ASSEMBLY FOR AN AIRCRAFT COMPRISING MEANS FOR FIXING A WING TO AN ENGINE PYLON

FLUIDIC PROPULSIVE SYSTEM

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

AIRCRAFT COMPRISING AN IMPROVED CONTROL SYSTEM FOR THRUST REVERSERS OR FOR OPENING AND CLOSING ENGINE COWLS

ASSEMBLY FOR AN AIRCRAFT HAVING MEANS FOR FASTENING A WING TO AN ENGINE PYLON

IN-FLIGHT MEASURED PROPULSION MASS FLOW AND THRUST ON AIRCRAFT

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

Uniform Exhaust Sheet and Flow Turning Control

TRUSS-BRACED WING AIRCRAFT ENGINE MOUNTING AND ASSOCIATED SYSTEMS

VERTICAL TAKE-OFF AND LANDING AIRCRAFT

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

PROPULSION SYSTEM FOR AN AIRCRAFT

FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES

PROPULSION SYSTEM FOR AN AIRCRAFT COMPRISING A TURBOJET, A PYLON AND ENGINE ATTACHMENT

ASSEMBLY FOR AN AIRCRAFT COMPRISING A WING AND A REACTOR MAST FOR COUPLING A PROPULSION SYSTEM TO SAID WING

IN-FLIGHT MEASURED PROPULSION MASS FLOW AND THRUST ON AIRCRAFT

Engine pylon rear secondary structure

PROPULSION SYSTEM FOR AN AIRCRAFT COMPRISING A TURBOJET, A PYLON AND ENGINE ATTACHMENT

FRONT ENGINE ATTACHMENT SYSTEM INTENDED FOR AN AIRCRAFT ENGINE AND HAVING A COMPACT STRUCTURE

AIRCRAFT PROPULSION ASSEMBLY HAVING A JET ENGINE, A PYLON AND MEANS FOR ATTACHING THE JET ENGINE TO THE PYLON

AIRCRAFT PROPULSION ASSEMBLY HAVING A JET ENGINE, A PYLON AND MEANS FOR ATTACHING THE JET ENGINE TO THE PYLON

AIRCRAFT PROPULSION ASSEMBLY HAVING A JET ENGINE, A PYLON AND MEANS FOR ATTACHING THE JET ENGINE TO THE PYLON

AIRCRAFT PROPULSION ASSEMBLY HAVING A JET ENGINE, A PYLON AND MEANS FOR ATTACHING THE JET ENGINE TO THE PYLON

PROPULSION SYSTEM FOR A NON-ROTARY-WING AIRCRAFT, AND ASSOCIATED AIRCRAFT

MULTI-MATERIAL JOINT

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

AIRCRAFT PROPULSION ASSEMBLY HAVING A JET ENGINE, A PYLON AND MEANS FOR ATTACHING THE JET ENGINE TO THE PYLON

HEAT SHIELD FOR AN AIRCRAFT AND METHOD OF USING THE SAME

FLUIDIC PROPULSIVE SYSTEM

Open rotor pylon fairing

Fluidic propulsive system and thrust and lift generator for aerial vehicles

EJECTOR AND AIRFOIL CONFIGURATIONS

Engine backbone bending reduction

Propulsion System for an Aircraft

AC electrical power system for a vehicle

Exhaust-gas treatment device for an aircraft engine

Aircraft

Flow aperture method and apparatus

Heat shield assembly for use with an aircraft engine

AIRCRAFT PROPULSION ASSEMBLY HAVING A JET ENGINE, A PYLON AND MEANS FOR ATTACHING THE JET ENGINE TO THE PYLON

In-flight measured propulsion mass flow and thrust on aircraft

AC electrical power system for a vehicle

Front engine attachment system for an aircraft engine, comprising a more a lightweight structure

Device for connecting an aircraft engine and a primary structure of an aircraft pylon comprising a rudder and a system for limiting the displacement of the rudder incorporating a double stop, aircraft comprising such a device

Mounting system for aircraft engine

Gas-electric propulsion system for an aircraft

Automated Initiation of Starter Motor Operation for Starting an Aircraft Engine

Aircraft assembly

Apparatuses based on jet-effect and thermoelectric effect

Aircraft and method of operating same

AN AIRCRAFT

Nacelle

FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES

Junction of a pylon with an aircraft wing

Synergistic hybrid propulsion

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

Aircraft propulsion system nozzle with internal flow passage

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

COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS

COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS

COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS

Engine attachment for an engine of an aircraft comprising a yoke, a connecting rod and a wearing part between the yoke and the connecting rod

