Turbine engine stator vane, fan casing comprising such a vane, thrust reverser system of a turbine engine equipped with such a vane and turbine engine equipped with said vane, said casing or said system

Combined hybrid thermionic and thermoelectric generator

Convertible engine exhaust for rotocraft

EXHAUST INFRARED SIGNATURE REDUCTION ARRANGEMENT AND METHOD OF REDUCING TEMPERATURE OF AT LEAST A PORTION OF AN EXHAUST DUCT

Vibration damping drag link fitting for a thrust reverser

Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices

Gas turbine engine cover

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

INTEGRATED AIRCRAFT PROPULSION SYSTEM

Ejector and airfoil configurations

Fluidic propulsive system

Fluidic propulsive system and thrust and lift generator for aerial vehicles

Turboprop engine assembly with combined engine and cooling exhaust

Telescoping electrical cable

Preloaded AFT vent area for low pressure fan ducts

Thrust recovery in airplanes

GENERATOR FOR AN AIRCRAFT

Adaptive engine exhaust signature suppressor

Aircraft

Suspension of a tubular element in an aircraft compartment

Exhaust arrangement for aircraft having sensor

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

HIGH TURNING ANGLE EJECTOR COOLED TURBINE ENGINE EXHAUST DUCT

Slat-thrust reverser clearance

Automatic bifurcation latch systems for a thrust reverser

Alignment system for exhaust installation

Divergent flap

Aircraft with a fuselage that defines at least an interior region and a drive system accommodating region

Nacelle for an aircraft engine with variable section nozzle

ACTIVE LOCK WITH MOBILIZATION ASSISTANCE AND THRUST REVERSER INCORPORATING SUCH A LOCK

Vehicle attitude control using jet paddles and/or movable mass

Aircraft and airborne electrical power and thermal management system

Stepped fairing modulated exhaust cooling

Nacelle for a turbojet engine with a variable nozzle

Device for controlling the power of an engine and for controlling a thrust reverser device

Nacelle

Core cowl for a turbofan engine

Aerodynamic track fairing for a gas turbine engine fan nacelle

Reverse core engine with thrust reverser

Asymmetric fan nozzle in high-BPR separate-flow nacelle

System, apparatus, and method for thrust vectoring

HYDRAULICALLY ACTUATED MECHANICAL LOCK ASSEMBLY

AFT pylon fairing for aircraft

System and method for aft mount of gas turbine engine

Aircraft with an engine having a by-pass air inlet opening and a bleed air outlet

Optimising the availability of a thrust reverser

Gas turbine engine with embedded distributed fans

Methods and apparatus for passive thrust vectoring and plume deflection

Method and device for controlling at least one actuator control system of an aircraft, associated computer program product and aircraft

Box wing with angled gas turbine engine cores

Laser-charged high-speed propulsion system and method for production of high-powered laser

Compact Nacelle With Contoured Fan Nozzle

AIRCRAFT ENGINE

Turbojet engine nacelle with downstream section

Clocked thrust reversers

Aircraft with forward sweeping T-tail

Asymmetric thrust reversers

Aircraft vapour trail control system

Aircraft vapour trail control system

Turbomachine comprising a device for the cooling of a pylon

Stabilizer with structural box and sacrificial surfaces

Aircraft comprising a control device for a jet pipe nozzle with variable cross-section powered by two independent electrical power supplies

Engine pylon having a drain

Thrust deflecting device and aircraft engine

Airtrain & Hydroairtrain

Bifurcated ducts including plenums for stabilizing flow therethrough and exhaust systems including the same

Detection-cord attachment device, in particular for an overheating and leak detection system on a gas pipe in an aircraft

Nacelle

Duct apparatus for use with aircraft and related methods

AIRCRAFT GAS TURBINE COMPRISING AN ENGINE COWLING WITH A THRUST-REVERSER DEVICE

Exhaust stream mixer

Gas turbine cowl

FLAP DRIVING DEVICE IN PARTICULAR FOR AN ADAPTIVE NOZZLE

AIRCRAFT AND AIRBORNE ELECTRICAL POWER AND THERMAL MANAGEMENT SYSTEM

Thrust-reversal device for an aircraft including at least two thrust reversers

Gimbal pin for jet propulsion system

THRUST REVERSER DOORS HAVING SIDE OPENINGS

Exhaust centerbody for a turbine engine

Thrust reverser control system

Aircraft wing

Method for discharging exhaust gas from a gas turbine and exhaust assembly having optimised configuration

Flattened nacelle of a turbojet engine

Nacelle for a high bypass ratio engine with multiple flow paths

Actuator for aircraft turbine engine nacelle with notably one-piece annular rear part

Reverse core engine thrust reverser for under wing

Rotary wing aircraft having collocated exhaust duct and propeller shaft

AFT exhaust system for rotary wing aircraft

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

System for supplying an aircraft with inert gas, method for supplying an aircraft with inert gas, use of a membrane and aircraft

Aircraft turbojet engine thrust reverser with a reduced number of latches

Upturned exhaust system for rotary wing aircraft

Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method

AFT cascade translating variable area fan nozzle

Fluid management apparatus and method

Pipe having an upstream core having a sharp curvature

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

Turbojet engine nacelle reinforcing structure

Turbojet engine nacelle with variable ventilation outlet cross section

Nacelle for an aircraft bypass turbojet engine

Nacelle

Method for cooling a thermal protection floor of an aft aerodynamic fairing of a structure for mounting an aircraft propulsion system

