72599 ⎘
Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
INJECTOR FOR DE-ICING DEVICE FOR AN AIR INTAKE OF AN AIRCRAFT TURBOJET NACELLE, AND ASSOCIATED METHOD
#2ICE-INTERFERENCE FEATURES FOR AIRCRAFT
#3ICE REDUCTION MECHANISM FOR TURBOFAN ENGINE
#4AIRCRAFT PROVIDED WITH A HEATING SYSTEM FOR A TURBOSHAFT ENGINE PLENUM
#5AIR INTAKE LIP OF AN AIRCRAFT ENGINE NACELLE PROVIDED WITH A PASSIVE SHUT-OFF DEVICE FOR AN EXHAUST DEVICE
#6VANE HEATING SYSTEM AND METHOD
#7Laminate Structure with Integrated Power Distribution
#8Compressed Air System for Aircraft
#9ICE PROTECTION SYSTEM FOR AN AIRCRAFT
#10SYSTEM AND METHOD FOR FORMING A COMPONENT
#11VARIABLE INLET GUARD SCREEN FOR AN INLET OF AN AIRCRAFT ENGINE
#12DE-ICING OF AN AIRCRAFT PART
#13ICE REDUCTION MECHANISM FOR TURBOFAN ENGINE
#14SEGMENTED NACELLE INLET LIP WITH ELECTRIC ANTI-ICING SYSTEM
#15Segmented nacelle inlet lip with electric anti-icing system
#16Outer barrel support structure for nacelle inlet structure
#17ACOUSTIC ATTENUATION PANEL COMPRISING AN INDUCTION-BASED FROST TREATMENT SYSTEM, AIR INTAKE OF AN AIRCRAFT NACELLE AND AIRCRAFT COMPRISING SUCH A PANEL
#18AIR INTAKE MODULE FOR AN AIRCRAFT TURBOMACHINE AND METHOD FOR DE-ICING THEREOF
#19AIRCRAFT AIR SYSTEM WITH DEDICATED COMPRESSOR(S)
#20NACELLE INLET STRUCTURE WITH FOAM CORE
#21SEGMENTED NACELLE INLET LIP WITH ELECTRIC THERMAL ANTI-ICING SYSTEM
#22AIRCRAFT TURBOPROP ENGINE INLET COMPACT PROFILE CONFIGURATION
#23AIRCRAFT ANTI-ICING SYSTEM
#24LIP SKIN FOR AN AIRCRAFT AEROSTRUCTURE
#25ICE PROTECTION BACKUP TEMPERATURE CONTROL LOGIC
#26AIRCRAFT THERMAL ANTI-ICING SYSTEM
#27Inlet cone for an aircraft turbomachine
#28Ice protection backup temperature control logic
#29THERMAL ANTI-ICING SYSTEM FOR AN AIRCRAFT PROPULSION SYSTEM
#30Supersonic speed attenuator of an air intake of an aircraft propulsion assembly comprising a de-icing device and de-icing method
#31Aircraft fluid ice protection system
#32Ice reduction mechanism for turbofan engine
#33Assembly for a turbomachine
#34TURBINE ENGINE MODULE EQUIPPED WITH A PROPELLER AND STATOR VANES SUPPORTED BY RETAINING MEANS AND CORRESPONDING TURBINE ENGINE
#35Selectively meltable adhesives for bonding of deicers
#36Ice reduction mechanism for turbofan engine
#37Microwave thermal anti-icing system for aircraft acoustic structure
#38Integrated microwave thermal anti-icing system
#39Valve assembly
#40Rotor blade retention system for a gas turbine engine
#41Ice accumulation and shedding mitigation for sensor probe
#42Air intake of an aircraft turbine engine nacelle
#43AIR INTAKE LIP OF AN AIRCRAFT ENGINE NACELLE, COMPRISING AT LEAST ONE INFRARED EMISSION SOURCE
#44AIR INTAKE LIP OF A TURBOMACHINE NACELLE COMPRISING AN ACOUSTIC DEVICE AND METHOD FOR PRODUCING SUCH A LIP
#45Anti-icing for gas turbine system
#46Anti-icing system with a flow-deflector assembly
#47Thermal management system for a gas turbine engine
#48Pressure regulating valve assembly
#49Additively manufactured booster splitter with integral heating passageways
#50Vehicle provided, at the intake, with an heatable air filter provided and corresponding heatable air filter
#51Advanced inlet design
#52Nozzle for a thermal anti-icing system
#53Variable diameter piccolo tube for anti-icing system
#54Turbofan engine, nacelle thereof, and associated method of operation
#55Aircraft part anti-icing treatment method
#56Air inlet, nacelle, propulsive assembly and aircraft with grooved lip
#57Anterior part of a nacelle of an aircraft propulsion system having a shield in front of its rigidifying frame
#58Fan blade, engine, and structure with anti-icing and de-icing functions
#59Auxiliary power unit startup condition prediction
#60Defrosting and acoustic treatment device for an air intake lip of a turbojet engine nacelle
#61Aircraft propulsion system including a heat exchanger system