AIRCRAFT WINGS WITH REDUCED WINGSPAN

Nacelle auxiliary landing gear

PYLON SHAPE WITH GEARED TURBOFAN FOR STRUCTURAL STIFFNESS

COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS

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

Engine pylon for coupling a jet engine to a wing of an aircraft

Flying vehicle and propulsion device thereof

Aircraft engine exhaust systems enabling reduced length aft strut fairings

MOUNTING SYSTEM FOR AIRCRAFT ENGINE

Personal flight apparatus with vertical take-off and landing

AIRCRAFT

Fail-safe engine support system

Forward engine attachment system for an aircraft engine comprising a direct coupling between the jet engine pylon and the engine

Total underwing nacelle and engine installation

FLUIDIC PROPULSIVE SYSTEM

Leading-edge device for an aircraft

METHOD FOR MANUFACTURING AN ACOUSTIC ABSORPTION STRUCTURE USING AT LEAST ONE CAUL PLATE, ACOUSTIC ABSORPTION STRUCTURE OBTAINED FROM SAID METHOD AND AIRCRAFT COMPRISING SAID ACOUSTIC ABSORPTION STRUCTURE

Winglet ejector configurations

System of using compressed air as a force source and method thereof; airplane

Propulsion system for an aircraft

Aircraft nacelle comprising at least one heat exchanger

Piezoelectric thrust vector control for dual-mode unmanned aerial vehicle

AIRCRAFT PYLON FAIRING

Shockwave mitigation system for supersonic aircraft

Aircraft assembly comprising a mounting pylon, a wing and two fixing systems fixing the mounting pylon to the wing

Propulsion unit for aircraft

Jet engine nacelle comprising a mobile assembly and a reinforced fixed structure

Method For Assembling An Aircraft Pylon

BLI PROPULSION SYSTEM WITH THREE AFT PROPULSION UNITS

Aircraft propulsion system including a heat exchanger system

Propulsion assembly for an aircraft, comprising a load support

HIGH-SPEED HYBRID PROPULSION FOR AIRCRAFT

Leading-edge slat for an aircraft

Supersonic jet aircraft

Gas-electric propulsion system for an aircraft

Blocker door pressure relief systems and methods

STRUCTURE, SUSPENSION SYSTEM, ENGINE ASSEMBLY AND AIRCRAFT

Method for mounting an aircraft pylon

AIRCRAFT JET ENGINE COMPRISING MEANS FOR VARYING ITS OUTPUT SURFACE AREA

Fluidic propulsive system and thrust and lift generator for aerial vehicles

Pylon shape with geared turbofan for structural stiffness

Mounting pylon for a jet engine of an aircraft comprising a particular structure

GAS TURBINE ENGINE

Wing, aircraft, and method for delaying wing stall of an aircraft

PROPULSION SYSTEM OF AN AIRCRAFT COMPRISING A DUAL-FLOW JET ENGINE AND AN AIR-DRAWING SYSTEM WITH REDUCED BULK

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

Systems and methods for cooling bleed air from an aircraft engine

Assembly for an aircraft engine mounting comprising an articulation axis supported by a yoke joint and translationally immobile

HYPERSONIC VEHICLE USING SCRAMJET

Assembly for aircraft comprising a primary mounting pylon structure fixed to an airfoil box using a bolted link

Aircraft pylon comprising a coaxial heat exchanger

Engine nacelle for an aircraft

Propulsion unit for an aircraft, with reduced aerodynamic drag

Assembly for an aircraft comprising a primary structure for an attachment pylon secured to a wing box by means of fittings that are more compact in the leading edge region

Assembly for an aircraft comprising a primary structure for an attachment pylon secured to a wing box by means of fittings that are more compact in the leading edge region

High altitude air launched rocket

Fluidic propulsive system and thrust and lift generator for aerial vehicles

Under the wing-mounted jet engine with pivotal swivel joint to produce directional thrust vectoring thru swivel angle

Assembly for aircraft, comprising a primary attachment-pylon structure fixed to a wing box by fasteners partially embedded in the primary structure

Dendritic heat exchangers and methods of utilizing the same

Methods and aircraft for optimized reverse thrust operation during landing

Fluidic propulsive system and thrust and lift generator for aerial vehicles

Fluidic propulsive system and thrust and lift generator for aerial vehicles

Aircraft engine pylon to wing mounting assembly

Aircraft engine assembly

Bleed valve module with position feedback and cooling shroud

Ejector and airfoil configurations

Lightweight primary structure for aircraft engine mounting pylon

Nacelle

Air flow deflector assembly for a thrust reverser system for reducing re-ingestion of reverse efflux air flow and method for the same

