PROPULSION SYSTEM FOR AN AIRCRAFT COMPRISING AN AT LEAST PARTIALLY VENTILATED PIPE CIRCUIT

THERMAL PROTECTION DEVICE FOR A LOWER LONGITUDINAL MEMBER OF AN AIRCRAFT BOX STRUCTURE

PROPULSION ASSEMBLY COMPRISING A DAMPING REAR ENGINE ATTACHMENT, AIRCRAFT HAVING AT LEAST ONE SUCH PROPULSION ASSEMBLY

HYBRID ELECTRIC IDLE AND BRAKING FOR AN AIRCRAFT

ELECTRIC MACHINES FOR AIRCRAFT ENGINE FAULT DETECTION

PARALLEL POWER SOURCE FOR AIRCRAFT

TURBOFAN ENGINE INCLUDING A FAN ACTUATION SYSTEM

METHOD AND UNIT FOR CONTROLLING A MOTOR ASSEMBLY

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

HIGH-POWER HYBRID-ELECTRIC PROPULSION SYSTEMS AND METHODS

AIRCRAFT HYBRID ELECTRIC PROPULSION AND ATTITUDE CONTROLLER

Parallel power source for aircraft

PARALLEL HYBRID POWERPLANT WITH TURBOFAN ENGINE CORE

AIRCRAFT WITH HIGH TRANSPORT EFFICIENCY AND A METHOD OF OPERATION

PROPULSION SYSTEM ARCHITECTURE

Electric jet engine

MONITORING AN ANTI-LEAK VALVE IN A JET ENGINE

HYBRID PROPULSION SYSTEM FOR AIRCRAFT

PROPULSION SYSTEM ARCHITECTURE

NARROW VEHICLES AND AIRCRAFT VEHICLES

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

HYBRID-ELECTRIC SINGLE ENGINE DESCENT FAILURE MANAGEMENT

Electric power system for a vehicle

High-speed VTOL drive-shaft systems and methods

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

Hybrid-electric single engine descent failure management

Jam detection and jam tolerant motion control

Nacelle air outlet for aircraft turbojet engine comprising a straightening device for facilitating a reverse thrust phase

Machine for generating lift using compressed air as power source and operation method thereof

Hybrid electric engine including auxiliary compressor

Electrical connection for an electric machine in an aircraft turbomachine

Methods for reforming ammonia

Hybrid electric engine with electric tip clearance mechanism

Systems and methods for processing ammonia

Aircraft engine with opposed piston engine

RENEWABLE FUEL POWER SYSTEMS FOR VEHICULAR APPLICATIONS

Hybrid electric idle and braking for an aircraft

APPARATUS AND METHOD FOR FLUID MANIPULATION

Aircraft propulsion system with hydrocarbon and hydrogen fuel adaption for reduced condensation trail impact

Aircraft electric motor

Turbo engine with cooler for cooling inlet air and turbine for expanding cryogenic fuel

ELECTRIC POWER SYSTEM FOR A VEHICLE

FLAT PLATE AIRFOIL PLATFFORM VEHICLE

VEHICLE AND PROPULSION SYSTEM WITH GASEOUS FUEL SYSTEM

Aircraft propulsion device

Dual drive hybrid electric power plant for aircraft

GAS TURBINE ENGINE WITH CABIN BLOWER SYSTEM

Aircraft engines with a fuel cell

Turbojet engine fan casing

Personal Aircraft Assembly

Assembly for an aircraft having a wing and an engine pylon for coupling a jet engine to said wing

Electric power system for a vehicle

High temperature clamp for a sensing assembly

Suspension assembly for a turbine engine

System for converting and transporting electrical energy for the internal hybridization of an aircraft with turbojet engines

Flight system

Electric architecture for hybrid propulsion

Turbomachine comprising a means of suspension

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

COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS

COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS

COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS

Ducted fans having fluidic thrust vectoring

Ducted fans having edgewise flow augmentation

Fluidic roll control systems for use in forward flight

Fluidic yaw control systems for use in hover

Exhaust cone with flexible fitting

Gas turbine engine with axial movable fan variable area nozzle

Assembly for aircraft turbine engine comprising an improved system for lubricating a fan drive reduction gear in case of autorotation of the fan