#62Method and apparatus for aircraft anti-icing
#63METHOD FOR THE CONTROL OF THE ANTI-ICING SYSTEM OF THE AIRCRAFT GAS TURBINE ENGINE
#64Anti-icing system for gas turbine engine
#65Anti-icing system for a gas turbine
#66Method for manufacturing a cellular core for an acoustic panel
#67Icing detector
#68Selectively meltable adhesives for bonding of deicers
#69Anti-ice double walled duct system
#70NACELLE INLET STRUCTURE
#71Turbomachine having an air intake de-icing system
#72Aircraft ice protection system and method
#73Leading-edge slat for an aircraft
#74Anti-icing system for an aircraft nacelle
#75Aircraft engine nacelle comprising a system of ice protection
#76Aircraft engine nacelle comprising an anti-icing protection system
#77Method of using printed highly flexible conductive ink bus bars to transfer power to heated components
#78Nacelle inlet with reinforcement structure
#79Device For Reducing Or Even Eliminating Tonal Noise For An Aircraft Powerplant De-Icing System
#80Method for manufacturing deicing acoustic skin for an aircraft acoustic panel, using a fiber spacing device
#81Ported shroud system for turboprop inlets
#82Systems and methods of optimizing cooling and providing useful heating from single phase and two phase heat management in propulsion systems
#83Aircraft equipped with a structurally integrated de-icing system
#84Gas turbine engine
#85Anti-ice system exhaust air disruptor
#86Engine enclosure air inlet section
#87Method of regulating air pressure in anti-icing system
#88Ice shedding aircraft engine
#89Aircraft engine nacelle provided with an icing protection system and associated protection method
#90PERIODIC HEATING FOR ELECTRIC ICE PROTECTION
#91Vehicle provided, at the intake, with an air filter provided with a heating device
#92Metal and composite leading edge assemblies
#93Additively manufactured booster splitter with integral heating passageways
#94Routable backup power control units
#95Method and apparatus for detecting ice accretion
#96Frost protection system for an aircraft engine nacelle
#97Control method for controlling an air intake system which supplies air to an engine of a vehicle
#98Air inlet lip of an aircraft engine comprising a de-icing system
#99Combined fluid ice protection and electronic cooling system
#100Advanced inlet design
#101Acoustic honeycomb panel with integrated electrical heater
#102Eductor driven anti-ice system
#103Aircraft incorporating a low-temperature bleed system
#104Air inlet for a nacelle for an aircraft and its process for manufacturing
#105Gas turbine engine de-icing system
#106Turbofan engine de-icing compressor and de-icing process
#107Weeping ferrofluid anti-ice system
#108Passive internal ice protection systems for engine inlets
#109Pulsed deicing system
#110LED light unit and method of producing an LED light unit
#111Core-protecting fan modules and turbofan engines containing the same
#112Deicing Apparatuses Comprising at least one standoff
#113LED light unit and method of replacing an LED light unit
#114ANTI-ICING SYSTEM FOR GAS TURBINE ENGINE
#115Aircraft bleed system
#116DEVICE FOR DE-ICING AN AIRCRAFT TURBOJET ENGINE NACELLE AIR INTAKE LIP
#117Air intake structure for an aircraft nacelle
#118Method and system for ice tolerant bleed takeoff
#119Nacelle inner lip skin with heat transfer augmentation features
#120STRUCTURE FOR PROPULSIVE AIRCRAFT ASSEMBLY, ASSOCIATED PROPULSIVE SYSTEM AND ASSEMBLY
#121Direct-acting valve
#122Heat exchanger with sliding aperture valve
#123Aircraft nacelle anti-ice systems and methods
#124Auxiliary power unit inlet assembly with particle separator
#125Auxiliary power unit inlet assembly with filter
#126Embedded aircraft heater repair
#127Icing condition detection using instantaneous humidity sensing
#128Turbofan engine fluid ice protection delivery system