TURBOFAN ENGINE

Translating turning vanes for a nacelle inlet

ROTATING DEVICES FOR MITIGATION OF ADVERSE FLOW CONDITIONS IN AN ULTRA-SHORT NACELLE INLET

Propulsion system for an aircraft

AIRCRAFT PROPULSION SYSTEM COMPRISING A NACELLE WITH AN ENHANCED OPENING SYSTEM

Segmented pylon for an aircraft propulsion system

Propulsion system for an aircraft

EJECTOR AND AIRFOIL CONFIGURATIONS

Propulsion system for an aircraft

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

Propulsion system for an aircraft

Electric motors with neutral voltage sensing

Systems and methods of power allocation for hybrid electric architecture

Mechanical flywheel for bowed rotor mitigation

Aircraft propulsion assembly equipped with a main fan and with at least one offset fan

Engine shaft integrated motor

Piezo-electric motor for bowed rotor mitigation

Electric propulsion system for an aircraft

Aircraft propulsion assembly equipped with a main fan and with a least one offset fan

AIR INTAKE STRUCTURE AND AIRFLOW CONTROL SYSTEM

Gas-electric propulsion system for an aircraft

Rainbow flowpath low pressure turbine rotor assembly

Aircraft with Under Wing Direct Drive Low Pressure Turbine

Turbojet engine nacelle comprising a thrust reverser drive mechanism

Propulsion system for an aircraft

Propulsion system for an aircraft

Propulsor assembly for an aircraft

System for reducing the installation noise of an aeroplane wing

Temperature sensitive self actuated heat boundary layer control device

SEMI-CONTINUOUS FIXATION OF AN ENGINE ATTACHMENT PYLON TO AN ATTACHMENT DEVICE BELONGING TO THE WINGS OF AN AIRCRAFT

Enhanced performance jet engine mounting struts

Method and system for aligning propulsion system and vehicle having such propulsion alignment

AIRCRAFT COMPRISING A COMMON STRUCTURE FOR SUPPORTING A POWER PLANT AND A LANDING GEAR ELEMENT

High speed electric machine with embedded rotor magnets

Integrated strut support fittings with underwing longerons

Commercial supersonic aircraft and associated systems and methods

Turboelectric Aircraft with Aft Propulsion

Fan nacelle trailing edge

Fan module with rotatable vane ring power system

Aircraft engine assembly, comprising flexible force transmitting devices radially arranged between the thrust reversal cowls and the engine

Translating nacelle wall for an aircraft tail mounted fan section

Nacelle for an aircraft aft fan

Aircraft having an AFT engine and stabilizer with a varying line of maximum thickness

Aircraft having an aft engine and internal flow passages

Embedded electric machine

Embedded electric machine

Propulsion engine for an aircraft

Thrust force generation device and aircraft

Turbine engine air guide assembly with improved aerodynamic performance

Shockwave mitigation system for supersonic aircraft

GAS TURBINE ENGINE

Stabilizer assembly for an aircraft AFT engine

Coated wire

Aircraft strut comprising at least one lateral frame in lattice form and aircraft comprising said strut

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

Aircraft propulsion assembly with a filtered cradle

Gas turbine engine with distributed fans

Propulsion engine for an aircraft

Turbine engine including a thermal protection member

ELECTRIC PROPULSION ENGINE FOR AN AIRCRAFT

WINGLET EJECTOR CONFIGURATIONS

Aircraft including a wing with improved acoustic treatment

ENGINE BLEED SYSTEM WITH TURBO-COMPRESSOR

METHOD AND SYSTEM FOR MOUNTING AN AIRCRAFT ENGINE

Propulsion system for an aircraft

Aircraft, aircraft engine, and aircraft engine nacelle

Aircraft with a propulsion unit with offset fan

Bleed valve module with position feedback and cooling shroud

Hybrid propulsion system for a gas turbine engine including a fuel cell

Aircraft engine assembly, comprising an attachment device for the engine equipped with a structural cover attached on a central box

Enhanced performance jet engine mounting struts

Support pylon for a turbomachine, provided with a thermal protection element

Optimized aircraft pylon fairing

Aircraft engine assembly comprising rear engine attachments in the form of shackles

