Nozzle and vane system for nacelle anti-icing

Nacelle short inlet for fan blade removal

Flow drag mitigation device

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

GAS TURBINE ENGINE WITH ROTATING INLET

Cylindrical case and jet engine

Anti-icing apparatus and system

Fan case for use in a turbofan engine, and method of assembling a turbofan engine

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

Composite material structure

Metal and composite leading edge assemblies

Nacelle core with insert

Front lip of a turbofan engine nacelle comprising hot-air bores upstream from acoustic panels

Nacelle fluid drain

Pressure relief latch

Turbofan engine and method of reducing air flow separation therein

Two-phase type heat transfer device for heat sources operating at a wide temperature range

Sandwich structure having hinge assemblies for accommodating differential in-plane expansion of face sheets

Compartmentalized structure for the acoustic treatment and the de-icing of an aircraft nacelle and aircraft nacelle incorporating said structure

Gas turbine engine cover

Trailing edge core compartment vent for an aircraft engine

Anisotropic reinforcement of composite structures

Aft engine for an aircraft

ACTIVE LAMINAR FLOW CONTROL SYSTEM WITH DRAINAGE

Aircraft having an aft engine

Synergetic noise absorption and anti-icing for aircrafts

Synergetic noise absorption and anti-icing for aircrafts

Fastener assembly for insulation blanket

Fan casing assemblies and method of mounting a cooler to a fan casing

Nacelle comprising an exchanger for cooling a stream of fluid

Pressure relief door assembly

Aircraft turbomachine comprising a heat exchanger of the precooler type

Device for retaining drained fluids for a propulsive assembly

Aircraft engine nacelle

Nacelle inlet with extended outer barrel

Drained fluid evacuation stub for a propulsion assembly

Multi-zone active laminar flow control system for an aircraft propulsion system

Aircraft propulsion assembly with fire extinguishing system

Nacelles for aircraft engines with de-icing systems using a two-phase fluid

Cooled cooling air system for a gas turbine

Detecting damage in a composite panel without removing overlying insulation

Composite fan inlet blade containment

High temperature composite inlet

Propulsion assembly comprising a box for retaining drained fluids

Combined inlet laminar and thrust reverser cascade efflux flow control system

Engine cowling of an aircraft gas turbine

Isentropic compression inlet for supersonic aircraft

Heavy duty gas turbine inlet system

Method of attaching nacelle structure to minimize fatigue loading

Gas-turbine engine with oil cooler in the engine cowling

Track fairing assembly for a turbine engine nacelle

Thrust reverser sliding door assembly

Quick release hinge

Convergent divergent exit nozzle for a gas turbine engine

Core case heating for gas turbine engines

Plated polymer nosecone

Acoustic attenuation with adaptive impedance

Non-metallic engine case inlet compression seal for a gas turbine engine

Turbine engine assembly and method of manufacturing thereof

Method of controlling boundary layer flow

Ventilation of a turbomachine nacelle

Wireless engine monitoring system

NACELLE

Sound-damping arrangement for an engine nacelle and engine nacelle comprising such an arrangement

Automatic deflection limiting latches for a thrust reverser

Methods and apparatus for supporting engines and nacelles relative to aircraft wings

Aerodynamic track fairing for a gas turbine engine fan nacelle

Foldable guiding ventilator cover for an aircraft engine assembly

Positionable ejector member for ejector enhanced boundary layer alleviation

Cowl with pressure driven latch

Propulsion unit for an aircraft

Ventilated drainage system

Aircraft nacelle comprising an improved air intake

Aircraft engine nacelle bulkheads and methods of assembling the same

Ladder cascade torque box

Turbomachine comprising a device for the cooling of a pylon

Bilaterally asymmetric design for minimizing wave drag

Hybrid structure including built-up sandwich structure and monolithic SPF/DB structure

Liquid drainage installation for a rotorcraft engine compartment

Aircraft turbojet engine nacelle comprise an increased-rigidity air intake

Aerodynamic fairing divided into sub-portions

Nacelle inlet lip skin with pad-up defining a developable surface having parallel ruling lines

Tandem thrust reverser with multi-point actuation

Tandem thrust reverser with multi-bar linkage

Jet engine with deflector

Gimbal pin for jet propulsion system

METHOD FOR PRODUCING FOAM PANELS, ESPECIALLY FOR THE FIELD OF AERONAUTICS

Arrangement for a tank between a nacelle cowling and a turbomachine

Firewall, pylon of aircraft, and aircraft

Fireshield fastener hood

Pivot thrust reverser with multi-point actuation

Air inlet structure for a turbojet engine nacelle of laminar type

Low shock strength propulsion system

Jet engine with deflector

Composite panel having a built-in duct

Apparatus and method for configuring control message in broadcasting system

Nacelle for a high bypass ratio engine with multiple flow paths

Monolithic fan cowl of an aircraft engine and a manufacturing method thereof

Tandem thrust reverser with sliding rails

Pivot thrust reverser surrounding inner surface of bypass duct

Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system

Tilt rotor aircraft with fixed engine arrangement

Method of manufacturing a sound absorbing panel

Engine cowl incorporating an equipment ventilation circuit

Lip unit for an electrically deiced turbojet engine nacelle

System and method for minimizing wave drag through bilaterally asymmetric design

Acoustic structure with increased bandwidth suppression

Gas-turbine engine with telescope-type air inlet of the engine cowling (nacelle)

