BLENDED WING AIRCRAFT

OPEN ROTOR AIRCRAFT PROPULSION SYSTEM WITH MULTI-GEAR SYSTEM GEARTRAIN

VEHICLE ELECTRICAL POWER SYNCHRONIZATION VIA HYDRAULICS

REMOTE MOUNTED ACCESSORY GEARBOX

BLENDED WING BODY AIRCRAFT WITH REAR ENGINES

AIRCRAFT WITH A FUSELAGE ACCOMMODATING AN UNDUCTED TURBINE ENGINE

HYBRID ELECTRIC AIRCRAFT WITH GYROSCOPIC STABILIZATION CONTROL

ENGINE SUPPORT ASSEMBLY

AIRCRAFT WITH A FUSELAGE ACCOMMODATING AN UNDUCTED TURBINE ENGINE

AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET

Adaptive vertical take-off and landing propulsion system

FLUIDIC PROPULSIVE SYSTEM

AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)

AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S)

Build plate integrated into additive manufactured component

Aircraft with a fuselage accommodating an unducted turbine engine

Hybrid-electric single engine descent failure management

Aircraft propulsion system

Hybrid electric aircraft with gyroscopic stabilization control

Power management methods for multi engine rotorcraft

Method for assisting the piloting of a rotorcraft at high altitudes by supplying mechanical power from an electrical power plant

Aircraft

AIRCRAFT HAVING AN AIRCRAFT BODY INCLUDING A FEATURE

Fan powered folding wing bicycle apparatus

AIRCRAFT INTERNAL COMBUSTION ENGINE

Supercritical carbon dioxide-cooled generator and turbine

Hybrid aircraft propulsion power plants

Aircraft propulsion system with propeller and cooling fan

Tiltrotor propulsion system for an aircraft

AIRCRAFT PROPULSION SYSTEM AND METHOD FOR OPERATING SUCH A SYSTEM

Gas turbine engine inlet wall design

Aircraft Design and Technology

Adaptive aircraft electrical power distribution system

Systems and methods for hybrid electric gas turbine engines

Mechanically-distributed propulsion drivetrain and architecture

Compound helicopters having auxiliary propulsive systems

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

Aircraft comprising a gas turbine engine having an axially adjustable intake and a nacelle

Systems and methods of retrofitting an aircraft engine to an aircraft

Aircraft propulsion system and aircraft powered by such a propulsion system built into the rear of an aircraft fuselage

Nacelle for an aircraft aft fan

Multimode powertrains for multi engine rotorcraft

Bearing preload using external gearbox reaction

Electrically controlled vertical takeoff and landing aircraft system and method

Aircraft with bifurcated air inlet

Power management systems for multi engine rotorcraft

Hybrid gas turbine engine with bleed system improvements

Nacelle for a boundary layer ingestion propulsor

Drag recovery scheme for nacelles

Aircraft nacelle having electric motor and thrust reversing air exhaust flaps

ADAPTIVE VERTICAL TAKE-OFF AND LANDING PROPULSION SYSTEM

Hybrid aircraft propulsion power plants

Hybrid aircraft propulsion power plants

Hybrid aircraft propulsion power plants

Aircraft having embedded engines

Compound helicopters having auxiliary propulsive systems

TANDEM FAN FOR BOUNDARY LAYER INGESTION SYSTEMS

DEDICATED CORE INFLOW INLET FOR CONVERTIBLE ENGINE

Power supply device and flying body

Hybrid propulsion systems

Articulated mounts

Hybrid flight vehicle using engine gyro effect for stabilization

Tiltrotor propulsion system for an aircraft

Mechanically-distributed propulsion drivetrain and architecture

Ring-shaped airfoil aircraft capable of taking off and landing vertically, and hovering