Gas turbine engine

Propulsive wing of an aircraft

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

Tilt-rotor over-torque protection from asymmetric gust

Link member for connecting aircraft pylon to wing of aircraft, aircraft pylon, and aircraft

Aft engine for an aircraft

Aircraft propulsion system having at least one anti-fire tank

Aircraft engine assembly comprising at least two rear engine attachments axially shifted from each other

Aircraft engine pylon to wing mounting assembly

Aircraft engine pylon to wing mounting assembly

Aircraft engine unit comprising an improved front engine attachment

Ejector and airfoil configurations

Fluidic propulsive system

Fluidic propulsive system and thrust and lift generator for aerial vehicles

Aircraft vapour trail control system

Engine cowling of an aircraft gas turbine

Fixed structure of a thrust reverser device

Trans-orbital freight and passenger carrier apparatuses supporting trans-orbital pipeline operations

Assembly for an aircraft including a fitting secured to the upper surface of a wing box, for mounting an engine strut to said wing box

Propulsion assembly incorporating a turbofan and a mounting pylon enabling a new distribution of the forces between the turbofan and the wing

Gas-electric propulsion system for an aircraft

Pusher fan engine with in wing configuration

Vertical take-off and landing (VTOL) fixed wing aircraft

Aircraft with counter-rotating turbofan engines

Aircraft engine pylon

Propulsion system for an aerial vehicle

Aerospace plane system

METHOD OF FLYING AN AIRCRAFT

Integrated pusher turbofan for aircraft

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

Aircraft with a nacelle-housed main landing gear

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

Engine mounting system

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

Bilaterally asymmetric design for minimizing wave drag

Pylon shape with geared turbofan for structural stiffness

Electric wire structure and method for electromagnetic shielding of electric wire

Aircraft including turbofan engine and igniter cable

Gas turbine engine with distributed fans

Assembly for an aircraft, comprising an engine attachment body equipped with at least one shackle support fitting that passes into the box section of the attachment pylon

Assembly for an aircraft, comprising an engine attachment body partially produced in one piece with an internal stiffening rib of an attachment pylon box section

Integrated pylon structure for propulsion system

Aircraft pylon and aircraft

Method for mounting a pylon to an aircraft

Device for suspending a turbojet engine

Thermal insulation support

AIRCRAFT

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

System and method for mounting an aircraft engine

Thrust reverser supporting structure including composite reinforcements and a base having an unclosed cross section

Bleed valve module with position feedback and cooling shroud

Aircraft engine mounting structure, assembly comprising this structure and associated aircraft

Aircraft assembly including an element for mounting an engine and associated aircraft

Assembly for an aircraft comprising a turbomachine attachment strut of which the means for attachment to the wing are arranged in a T shape

Engine assembly for an aircraft the engine attachment strut of which includes a structural case forming an internal radial delimitation of the secondary flow

Pylon arrangement for open structure

Variable geometry aircraft pylon structure and related operation techniques

Spigot-type fastener provided with at least one means for measuring the force generated by an aircraft engine

Aircraft engine attachment pylon comprising two front wing system attachments with orthogonal shearing pins

AIRPLANE WING

Active aircraft pylon noise control system

Linking device for linking a first body to a second body, in particular for an aircraft engine assembly

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

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

Integrated aircraft

Integrated nacelle assembly

Engine mount of aircraft and aircraft

Fan cowl support cradle mounted on the attachment pylon and on the air inlet of the nacelle

Truss-shaped engine pylon and method of making same

Ball slide bearing and connecting device associated with a mast for hooking a gas turbine engine under an aircraft wing comprising such a bearing

Aircraft engine attachment pylon comprising a box with a circular or elliptical shaped section

Noise reducing device and jet propulsion system

Aircraft engine pylon attachment

Hydraulic drive, hydraulic supply device, airplane with a hydraulic supply device and method for configuring a hydraulic supply device

Assembly for an aircraft including a wing element and a suspension pylon

Securing plate and longitudinal handling member for a one-piece aircraft propulsion unit

Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft

Monolithic structure for mounting aircraft engine

Fail safe extended torque box strut-to-wing mount

Bypass turbojet engine nacelle

Aircrft Structure

PRIMARY ENGINE STRUT STRUCTURE OF AN AIRCRAFT

Aircraft engine assembly comprising a fan cowl-supporting cradle mounted on two separate elements

Pylon for suspending a turboengine

Structural nacelle

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

Aircraft wing, fastening arrangement, and intermediate support

Thermal management system integrated pylon

Connecting a propulsion system to a structural element of an aircraft

Mounting system for a gas turbine engine