139180 ⎘
Features, components parts, details or accessories, not provided for in, or of interest apart form groups - ; Air intakes for jet-propulsion plants; Air intakes for gas-turbine plants or jet-propulsion plants Heating to prevent icing
METHODS AND APPARATUS FOR ANTI-ICE HEAT SUPPLY FROM WASTE HEAT RECOVERY SYSTEMS
#2TURBINE ENGINE HAVING A VARIABLE ENGINE INTAKE SYSTEM
#3ACOUSTIC STRUCTURE WITH ARRAY OF INTERCONNECTED RESONATORS, AND ANTI-ICING SYSTEM
#4POWER SWITCHING SYSTEM OF AN ANTI-ICE SYSTEM FOR USE WITH A MAIN POWERSUPPLY AND AN AUXILIARY POWER SUPPLY
#5INJECTOR FOR DE-ICING DEVICE FOR AN AIR INTAKE OF AN AIRCRAFT TURBOJET NACELLE, AND ASSOCIATED METHOD
#6Gas Turbine Engine Inlet Anti-Ice System
#7ICE-INTERFERENCE FEATURES FOR AIRCRAFT
#8PROPELLER OF AN AIRCRAFT TURBINE ENGINE AND METHOD FOR DE-ICING SAME
#9ICE REDUCTION MECHANISM FOR TURBOFAN ENGINE
#10Engine-Integrated Heat Exchanger
#11ICE PROTECTION SYSTEMS FOR AIRCRAFT FUELED BY HYDROGEN
#12GAS TURBINE ENGINE HAVING A COMBUSTION SECTION WITH STEAM PROVIDED TO SECOND COMBSUTOR PLENUM
#13VANE HEATING SYSTEM AND METHOD
#14POWER SWITCHING SYSTEM OF AN ANTI-ICE SYSTEM FOR USE WITH A MAIN POWER SUPPLY AND AN AUXILIARY POWER SUPPLY
#15ICE REDUCTION MECHANISM FOR TURBOFAN ENGINE
#16ANTI-ICING AND BLEED HEAT SYSTEM FOR A GAS TURBINE SYSTEM
#17ANTI-ICING AND BLEED HEAT SYSTEM FOR A GAS TURBINE SYSTEM
#18SEGMENTED NACELLE INLET LIP WITH ELECTRIC ANTI-ICING SYSTEM
#19SEGMENTED NACELLE INLET LIP WITH ELECTRIC ANTI-ICING SYSTEM
#20Outer barrel support structure for nacelle inlet structure
#21Anti-ice system for gas turbine engine and inlet guide vane
#22AIR INTAKE MODULE FOR AN AIRCRAFT TURBOMACHINE AND METHOD FOR DE-ICING THEREOF
#23Piping support structure, intake duct, and gas turbine
#24AIRCRAFT AIR SYSTEM WITH DEDICATED COMPRESSOR(S)
#25AIRCRAFT PRECIPITATION MONITORING SYSTEM
#26AIR-HEATED GUIDE VANE WITH TIP HEATING
#27AIRCRAFT TURBOPROP ENGINE INLET COMPACT PROFILE CONFIGURATION
#28LIP SKIN FOR AN AIRCRAFT AEROSTRUCTURE
#29Icing condition identification for gas turbine engine
#30Heater design for carbon allotrope ice protection systems
#31THERMAL ANTI-ICING SYSTEM FOR AN AIRCRAFT PROPULSION SYSTEM
#32ICE PROTECTION SYSTEMS FOR AIRCRAFT FUELED BY HYDROGEN
#33Supersonic speed attenuator of an air intake of an aircraft propulsion assembly comprising a de-icing device and de-icing method
#34Supersonic air inlet of an aircraft propelling assembly comprising a support arm de-icing device and de-icing method
#35Method for producing electrical and/or mechanical energy for a consumer system and associated production system
#36Ice reduction mechanism for turbofan engine
#37Air inlet of a turbomachine nacelle including a circulation conduit of a hot air flow between a movable upstream part and a fixed downstream part
#38Jet pump system
#39ELECTRICAL ASSISTED ICE REDUCTION MECHANISMS FOR GAS TURBINE ENGINE OR AIRCRAFT
#40Heat transfer system for gas turbine engine
#41TURBINE ENGINE MODULE EQUIPPED WITH A PROPELLER AND STATOR VANES SUPPORTED BY RETAINING MEANS AND CORRESPONDING TURBINE ENGINE
#42Vane assembly for a gas turbine engine
#43Ice reduction mechanism for turbofan engine
#44System and method for controlling low pressure recoup air in gas turbine engine
#45Gas turbine engine having hollow low-pressure shaft with integrated valve for delivering hot compressed air to a fan disk
#46Air inlet and method for de-icing an air inlet into a nacelle of an aircraft turbojet engine
#47Valve assembly
#48Three-stream engine having a heat exchanger
#49Nacelle air intake provided with a mixed ice protection system
#50Rotor blade retention system for a gas turbine engine
