An ice protection system for an aircraft component includes a plurality of heaters. The aircraft component has at least two section and a junction area. At least one of the heaters is an H-shape carbon allotrope heater designed to apply heat to the junction area and prevent ice accumulation in the junction area.
HEATER DESIGN FOR CARBON ALLOTROPE ICE PROTECTION SYSTEMS
CONCEPTION D`UN CHAUFFAGE POUR LES SYSTEMES DE PROTECTION CONTRE LA GLACE UTILISANT L`ALLOTROPE DE CARBONE
2020-04-22
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / H05B ELECTRIC HEATING , Elektrische Heizung |
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