TURBO-COMPOUNDED ENGINE WITH EXHAUST DUCT ACOUSTIC ARRANGEMENT

COMBUSTOR FOR A TURBINE ENGINE INCLUDING AN INSULATING MEMBER

COUPLING ASSEMBLY FOR A TURBINE ENGINE

COOLED VARIABLE AREA NOZZLE FOR AN AIRCRAFT ENGINE

ARTICULATABLE DUCTING SYSTEMS

ASSEMBLY FOR AN EJECTION CONE OF AN AIRCRAFT TURBOMACHINE

TURBO-COMPOUNDED ENGINE WITH EXHAUST DUCT ACOUSTIC ARRANGEMENT

Seal system using layers of seal segments forced into sealing engagement using tension cable

EVANESCENT OR FUGACIOUS THRUST DEFLECTOR

Coupling assembly for a turbine engine

EXHAUST ASSEMBLY FOR PURGING A NACELLE CAVITY OF A PROPULSION SYSTEM

Methods involving and apparatuses for a turbine engine fairing

Fluoroelastomer erosion coating repair

Combustor assembly for a turbine engine

Featured bullnose ramp for a thrust reverser system

CMAS resistant environmental barrier coating system

Core duct assembly

Structural panel with integrated coupler

Flexible aft cowls for aircraft

Exhaust nozzle of a gas turbine engine

Method to re-loft a redesigned jet engine primary exhaust nozzle for an existing airplane to provide clearance to aircraft heat shield structure to prevent contact, fracture, and liberation of portions of the nozzle which might cause hazard to continued safe flight

Method for injecting a loaded slurry into a fibrous texture

Seal coats to prevent silicon loss during re-melt infiltration of Si containing composites

Rotating detonation propulsion system

ROTATING DETONATION ACTUATOR

Combustor assembly for a turbine engine

Slat-thrust reverser clearance

Variable area fan nozzle with wall thickness distribution

Nacelle

Engine assembly with combined engine and cooling exhaust

Methods for forming vertically cracked thermal barrier coatings and articles including vertically cracked thermal barrier coatings

Reinforced oxide-oxide ceramic matrix composite (CMC) component and method of making a reinforced oxide-oxide CMC component

Aircraft component and gas turbine engine for aircraft

Convergent divergent exit nozzle for a gas turbine engine

Gimballed Augmentation Shroud

Gas turbine duct liner coupling assembly

EXHAUST ASSEMBLY WITH VORTEX GENERATOR

Nacelle

Method of manufacturing a composite sandwich panel for an aircraft propulsion unit

Attachment of ceramic matrix composite panel to liner

Self-locking alignment at a nacelle interface

Fan nacelle trailing edge

SYSTEM AND METHOD FOR REDUCTION OF TURBINE EXHAUST GAS IMPINGEMENT ON ADJACENT AIRCRAFT STRUCTURE

Gas turbine exhaust assembly

Seal coats to prevent silicon loss during re-melt infiltration of Si containing composites

Nacelle

Infrared suppression system in a gas turbine engine

Composite component

Engine assembly with combined engine and cooling exhaust

Ultra hush exhaust system (UHES)

GAS TURBINE ENGINE VANE SPLITTER

Compression cowl for jet engine exhaust

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

Trailing edge core compartment vent for an aircraft engine

Variable area fan nozzle with wall thickness distribution

ROUNDED EDGES FOR GAS PATH COMPONENTS

Methods for treating field operated components

Fan case and fan case manufacturing method

Slat-thrust reverser clearance

Protective panel and frame therefor

Large displacement high temperature seal

Convergent divergent exit nozzle for a gas turbine engine

High performance convergent divergent nozzle

Low-thickness thermostructural composite material part, and manufacture method

Method for controlling a lifting jack for an aircraft engine nacelle, a jack-type lifting system implementing the method and the thus equipped nacelle

Jet noise suppressor

Ceramic matrix composite article and process of fabricating a ceramic matrix composite article

Nacelle

Hybrid Flow Control Method

Adjustable cable for exhaust duct liner hanger

Duct

Non-Axisymmetric Exit Guide Vane Design

Compliant heat shield liner hanger assembly for gas turbine engines

Attachment of ceramic matrix composite panel to liner

Hybrid IFS with metallic aft section

Industrial gas turbine exhaust system diffuser inlet lip

Exhaust centerbody for a turbine engine

Structure for fastening after-body parts of an aeroengine

Exhaust duct liner rod hanger

Panel attachment system

Panel attachment system

Convergent-divergent nozzle for a turbine engine

Panel attachment system

Panel attachment system and a method of using the same

Variable area fan nozzle with wall thickness distribution

Spherical collet for mounting a gas turbine engine liner

Reduced pressure-drop pipe element

Adjustable hanger and method for gas turbine engine exhaust liner

Leaf spring hanger for exhaust duct liner

Variable jet engine outlet with a mainly circle sector-formed cross section

Seal assembly for liners of exhaust nozzle

Panel support hanger for a turbine engine

Sliding U-joint hanger for gas turbine engine nozzle

Spherical button washer for exhaust duct liner hanger

Adjustable cable for exhaust duct liner hanger

Pipe having an upstream core having a sharp curvature

Liner hanger with spherical washers

Seal assembly

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

Thermoelectric generator in turbine engine nozzles

Nacelle

Method for mounting shielding on a turbine casing, and mounting assembly for implementing same

Lateral turbojet improved in order to limit the deformation thereof

Blind retention mount

Method and apparatus for supplying heated, pressurized air

Gas path liner for a gas turbine engine

Low-thickness thermostructural composite material part, and manufacture method

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

Flade discharge in 2-D exhaust nozzle

Thermal integration of thermoelectronic device

Thermoelectric generation for a gas turbine

Combustor liner for a turbine engine with venturi and air deflector

Liner for a turbine section, a turbine section, a gas turbine engine and an aeroplane provided therewith

Bushing for torque load transfer attachment hardware

Engine assembly, acoustical liner and associated method of fabrication

Gas turbine engine systems involving variable nozzles with flexible panels

Metal injection molding attachment hanger system for a cooling liner within a gas turbine engine swivel exhaust duct

Exhaust nozzle seal with segmented basesheet disposed between side rails

Swept fan ramp for pivot door thrust reverser

Thermoelectric generation system

Exhaust liner attachment arrangement

Gate valve for a system for circulating cooling air through a turbomachine

Variable area nozzle with woven sleeve extension

Duct burning mixed flow turbofan and method of operation

Combined control for supplying cooling air and support air in a turbine engine nozzle

Liner panel

Ceramic matrix composite capped bolt attachment

Method of Optimum Controlled Outlet, Impingement Cooling and Sealing of a Heat Shield and a Heat Shield Element

Torque load transfer attachment hardware

Damped coil pin for attachment hanger hinge

Cooled duct for gas turbine engine

Methods and apparatus to reduce turbine engine nozzle basesheet stresses

Passive bypass for mitigation of inlet buzz in supersonic or hypersonic air-breathing engines

Hydrogen fuel system for a gas turbine engine