LOWER FIREWALL PLATE GROMMET

Nacelle electrical locking system for leading edge of openable panel

Nacelle scoop inlet

AFT cascade translating variable area fan nozzle

Anti-fire seal assembly and nacelle comprising such a seal

Propfan engine

Acoustic structure with increased bandwidth suppression

Thermal insulation support

Aerodynamic element for an aircraft nacelle

Turbojet engine nacelle with variable ventilation outlet cross section

Seal assembly

Two-surface sandwich structure for accommodating in-plane expansion of one of the surfaces relative to the opposing surface

Nacelle with longitudinal translating cowling and rotatable sleeves

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

Engine inlet varying impedance acoustic liner section

Nacelle

Aeroelastic tuned mass damper

AIR INLET DUCT FOR A TURBOJET NACELLE

Low shock strength propulsion system

Supersonic aircraft jet engine installation

Fireshield fastener hood

Nacelle flow assembly

TURBOJET ENGINE NACELLE PROVIDED WITH A COOLING ASSEMBLY FOR COOLING A COMPONENT

AIRCRAFT ENGINE COWL AND PROCESS THEREFOR

Aircraft gas-turbine engine with oil cooler in the engine cowling

CONNECTING DEVICE PARTICULARLY ADAPTED FOR THE CONNECTION BETWEEN AN AIR INTAKE AND AN ENGINE OF AN AIRCRAFT NACELLE

Nacelle incorporating an element for connecting a lip and an acoustic attenuation panel together

Fluid-cooling device for a turbine engine propulsive unit

Tilt rotor aircraft with fixed engine arrangement

Isentropic compression inlet for supersonic aircraft

ATTENUATION OF OPEN ROTOR NOISE

Apparatus and method for shielding a thrust reverser structure from engine heat

Spring loaded pressure relief door

LEADING EDGE STRUCTURE, IN PARTICULAR FOR THE AIR INTAKE OF THE NACELLE OF AN AIRCRAFT ENGINE

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

Isentropic compression inlet for supersonic aircraft

Air discharging device for an aircraft double-flow turbine engine

Engine and pod assembly for an aircraft, equipped with an anti-icing device including a source of radiation and pulse control unit connected to the source of radiation

Rear section of aircraft nacelle and nacelle equipped with such rear section

SEALING JOINT WITH INTEGRATED MATING SURFACE

Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser

Unitized engine nacelle structure

OVERPRESSURE HATCH INTENDED TO BE MOUNTED ON A WALL OF A TURBOJET ENGINE NACELLE

Single effect hydraulic cylinder

Double-ducted fan

HOUSING ASSEMBLY FOR AN ELECTRICAL DEVICE

Jet engine nacelle having dampers for half-shells

Aircraft propulsion system

COUPLING FOR INDUCING HIGH TEMPERATURE DROPS BETWEEN CONNECTED PARTS ON AN AIRCRAFT

Method for making deicing system on a nacelle panel

Aircraft de-icing device and engine nacelle of an aircraft gas turbine with de-icing device

Thermally actuated passive gas turbine engine compartment venting

Nacelle flow assembly

Double seal

Wireless engine monitoring system

Monolithic structure for mounting aircraft engine

Aircraft engine nacelle with translating inlet cowl

Nacelle rear assembly for turbojet engine

Integrated inlet design

Detecting ice buildup on an aircraft engine and actuating the turbofan exit nozzle to break the ice

Low shock strength propulsion system

Lockable guiding system for a mobile part of a nacelle

Gas turbine engine nacelle having a symmetric flowpath

Structural nacelle

Wireless engine monitoring system

Aircraft engine structure-mounted aim-point biasing infrared countermeasure apparatus and method

Thermal management system integrated pylon

Fixing System for a Component of a Turbojet Pod

Nacelle flow assembly

Low shock strength inlet

Articles with reduced fluid dynamic drag

Systems Involving Inlet-Mounted Engine Controls

Wireless engine monitoring system

Engine cooling

NACELLE WITH ARTICULATING LEADING EDGE SLATES

Isentropic compression inlet for supersonic aircraft

NACELLE ASSEMBLY WITHOUT LOWER BI-FI SPLITTER

Joint for a shape memory material

Aeroengine drain assembly

Protection panel for aircrafts

Nacelle drag reduction device for a turbofan gas turbine engine

Aircraft engine structure-mounted aim-point biasing infrared countermeasure apparatus and method

Turboprop unit for aircraft with improved aerodynamic installation

Air input device for a turboprop engine

Apparatus and methods for support of propulsion systems interconnect members

Wireless engine monitoring system

Cowl structure for a gas turbine engine

Engine cooling

Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position

Soundproofing panel with beads, and a method of manufacture

Annular acoustic panel

Laminar flow nacelle for an aircraft engine

Wireless engine monitoring system

Tailcone and conduit ventilation system with variable internal flow distribution

Turbine engine having a variable engine intake system

Apparatus for ingesting boundary layer flow for an aircraft

Engine controller for a gas turbine engine

Translating wire harness

High flow plug nozzle apparatus and method of using the same

Method for making contoured acoustic structures

Methods and apparatus for supporting engines and nacelles relative to aircraft wings