandwich structure with optimized doubler

Airplane suspension cowling structure with wing-mounted arrangement

Stress-relieving joint between materials with differing coefficients of thermal expansion

Nacelle

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

Aircraft engine mounting system

Aerodynamic track fairing for a gas turbine engine fan nacelle

Foldable guiding ventilator cover for an aircraft engine assembly

AFT pylon fairing for aircraft

AIRCRAFT PROPULSION ASSEMBLY COMPRISING AT LEAST ONE BRUSH SEAL RESISTANT TO HIGH-TEMPERATURE

Aerodynamic fairing

Compact Nacelle With Contoured Fan Nozzle

Aerodynamic fairing

Nacelle-To-Pylon Fairing

ASSEMBLY FOR AN AIRCRAFT COMPRISING AN ATTACHMENT PYLON PRIMARY STRUCTURE FORMED WITH THREE INDEPENDENT ELEMENTS

Gas turbine inlet

Rotatable fairing and engine inlet system for high-speed aircraft

Bilaterally asymmetric design for minimizing wave drag

Engine pylon structure

Non-circular aft nacelle cowling geometry

Engine pylon having a drain

Electric wire structure and method for electromagnetic shielding of electric wire

Aircraft including turbofan engine and igniter cable

Cylindrical case and manufacturing method of cylindrical case

Nacelle

PROPULSION DEVICE USING FLUID FLOW

Aerodynamic fairing divided into sub-portions

System and method for cooling an aircraft wing

Inner cowl structure for aircraft turbine engine

Attachment pylon for a turbine engine

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

Nacelle

Aft aerodynamic fairing with improved thermal resistance for a pylon for attaching an aircraft propelling assembly

Method and device for displaying meteorological data on an aircraft screen

Aircraft engine pylon AFT aerodynamic fairing

Nacelle

Aft pylon fairing for aircraft engine suspension system, comprising a heat shield capable of expanding freely

Propulsive unit for an aircraft

Aerodynamic aft fairing of an aircraft engine suspension pylon

Turboshaft engine supporting pylon covered with a porous material and turboshaft engine/pylon assembly

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

Heteroaryl Amide Analogues

Jet engine installation

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

Non-circular aft nacelle cowling geometry

Mast having modifiable geometry for securing an engine to an aircraft wing

Aircraft engine inlet having zone of deformation

AFT pylon fairing for an aircraft engine suspension system

Systems and methods for passively directing aircraft engine nozzle flows

Air outlet system for aircraft leading edge

NACELLE WITH SIMPLIFIED COWLING ARRANGEMENT

Engine nacelle of an aircraft comprising a vortex generator arrangement

Aircraft comprising a device for reducing the induced drag

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

Rear lower aerodynamic fairing for the attachment device of an aircraft engine

Systems and methods for reducing noise from jet engine exhaust

Engine pod for an aircraft with a vortex generator arrangement

Pylon for suspending a turboengine

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

Ceramic heat shield

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

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

Superplastic forming of titanium assemblies

Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods

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

Main wing structure of aircraft

Systems and methods for passively directing aircraft engine nozzle flows

Vortex generator at hot gas output

Aircraft engine inlet having zone of deformation

GAS TURBINE ENGINE AND METHOD OF OPERATING SAME

Superplastic forming of titanium assemblies

Drain particularly for engine support strut

Turbine engine arrangements

Nacelle chine installation for drag reduction

Aircraft wing and aeroengine arrangement for attenuating engine noise

Supersonic aircraft

Quiet urban air delivery system

Engine wing