72486 ⎘
De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid Hot gas application
SYSTEMS AND METHODS FOR GAS GENERATOR FOR PNEUMATIC DEICER
#2INJECTOR FOR DE-ICING DEVICE FOR AN AIR INTAKE OF AN AIRCRAFT TURBOJET NACELLE, AND ASSOCIATED METHOD
#3BLENDED WING AIRCRAFT
#4ICE PROTECTION SYSTEMS FOR AIRCRAFT FUELED BY HYDROGEN
#5COOLING OF GAS FLOWING OVER AIRCRAFT STRUCTURE
#6METHOD FOR DETECTING AN ANOMALY IN A SYSTEM OF AN AIRCRAFT
#7AIRCRAFT HAVING AN AFT ENGINE AND AUXILIARY POWER UNIT
#8ICE PROTECTION USING REGENERATIVE HIGH TEMPERATURE EXHAUST AIR
#9OPEN ROTOR AIRCRAFT PROPULSION SYSTEM WITH ANTI-ICING SYSTEM
#10DE-ICING OF AN AIRCRAFT BY MEANS OF A REFORMER FOR HYDROGEN GENERATION
#11SYSTEMS AND METHODS FOR POWER GENERATION AND AIRCRAFT COMPRISING THE SAME
#12AIRCRAFT THERMAL ANTI-ICING SYSTEM
#13HEATED LEADING-EDGE STRUCTURE FOR AN AIRCRAFT
#14MULTIFUNCTIONAL AIR SYSTEM FOR FUEL CELL POWERED AIRCRAFT
#15ICE PROTECTION SYSTEMS FOR AIRCRAFT FUELED BY HYDROGEN
#16Aircraft anti-icing protection system using blown hot air with reduced energy penalty
#17SUPPORT ARRANGEMENT FOR A LEADING-EDGE HIGH LIFT DEVICE WITH A FLUID DUCT
#18HYDROGEN-FUELLED GAS TURBINE ENGINE WITH FUEL-TO-AIR TURBOCHARGER
#19HYDROGEN ENERGY CONVERSION SYSTEM
#20MIXING DEVICE FOR A PRIMARY FLUID FLOW IN FIRST TUBE WITH AT LEAST ONE SECONDARY FLUID FLOW, A METHOD FOR MIXING AND AIRCRAFT ENGINE
#21Systems and methods for gas generator for pneumatic deicer
#22Fail safe multi-engine turboprop airframe thermo-pneumatic anti-icing systems
#23TURBINE ENGINE MODULE EQUIPPED WITH A PROPELLER AND STATOR VANES SUPPORTED BY RETAINING MEANS AND CORRESPONDING TURBINE ENGINE
#24Thermal anti-ice bypass systems for use with aircraft
#25Ice protection for electrically powered rotors
#26Control of electric pump-driven deicer
#27Gas turbine engine having hollow low-pressure shaft with integrated valve for delivering hot compressed air to a fan disk
#28Propeller deicing systems and methods
#29Piccolo tube for de-icing an airfoil structure of an aircraft, de-icing system and airfoil structure
#30Air intake of an aircraft turbine engine nacelle
#31Thermal relief doors for overheat prevention of anti-ice systems on aircraft
#32Ice protection and boundary layer suction system for an aircraft aerofoil
#33DISTRIBUTED PNEUMATIC SUPPLY SYSTEM OF AN AIRCRAFT
#34De-icing device for an air intake of an aircraft turbojet engine nacelle
#35Efficient low-noise aircraft propulsion system
#36Pressure regulating valve assembly
#37Leading-edge arrangement for an aircraft
#38Flow body for an aircraft having a solid trailing-edge component
#39AIR ACCELERATION AT LEADING EDGE OF WING
#40Air intake of an aircraft turbojet engine nacelle comprising ventilation orifices for a de-icing flow of hot air
#41Panels for obstructing air flow through apertures in an aircraft wing
#42Ice protection system for a component of an aerodynamic system
#43Apparatus and method for heating an aircraft structure
#44Thermally isolated sensor for gas turbine engine
#45Passive heater for aircraft de-icing and method
#46Aircraft anti-icing system
#47Swirl anti-icing injector head nozzle configurations
#48Variable diameter piccolo tube for anti-icing system
#49Aircraft wing ice protection system and method
#50EFFICIENT LOW-NOISE AIRCRAFT PROPULSION SYSTEM
#51ENVIRONMENTAL CONTROL SYSTEM
#52Turbofan engine, nacelle thereof, and associated method of operation
#53GAS TURBINE ENGINE, NACELLE THEREOF, AND ASSOCIATED METHOD OF OPERATING A GAS TURBINE ENGINE
#54Aircraft part anti-icing treatment method
#55Thermal anti-icing system with non-circular piccolo tube
#56Aircraft Having an Aft Engine and Auxiliary Power Unit
#57Air inlet, nacelle, propulsive assembly and aircraft with grooved lip
#58ANTI-ICE VALVE
#59LEADING EDGE MEMBER FOR AN AIRFOIL OF AN AIRCRAFT
#60Leading-edge thermal anti-ice systems and methods
#61Hybrid gas turbine engine with bleed system improvements
#62Advanced FuelCell Integration Into Aircraft
