ANTI-ICE/DE-ICE SYSTEM

Ice Detection and Precautionary System Shut-Down Event Reduction Systems and Related Methods

ICE-INTERFERENCE FEATURES FOR AIRCRAFT

FAN GUIDE VANE WITH LEADING EDGE DEICING

VANE HEATING SYSTEM AND METHOD

AIR INTAKE LIP FOR A NACELLE OF AN AIRCRAFT PROPULSION ASSEMBLY

SEGMENTED NACELLE INLET LIP WITH ELECTRIC ANTI-ICING SYSTEM

Segmented nacelle inlet lip with electric anti-icing system

SYSTEMS AND METHODS FOR MATERIAL ACCRETION DETECTION AND REMOVAL

Anti-ice system for gas turbine engine and inlet guide vane

AIR INTAKE MODULE FOR AN AIRCRAFT TURBOMACHINE AND METHOD FOR DE-ICING THEREOF

AIR-HEATED GUIDE VANE WITH TIP HEATING

ENGINE HAVING AN OPEN FAN WITH REDUCED BOUNDARY LAYER INDUCED DISTORTION

SEGMENTED NACELLE INLET LIP WITH ELECTRIC THERMAL ANTI-ICING SYSTEM

Compressor with anti-ice inlet

ENGINE HAVING AN OPEN FAN WITH REDUCED BOUNDARY LAYER INDUCED DISTORTION

SPLITTER FOR AERONAUTIC TURBOMACHINE

AIRCRAFT ANTI-ICING SYSTEM

Pressure and temperature sensors and methods of controlling ice accretion on pressure and temperature sensors

Inlet cone for an aircraft turbomachine

Pressure and temperature sensors and methods of removing ice from pressure and temperature sensors

GASTURBINE ENGINE AND METHOD FOR THERMAL MANAGEMENT OF A FAN BLADE AND/OR AN INLET CONE

Method and system for component alignment in turbine casing and related turbine casing

Nacelle inlet assembly with composite lipskin

Blade comprising a shield having a defrosting air passage duct

METHODS AND APPARATUS TO HEAT ROTOR BLADES

Fluid measurement system and method for operating same

LEAK DETECTION SYSTEM FOR ANTI-ICE DUCTS

TURBINE ENGINE MODULE EQUIPPED WITH A PROPELLER AND STATOR VANES SUPPORTED BY RETAINING MEANS AND CORRESPONDING TURBINE ENGINE

Methods and apparatus to provide damping of an airfoil

SYSTEM AND METHOD TO INCREASE THE TEMPERATURE OF OIL USED TO ANTI-ICE A GAS TURBINE PROPULSION ENGINE

Vane assembly for a gas turbine engine

APPARATUSES FOR DEICING FAN BLADES AND METHODS OF FORMING THE SAME

Anti-icing systems and airfoils for a fan section of a turbine engine

Ice crystal protection for a gas turbine engine

Method and system for component alignment in turbine casing and related turbine casing

Rotor blade retention system for a gas turbine engine

EJECTOR DRIVEN SCAVENGE SYSTEM FOR PARTICLE SEPARATOR ASSOCIATED WITH GAS TURBINE ENGINE

Turbomachine comprising a system for deicing the upstream cone, and associated method

Inlet cone for an aircraft turbine engine and associated aircraft turbine engine

Separation nozzle for aeronautic turbomachine

Ice detection and precautionary system shut-down event reduction systems and related methods

Pressure regulating valve assembly

Additively manufactured booster splitter with integral heating passageways

DEVICE FOR DE-ICING A TURBOMACHINE NOZZLE

Core duct assembly

Pressure and temperature sensors and methods of removing ice from pressure and temperature sensors

Closed loop fan inlet vane anti icing system

Pressure and temperature sensors and methods of controlling ice accretion on pressure and temperature sensors

Pressure and temperature sensors and related methods

Frame for a heat engine

Ice crystal protection for a gas turbine engine

Anti-icing system having a nozzle with a deflector plate and method

Thermal-anti-icing system with microwave system

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

Thermal anti-icing system with non-circular piccolo tube

Assembly for sealing an annular gap between an inner structure and an outer structure

