An aircraft wing may comprise an airfoil (206) having deicing zone, an anti-icing zone, and an ice runback control zone. An aircraft wing may comprise an electro-thermal ice protection system disposed in the aircraft wing. The electro-thermal ice protection system may be disposed along the deicing, anti-icing, and ice runback control zones of the airfoil (206) to improve aerodynamic performance of the aircraft and reduce ice formation along the wings of the aircraft.
SYSTEMS AND METHODS FOR AN ICE RUNBACK CONTROL ZONE IN AN ELECTROTHERMAL ICE PROTECTION SYSTEM
SYSTEME UND VERFAHREN FÜR EINE EISRÜCKLAUFSTEUERUNGSZONE IN EINEM ELEKTROTHERMISCHEN EISSCHUTZSYSTEM
SYSTÈMES ET PROCÉDÉS POUR UNE ZONE DE COMMANDE DE REFLUX DE GLACE DANS UN SYSTÈME DE PROTECTION CONTRE LA GLACE ÉLECTROTHERMIQUE
2024-01-03
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
SYSTEMS AND METHODS FOR AN ICE RUNBACK CONTROL ZONE IN AN ELECTROTHERMAL ICE PROTECTION SYSTEM
Europäisches Patentamt | 2023
|SYSTEMS AND METHODS FOR AN ICE RUNBACK CONTROL ZONE IN AN ELECTROTHERMAL ICE PROTECTION SYSTEM
Europäisches Patentamt | 2023
|