#129Method for detecting a fluid leak in a turbomachine and fluid distribution system
#130Anti-icing exhaust system
#131Electro-expulsive deicing apparatuses comprising at least one standoff
#132RESISTANCE-HEATING METAL OR METAL ALLOY COATING
#133Engine air inlet having a double-panel heated wall
#134SYSTEM OF OPERATING A GAS TURBINE ENGINE
#135Nacelle anti ice system
#136Dynamic resonance system and method for the anti-icing and de-icing of inlet grids
#137Inline pressure regulating valve assembly with inlet pressure bias
#138Device for de-icing a splitter nose of an aviation turbine engine
#139Directed flow nozzle swirl enhancer
#140ENGINE BLEED SYSTEM WITH TURBO-COMPRESSOR
#141Internally heated engine inlet screen for aircraft engines
#142Engine bleed system with motorized compressor
#143THERMAL MANAGEMENT SYSTEM FOR DEICING AIRCRAFT WITH TEMPERATURE BASED FLOW RESTRICTOR
#144Deicing apparatuses comprising at least one standoff
#145Thermally biased valve and anti-icing system
#146Flow drag mitigation device
#147Thermal management system
#148Anti-icing apparatus and system
#149Passive internal ice protection systems for engine inlets
#150Gas turbine engine variable area fan nozzle with ice management
#151Metal and composite leading edge assemblies
#152Front lip of a turbofan engine nacelle comprising hot-air bores upstream from acoustic panels
#153De-icing device for a splitter nose of an axial turbine engine compressor
#154Forming a nacelle inlet for a turbine engine propulsion system
#155Compartmentalized structure for the acoustic treatment and the de-icing of an aircraft nacelle and aircraft nacelle incorporating said structure
#156Pulsed deicing system
#157Injector nozzle configuration for swirl anti-icing system
#158Synergetic noise absorption and anti-icing for aircrafts
#159Injector nozzle configuration for swirl anti-icing system
#160Synergetic noise absorption and anti-icing for aircrafts
#161Dynamic resonance system and method for the anti-icing and de-icing of inlet grids
#162De-icing splitter for an axial turbine engine compressor
#163Aircraft heating assembly with liquid cooled internal combustion engine and heating element using waste heat
#164Turbine engine with anti-ice valve assembly, bleed air valve, and method of operating
#165Splitter nose of a low-pressure compressor of an axial turbomachine with annular deicing conduit
#166Jet engine anti-icing and noise-attenuating air inlets
#167Nacelles for aircraft engines with de-icing systems using a two-phase fluid
#168Weeping ferrofluid anti-ice system
#169High temperature composite inlet
#170Acoustic controlled ice deflecting auxiliary power unit inlet system
#171Device for de-icing the inlet of a nacelle of an aircraft engine, method for producing such a de-icing device, and aircraft engine nacelle provided with such a de-icing device
#172Anti-icing system for an aircraft
#173Gas-turbine engine with oil cooler in the engine cowling
#174Anti-icing systems
#175CIRCUIT FOR DE-ICING AN AIR INLET LIP OF AN AIRCRAFT PROPULSION ASSEMBLY
#176Splitter nose with plasma de-icing for axial turbine engine compressor
#177De-icing and conditioning device for an aircraft
#178Anti-icing core inlet stator assembly for a gas turbine engine
#179Aircraft element requiring an anti-frost treatment
#180System for preventing icing on an aircraft surface using a plasma actuator
#181Nacelle equipped with an oil-cooling circuit comprising an intermediate heat exchanger
#182Electric redundant circuit
#183De-icing system with thermal management
#184Enhanced temperature control anti-ice nozzle
#185Aircraft engine anti-icing (EAI) barrier assembly, system and method
#186Helicopter engine air intake with increased bypass flow
#187ELECTRICAL HEATING ASSEMBLY FOR A DEFROSTING DEVICE
#188Anti-icing system for aircraft
