COMBUSTOR FOR A TURBINE ENGINE INCLUDING AN INSULATING MEMBER

DOVETAIL FEATURES ON PANEL RAILS OR IMPINGEMENT SHEET TO HOLD PANELS

EXHAUST NOZZLE ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM

SYSTEMS AND METHODS FOR COOLING AN INNER WALL OF A THRUST REVERSER OF AN ENGINE OF AN AIRCRAFT

COUPLING ASSEMBLY FOR A TURBINE ENGINE

COOLED VARIABLE AREA NOZZLE FOR AN AIRCRAFT ENGINE

TURBOMACHINE COMPRISING AN OUTLET CONE INCORPORATING COMPONENTS COOLED BY CIRCULATION OF A COOLING FLOW

REAR ASSEMBLY FOR A TURBOJET ENGINE NACELLE

ENGINE

PROPULSION ASSEMBLY COMPRISING A FUEL CONDITIONING SYSTEM POSITIONED BEHIND A DEBRIS EJECTION ZONE, AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION ASSEMBLY

Coupling assembly for a turbine engine

Precursor derived semiconductor devices having PN junctions

Integral ceramic matrix composite fastener with non-polymer rigidization

Integral ceramic matrix composite fastener with polymer rigidization

ARTICLE WITH COOLING HOLES AND METHOD OF FORMING THE SAME

Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle comprising cooling air circulation ducts connected through contact surfaces

Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle, the flaps of which each comprise a cooling air circulation duct

Gas turbine engine having a heat exchanger arrangement having at least one heat exchanger module overlapping another heat exchanger module

Turbofan engine comprising an outlet cone cooled by its secondary flow

Engine components with cooling holes having tailored metering and diffuser portions

Cooling system for an engine assembly

Passive internal compartment exhaust for an aircraft propulsion system

Nacelle cowl deflection limiter

Combustor liner for a gas turbine engine and an associated method thereof

Regeneration cooler of ramjet engine, and manufacturing method of the same

Systems and methods for manufacturing film cooling hole diffuser portion

Ceramic materials comprising preceramic resin formulations, and related articles and methods

Fastening device for a heat-shield panel

Heat shield for signature suppression system

Exhaust casing for a gas turbine engine

Integral ceramic matrix composite fastener with non-polymer rigidization

Flow control wall for heat engine

Cooling hole with shaped meter

AIRCRAFT NOZZLE

Self-regulating back-side pressurization system for thermal insulation blankets

PULSE COMBUSTOR PERFORMANCE IMPROVEMENT WITH AIRSPEED

Composite-Overwrapped Multi-Metallic Thrust Chamber Liner

Seal-Free Multi-Metallic Thrust Chamber Liner

Exhaust liner deflection limiter

Pull-plane effusion combustor panel

AIRCRAFT NOZZLE

AIRCRAFT NOZZLE

Combustor liner for a gas turbine engine and an associated method thereof

Gas turbine exhaust cooling system

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

Thermal panel with a corrugated ceramic composite sheet having unequal ridge widths

Ceramic matrix composite articles

Fastener system for a thermal protection system

Component for a turbine engine with a cooling hole

Heat shield for signature suppression system

Preceramic resin formulations, ceramic materials comprising the preceramic resin formulations,and related articles and methods

Integral ceramic matrix composite fastener with polymer rigidization

Systems and methods for manufacturing film cooling hole diffuser portion

Coil spring hanger for exhaust duct liner

Combustor, gas turbine including the same and method of distributing compressed air in combustor

Multi-layer thermal insulator apparatus and methods

EXHAUST COOLING ARRANGEMENT

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

Panel surface pockets for coating retention

Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustor

Impingement cooled nozzle liner

Gas turbine exhaust cooling system

Vehicle mechanical component and piston

Method for manufacturing of at least one part of an engine component by means of a blank of intumescent material

Acoustic liners and method of shaping an inlet of an acoustic liner

Method and apparatus for variable supplemental airflow to cool aircraft components

Cooling hole with shaped meter

Engine components with cooling holes having tailored metering and diffuser portions

Insulation materials comprising fibers having a partially cured polymer coating thereon, structures including such insulation materials, and methods of insulating such structures

TURBOMACHINE COMPONENT, PARTICULARLY A GAS TURBINE ENGINE COMPONENT, WITH A COOLED WALL AND A METHOD OF MANUFACTURING

Assembly of an inner fixed structure of a turbojet engine nacelle and of a thermal protection