#63Defrosting and acoustic treatment device for an air intake lip of a turbojet engine nacelle
#64Aircraft propulsion system including a heat exchanger system
#65Method and apparatus for aircraft anti-icing
#66Method and apparatus for aircraft anti-icing
#67Anti-ice pulsed jet hiller reactor
#68Method and apparatus for aircraft anti-icing
#69Leading-edge device for an aircraft
#70Articulated cover assembly for wing leading edge slat telescopic tube duct
#71AIRCRAFT PROPULSION SYSTEM INCLUDING A HEAT EXCHANGER SYSTEM
#72Aerofoil leading edge structures
#73Method for manufacturing a cellular core for an acoustic panel
#74APPARATUS AND METHODS FOR PROVIDING AIR TO PNEUMATIC LOADS ONBOARD AIRCRAFT
#75Anti-ice double walled duct system
#76NACELLE INLET STRUCTURE
#77Turbomachine having an air intake de-icing system
#78Leading-edge slat for an aircraft
#79Cooling and gas dehumidifying system, transport means, and method for operating a cooling and gas dehumidifying system
#80Vented leading-edge assembly and method for manufacturing a vented leading-edge assembly
#81Control system for aircraft anti-icing
#82Self modulating valve
#83Aircraft engine nacelle comprising a system of ice protection
#84Aircraft engine nacelle comprising an anti-icing protection system
#85Nacelle inlet with reinforcement structure
#86Device For Reducing Or Even Eliminating Tonal Noise For An Aircraft Powerplant De-Icing System
#87Nozzle for an aircraft propulsion system
#88Air intake structure of an aircraft nacelle
#89Systems and methods of optimizing cooling and providing useful heating from single phase and two phase heat management in propulsion systems
#90Aircraft equipped with a structurally integrated de-icing system
#91Vane assembly for distribution of a stratified fluid in an aircraft
#92Anti-ice system exhaust air disruptor
#93Ice protection system for a component of an aerodynamic system
#94Method of regulating air pressure in anti-icing system
#95Fluid systems that prevent the formation of ice
#96METHOD OF THERMAL ICE PROTECTION FOR AN AIRCRAFT WING
#97Efficient low-noise aircraft propulsion system
#98Apparatus and method for heating an aircraft structure
#99Flying object with a sensor device including a dynamic pressure probe having an inner and outer body
#100Surface deicing device configured not to generate electromagnetic interference
#101Temperature monitoring unit for aircraft wing structure and associated installation method
#102Assembly and method for conditioning engine-heated air onboard an aircraft
#103Leading edge structure for a flow control system of an aircraft
#104Panels for obstructing air flow through apertures in an aircraft wing
#105Frost protection system for an aircraft engine nacelle
#106Aircraft anti-icing system
#107METHOD AND SYSTEM FOR PREDICTING WING ANTI-ICE FAILURE
#108Sensor with integral vortex tube for warming
#109Device for deicing a splitter nose and inlet guide vanes of an aviation turbine engine
#110Non-propulsive utility power (NPUP) generation system for providing secondary power in an aircraft
#111Eductor driven anti-ice system
#112Integrated fuel and bleed system control architecture
#113Aircraft incorporating a low-temperature bleed system
#114EXHAUST ASSEMBLY WITH VORTEX GENERATOR
#115Gas turbine engine de-icing system
#116Pulsed deicing system
#117AIR INTAKE STRUCTURE AND AIRFLOW CONTROL SYSTEM
#118Aircraft bleed system
#119DEVICE FOR DE-ICING AN AIRCRAFT TURBOJET ENGINE NACELLE AIR INTAKE LIP
#120Heat exchanger assembly for engine bleed air
#121Nacelle inner lip skin with heat transfer augmentation features
#122System for dual management of anti-icing and boundary layer suction on an aerofoil of an aircraft, including a function of collecting the anti-icing air
#123Leading edge ice-protection system
#124Direct-acting valve
#125SYSTEMS AND METHODS FOR DIAGNOSING TURBOSHAFT ENGINE BLEED VALVES
#126Electrically boosted regenerative bleed air system
#127TURBO-GENERATOR BASED BLEED AIR SYSTEM
#128Air distribution system with drag reducing inlet
#129AIRCRAFT DEICING SYSTEM