Aircraft brake cooling systems and methods

Flying object

Electrical power generation from turbine engines

Electrical harness for a turbomachine

Reduction gear for turbomachine equipped with an electric generator

Dual voltage low spool generator

Efficient engine start

Method and system to promote ice shedding from rotor blades of an aircraft engine

Turbomachine nozzle with an airfoil having a circular trailing edge

COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS

Fire fighting system using drone

Vehicle system

Suspension device

Lightweight parallel combustion lift system for vertical takeoff aircraft

Load-bearing structure intended to be mounted on a gas generator

CONVERTIPLANE

Propelling nozzle for a turbofan engine on a supersonic aircraft

Aircraft propulsion assembly provided with a rotary transformer for supplying the blades with electrical energy

Compound helicopter having a tiltable jet engine

Rocket propelled drone

Method and tool for optimizing fuel/electrical energy storage allocation for hybrid-electric aircraft

Nacelle

Turbo engine with cooler for cooling inlet air and turbine for expanding cryogenic fuel

Nacelle for turbojet engine, comprising openings of front cowls for access to fixing points of the nacelle

Method for manufacturing a structural and/or acoustic panel for a nacelle of an aircraft propulsion unit, and corresponding device

Propulsion unit for aircraft comprising an assembly box-type structure in the six o'clock position

Fastening device for a heat-shield panel

Gas turbine engine with differing effective perceived noise levels at differing reference points and methods for operating gas turbine engine

Rectification structure body and flying vehicle

Power driver of unmanned aerial vehicle

Aircraft propulsion system comprising a mobile articulated cowl

Aircraft engine assembly with boundary layer ingestion including an electric motor and a cooling system partially arranged in the exhaust cone

Propulsion engine thermal management system

Fuel pump override control method

Isolated turbine engine cooling

Concentric turbomachine with electric machine

Supersonic aircraft propulsion installation

ADJUSTMENT FEATURES FOR ENGINE COWL DOOR

SUPERCHARGING SYSTEMS FOR AIRCRAFT ENGINES

Hybrid propulsion engines for aircraft

Hybrid propulsion engines for aircraft

ROTARY-WINGED VEHICLE SYSTEMS AND DEVICES

Electric propulsion motor cooling system and method

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

Method and system for setting an acceleration schedule for engine start

Slope-based event detection for turbine engines

Reinforced composite blade and method of making a blade

Air start unit for starting and servicing jet engines in aircraft

Multi-Hybrid Aircraft Engine

Use of infrared transparent airframe materials for passive cooling of internal components

Seal system for variable geometry gaps in aircraft systems

Gas turbine engine with axial movable fan variable area nozzle

Hybrid aircraft propulsors having electrically-driven augmentor fans

Scramjets and associated aircraft and methods

Nacelle

Cooling system in a hybrid electric propulsion gas turbine engine for cooling electrical components therein

System for controlling the pitch of fan blades of a turbine engine, the system having a feathering-locking peg

System and method of operating a ducted fan propulsion system during aircraft taxi

Hybrid-electric propulsion system for an aircraft

PROPULSION SYSTEM FOR AN AIRCRAFT

PROPULSION SYSTEM FOR AN AIRCRAFT

Engine and electrical machine health monitoring

Method for rating a propulsion unit comprising a main engine and an auxiliary engine

Adjustable length beam between cowl hinges

Methods for balancing aircraft engines based on flight data

Methods for optimized engine balancing based on flight data

Lifting system machine with methods for circulating working fluid

Reducing an acoustic signature of a gas turbine engine

Flight vehicle air breathing propulsion system with isolator having obstruction

Flight vehicle air breathing engine with isolator having bulged section

Composite structure assembly having an interconnected layered core

Propulsion system for an aircraft

Kevlar wrap removal from fan casing

Method and system for setting an acceleration schedule for engine start

Modified start sequence of a gas turbine engine

PROPULSION UNIT COMPRISING A MAIN ENGINE AND AN AUXILIARY ENGINE

Method of displaying data in an aircraft

TURBOFAN NACELLE INCLUDING A REVERSER FLAP

Acoustic absorber cell for a turbojet, and an associated acoustic treatment panel

