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
18.04.2024
Patent
Elektronische Ressource
Englisch
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