BOUNDARY LAYER INGESTING FAN

VERTICAL TAKE-OFF AND LANDING AIRCRAFT

Aircraft having an aft engine

Multi-rotor aircraft and related systems and methods

Moveable aircraft cowl and bypass section

VERTICAL TAKE-OFF AND LANDING AIRCRAFT

Thrust reversal on aircraft fuselage with a wing profile

Mast lockout systems for tiltrotor aircraft

Aircraft having an AFT engine

Connection assembly for mounting engine and engine mounting system comprising the same

AIRCRAFT DESIGN AND TECHNOLOGY

Integrated support structure for an aircraft engine and its auxiliary components

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

Drive device for an aircraft

System and method for operating a boundary layer ingestion fan

Exhaust arrangement for aircraft having sensor

Aft fan counter-rotating turbine engine

Turbine engine propelled airplane having an acoustic baffle

Turbojet of the unducted rotor type

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

Variable-geometry boundary layer diverter

Passive internal ice protection systems for engine inlets

Aircraft comprising a propulsion assembly including a pair of propellers at the rear of the fuselage

Rotorcraft having increased altitude density ceiling

Aircraft comprising a rear fairing propulsion system with inlet stator comprising a blowing function

Dual function aircraft

Aircraft comprising a turbine engine incorporated into the rear fuselage comprising a system for blocking the fans

Aircraft comprising two contra-rotating fans to the rear of the fuselage, with spacing of the blades of the downstream fan

Aircraft comprising a turbine engine incorporated into the rear fuselage with variable supply

Aircraft comprising a propulsion assembly including a fan on the rear of the fuselage

Control system for rotorcraft in-flight engine restarting

Engine cooling systems for aircraft

Boundary layer ingestion integration into aft fuselage

AIRCRAFT HAVING A REAR SECTION WITH A CONTINUOUS SKIN FOR THE FUSELAGE AND THE VERTICAL TAIL PLANE

Twin shafts driving adjacent fans for aircraft propulsion

System and method for dynamically controlling the operation of an aircraft

Nacelle for an aircraft aft fan

Aircraft having an aft engine

Tiltrotor propulsion system for an aircraft

Tiltrotor propulsion system for an aircraft

TILTROTOR PROPULSION SYSTEM FOR AN AIRCRAFT

Aircraft propulsion unit comprising an unducted-fan turbine engine and an attachment pylon

Aircraft

Direct drive aft fan engine

Exhaust duct for turbine forward of fan

Direct drive aft fan engine

Aircraft comprising a turbojet engine integrated into the rear fuselage comprising a fairing allowing the ejection of blades

Stabilizer assembly for an aircraft AFT engine

Assembly for aircraft comprising engines with boundary layer ingestion propulsion

Aircraft engine assembly comprising a pylon leading edge incorporated with an annular row of unfaired after-guide vanes

DEVICE FOR REDUCING AERODYNAMIC DISTURBANCES IN THE WAKE OF AN AERODYNAMIC PROFILE BY VARIABLE-DISTRIBUTION BLOWING ON THE TOP SIDE AND THE UNDERSIDE

Propeller for an aircraft turbo engine, including safety means for controlling blade angle of attack

Doors for an easy access to the pressurized housing of a flying wing, from the trailing edge

Aerodynamic lift enhancing system for a flying automotive vehicle

Air intake turboprop assemblies

Aircraft with a propulsion unit comprising a fan at the rear of the fuselage

Turboshaft engine, twin-engine helicopter equipped with such a turboshaft engine, and method for optimising the zero-power super-idle speed of such a twin-engine helicopter

Aircraft

Double propulsor imbedded in aircraft tail with single core engine

AFT engine nacelle shape for an aircraft

Non-axis symmetric aft engine

Aft engine for an aircraft

Aircraft having an aft engine

Link for aircraft component mounting

Articulated mounts

Noise attenuation for an open rotor aircraft propulsion system

Stealth aerial vehicle

Aircraft with a protective shield against an engine blade release

Exhaust arrangement for aircraft having sensor

Transverse-mounted power turbine drive system

Aircraft

Propeller for an aircraft turbomachine, including a blade retaining structure through which the aerodynamic part of each blade passes

