An ice protection system for an aircraft component includes a plurality of heaters (38, 40). The aircraft component has at least two sections (32, 34) and a junction area (36). At least one of the heaters is an H-shape carbon allotrope heater (40) designed to apply heat to the junction area and prevent ice accumulation in the junction area.
HEATER DESIGN FOR CARBON ALLOTROPE ICE PROTECTION SYSTEMS
HEIZUNGSENTWURF FÜR KOHLENSTOFF-ALLOTROPE EISSCHUTZSYSTEME
CONCEPTION D'ÉLÉMENT CHAUFFANT POUR SYSTÈMES DE PROTECTION CONTRE LA GLACE À ALLOTROPE EN CARBONE
2022-09-07
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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