#130Icing condition detection using instantaneous humidity sensing
#131Method for detecting a fluid leak in a turbomachine and fluid distribution system
#132Anti-icing exhaust system
#133Aircraft having a redundant and efficient bleed system
#134Apparatus for obstructing air flow through an aperture for a duct in an aircraft wing
#135Nacelle anti ice system
#136Method and assembly for providing an anti-icing airflow
#137Inline pressure regulating valve assembly with inlet pressure bias
#138Dual-use air turbine system for a gas turbine engine
#139Device for de-icing a splitter nose of an aviation turbine engine
#140Directed flow nozzle swirl enhancer
#141Systems and methods for preventing ice formation on portions of an aircraft
#142Arrangements and methods for supplying heated air to a wing anti-icing system
#143Anti-icing system of aircraft, aircraft including anti-icing system, program for controlling anti-icing system, and method for controlling anti-icing system
#144Heat exchanger outlet deflector
#145Engine bleed system with multi-tap bleed array
#146ENGINE BLEED SYSTEM WITH TURBO-COMPRESSOR
#147Internally heated engine inlet screen for aircraft engines
#148Engine bleed system with motorized compressor
#149THERMAL MANAGEMENT SYSTEM FOR DEICING AIRCRAFT WITH TEMPERATURE BASED FLOW RESTRICTOR
#150Shielded anti-icing system and methods
#151TURBOCOMPRESSOR FOR AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM
#152Actuated outlet door for aircraft high-temperature exhaust
#153Anti-icing system and aircraft
#154Thermally biased valve and anti-icing system
#155Methods and apparatus to adjust bleed ports on an aircraft engine
#156Anti-icing system and aircraft
#157System for the dual management of anti-icing and boundary-layer suction on an aerofoil of an aircraft
#158Anti-icing system and aircraft
#159Nozzle and vane system for nacelle anti-icing
#160Aircraft brace housing a fluid transfer line
#161Gas turbine engine with short inlet, acoustic treatment and anti-icing features
#162Method and system for inlet guide vane heating
#163Integrated fuel cell aircraft pressurization and cooling system
#164Anti-icing apparatus and system
#165Front lip of a turbofan engine nacelle comprising hot-air bores upstream from acoustic panels
#166De-icing device for a splitter nose of an axial turbine engine compressor
#167Compartmentalized structure for the acoustic treatment and the de-icing of an aircraft nacelle and aircraft nacelle incorporating said structure
#168Pulsed deicing system
#169Injector nozzle configuration for swirl anti-icing system
#170Injector nozzle configuration for swirl anti-icing system
#171De-icing splitter for an axial turbine engine compressor
#172Electric compressor for use with a wing anti-ice system
#173Turbine engine with anti-ice valve assembly, bleed air valve, and method of operating
#174Splitter nose of a low-pressure compressor of an axial turbomachine with annular deicing conduit
#175Nacelle anti-ice system and method with equalized flow
#176Aircraft turbomachine comprising a heat exchanger of the precooler type
#177SYSTEMS AND METHODS FOR PREVENTING ICE ACCUMULATION
#178Heat exchanger for laminar-flow aircraft
#179Double-walled pipe with integrated heating capability for an aircraft or spacecraft
#180Device 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
#181Anti-icing system for an aircraft
#182Gas-turbine engine with oil cooler in the engine cowling
#183Heated valve
#184Anti-icing / de-icing system for aircraft door and aircraft door equipped with such a system
#185De-icing and conditioning device for an aircraft
#186De-icing system with thermal management
#187Enhanced temperature control anti-ice nozzle
#188Aircraft anti-icing systems having deflector vanes
#189Non-propulsive utility power (NPUP) generation system for providing full-time secondary power during operation of an aircraft
#190Anti-icing system for aircraft
#191Concentric nozzles for enhanced mixing of fluids
#192Method for regulating the de-icing of a leading edge of an aircraft and device for its implementation
