A system for inductive heating of an aircraft surface includes a conductive outer layer configured to be located on an outer portion of the aircraft surface. The system further includes a carbon nanotube (CNT) yarn configured to receive and conduct electrical current. The system further includes an insulator located between the conductive outer layer and the CNT yarn such that the electrical current flowing through the CNT yarn generates induction heating on the conductive outer layer.
CARBON NANOTUBE (CNT) OR CARBON ALLOTROBE BASED INDUCTION HEATING FOR AIRCRAFT ICE PROTECTION
30.06.2022
Patent
Elektronische Ressource
Englisch
CARBON NANOTUBE (CNT) OR CARBON ALLOTROBE BASED INDUCTION HEATING FOR AIRCRAFT ICE PROTECTION
Europäisches Patentamt | 2023
|Carbon nanotube (CNT) or carbon allotrobe based induction heating for aircraft ice protection
Europäisches Patentamt | 2024
|Walkway including carbon nanotube based planar heating element
Europäisches Patentamt | 2025
|HEATING ELEMENT INCLUDING CARBON NANOTUBE (CNT) LAYER
Europäisches Patentamt | 2017
|