A system for inductive heating of an aircraft surface includes a conductive outer layer (108) configured to be located on an outer portion (106) of the aircraft surface (104). The system further includes a carbon nanotube (CNT) yarn (110) configured to receive and conduct electrical current. The system further includes an insulator (118) 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
KOHLENSTOFFNANORÖHREN- ODER KOHLENSTOFFALLOTROP-BASIERTE INDUKTIONSHEIZUNG FÜR DEN EISSCHUTZ VON FLUGZEUGEN
CHAUFFAGE PAR INDUCTION BASÉ SUR NANOTUBE (CNT) OU ALLOTROBE À BASE DE CARBONE POUR PROTECTION ANTIGIVRE D'AÉRONEF
2023-10-04
Patent
Electronic Resource
English
Carbon nanotube (CNT) or carbon allotrobe based induction heating for aircraft ice protection
European Patent Office | 2024
|CARBON NANOTUBE (CNT) OR CARBON ALLOTROBE BASED INDUCTION HEATING FOR AIRCRAFT ICE PROTECTION
European Patent Office | 2022
|Walkway including carbon nanotube based planar heating element
European Patent Office | 2025
|Carbon Nanotube (CNT) Based Ice Protection System Applied to a Small Aircraft (AIAA 2017-3069)
British Library Conference Proceedings | 2017
|