#51Turbomachine comprising a system for deicing the upstream cone, and associated method
#52Inlet cone for an aircraft turbine engine and associated aircraft turbine engine
#53AIR INTAKE LIP OF AN AIRCRAFT ENGINE NACELLE, COMPRISING AT LEAST ONE INFRARED EMISSION SOURCE
#54AIR INTAKE LIP OF A TURBOMACHINE NACELLE COMPRISING AN ACOUSTIC DEVICE AND METHOD FOR PRODUCING SUCH A LIP
#55Anti-icing for gas turbine system
#56Anti-icing system with a flow-deflector assembly
#57Inlet air heating system for a gas turbine system
#58De-icing device for an air intake of an aircraft turbojet engine nacelle
#59Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air
#60Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air
#61Pressure regulating valve assembly
#62Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air
#63Additively manufactured booster splitter with integral heating passageways
#64Air intake and method for de-icing an air intake of a nacelle of an aircraft jet engine
#65Ice protection system for a component of an aerodynamic system
#66DEVICE FOR DE-ICING A TURBOMACHINE NOZZLE
#67GAS TURBINE ENGINE WITH PARTIAL INLET VANE
#68Advanced inlet design
#69Engine bleed power recovery systems and related methods
#70Swirl anti-icing injector head nozzle configurations
#71Nozzle for a thermal anti-icing system
#72Variable diameter piccolo tube for anti-icing system
#73Fan blade anti-icing concept
#74Closed loop fan inlet vane anti icing system
#75Frame for a heat engine
#76Frame for a heat engine
#77Anti-icing system having a nozzle with a deflector plate and method
#78Thermal-anti-icing system with microwave system
#79JET ENGINE AIR INLET ARRANGEMENT AND METHOD FOR MANUFACTURE THEREOF
#80Turbofan engine, nacelle thereof, and associated method of operation
#81GAS TURBINE ENGINE, NACELLE THEREOF, AND ASSOCIATED METHOD OF OPERATING A GAS TURBINE ENGINE
#82Aircraft part anti-icing treatment method
#83Thermal anti-icing system with non-circular piccolo tube
#84Fan blade anti-icing concept
#85Turbine engine comprising a heat exchanger in the secondary path
#86Anterior part of a nacelle of an aircraft propulsion assembly having a thermal transition region
#87Air inlet, nacelle, propulsive assembly and aircraft with grooved lip
#88Assembly for sealing an annular gap between an inner structure and an outer structure
#89Composite components having piezoelectric fibers
#90Anti icing method and apparatus
#91Inlet bleed heat system for use in a turbine engine
#92Gas turbine impeller nose cone
#93LIMITING SPOOL SPEEDS IN A GAS TURBINE ENGINE
#94Fan blade, engine, and structure with anti-icing and de-icing functions
#95MAGNET ANTI-ICE SYSTEM
#96Nacelle with a translatable inlet for an aircraft propulsion system
#97Defrosting and acoustic treatment device for an air intake lip of a turbojet engine nacelle
#98Inlet bulkhead with ventilation groove
#99Aircraft propulsion system including a heat exchanger system
#100METHOD FOR THE CONTROL OF THE ANTI-ICING SYSTEM OF THE AIRCRAFT GAS TURBINE ENGINE
#101Anti-icing system for gas turbine engine
#102Air inflow lip for turbojet nacelle
#103Method of shedding ice and fan blade
#104Anti-icing system for a gas turbine
#105Method and apparatus for an engine inlet for a ram-air system with an icing bypass
#106Inlet anti-ice double walled duct with supply line seal
#107Method for manufacturing a cellular core for an acoustic panel
#108DE-ICING SYSTEM
#109Aircraft systems and methods utilizing waste heat in fuel
#110Aircraft propulsion system including a heat exchanger system
#111Water and ice detection
#112Anti-ice double walled duct system
#113NACELLE INLET STRUCTURE
#114Turbomachine having an air intake de-icing system
#115Hydraulic system