ARTICLES FOR MANIPULATING IMPINGING LIQUIDS AND ASSOCIATED METHODS

Fan blade, engine, and structure with anti-icing and de-icing functions

MAGNET ANTI-ICE SYSTEM

Method of ice removal by inducing sudden variation of rotor speed in a gas turbine engine

Anti-icing system for gas turbine engine

Method of shedding ice and fan blade

Core duct assembly

BLADE DE-ICING

Turbofan engine and core link therefore

Anti-icing system for a gas turbine

Ice crystal protection for a gas turbine engine

DE-ICING SYSTEM

Aircraft systems and methods utilizing waste heat in fuel

Anti-ice double walled duct system

Turbomachine having an air intake de-icing system

Self modulating valve

Aircraft engine nacelle comprising a system of ice protection

System and method for cleaning cooling passages of a combustion chamber

Compositions and methods for fabricating coatings

Ported shroud system for turboprop inlets

ICE SEPARATOR OF A FUEL SYSTEM FOR A GAS TURBINE ENGINE

Icephobic vane for a compressor of an axial turbine engine

Airfoil deicing system

Systems and methods of optimizing cooling and providing useful heating from single phase and two phase heat management in propulsion systems

Bleed air selector valve

Systems and methods for fan blade de-icing

Gas turbine engine

Anti-ice system exhaust air disruptor

Method of regulating air pressure in anti-icing system

De-icing shroud for a compressor of turbomachine

Ice shedding aircraft engine

Additively manufactured booster splitter with integral heating passageways

Articles for manipulating impinging liquids and methods of manufacturing same

Methods, computer programs, non transitory computer readable storage mediums, signals, and apparatus for controlling electrical power supplied to a component of a vehicle

Aircraft propulsion system comprising a member covered with a grooved structure

Ice phobic material to reduce runback ice

Air inlet lip of an aircraft engine comprising a de-icing system

GAS TURBINE SYSTEM

INLET FRAME FOR A GAS TURBINE ENGINE

Device for deicing a splitter nose and inlet guide vanes of an aviation turbine engine

Ice detection

Pneumatic deicer with sensors

Gas turbine engine de-icing system

Turbofan engine de-icing compressor and de-icing process

Electrical bus arrangement for ice protection systems

Gas turbine system

Gas turbine system and control apparatus and method thereof

Turbine engine airfoil with a modified leading edge

De-icing by integral electric heat generation

METHOD FOR LIMITING THE CORE ENGINE SPEED OF A GAS TURBINE ENGINE DURING ICING CONDITIONS

Anti-icing system for a turbine engine vane

Compressor with segmented inner shroud for an axial turbine engine

Method and system for ice tolerant bleed takeoff

Nacelle inner lip skin with heat transfer augmentation features

Sanitation systems and components thereof having a slippery surface

Direct-acting valve

Geared turbofan with high speed generator

Turbine engine having a three-phase transformer for powering electrical deicer elements

Containers, bottles, drums, vats, and tanks having a slippery surface

Deicing nose of an axial turbine engine compressor

Embedded aircraft heater repair

GAS TURBINE ENGINE

GAS TURBINE ENGINE

COMPRESSOR STAGE

Heating device

Ice protection system for gas turbine engines

Annular heatshield

SYSTEM OF OPERATING A GAS TURBINE ENGINE

Nacelle anti ice system

Dynamic resonance system and method for the anti-icing and de-icing of inlet grids

Method and assembly for providing an anti-icing airflow

Vane for turbomachinery, such as an aircraft turbojet or turbofan engine or an aircraft turboprop engine

Device for de-icing a splitter nose of an aviation turbine engine

Axial Turbine Engine Compressor De-Icing Blade

SYSTEM AND METHOD FOR OPERATING A PRECOOLER IN AN AIRCRAFT

Heat exchange system for a power gear box, a power gear box and a turbo engine with a power gear box