#189Concentric nozzles for enhanced mixing of fluids
#190Method for regulating the de-icing of a leading edge of an aircraft and device for its implementation
#191Splitter nose with a sheet that forms a surface to guide the flow and acts as a de-icing duct
#192Systems and methods for acoustic resonance mitigation
#193Turbine engine nacelle fitted with a heat exchanger
#194System and method for cooling an aircraft wing
#195LED light unit and method of replacing an LED light unit
#196LED light unit and method of producing an LED light unit
#197Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
#198Method of manufacturing a sound absorbing panel
#199Lip unit for an electrically deiced turbojet engine nacelle
#200Heated screen for air intake of aircraft engines
#201Panel for the acoustic treatment comprising hot air ducts and at least one stabilization chamber
#202Panel for the acoustic treatment comprising hot air ducts and at least one annular channel
#203Gas turbine engine variable area fan nozzle with ice management
#204Anti-icing core inlet stator assembly for a gas turbine engine
#205Gas turbine engine mounting arrangements
#206Method and controller for detecting ice
#207Electrothermal heater mat
#208Air intake of an aircraft nacelle that incorporates a reinforced lip with a defrost system by joule-effect
#209Process for the production of an acoustic treatment panel that integrates channels juxtaposed with an alveolar structure
#210Process for the production of a panel for the acoustic treatment incorporating the frost treatment function with hot air
#211ICE SHED REDUCTION FOR LEADING EDGE STRUCTURES
#212Electrothermal heater mat
#213Flow device and method and system using the flow device
#214Aircraft nacelle air intake incorporating optimized ice-treatment hot air injection means
#215Air inlet of an aircraft nacelle including optimized frost treatment
#216Heated booster splitter plenum
#217Passive control of ice shedding
#218Method for making a network of drainage pipes and acoustic processing panel including such a network of drainage pipes
#219LEADING EDGE STRUCTURE, IN PARTICULAR FOR THE AIR INTAKE OF THE NACELLE OF AN AIRCRAFT ENGINE
#220Acoustic processing panel, more particularly adapted for an air intake in an aircraft nacelle
#221Method and system for vehicle thermal management
#222Aircraft nacelle including an optimised acoustic processing system
#223De-icing device, in particular for an aircraft nacelle
#224Engine inlet ice protection system having embedded variable watt density heaters
#225Aircraft heating system
#226Electric de-icing device and related monitoring system
#227De-icing device comprising means for detection of a leakage in a hot air supply system
#228Method for controlling an electrical deicing system
#229Turbomachine nacelle and anti-icing system and method therefor
#230Method for making a nacelle de-icing element
#231Method for making an acoustic panel for the air intake lip of a nacelle
#232Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatment
#233COUPLING FOR INDUCING HIGH TEMPERATURE DROPS BETWEEN CONNECTED PARTS ON AN AIRCRAFT
#234Method for making deicing system on a nacelle panel
#235Acoustic attenuation panel for aircraft for engine nacelle
#236Assembly of components connected by a device that maintains the integrity of the surface of one of the components
#237Aircraft de-icing device and engine nacelle of an aircraft gas turbine with de-icing device
#238Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone
#239Air inlet for an aircraft turbine engine, an aircraft provided with such an air inlet, and a method of optimizing the operation of an aircraft turbine engine with the help of an air inlet
#240Ice protection system and method
#241De-icing and/or anti-icing system for the leading edge of an aircraft wing
#242Air intake structure for an aircraft nacelle