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

Hybrid thrust reverser inner wall for aircraft engines

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

Afterburner and aircraft engine

Trailing edge core compartment vent for an aircraft engine

Door-type thrust reverser device for aircraft turbojet engine nacelle

Gas turbine engine wall assembly interface

Preloaded AFT vent area for low pressure fan ducts

Methods for treating field operated components

Turbofan bypass air cooled oil cooler fairings

Afterburner and aircraft engine

Cooling a quench aperture body of a combustor wall

Coated cooling passage

Exhaust gas liner for a gas turbine and gas turbine with such an exhaust gas liner

Gas turbine engine wall assembly with offset rail

Integral ceramic matrix composite fastener with polymer rigidization

Automated weld repair of combustor liners

Attachment assembly for protective panel

BACKSIDE COATING COOLING PASSAGE

Divergent flap

Structural honeycomb panel

Multi-component fastener and method of producing the same

Ceramic liner for a turbine exhaust case

Wall for a hot gas channel in a gas turbine

Protective panel and frame therefor

Stepped fairing modulated exhaust cooling

Gas turbine engine with ceramic panel

Jet noise suppressor

Heat exchanger arrangement for turbine engine

Nozzle for an aircraft turboprop engine with an unducted fan

Gas turbine engine component having shaped pedestals

Retractable exhaust liner segment for gas turbine engines

Exhaust duct

Exhaust system having a flow path liner supported by structural duct segments

Adjustable cable for exhaust duct liner hanger

Exhaust liner flange cooling

Serpentine baffle for a gas turbine engine exhaust duct

Compliant heat shield liner hanger assembly for gas turbine engines

Turbine engine wall having at least some cooling orifices that are plugged

Gas turbine engine systems and methods involving enhanced fuel dispersion

METHOD AND APPARATUS FOR COOLING COMBUSTOR LINER IN COMBUSTOR

Turbomachine comprising a device for the cooling of a pylon

Thermal barrier coatings for turbine engine components

Exhaust stream mixer

Aircraft thrust reversing assembly IFS support structure

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

Hybrid inner fixed structure with metallic and composite construction

Secondary nozzle for jet engine

Multi-nozzle flow diverter for jet engine

Device for Fastening a Hollow Part

Gas turbine exhaust diffuser with helical turbulator

Aerodynamically active stiffening feature for gas turbine recuperator

Insulation materials comprising fibers having a partially cured polymer coating thereon, articles including such insulation materials, and methods of forming such materials and articles

Push-lock pin connector

MODULATED EJECTOR COOLING

Support system bumper for exhaust duct liner hanger

Thermally free hanger with length adjustment feature

Low profile thermally free blind liner hanger attachment for complex shapes

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

Ceramic matrix composite liner attachment

Adjustable hanger and method for gas turbine engine exhaust liner

Coil spring hanger for exhaust duct liner

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

Support hanger for flexibly connecting a plurality of panels

Turbine exhaust plume mitigation system

Sliding U-joint hanger for gas turbine engine nozzle

Liner bracket for gas turbine engine

Pivoting ball stop for exhaust duct liner hanger

Adjustable cable for exhaust duct liner hanger

Gas turbine engine exhaust duct

Diffuser for the exhaust section of a gas turbine and gas turbine with such a diffuser

System and method for operating a precooler in an aircraft

Turbomachine flow control device

Thermally insulative attachment

Liner hanger cable

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

THERMAL INSULATION OF ROCKET ENGINES

Multi-channel cooling plenum

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

Gas turbine engine duct blocker that includes a duct blocker rotor with a plurality of roller elements

Gas turbine engine duct blocker with rotatable vane segments

Turbomachine component machining method

Exhaust impingement cooling

Retractable exhaust liner segment for gas turbine engines

Gas duct for a gas turbine and gas turbine having such a gas duct

Impingement cooled nozzle liner

Seal land with air injection for cavity purging

METHOD AND APPARATUS FOR COOLING COMBUSTOR LINER IN COMBUSTOR

Gas turbine engine and cooling system

Coating a perforated surface

METHOD FOR INSTALLING HEAT SHIELDING ON A FIXED INTERNAL STRUCTURE OF A JET ENGINE NACELLE

Exhaust washed structure and associated composite structure and method of fabrication

