AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

GAS TURBINE ENGINE HAVING A SENSOR ASSEMBLY FOR MONITORING PROPELLER WHIRL

Aircraft and Method for Operating

AIRCRAFT INCLUDING AT LEAST ONE WING ATTACHMENT SYSTEM ENSURING OPTIMUM TRANSMISSION OF THRUST FORCES

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

HYBRID-ELECTRIC PROPULSION SYSTEM FOR AN AIRCRAFT AND A CONTROL SYSTEM FOR A HYBRID ELECTRIC PROPULSION SYSTEM

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

PROPULSION ASSEMBLY FOR AN AIRCRAFT PROVIDED WITH A PROPELLER AND A CYCLIC PITCH DEVICE FOR THE BLADES OF THE PROPELLER AND METHOD FOR REGULATING THE CYCLIC PITCH OF THE BLADES OF THE PROPELLER

PROPULSION ENGINE ASSEMBLIES PROVIDING ACCESS TO COMPONENTS WITHIN PROPULSOR CAVITIES

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

Unducted Thrust Producing System

AIRCRAFT COMPRISING AT LEAST ONE WING MOUNT SYSTEM, WHICH COMPRISES AT LEAST ONE LATERAL CONNECTING ROD

REDUCTION OF COMMON MODE EMISSION OF AN ELECTRICAL POWER CONVERTER

PROPULSION SYSTEM FOR AN AIRCRAFT

HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM AND METHOD

GAS TURBINE ENGINE

GAS TURBINE ENGINE

GAS TURBINE ENGINE

GAS TURBINE ENGINE

GAS TURBINE ENGINE

GAS TURBINE ENGINE

SUSPENSION ASSEMBLY FOR A TURBINE ENGINE

GAS TURBINE ENGINE

GAS TURBINE ENGINE

GAS TURBINE ENGINE

PROPULSION SYSTEM FOR AN AIRCRAFT

FUEL DELIVERY

AIRCRAFT WITH AN UNDUCTED FAN PROPULSOR

GAS TURBINE ENGINE

GAS TURBINE ENGINE WITH CLUTCH ASSEMBLY

PROPULSION SYSTEM AND METHOD FOR OPERATION

AIRCRAFT HAVING A DIHYDROGEN SUPPLY PIPE SEATED IN A CORRIDOR DELIMITED BETWEEN TWO SPARS OF A WING

CRYOGENIC FUELED AIRCRAFT

ELECTRICAL POWER SYSTEM FOR A VEHICLE

PROPULSION ASSEMBLY FOR AN AIRCRAFT

MOUNTING ASSEMBLY FOR GAS TURBINE ENGINE

OPEN ROTOR PYLON FAIRING

OPEN ROTOR PYLON FAIRING

OPEN ROTOR PYLON FAIRING

GAS TURBINE ENGINE ACCESSORY PACKAGING

Outlet guide vane assembly for a turbofan engine

INNER COWL ARRANGEMENT FOR GAS TURBINE ENGINE

Gas turbine engine

Apparatus comprising a device for regulating a concentration of dihydrogen

GAS TURBINE ENGINE MOUNT

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

Propulsive assembly for aircraft

PROPULSION ASSEMBLY FOR AN AIRCRAFT

SYSTEM AND METHOD FOR USING AMMONIA AS A FUEL SOURCE FOR ENGINES

Propulsion System for an Aircraft

POWERPLANT FOR AN AIRCRAFT

Powerplant for an aircraft

ENGINE CHARACTERISTICS MATCHING

Hybrid-electric powertrains for aircraft

MULTI-DRIVE UNIT POWERPLANT FOR AN AIRCRAFT

ADVANCE RATIO FOR SINGLE UNDUCTED ROTOR ENGINE

REDUCTION OF COMMON MODE EMISSION OF AN ELECTRICAL POWER CONVERTER

Systems and methods for aircraft wing plug

Electrical power system for a vehicle

Electrical power system for a vehicle

AIRCRAFT HAVING A DRIVE-AND-ENERGY SYSTEM FOR LOW-EMISSION CRUISING FLIGHT

ENGINE ATTACHMENT SYSTEM FOR AIRCRAFT AND METHOD FOR ATTACHING AN ENGINE

Fuel delivery

Hydrogen steam and inter-cooled turbine engine

BLENDED WING BODY AIRCRAFT

CRYOGENIC COOLING SYSTEM FOR AN AIRCRAFT

PROPULSION ASSEMBLY FOR AN AIRCRAFT, COMPRISING A LOAD BEARER

HYBRID POWER SYSTEM

Aircraft engine attachment assembly

Propulsion assembly for an aircraft

GAS TURBINE ENGINE NOISE REDUCTION

Aircraft having a heat engine and device for using the exhaust gases from the heat engine

Reduction of common mode emission of an electrical power converter