Gas turbine engine with short inlet, acoustic treatment and anti-icing features

Method and system for inlet guide vane heating

Heat exchange system for power gear box, a power gear box and a turbo engine with a power gear box

Device for de-icing a rotor blade, rotor blade provided with such a device, rotor, turbomachine and aircraft

Heat exchanger designs using variable geometries and configurations

ARTICLES FOR MANIPULATING IMPINGING LIQUIDS AND METHODS OF MANUFACTURING SAME

Self-contained lubrication cooling system with heat exchanger integrated with sump

De-icing device for a splitter nose of an axial turbine engine compressor

De-icing nose for low-pressure compressor of an axial turbine engine

Compressor endwall treatment to delay compressor stall

Injector nozzle configuration for swirl anti-icing system

Dynamic resonance system and method for the anti-icing and de-icing of inlet grids

De-icing splitter for an axial turbine engine compressor

Turbine engine with anti-ice valve assembly, bleed air valve, and method of operating

Splitter nose of a low-pressure compressor of an axial turbomachine with annular deicing conduit

Slippery surfaces with high pressure stability, optical transparency, and self-healing characteristics

Dual pressure deicing system

Embedded turbofan deicer system

Method of determination and gas turbine

Fan nacelle inlet flow control

De-icing splitter lip for axial turbomachine compressor

Thermal management system and method of circulating air in a gas turbine engine

Fan case ice liner for turbofan engine

Gas-turbine engine with oil cooler in the engine cowling

Imaging assisted gas turbine anti-icing system

Method to integrate multiple electric circuits into organic matrix composite

Icing prevention of a gas turbine engine pressure sensing assembly

Icephobic Flowpath for a Nose Cone and Method Therefor

Anti-icing systems

Gas turbine engines with heated cases

Core case heating for gas turbine engines

Plated polymer compressor

Plated polymer fan

System and method to manage transients for rapid power demand changes

Thermal management system for a gas turbine engine with an integral oil tank and heat exchanger in the nacelle

COMBINED FAN CASE ICE LINER AND REAR LINER

Ice-shedding spinner for ram air turbine

Splitter nose with plasma de-icing for axial turbine engine compressor

Anti-ice splitter nose

GAS TURBINE ENGINE AND A METHOD OF WASHING A GAS TURBINE ENGINE

Anti-icing core inlet stator assembly for a gas turbine engine

METHOD OF MANUFACTURING ICE PANEL SEGMENTS

Gas turbine engine anti-icing system

Device for deicing a separator nose of an aviation turbine engine

Gas turbine and method for operating the gas turbine

Gas turbine engine de-icing system

COOLING DEVICE FOR A TURBOJET ENGINE OF AN AIRCRAFT NACELLE

System for preventing icing on an aircraft surface using a plasma actuator

De-icing by integral electric heat generation

Removable film for airfoil surfaces

High temperature aluminum valve components

Organic matrix composite structural inlet guide vane for a turbine engine

Heated inlet guide vane

Geared turbofan with high speed generator

Anti-icing internal manifold

Aircraft engine nacelle bulkheads and methods of assembling the same

ELECTRIC DE-ICING DEVICE FOR TURBOJET ENGINE NACELLE ELEMENT

Aircraft anti-icing systems having deflector vanes

Electrical power supply system comprising an asynchronous machine, and an engine fitted with such an electrical power supply system

Total air temperature sensors

Anti-icing system for a gas turbine

Splitter nose with a sheet that forms a surface to guide the flow and acts as a de-icing duct

Method and device for suppressing the formation of ice on structures at the air intake of a turbomachine

System and method for controlling ice formation on gas turbine inlet guide vanes

Nacelle anti-ice valve utilized as compressor stability bleed valve during starting