Multi-layer thermal insulator apparatus and methods

Flying object

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

Systems for generating auxiliary electrical power for jet aircraft propulsion systems

Engine turning motor via pneumatic or hydraulic motor

Flight vehicle engine with finned inlet

AIRCRAFT GAS TURBINE HAVING A VARIABLE OUTLET NOZZLE OF A BYPASS FLOW CHANNEL

Modified start sequence of a gas turbine engine

Heat exchanger assembly for a gas turbine engine propulsion system

Thrust reverser actuating

SUPPLY DEVICE FOR AN ELECTRIC ACTUATOR SYSTEM

VTOL aircraft with jet engine coupled to downward thrust nozzles

Twin shafts driving adjacent fans for aircraft propulsion

Acoustic attenuation structure with a plurality of attenuation degrees for a propulsion assembly of an aircraft

Propulsion assembly comprising a duct for feeding the gas generator in an inter-duct casing

Commercial supersonic aircraft and associated systems and methods

Fully integrated hybrid electric jet engine

SYSTEM AND METHOD FOR AUGMENTING A PRIMARY POWERPLANT

Fan cowl fairing restraining system

Control system for a cabin blower system

Hidden thrust reverser blocker door link arm fitting

Fluid flow machine with high performance

AIRCRAFT GAS TURBINE ENGINE NACELLE

Gas turbine engine with axial movable fan variable area nozzle

Gas turbine engine with axial movable fan variable area nozzle

Turbine engines with variable area nozzle

ELECTRIC HEATING FOR FUEL SYSTEM COMPONENTS

Gas turbine engine with axial movable fan variable area nozzle

Acoustically-Enhanced Separators for Aircraft Engines

Power system for aircraft parallel hybrid gas turbine electric propulsion system

Descent operation for an aircraft parallel hybrid gas turbine electric propulsion system

Tip clearance control system

Aircraft with injection cooling system and injection cooling system

Method and system for bowed rotor start mitigation using rotor cooling

Aircraft turbojet engine nacelle

Electrical assist for aircraft

Nacelle rear assembly for a turbojet engine comprising a suspension cradle

Nacelle rear assembly for a turbojet engine comprising a cradle for a core-type mast

IMAGING A ROTATING COMPONENT

Aircraft propulsion assembly with a filtered cradle

Apparatus for supporting a nacelle of an aircraft engine

SECURING A TRANSLATING FANLET FOR AN AIRCRAFT PROPULSION SYSTEM NACELLE

ADJUSTMENT FEATURES FOR ENGINE COWL DOOR

Auxiliary drive bowed rotor prevention system for a gas turbine engine through an engine accessory

Modified start sequence of a gas turbine engine

Thrust reverser actuating

Methods and apparatus to adjust bleed ports on an aircraft engine

Inlet turbine for high-mach engines

Turbine blade monitoring

Nozzle and vane system for nacelle anti-icing

Centripetal aerodynamic platform spacecraft

Core compartment ventilation devices for nacelles of gas turbine engines for cooling a core compartment of a gas turbine engine

Device for attaching an air inlet onto a fan casing of an aircraft turbojet nacelle

Cylindrical case and jet engine

Propulsion unit for an aircraft and method for opening a movable cowl of said propulsion unit

EXHAUST NOZZLE FOR GAS TURBINE ENGINE

REDUCED NOISE TURBOFAN AIRCRAFT ENGINE

Hybrid exhaust nozzle

Detachable Pilotable Capsules and Aircrafts Including Detachable Pilotable Capsules

Manhattan dual FDGS aux pump design

Turbine blade and aircraft engine comprising same

Turbofan engine and method of reducing air flow separation therein

Propulsive assembly for aircraft comprising a turbojet fitted with a fan with removable blades