#243Piezoelectric de-icing of an air inlet
#244AIR INTAKE LIP FOR TURBOJET NACELLE
#245Aircraft nacelle including hot air discharge means
#246Engine 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
#247Acoustic coating for an aircraft incorporating a frost treatment system by joule effect
#248Aircraft leading edge
#249Electrical power supply circuit in an aircraft for electrical equipment including a de-icing circuit
#250Aircraft propulsion assembly comprising hot air bleed systems
#251Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle
#252Aircraft nacelle guidance system installation
#253Aircraft nacelle including an optimised ice treatment system
#254Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure
#255System for defrosting the leading edge sheath of an air inlet hood for a turboengine
#256SYSTEME D'ANTI GIVRAGE ET DE DEGIVRAGE DE NACELLE DE MOTEUR D'AERONEF A TAPIS RESISTIF
#257Coating for acoustic treatment that integrates the function of hot-air treatment of frost
#258Thermal anti-icing system
#259Method and apparatus for aircraft anti-icing
#260Anti-icing system and method for preventing ice accumulation
#261Ice protection system for a multi-segment aircraft component
#262Dual valve apparatus for aircraft engine ice protection and related methods
#263STRUCTURAL ELEMENT OF AN AIRCRAFT
#264Device for protection against icing for aircraft engines and related de-icing method
#265Ice shed reduction for leading edge structures
#266Distributed zoning for engine inlet ice protection
#267Engine inlet ice protection system with power control by zone
#268Anti-icing apparatus and method for aero-engine nose cone
#269Icing protection for aircraft air inlet scoops
#270Nacelle inlet thermal anti-icing spray duct support system
#271Modular air inlet lip with electric defrosting for a turbojet pod
#272Anti-icing apparatus and method for aero-engine nose cone
#273ICING PROTECTION SYSTEM AND METHOD FOR ENHANCING HEAT TRANSFER
#274Aircraft engine protection unit (A.E.P.U)
#275Power distribution architecture for an ice protection system
#276Method of de-icing the leading edge of an aerodynamic surface and aircraft implementing such a method
#277System for deicing an air inlet cowl for a turbine engine
#278Aircraft engine nacelle inlet having access opening for electrical ice protection system
#279Aircraft engine nacelle inlet having access opening for electrical ice protection system
#280Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein
#281System for deicing the leading edge of a nose inlet cowl turbine engine
#282Ice protection system and method including a plurality of segmented sub-areas and a cyclic diverter valve
#283System for deicing an aircraft turbine engine inlet cone
#284Composite ice protection heater and method of producing same
#285Aircraft engine nacelle ice protection system
#286Device and an aircraft anti-icing system comprising such a device
#287Aircraft engine nacelle inlet having electrical ice protection system
#288Aircraft engine nacelle inlet having access opening for electrical ice protection system
#289Intake duct
#290Air intake appliance for an aircraft engine
#291Foreign object damage tolerant nacelle anti-icing system
#292Nacelle inlet lip anti-icing with engine oil
#293Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip
#294Shielded swirl gas turbine engine inlet anti-icing system
#295Ice-interference features for aircraft
#296Inlet guard screen for an inlet of an aircraft engine
#297Aircraft turboprop engine inlet compact profile configuration to improve air intake efficiency and without loss of anti-icing ability
#298Three dimensional graphene foam reinforced composite coating and deicing systems therefrom
#299Aircraft engine icing event avoidance and mitigation through real-time simulation and controls