#193Systems and methods for acoustic resonance mitigation
#194Turbine engine nacelle fitted with a heat exchanger
#195Thermal pneumatic deicing system for an aircraft RAM air heat exchanger
#196System and method for cooling an aircraft wing
#197NACELLE INLET THERMAL ANTI-ICE SPRAY DUCT
#198Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
#199Method of manufacturing a sound absorbing panel
#200Method and device for using hot air to de-ice the leading edges of a jet aircraft
#201Condenser ice removal for environmental control system
#202Inlet icing protection simulation system
#203Panel for the acoustic treatment comprising hot air ducts and at least one stabilization chamber
#204Aircraft energy management system including engine fan discharge air boosted environmental control system
#205Turboprop-powered aircraft with thermal system
#206Panel for the acoustic treatment comprising hot air ducts and at least one annular channel
#207Icing protection system for an aircraft and method for operating an icing protection system
#208Aircraft ice protection system and aircraft provided with the same
#209Buffer system for communicating one or more buffer supply airs throughout a gas turbine engine
#210Bleed air duct joint insulation means
#211DEICING DEVICE FOR WING LEADING EDGE OF AIRCRAFT AND AIRCRAFT MAIN WING
#212Process for the production of a panel for the acoustic treatment incorporating the frost treatment function with hot air
#213De-icing device of an aircraft gas-turbine engine
#214Flow device and method and system using the flow device
#215Air inlet of an aircraft nacelle including optimized frost treatment
#216Aircraft slat assembly with anti-icing system
#217Deicing device for propfan-type propeller blades
#218Acoustic processing panel, more particularly adapted for an air intake in an aircraft nacelle
#219Method and system for vehicle thermal management
#220Aircraft nacelle including an optimised acoustic processing system
#221De-icing device comprising means for detection of a leakage in a hot air supply system
#222Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatment
#223Assembly of components connected by a device that maintains the integrity of the surface of one of the components
#224Aircraft de-icing device and engine nacelle of an aircraft gas turbine with de-icing device
#225Attachment pylon for an aircraft turbo-shaft engine with concentric hot air channels
#226De-icing system for an aircraft
#227Aircraft nacelle including hot air discharge means
#228Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle
#229Aircraft nacelle including an optimised ice treatment system
#230Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure
#231Anti-icing piccolo tube standoff
#232Thermal anti-icing system
#233Method and apparatus for aircraft anti-icing
#234Aircraft component exposed to streaming surrounding air
#235Anti-icing apparatus for honeycomb structures
#236Dual valve apparatus for aircraft engine ice protection and related methods
#237STRUCTURAL ELEMENT OF AN AIRCRAFT
#238Device for protection against icing for aircraft engines and related de-icing method
#239Icing protection for aircraft air inlet scoops
#240ICING PROTECTION SYSTEM AND METHOD FOR ENHANCING HEAT TRANSFER
#241Method of de-icing the leading edge of an aerodynamic surface and aircraft implementing such a method
#242System for deicing an air inlet cowl for a turbine engine
#243Ice protection system and method including a plurality of segmented sub-areas and a cyclic diverter valve
#244Aircraft component exposed to streaming surrounding air
#245System for deicing an aircraft turbine engine inlet cone
#246Device and an aircraft anti-icing system comprising such a device
#247Bush and method of manufacturing a bush
#248Foreign object damage tolerant nacelle anti-icing system
#249Gas turbine engine with compartment anti-icing system
#250Thermal management system
#251Microtube heat exchanger
#252Wing leading edge architecture suitable for laminar flow