COMPOSITE COMPRESSOR VANE OF AN AXIAL TURBINE ENGINE

Aircraft pneumatic system

Aircraft propulsion assembly

Containment for a continuous flow machine

Directed Energy Deposition to Facilitate High Speed Applications

Gas turbine engine with axial movable fan variable area nozzle

Gas turbine engine with axial movable fan variable area nozzle

Gas turbine engine with axial movable fan variable area nozzle

System and method for propeller pitch control

Pitch change mechanism for a bladed rotor

Battery arrangments for gas turbine engines

Rotary machine

Injector nozzle configuration for swirl anti-icing system

Fluidic propulsive system and thrust and lift generator for aerial vehicles

INFLIGHT POWER MANAGEMENT FOR AIRCRAFT

Propulsion assembly for an aircraft

Casing made of organic matrix composite material that facilitates the discharge of smoke

Telescoping electrical cable

Back mounted flight machine

Unducted propeller turboshaft engine provided with a reinforcing shell integrating pipe segments

Aircraft gas turbine propulsion engine control without aircraft total air temperature sensors

PITCH CONTROL OF CONTRA-ROTATING AIRFOIL BLADES

Adaptive aircraft engine and aircraft having an adaptive engine

Disc-shaped turbo-jet aircraft

Nacelle for an airplane turbojet

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

Test bench for an aircraft turbojet engine, with shutters

Engine cowling of an aircraft gas turbine

Flying car or drone

Isentropic compression inlet for supersonic aircraft

METHOD FOR REPAIRING SANDWICH PANELS MADE OF COMPOSITE MATERIALS INVOLVING THE CREATION OF A CORE OR OF A MOULD USING STEREOLITHOGRAPHY

Engine system for vertical and short take off and landing (V/STOL) aircraft

Isostatic suspension of a turbojet by rear double support

Method and module for filtering a raw setpoint

Aircraft with counter-rotating turbofan engines

VARIABLE PITCH MOUNTING FOR AIRCRAFT GAS TURBINE ENGINE

AIRCRAFT

Systems for generating auxiliary electrical power for jet aircraft propulsion systems

Propulsion unit for an aircraft

VTOL aircraft with a thrust-to-weight ratio smaller than 0.1

REMOTELY OR AUTONOMOUSLY PILOTED REDUCED SIZE AIRCRAFT WITH VERTICAL TAKE-OFF AND LANDING CAPABILITIES

Device for suspending a casing, a turbine engine and a propulsion assembly

System and method for minimizing wave drag through bilaterally asymmetric design

Driven aircraft, in particular an aircraft designed as a flying wing and/or having a low radar signature

Apparatuses and systems with vertically and longitudinally offset mounting flanges

Pitch control of contra-rotating airfoil blades

Supersonic aircraft jet engine installation

Aircraft with rear annular tail

Isentropic compression inlet for supersonic aircraft

Aircraft, propulsion system, and system for taxiing an aircraft

Aircraft and propulsion system

Isentropic compression inlet for supersonic aircraft

Gas turbine engine with axial movable fan variable area nozzle

Aircraft turbine engine and use of such a turbine engine

Hybrid propulsive engine including at least one independently rotatable propeller/fan

Hybrid propulsive engine including at least one independently rotatable compressor stator

Hybrid propulsive engine including at least one independently rotatable compressor rotor

Hybrid propulsive engine including at least one independently rotatable turbine stator

Aircraft with jet engines arranged at the rear

Systems Involving Inlet-Mounted Engine Controls

Solar energy augmented jet aircraft

THRUST GENERATOR FOR A PROPULSION SYSTEM

Air-Jet Propeller

Isentropic compression inlet for supersonic aircraft

Quiet airplane configuration

Turbofan or turbojet arrangement for vehicles, craft, aircraft and the like

Aircraft engine mounting assembly

Low observable aircraft having a unitary lift fan

Centrifugal-force-propulsion and control system (CFPandCS) and applications

System and method of operating a ducted fan propulsion system inflight

Energy-efficient launch system for aerial vehicles

Jet engine gas lasers

Thermal management system