#116Anti-icing system for an aircraft nacelle
#117Heater design for carbon allotrope ice protection systems
#118Self modulating valve
#119Inlet air heating systems for combined cycle power plants
#120Aircraft engine nacelle comprising a system of ice protection
#121Engine intake assembly with selector valve
#122Nacelle inlet with reinforcement structure
#123Ported shroud system for turboprop inlets
#124Nozzle for an aircraft propulsion system
#125Air intake structure of an aircraft nacelle
#126Sound-absorbing panel with a cellular core and a de-icing system
#127Using aircraft electric icing protection system for electrical power system quality
#128Aircraft propulsion assembly comprising air-liquid heat exchangers
#129Systems and methods of optimizing cooling and providing useful heating from single phase and two phase heat management in propulsion systems
#130Sweeping jet swirl nozzle
#131Anti-ice systems for engine airfoils
#132Gas turbine engine
#133Ice protection system for a component of an aerodynamic system
#134SEGREGATED ANTI-ICE DUCT CHAMBER
#135Inlet—NAI exhaust hole definition for reduced D-duct resonance noise and diluted exhaust plume for thermal control
#136Engine enclosure air inlet section
#137Method of regulating air pressure in anti-icing system
#138Aircraft anti-icing system
#139Pressure relief valve
#140Air intake system
#141SYSTEM AND METHOD TO PROMOTE EARLY AND DIFFERENTIAL ICE SHEDDING
#142Gas turbine with oil warming anti-ice circuit
#143Bleed air systems for use with aircraft and related methods
#144De-icing shroud for a compressor of turbomachine
#145Aircraft engine nacelle provided with an icing protection system and associated protection method
#146Generator air gap heater
#147Slope-based event detection for turbine engines
#148Additively manufactured booster splitter with integral heating passageways
#149Aircraft pylon comprising a coaxial heat exchanger
#150Vehicle provided, at the intake, with an air filter provided with a heating device
#151Methods, computer programs, non transitory computer readable storage mediums, signals, and apparatus for controlling electrical power supplied to a component of a vehicle
#152DE-ICING SYSTEM AND METHOD
#153Aircraft propulsion system comprising a member covered with a grooved structure
#154Gas turbine engine with mid-compressor bleed
#155Ice phobic material to reduce runback ice
#156Frost protection system for an aircraft engine nacelle
#157Control method for controlling an air intake system which supplies air to an engine of a vehicle
#158Aircraft anti-icing system
#159Air inlet lip of an aircraft engine comprising a de-icing system
#160Gas turbine engine with partial inlet vane
#161Advanced inlet design
#162INLET FRAME FOR A GAS TURBINE ENGINE
#163Acoustic honeycomb panel with integrated electrical heater
#164Sensor with integral vortex tube for warming
#165Device for deicing a splitter nose and inlet guide vanes of an aviation turbine engine
#166Ice detection
#167Inlet bleed heat system for use in a turbine engine
#168Air inlet for a nacelle for an aircraft and its process for manufacturing
#169NACELLE ANTI-ICING TROUBLESHOOTING FOR A TWO VALVE SYSTEM
#170Cooling and insulating manifold seal assembly for a propulsion system
#171Gas turbine engine de-icing system
#172Turbofan engine de-icing compressor and de-icing process
#173Heat recuperation system for the family of shaft powered aircraft gas turbine engines
#174Gas turbine system and control apparatus and method thereof
#175Turbomachine thermal management
#176Passive internal ice protection systems for engine inlets
#177Systems and methods for icing detection of compressors
#178Pulsed deicing system