Device for de-icing a leading edge of a turbine engine by slanting notches

Anti-ice supply system for inlet guide vanes

Axial turbomachine blade with platforms having an angular profile

Electrical power transfer system for propeller system

Device for de-icing a turbomachine separator

Aircraft engine control during icing of temperature probe

System and method for operating a precooler in an aircraft

System and method for heat recovery in a gas turbine engine

Turbomachine thermal management

STRUCTURES AND METHODS FOR INTERCOOLING AIRCRAFT GAS TURBINE ENGINES

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

Nano-metal coated vane component for gas turbine engines and method of manufacturing same

Aircraft ice protection system and aircraft provided with the same

Anti-icing core inlet stator assembly for a gas turbine engine

FLUID PRESSURE BASED ICING DETECTION FOR A TURBINE ENGINE

Gas turbine engine mounting arrangements

Apparatus and method for separating ice from fuel in a gas turbine engine

Articles for manipulating impinging liquids and methods of manufacturing same

ICE SHED REDUCTION FOR LEADING EDGE STRUCTURES

Wetting resistant materials and articles made therewith

Gas flow separator with a thermal bridge de-icer

Heated booster splitter plenum

INTEGRATION OF A SURFACE HEAT-EXCHANGER WITH REGULATED AIR FLOW IN AN AIRPLANE ENGINE

Fluid impingement arrangement

Aircraft engine control during icing of temperature probe

Method of avoiding a grid clogging, a grid and an air intake implementing such a method

Apparatus for preventing ice accretion

Heat transfer arrangement for fluid-washed surfaces

Wetting resistant materials and articles made therewith

Jet engine shield and deicer

Turbo-engine compressor tip comprising de-icing means

HEATED GUIDE VANE

Heat transfer system and method for turbine engine using heat pipes

Connector for heater

Wetting resistant materials and articles made therewith

Wetting resistant materials and articles made therewith

Wetting resistant materials and articles made therewith

Systems And Methods For Modifying An Ice-To-Object Interface

Air cycle machine turbine outlet heated diffuser

Ice shed reduction for leading edge structures

Variable stator vane

Distributed zoning for engine inlet ice protection

Anti-icing apparatus and method for aero-engine nose cone

AIR-OIL HEAT EXCHANGER PLACED AT THE LOCATION OF THE AIR SEPARATOR NOSE OF A TURBOJET, AND A TURBOJET INCLUDING SUCH AN AIR-OIL HEAT EXCHANGER

Anti-icing apparatus and method for aero-engine nose cone

Compressor inlet guide vane flow based anti-ice formation control system and method

Turbocharger with variable nozzle mechanism

Bushing and clock spring assembly for moveable turbine vane

Slipring bushing assembly for moveable turbine vane

Compressor inlet guide vane de-ice control system and method

Method for detecting ice ingestion in a gas turbine engine

Heated engine nose cone using spiral channels

Temperature controlling apparatus

System for deicing the nose cone of an aircraft turbojet with oil

Surface mounted flexible heater for gas turbine engine application

Heat transfer system for turbine engine using heat pipes

Titanium foil as a structural heater element

Heater assembly for deicing and/or anti-icing a component

Surface treatment for a thin titanium foil

Apparatus for preventing ice accretion

Connector for heater

Methods and apparatus for operating gas turbine engines

System for deicing an aircraft turbine engine inlet cone

Heater assembly for deicing and/or anti-icing a component

Methods and apparatus for gas turbine engines

Low power, pulsed, electro-thermal ice protection system

Methods and apparatus for gas turbine engines

Systems and methods for modifying an ice-to-object interface

Electrothermal inlet ice protection system

Methods and apparatus for deicing airfoils or rotor blades

Methods for operating gas turbine engines

Methods and apparatus for operating gas turbine engines

Methods for modifying friction between an object and ice or snow

Inlet guide vane

Gas turbine engines with inlet guide vanes

Thermally activated flow control device

Ice-interference features for aircraft

Thermal management system for gas turbine engine with open propulsor

Engine nacelle anti-ice swirl system with unsteady fluid flow

Composite airfoil with integrated anti-icing for an aircraft propulsion system

Combustor blade and vane spacing for ice crystal protection for a gas turbine engine

Three dimensional graphene foam reinforced composite coating and deicing systems therefrom