Aircraft including an engine attachment with a control surface

Stealth aerial vehicle

System and method for aft mount of gas turbine engine

Suspension structure with variable geometry of a turboprop engine on a structural element of an aircraft

Box wing with angled gas turbine engine cores

Gas turbine engine inlet wall design

Asymmetric thrust reversers

Aircraft propelled by a turbojet engine with contrarotating fans

Modular power plant and an aircraft provided with a lift rotor

Contra-rotating open rotor distributed propulsion system

Stabilizer with structural box and sacrificial surfaces

Hybrid gas turbine propulsion system

Aircraft powerplant

Aircraft using turbo-electric hybrid propulsion system for multi-mode operation

Intermediate structure for independently de-mountable propulsion components

Free stream intake with particle separator for reverse core engine

De-couple geared turbo-fan engine and aircraft

Engine installation

Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan

Gas turbine engine having fan rotor driven by turbine exhaust and with a bypass

Unducted propeller gas turbine engine attachment structure

Twin Tip Turbine Propulsors Powered by a Single Gas Turbine Generator

Airplane having a rear propulsion system

Intermediate structure for independently de-mountable propulsion components

Propulsion system with movably mounted engines

Engine attachment pylon

Aircraft with fuselage-mounted engines and an internal shield

Impact resistant and damage tolerant aircraft fuselage

Turboshaft engine attached to a pylon of the fuselage of an aircraft by a failsafe suspension system

Transverse mounted gas turbine engine

Fuselage and method for reducing drag

REINFORCED AIRCRAFT FUSELAGE

Streamlined profile reducing the speed deficit in its wake

HYBRID FREE-AIR GAS TURBINE ENGINE

Remote shaft driven open rotor propulsion system with electrical power generation

Method and apparatus for reducing aircraft noise

Support structure

Rear part of an aircraft including an engine support structure assembled so as to oscillate on the fuselage

Rigid aircraft pylon fitted with a rib extension for taking up the moment in the lengthways direction

Rigid aircraft pylon structure in contact with a fuselage lateral extension for attachment

Attachment system of aircraft components

Impact resistant and damage tolerant aircraft fuselage

Rear part of an aircraft comprising a structure for supporting engines, extending through the fuselage and connected thereto by at least one connecting rod

Rear part of an aircraft comprising a structure for supporting engines, extending through the fuselage and connected thereto by at least one connecting rod

Rear part of an aircraft comprising a structure for supporting engines, connected to the fuselage by at least one blocking element under compression loading

Air inlet of an aeroengine having unducted pusher propellers

Air ejector nozzle tube for an oil heat exchanger of an aircraft engine

Aircraft engine supporting pylon

Arrangement for the suspension of a jet engine to a supporting structure

Attachment pylon for an aircraft turbo-shaft engine with concentric hot air channels

Airplane configuration

Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan

Method for producing an aircraft with reduced environmental impact and the aircraft thus obtained

Turboprop propulsion unit with pusher propeller

Aircraft with tail propeller-engine layout

Optimized configuration of engines for aircraft

Acoustically attenuated fuselage for aircraft

Impact resistant aircraft fuselage

Arrangement for mounting an engine on the airframe of an aircraft

Aircraft with reduced environmental impact

Aircraft having reduced environmental impact

Aircraft having a reduced environmental impact

Airplane configuration

Unconventional integrated propulsion systems and methods for blended wing body aircraft

Aircraft airframe architectures

Fuel efficient fixed wing aircraft

Vertical tail unit for aircraft and aircraft equipped with same

Aircraft propulsion system

Blended wing aircraft

Aircraft propulsion system with core flowpath inlet forward of fan rotor

Blended wing aircraft

Modular aircraft system