#179Systems and methods for controlling overboard bleed heat of a turbine inlet filter
#180De-icing by integral electric heat generation
#181ANTI-ICING SYSTEM FOR GAS TURBINE ENGINE
#182Bonding of Turbomachinery Components
#183Aircraft bleed system
#184DEVICE FOR DE-ICING AN AIRCRAFT TURBOJET ENGINE NACELLE AIR INTAKE LIP
#185Anti-icing system for a turbine engine vane
#186Gas turbine control device and method, non-transitory storage medium, and gas turbine
#187Compressor with segmented inner shroud for an axial turbine engine
#188Air intake structure for an aircraft nacelle
#189Method and system for ice tolerant bleed takeoff
#190Nacelle inner lip skin with heat transfer augmentation features
#191COMBINED ELECTRO-THERMAL AND PNEUMATIC BOOT DEICING SYSTEM
#192Engine intake assembly with selector valve
#193Erosion strip integrated with carbon allotrope-based deicing/ anti-icing elements
#194STRUCTURE FOR PROPULSIVE AIRCRAFT ASSEMBLY, ASSOCIATED PROPULSIVE SYSTEM AND ASSEMBLY
#195Direct-acting valve
#196Turbine engine having a three-phase transformer for powering electrical deicer elements
#197Turbine engine fan module including a turbine engine inlet cone de-icing system, and a de-icing method
#198Deicing nose of an axial turbine engine compressor
#199Embedded aircraft heater repair
#200Anti-icing apparatus for a nose cone of a gas turbine engine
#201COMPRESSOR STAGE
#202Method for detecting a fluid leak in a turbomachine and fluid distribution system
#203Thermal barrier washer
#204Bleed air systems for use with aircraft and related methods
#205Anti-icing exhaust system
#206Ice protection system for gas turbine engines
#207TURBOMACHINE COMPRISING A HEAT MANAGEMENT SYSTEM
#208Annular heatshield
#209Ram air turbine cooling inlet screen heating system
#210Engine air inlet having a double-panel heated wall
#211SYSTEM OF OPERATING A GAS TURBINE ENGINE
#212Nacelle anti ice system
#213Pressure regulation valve
#214Method and assembly for providing an anti-icing airflow
#215Inline pressure regulating valve assembly with inlet pressure bias
#216Vane for turbomachinery, such as an aircraft turbojet or turbofan engine or an aircraft turboprop engine
#217Device for de-icing a splitter nose of an aviation turbine engine
#218System to determine a state of a valve
#219Directed flow nozzle swirl enhancer
#220Air circulation device for a turbomachine comprising a hot air bypass system to a heat exchanger
#221Systems and methods for preventing ice formation on portions of an aircraft
#222Short inlet with integrated liner anti-icing
#223Valved airflow passage assembly for adjusting airflow distortion in gas turbine engine
#224ENGINE BLEED SYSTEM WITH TURBO-COMPRESSOR
#225Internally heated engine inlet screen for aircraft engines
#226THERMAL MANAGEMENT SYSTEM FOR DEICING AIRCRAFT WITH TEMPERATURE BASED FLOW RESTRICTOR
#227Acoustic nozzles for inlet bleed heat systems
#228Thermally biased valve and anti-icing system
#229INLET BLEED HEAT SYSTEM AND METHOD OF ASSEMBLING THE SAME
#230Nozzle and vane system for nacelle anti-icing
#231Gas turbine engine with one piece acoustic treatment
#232Gas turbine engine with short inlet, acoustic treatment and anti-icing features
#233Method and system for inlet guide vane heating
#234Heat exchanger designs using variable geometries and configurations
#235Inlet bleed heat control system
#236Thermal management system
#237Passive internal ice protection systems for engine inlets
#238Air-inlet duct having a particle separator and an agglomerator for a gas turbine engine
#239Aircraft turbine engine air intake duct
#240Front lip of a turbofan engine nacelle comprising hot-air bores upstream from acoustic panels