Gas turbine engine with fan variable area nozzle for low fan pressure ratio

GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE

GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE FOR LOW FAN PRESSURE RATIO

Gas turbine engine with fan variable area nozzle to reduce fan instability

Gas turbine engine with fan variable area nozzle for low fan pressure ratio

AIRCRAFT

Propulsive unit for an aircraft

Arrangement of thrust reverser flap link rods on the internal fixed structure of a turbojet engine nacelle

Nacelle for an aircraft engine with variable cross-section nozzle having a rack and pinion actuator assembly

Cascade type thrust reverser having a pivoting door

Multi axis slide carriage system

Turbine engine with access door to engine core

NACELLE FOR VARIABLE SECTION NOZZLE PROPULSION UNIT

Distributed exhaust system

GAS TURBINE ENGINE TRANSITION DUCTS

Aircraft and airborne electrical power and thermal management system

Aircraft capable of hovering having an exhaust duct with thermoelectric conversion circuit

Heteroaryl Amide Analogues

CONVERGING BLOCKER DOOR SYSTEM FOR USE WITH A THRUST REVERSER

Gas turbine engine with variable area fan nozzle

Aircraft engine nacelle comprising a mobile cowl moved by electric motors

COMPLIANT SEALING JOINT

Variable geometry aircraft pylon structure and related operation techniques

Gas turbine engine with axial movable fan variable area nozzle

Actuation mechanism for a convertible gas turbine propulsion system

Actuator system for a mobile panel of a nacelle of a turbojet

Control system for a turboreactor nacelle

Pylon for attaching a gas turbine engine

Guide system for nacelle 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

Guide system for nacelle assembly

Integrated aircraft

Thrust reverser actuation

Nacelle with an adaptable outlet section

Exhaust eductor system with a recirculation baffle

HEAT RECOVERY SYSTEM

Nacelle with a variable nozzle section

Jet engine nozzle exit configurations and associated systems and methods

AFT pylon fairing for an aircraft engine suspension system

Exhaust for a gas turbine engine

Engine exhaust system with directional nozzle

Systems and methods for passively directing aircraft engine nozzle flows

Device for reducing turboprop infrared emissions

Nacelle for aircraft engine having a nozzle with a variable section

AIRCRAFT DRAG MANAGEMENT STRUCTURE

Jet engine nozzle exit configurations and associated systems and methods

Exhaust plenum for a turbine engine

Engine exhaust system

Jet engine exhaust nozzle and associated system and method of use

Turboprop propulsion unit with pusher propeller

Continuous composite fan duct and thrust reverser

Engine assembly for aircraft with sliding nacelle

Nacelle rear assembly for turbojet engine

Nacelle for double flow engine

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

Variable slope exhaust nozzle

Bypass turbojet engine nacelle

LOW NOISE AIRCRAFT

Systems and methods for reducing noise from jet engine exhaust

Actuation mechanism for a convertible gas turbine propulsion system

Fan nozzle of adjustable section

Aircraft pod and aircraft equipped with at least one such pod

Composite heat shield

Ceramic heat shield

AIRCRAFT DEFENSE SYSTEM AND METHOD

Solar energy augmented jet aircraft

Gas turbine engine with axial movable fan variable area nozzle

Superplastic forming of titanium assemblies

Single-stage hypersonic vehicle featuring advanced swirl combustion

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

Infrared suppression system

Arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine

Systems and methods for passively directing aircraft engine nozzle flows

Aircraft airframe architectures

Exhaust eductor system with a recirculation baffle

Turbofan jet engine

Vortex generator at hot gas output

Gas turbine engine flow reverser

Outlet device for a jet engine and a jet engine comprising such an outlet device

Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine

AIRFOIL HAVING A MOVABLE CONTROL SURFACE

Elbow-shaped propulsion gas exhaust assembly in an aircraft

Exhaust assembly forming a horizontal propulsion gas elbow in an aircraft

Method and apparatus for generating lift

Exhaust assembly forming a horizontal propulsion gas elbow in an aircraft

Turbofan exhaust system

Air guiding flap of an aircraft comprising control of the pressure forces impinging thereon, process for adjusting the position of an air guiding flap and ram air system including such an air guiding flap

Superplastic forming of titanium assemblies

Yaw control device for a nozzle having a rectangular outlet section

Helicopter defense system and method

Infrared suppression system

Fan cowl door elimination

Method for resistance welding two sheet metal elements together

Aircraft braking method and ducted fan jet engine for implementing the method

Method and apparatus for suppressing infrared signatures

Ejector cooled nozzle

Methods and apparatus for exhausting gases from gas turbine engines

Turbine engine arrangements

Aircraft protection method and system

Exhaust nozzle segmented basesheet and production method thereof

Variably angled propulsion/steering system

Control system for vertical take off and land (VTOL) aircraft

Blended wing aircraft

Turbine exhaust duct with stiffeners for aircraft engines

Blended wing aircraft

Blended wing aircraft

Exhaust case for aircraft engine

Bifurcated exhaust duct for hybrid aircraft powerplant

Variable area nozzle assembly for an aircraft propulsion system

Aircraft propulsion system with turbine engine and exhaust condenser

Aircraft propulsion system with turbine engine and exhaust condenser

Aircraft propulsion system with turbine engine and exhaust condenser

Dual flowpath exhaust for fuel cooling in a hypersonic propulsion system

Pressure equalization in a dual flow path exhaust of a hypersonic propulsion system

Processing vapor exhausted by thermal management systems

Systems and methods for improved runway and roadway braking

Mechanically attached thermal protection system

Aircraft contrail detection