Heated inlet guide vane

Method for detecting a fluid leak in a turbomachine and system for distributing a fluid

Anti-icing internal manifold

Gas turbine engine with fan-tied inducer section

Turbomachine thermal management

Bleed air systems for use with aircraft and related methods

Bleed air systems for use with aircraft and related methods

Enhanced temperature control anti-ice nozzle

Aircraft anti-icing systems having deflector vanes

Aircraft engine anti-icing (EAI) barrier assembly, system and method

Concentric nozzles for enhanced mixing of fluids

Inlet bleed heat system and related method for a compact gas turbine inlet

System and method for preventing ice crystal accretion in gas turbine engines

Method for regulating the de-icing of a leading edge of an aircraft and device for its implementation

System and method for an oxidant heating system

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

Turbine engine nacelle fitted with a heat exchanger

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

Gas turbine engine with bleed duct for minimum reduction of bleed flow and minimum rejection of hail during hail ingestion events

Return fluid air cooler system for turbine cooling with optional power extraction

Gas turbine power augmentation system

Turbomachine inlet bleed heating assembly

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

REGULATED OIL COOLING SYSTEM FOR A TURBINE ENGINE WITH DEICING OF THE NACELLE

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

Anti-ice supply system for inlet guide vanes

Heated rigid electrical harness for a gas turbine engine

Axial turbomachine blade with platforms having an angular profile

Gas turbine anti-icing system

EXHAUST HEAT RECOVERY FOR A GAS TURBINE SYSTEM

Magnetic de-icing

Heated screen for air intake of aircraft engines

Device for de-icing a turbomachine separator

Inlet air chilling system with humidity control and energy recovery

Aircraft engine control during icing of temperature probe

Panel for the acoustic treatment comprising hot air ducts and at least one stabilization chamber

Systems and methods for de-icing a gas turbine engine inlet screen and dehumidifying inlet air filters

GAS TURBINE ANTI-ICING SYSTEM

System and method for heat recovery in a gas turbine engine

Debris Intrusion Shield for Jet Engine Applications

Electrical raft with map

Actuator mounting system and method of mounting

Electrical structure having a grounding plane

Intake liner for a gas turbine engine

Turbomachine thermal management

Turbomachine thermal management

Turbomachine thermal management

GAS TURBINE INTAKE ANTI-ICING DEVICE

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

Gas turbine engine with fan-tied inducer section

APPARATUS AND METHOD FOR CONDITIONING AIR RECEIVED BY A POWER GENERATION SYSTEM

SYSTEM AND METHOD FOR GAS TURBINE INLET AIR HEATING

COMBUSTION TURBINE INLET ANTI-ICING RESISTIVE HEATING SYSTEM

Buffer system for communicating one or more buffer supply airs throughout a gas turbine engine

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

Fastening element and de-icing device of an aircraft gas-turbine engine

Electrical connectors

Electrical connectors

Gas turbine engine systems

Raft assembly

Gas turbine part having an electrical system embedded in composite material

Electronic unit mounting

Rigid raft

Electrical raft assembly

Inlet bleed heat system

Inlet bleed heat system

Gas turbine engine mounting arrangements

Fastening device particularly suitable for the fastening between an air intake and an engine of an aircraft nacelle

Method and controller for detecting ice

Gas turbine inlet heating system

Process for the production of a panel for the acoustic treatment incorporating the frost treatment function with hot air

ICE SHED REDUCTION FOR LEADING EDGE STRUCTURES

De-icing device of an aircraft gas-turbine engine

Wetting resistant materials and articles made therewith

Gas flow separator with a thermal bridge de-icer

Aircraft nacelle air intake incorporating optimized ice-treatment hot air injection means

METHOD AND APPARATUS FOR PROTECTING AIRCRAFT AND AIRCRAFT ENGINES AGAINST ICING

METHOD AND APPARATUS FOR PROTECTING AIRCRAFT ENGINES AGAINST ICING

Fuel system for gas turbine engine

Heated booster splitter plenum

Arrangement for maintaining flow to an air inlet of an auxiliary power unit assembly

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

Fluid impingement arrangement

Acoustic processing panel, more particularly adapted for an air intake in an aircraft nacelle

GAS TURBINE ENGINE WITH BLEED DUCT FOR MINIMUM REDUCTION OF BLEED FLOW AND MINIMUM REJECTION OF HAIL DURING HAIL INGESTION EVENTS

Intake air temperature control device and a method for operating an intake air temperature control device

Gas turbine manifold mounting arrangement including a clevis

Rotating inlet cowl for a turbine engine, comprising an eccentric forward end

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

Aircraft engine control during icing of temperature probe

Superconductive heat transfer system

Engine inlet ice protection system having embedded variable watt density heaters

Heat transfer arrangement for fluid-washed surfaces

Electric de-icing device and related monitoring system

Turbine inlet heat transfer system

System for heating an airstream by recirculating waste heat of a turbomachine

Wetting resistant materials and articles made therewith

Method for controlling an electrical deicing system

Coil arrangement for air intake system for gas turbine and methods

Jet engine shield and deicer

Turbomachine nacelle and anti-icing system and method therefor

Turbomachine nacelle and anti-icing system and method therefor

Method for making a nacelle de-icing element

Method for making an acoustic panel for the air intake lip of a nacelle

Intake air heating system of combined cycle plant

Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatment

Anti-icing system using radiant infrared energy from turbine exhaust flues

Method for making deicing system on a nacelle panel

Acoustic attenuation panel for aircraft for engine nacelle

Assembly of components connected by a device that maintains the integrity of the surface of one of the components

Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone

System for ice and/or frost prevention using guided wave energy

Gas turbine engine system providing simulated boundary layer thickness increase

Air intake structure for an aircraft nacelle

AIR INTAKE LIP FOR TURBOJET NACELLE

Apparatus for controlling intake air heating of gas turbine

Panel for supporting abradable material in a turbomachine

METHOD OF OPERATING A HEATED GUIDE VANE ASSEMBLY

HEATED GUIDE VANE

Nosecone ice protection system for a gas turbine engine

Engine intake flap for being arranged on the housing of an air intake of an aircraft engine, as well as engine with such an engine intake flap and aircraft system

Acoustic coating for an aircraft incorporating a frost treatment system by joule effect

Aircraft leading edge

Aircraft propulsion assembly comprising hot air bleed systems

Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure

Heat transfer system and method for turbine engine using heat pipes

Heat transfer system and method for turbine engine using heat pipes

Aircraft fluid diversion inlet louver

System for defrosting the leading edge sheath of an air inlet hood for a turboengine

SYSTEME D'ANTI GIVRAGE ET DE DEGIVRAGE DE NACELLE DE MOTEUR D'AERONEF A TAPIS RESISTIF

Inlet bleed heat system thermal lag mitigation using compressor interstage bleeds

Connector for heater

Wetting resistant materials and articles made therewith

Wetting resistant materials and articles made therewith

Wetting resistant materials and articles made therewith

Turbine inlet air heat pump-type system

Low grade heat recovery system for turbine air inlet

System and method for changing the efficiency of a combustion turbine

Device for de-icing the air intake of a gas turbine

Coating for acoustic treatment integrating the function of frost treatment with hot air

METHOD FOR MAKING AN ACOUSTIC TREATMENT COATING AND COATING THUS OBTAINED

Intake air heating system of combined cycle plant

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

Intake air heating control device for gas turbine

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

Ice protection system for a multi-segment aircraft component

Heater Assemblies, Gas Turbine Engine Systems Involving Such Heater Assemblies and Methods for Manufacturing Such Heater Assemblies

Dual valve apparatus for aircraft engine ice protection and related methods

STRUCTURAL ELEMENT OF AN AIRCRAFT

Cyclone separator

Device for protection against icing for aircraft engines and related de-icing method

Gas turbine engine assembly including accessory components within the nacelle

Ice shed reduction for leading edge structures

Variable stator vane

Distributed zoning for engine inlet ice protection

Heating architecture for a composite fairing

Engine inlet ice protection system with power control by zone

Utilizing inlet bleed heat to improve mixing and engine turndown

TURBINE ENGINE INLET STRUT DEICING

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

Turboengine air intake provided with a controlled filter system

Modular air inlet lip with electric defrosting for a turbojet pod

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

Aircraft engine protection unit (A.E.P.U)

Systems and methods for altering inlet airflow of gas turbine engines

COATED VARIABLE AREA FAN NOZZLE

Thermally powered turbine inlet air chiller heater

Aircraft engine nacelle inlet having access opening for electrical ice protection system

Aircraft engine nacelle inlet having access opening for electrical ice protection system

Gas turbine engine anti-ice formation device and system

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

Electrical connection for titanium metal heater in jet turbine applications

Operating line control of a compression system with flow recirculation

System for deicing the leading edge of a nose inlet cowl turbine engine

Titanium foil as a structural heater element

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

Gas turbine engine providing simulated boundary layer thickness increase

Engine arrangement

Heat transfer system and method for turbine engine using heat pipes

Connector for heater

Compressed-Air Generating System

Method and apparatus for pre-heating an aircraft engine

Methods and apparatus for operating gas turbine engines

System for deicing an aircraft turbine engine inlet cone

Isothermal de-iced sensor

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

Methods and apparatus for gas turbine engines

Aircraft engine nacelle ice protection system

Device and an aircraft anti-icing system comprising such a device

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

Control of engine intake door

Electrothermal inlet ice protection system

Aircraft engine nacelle inlet having electrical ice protection system

Aircraft engine nacelle inlet having access opening for electrical ice protection system

Intake duct

Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods

System for heating an air intake of turbine engine

Inlet muff anti-icing system for an auxiliary power unit

Aeroengine intake having a heat exchanger within an annular closed chamber

De-icing device for turbojet inlet guide wheel vane, vane provided with such a de-icing device, and aircraft engine equipped with such vanes

Methods and apparatus for operating gas turbine engines

Methods for modifying friction between an object and ice or snow

Nacelle inlet lip anti-icing with engine oil

Inlet guide vane

Gas turbine engine with compartment anti-icing system

Shielded swirl gas turbine engine inlet anti-icing system

Methods and apparatus for anti-ice heat supply from waste heat recovery systems

Ice-interference features for aircraft

Engine nacelle anti-ice swirl system with unsteady fluid flow

De-ice system and apparatus for turbine engines

Power switching system of an anti-ice system for use with a main power supply and an auxiliary power supply

Manifold assembly and anti-ice system for gas turbine engine

Systems and method for detecting and responding to icing conditions in gas turbine engines

Anti-ice mixing unit utilizing bleed air for a gas turbine engine

Anti-icing system and method for an aircraft propulsion system

Aircraft turboprop engine inlet compact profile configuration to improve air intake efficiency and without loss of anti-icing ability

System and method of anti-icing inlet guide vanes

Three dimensional graphene foam reinforced composite coating and deicing systems therefrom

Aircraft engine icing event avoidance and mitigation through real-time simulation and controls