#241De-icing device for a splitter nose of an axial turbine engine compressor
#242De-icing nose for low-pressure compressor of an axial turbine engine
#243Compartmentalized structure for the acoustic treatment and the de-icing of an aircraft nacelle and aircraft nacelle incorporating said structure
#244Pulsed deicing system
#245Injector nozzle configuration for swirl anti-icing system
#246Injector nozzle configuration for swirl anti-icing system
#247System and method for de-icing a gas turbine engine
#248De-icing splitter for an axial turbine engine compressor
#249Turbine engine with anti-ice valve assembly, bleed air valve, and method of operating
#250Splitter nose of a low-pressure compressor of an axial turbomachine with annular deicing conduit
#251Nacelle anti-ice system and method with equalized flow
#252Jet engine anti-icing and noise-attenuating air inlets
#253Heating System for Backup Generator
#254Dual pressure deicing system
#255Heat exchanger system for an aircraft turbomachine
#256Embedded turbofan deicer system
#257OPERATION OF A GAS TURBINE SYSTEM IN PART LOAD OPERATION
#258Nacelles for aircraft engines with de-icing systems using a two-phase fluid
#259Composite splitter lip for axial turbomachine compressor
#260Fan nacelle inlet flow control
#261De-icing splitter lip for axial turbomachine compressor
#262High temperature composite inlet
#263Thermal management system and method of circulating air in a gas turbine engine
#264Fan case ice liner for turbofan engine
#265Heavy duty gas turbine inlet system
#266Anti-icing system for an aircraft
#267Gas-turbine engine with oil cooler in the engine cowling
#268Imaging assisted gas turbine anti-icing system
#269COMPRESSION MOLDED FIBER REINFORCED FAN CASE ICE PANEL
#270Compound engine assembly with inlet lip anti-icing
#271Compound engine assembly with coaxial compressor and offset turbine section
#272Engine intake assembly with selector valve
#273Method to integrate multiple electric circuits into organic matrix composite
#274Anti-icing systems
#275Gas turbine engines with heated cases
#276Core case heating for gas turbine engines
#277Aircraft anti-icing system
#278Antifreeze system for a pipework
#279GAS TURBINE ENGINE NACELLE ANTI-ICING SYSTEM
#280System and method to manage transients for rapid power demand changes
#281Thermal management system for a gas turbine engine with an integral oil tank and heat exchanger in the nacelle
#282Ice-shedding spinner for ram air turbine
#283CIRCUIT FOR DE-ICING AN AIR INLET LIP OF AN AIRCRAFT PROPULSION ASSEMBLY
#284Splitter nose with plasma de-icing for axial turbine engine compressor
#285De-icing and conditioning device for an aircraft
#286Anti-ice splitter nose
#287Gas turbine engine with partial inlet vane
#288Anti-icing core inlet stator assembly for a gas turbine engine
#289Gas turbine engine anti-icing system
#290Device for deicing a separator nose of an aviation turbine engine
#291Gas turbine engine de-icing system
#292System for preventing icing on an aircraft surface using a plasma actuator
#293Rotating inlet cowl for a turbine engine, comprising an eccentric forward end
#294System and method for preventing objects from entering the intake of a jet engine
#295Integrated thermal management with nacelle laminar flow control for geared architecture gas turbine engine
#296De-icing by integral electric heat generation
#297NACELLE FOR AIRCRAFT, PROVIDED WITH A BUILT-IN SYSTEM FOR ANTI-ICING PROTECTION AND ACOUSTIC ABSORPTION
#298Systems and methods for utilizing gas turbine compartment ventilation discharge air
#299Environmental defense shield
#300SYSTEMS AND METHODS FOR DE-ICING INLET SCREENS AND DEHUMIDIFYING INLET AIR FILTERS FOR GAS TURBINE ENGINES