Ice protection systems (50) for aircraft (10), and methods of their manufacture, where the ice protection system includes a metallic substance (36) applied to a nonconductive substructure of the external skin portion (34) at a leading edge (30) of an aircraft, an electrical power source, and a conductor circuit (56) electrically connecting the power source across the metallic substance. In particular, the metallic substance may be applied to a nonconductive substructure on an annular inlet surface of an aircraft nacelle lip skin, and a power source can be electrically connected across the metallic substance.
AIRCRAFT ICE PROTECTION SYSTEMS
EISSCHUTZSYSTEME FÜR FLUGZEUG
SYSTÈMES DE PROTECTION CONTRE LE GIVRE POUR AÉRONEF
2023-09-06
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Raytheon aircraft protection systems
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