Casing body through which hot gases can flow and comprising an inner heat shield

Impingement cooling for turbofan exhaust assembly

Ejector purge of cavity adjacent exhaust flowpath

Cooled conduit for conveying combustion gases

Thermoelectric generation for a gas turbine

Sealing assembly

INSTALLATION HAVING A THERMAL TRANSFER ARRANGEMENT

AIR INTAKE STRUCTURE FOR A TURBINE ENGINE NACELLE

Heat Exchanger Mounting Assembly

Method of mounting a heat exchanger in a gas turbine engine assembly

Air flow passage liner

Attaching ceramic matrix composite to high temperature gas turbine structure

Thermally actuated passive gas turbine engine compartment venting

Low profile attachment hanger system for a cooling liner within a gas turbine engine swivel exhaust duct

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

Fuel-cooled heat exchanger with thermoelectric device compression

Fuel-cooled flexible heat exchanger with thermoelectric device compression

THERMALLY BALANCED MATERIALS

Bushing for torque load transfer attachment hardware

Gas turbine engine systems and methods involving enhanced fuel dispersion

Flow sleeve impingement cooling using a plenum ring

Impingement cooling for turbofan exhaust assembly

Cooling air bleed device in a turbomachine

Cooling air bleed device in a turbine engine

Slideable liner link assembly

Axially split nozzle liner for convergent nozzle

Slideable liner anchoring assembly

Exhaust washed structure and associated composite structure and method of fabrication

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

Stave and ring CMC nozzle

Recoatable exhaust liner cooling arrangement

Heat exchanger arrangement for turbine engine

Metering sheet and iso-grid arrangement for a non axi-symmetric shaped cooling liner within a gas turbine engine exhaust duct

Sandwich thermal insulation layer system and method for production

Single actuator controlled rotational flow balance system

Self-aligning liner support hanger

Convergent divergent nozzle with edge cooled divergent seals

Convergent divergent nozzle with slot cooled nozzle liner

Extended impingement cooling device and method

Joint between a metal part and a ceramic part based SiC and/or C

Fluidic vectoring for exhaust nozzle

Turbine component

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

System and method for controlling the temperature and infrared signature of an engine

Out-flow margin protection for a gas turbine engine

Linkage system with wear reduction

Turbojet engine comprising an afterburner duct cooled by a variable-throughput ventilation stream

Cooling device for the primary nozzle of a dual-flow turbojet engine

Low profile attachment hanger system for a cooling liner within a gas turbine engine swivel exhaust duct

Seal land with air injection for cavity purging

Elbow-shaped propulsion gas exhaust assembly in an aircraft

Exhaust assembly forming a horizontal propulsion gas elbow in an aircraft

Method and device for reducing engine noise

Torque load transfer attachment hardware

Exhaust dust flow splitter system

Damped coil pin for attachment hanger hinge

Heat shield for mounting on a heat-radiating object, particularly on a rocket engine

Cooling system for high-speed vehicles and method of cooling high-speed vehicles

System and method for cooling lateral edge regions of a divergent seal of an axisymmetric nozzle

Cooling scheme for scramjet variable geometry hardware

Cooled dual wall liner closeout

Inner plenum dual wall liner

Cooled duct for gas turbine engine

Yaw vectoring for exhaust nozzle

Multi-spectral air inlet shield and associated inlet structure

Method and device for reducing engine noise

Positioning bridge guide and its utilisation for the nozzle support pipe of a turboprop

Ventilation channels in an afterburner chamber confluence sheet

Divergent flap for a gas turbine engine

System and method for controlling the temperature and infrared signature of an engine

High temperature dynamic seal for scramjet variable geometry

Cooling scheme for scramjet variable geometry hardware

Device for supplying cooling air to exhaust nozzle flaps

Ablative afterburner

Convergent/divergent nozzle with modulated cooling

Extended impingement cooling device and method

Compact fastening collar and stud for connecting walls of a nozzle liner and method associated therewith

Split vane flow blocker

Ventilation system for a convergent divergent exhaust nozzle

Convergent-divergent turbojet nozzle

Thermoelectric power generator for a gas turbine engine

System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber

Tailcone and conduit ventilation system with variable internal flow distribution

Dovetail features on panel rails or impingement sheet to hold panels

Exhaust nozzle assembly for an aircraft propulsion system

Selectable inlet for aircraft propulsion system heat exchanger

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

Hydrogen fuel system for a gas turbine engine

Waste heat capture using tail cone of a gas turbine engine

Dual flowpath exhaust for fuel cooling in a hypersonic propulsion system

Jet engine attachment device