CRYOGENIC COOLING SYSTEM FOR AN AIRCRAFT

UNDUCTED THRUST PRODUCING SYSTEM

Aircraft and direct drive engine under wing installation

Turbine over-speed brake for hybrid electric gas turbine engine

Aeronautical car and associated features

AIRCRAFT ENGINE

Embedded electric machine

Wing assembly for an aircraft

PROPULSION SYSTEM COOLING CONTROL

Chilled working fluid generation and separation for an aircraft

Hybrid electric propulsion system and method of operation

Gas turbine engine mounted above wing and with camber

GAS TURBINE ENGINE MOUNTED ABOVE WING AND WITH CAMBER

Propulsion engine assemblies providing access to components within propulsor cavities

Synergistic hybrid propulsion

Propulsive assembly for aircraft

Motoring synchronization for multiple engines

Vertical take-off and landing aircraft using hybrid-electric propulsion system and the control method

Nacelle for gas turbine engine and aircraft comprising the same

Systems and methods for aircraft wing plug

Fuel delivery system having a fuel oxygen reduction unit

Layered fuselage shield

Multi-engine coordination during gas turbine engine motoring

Hydrogen propulsion systems for aircraft

Rocket-turbine-powered VTOL aircraft

Over-center gimbal actuation lock

Nacelle for gas turbine engine and aircraft comprising the same

Gas turbine engine with clutch assembly

Gas turbine engine outlet guide vane assembly

FUSELAGE SHIELD FOR AN AIRCRAFT WITH AN UNDUCTED ENGINE

PYLON SHAPE WITH GEARED TURBOFAN FOR STRUCTURAL STIFFNESS

Aircraft hybrid propulsion system

Determining presence of internal corrosion within a rotor blade by measuring magnetic characteristic(s)

Aircraft engine

Fan arrangement for a gas turbine engine

FAN ARRANGEMENT FOR A GAS TURBINE ENGINE

Aircraft engine assembly with a supply path to an inter-flow compartment tank of turbine engine

System and method for control for unducted engine

Mount for an airfoil

Fuel tank inerting system and method

VORTEX TURBINES FOR A HYBRID-ELECTRIC AIRCRAFT

Hybrid electric aircraft and powerplant arrangements

Pusher turboprop powerplant installation

Air management system

Aircraft installation for supplying pressurized air

High Speed Aircraft Flight Technologies

Aeronautical car and associated features

Mount arrangement for torque roll vibration isolation

FAN ARRANGEMENT FOR A GAS TURBINE ENGINE

Aero engine flow rate

Aircraft engine assembly with isolation valve outside uncontained rotor impact area

Aircraft nacelle having electric motor and thrust reversing air exhaust flaps

Propulsion system for an aircraft

LIGHT TWIN ENGINE AIRCRAFT

Prognostic health management control for adaptive operability recovery for turbine engines

Distributed propulsion configurations for aircraft having mixed drive systems

Vertical takeoff and landing airframe

Pre-start motoring synchronization for multiple engines

Fan arrangement for a gas turbine engine

Aero engine flow rate

Propulsion engine thermal management system

Heat shield for signature suppression system

Slat-thrust reverser clearance

Hybrid starter motor-generator

Method for mounting an aircraft pylon

Operation of a hybrid electric aircraft propulsion system

Hybrid electric propulsion system and method of operation

Synchronization of generator and electric motor in a hybrid electric aircraft propulsion system

