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
2024-04-18
Patent
Electronic Resource
English
Heater design for carbon allotrope ice protection systems
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