Hybrid electric propulsion system and method of operation

HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM

Aircraft having an aft engine

Gensets and methods of producing gensets from an engine and generator for hybrid electric propulsion

Aircraft electrical network

Geared turbofan gas turbine engine mounting arrangement

Air supply system for an aircraft

Pylon shape with geared turbofan for structural stiffness

Aircraft propulsion system with a low-fan-pressure-ratio engine in a forward over-wing flow installation, and method of installing the same

Hybrid electric aircraft system with distributed propulsion

Aircraft system with distributed propulsion

BATTERY POD UNMANNED AERIAL VEHICLE

Mounting system and mounting method for gas turbine aero engine

Hybrid aircraft propulsion system

Geared turbofan engine mount arrangement

Propeller propulsion unit comprising a heat engine and an electric motor and aircraft comprising such a propeller propulsion unit

Propulsion system cooling control

Chilled working fluid generation and separation for an aircraft

Cryogenic cooling system for an aircraft

Cradle for a turbopropeller engine with integrated air inlet duct

Inlet assembly for an aircraft aft fan

Vertical takeoff and landing airframe

Embedded electric machine

Aerofoil for an aircraft, and an aircraft

Hollow fastener for coupling aerospace structures

Thermal management system

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

Primary support structure for an aircraft power plant support pylon

Primary support strut structure for an aircraft

Compact heat exchange device incorporated into an aircraft pylon

Tiltrotor with inboard engines

ADAPTER RING FOR ABOVE-WING MOUNTING OF BELOW-WING ENGINE

Heat shield for signature suppression system

Propulsion system for an aircraft

Propulsion system for an aircraft

Engine and electrical machine health monitoring

Hinge assembly

Method and system for mounting an aircraft engine

Aircraft and direct drive engine under wing installation

Vertical takeoff and landing airframe

ENGINE ASSEMBLY FOR AN AIRCRAFT, COMPRISING A FRONT ENGINE MOUNT INCORPORATED WITH THE BOX OF THE MOUNTING PYLON

Propulsion system for an aircraft

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

Aircraft with multiple fan propulsion assembly fixed under the wing

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

Tiltrotor aircraft having vertical lift and hover augmentation

Hydraulic torque compensation device

Boundary layer ingestion integration into aft fuselage

Power extraction system and method for a gas turbine engine of a vehicle

Airplane with angled-mounted turboprop engine

BIPARTITE CRADLE WITH SLIDE FOR TURBOMACHINE

Turbine engine having horizontally offset axes

Aircraft having independently variable incidence channel wings with independently variable incidence channel canards

Tiltrotor propulsion system for an aircraft

Embedded electric machine

Embedded electric machine

Thrust force generation device and aircraft

AIR SUPPLY CONTROL DURING MOTORING OF A GAS TURBINE ENGINE

Multi-engine coordination during gas turbine engine motoring

Single engine, asymmetrical vertical take-off and landing (VTOL) aircraft

Pre-start motoring synchronization for multiple engines

Engine air inlet having a double-panel heated wall

Aircraft having a versatile propulsion system

Aircraft with selectively attachable passenger pod assembly

GAS TURBINE ENGINE

Stabilizer assembly for an aircraft AFT engine

VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH HYBRID POWER AND METHOD

Aircraft propulsion assembly with a filtered cradle

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

Propulsion engine for an aircraft

Thrust reverser honeycomb panel load distribution systems and methods

Upper bifi frame for a gas turbine engine and methods therefor

Asymmetry-proof multi-engine aircraft

Aircraft with a propulsion unit with offset fan

Wing leading edge features to attenuate propeller wake-wing acoustic interactions

Engine mount assemblies for aircraft

Aeronautical car and associated features

Propeller blades having icephobic coating

Method and system for open rotor engine fuselage protection

Mobile multi-mode power generation system with mode based adjustable drag configuration

Air intake turboprop assemblies

Ecology system ejector pump shutoff valve

Thermal management system

Tiltrotor with inboard engines

Method for balancing a turbofan engine or other rotating system

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

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

Method and system for cross engine debris avoidance

Aircraft with overlapped rotors

Trailing edge core compartment vent for an aircraft engine

Link for aircraft component mounting

AFT engine mounting link rotational stop collar

Engine assembly for an aircraft comprising a primary structure of a mounting pylon equipped with a box extension comprising two parts in the overall shape of an arch

Aircraft and method of countering aerodynamic effects of propeller wake

AIRCRAFT PROPULSION SYSTEM

ENGINE PROXIMATE NITROGEN GENERATION SYSTEM FOR AN AIRCRAFT

Aerofoil for an aircraft, and an aircraft

Engine installation of vertical take-off and landing (VTOL) aircraft

Rupture constraint mechanism

Aircraft assembly comprising a mounting pylon primary structure integrated to the structure of the wing element

Upper bifi frame for a gas turbine engine and methods therefor

Pusher fan engine with in wing configuration

Gas turbine engine with distributed fans with drive control

Gas turbine engine with embedded distributed fans

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

GAS TURBINE ENGINE WITH DISTRIBUTED FANS DRIVEN ON ANGLED DRIVE SHAFT

Turbomachine comprising a device for the cooling of a pylon

External core gas turbine engine assembly

Pylon for mounting an engine on the structure of an aircraft

Pylon shape with geared turbofan for structural stiffness

Aircraft including turbofan engine and igniter cable

Assembly comprising an articulation spindle supported by a clevis and immobilized in translation by a blocking device integrating a double anti-rotation system

Hybrid gas turbine propulsion system

Blade safety mechanism for open rotor engine system

Tiltrotor aircraft with inboard wing mounted fixed engine arrangement

Cross-wing Twin-Fuselage Aircraft

De-couple geared turbo-fan engine and aircraft

REVERSE FLOW GAS TURBINE ENGINE REMOVABLE CORE

Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan

Nacelle with longitudinal translating cowling and rotatable sleeves

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

Reduced flow field velocity for a propulsor

System and method for mounting an aircraft engine

System and method for reducing the noise of pusher type aircraft propellers

Pylon for fixing an aircraft engine having unducted pusher propellers

HYBRID FREE-AIR GAS TURBINE ENGINE

Support structure

Three wing, six-tilt propulsion unit, VTOL aircraft

Three-wing, six tilt-propulsion unit, VTOL aircraft

AIRCRAFT WITH AT LEAST TWO PROPELLER DRIVES ARRANGED AT A DISTANCE FROM ONE ANOTHER IN THE SPAN WIDTH DIRECTION OF THE WINGS

Device for fastening a turboprop, preferably under an aircraft wing

Three wing, six tilt-propulsion units, VTOL aircraft

Device for locking an engine on an aircraft pylon

Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan

Device for mounting an aircraft turboprop engine comprising hydraulic attachments

Hydraulic system for transmission of forces between an aircraft turboprop and an attachment device

Variable stroke rear landing gear strut

Aircraft fuselage

Torsionally de-coupled engine mount system

Aircraft propulsion unit in multi-fan design

Aircraft wing for over-the-wing mounting of engine nacelle

Noise-shielding wing configuration

Engine mounting structure interposed between an aircraft wing system and said engine

Aircraft engine mounting device attachment arrangement

Ducted open rotor apparatus and method

Aircraft propulsion system comprising four engines with pusher propellers

Torsionally de-coupled engine mount system

Engine mounting structure under an aircraft wing

Structure for mounting a turboprop under an aircraft wing

Engine mounting structure under an aircraft wing

Hanging device to connect an engine to an aircraft wing

Mounting structure for mounting a turboprop under an aircraft wing

Hybrid turbofan and solid oxide fuel cell propulsion system and related methods