An aircraft ice protection system (10) comprises an ice protection device (21), an onboard power source (30), a supply line (31) from the power source (30) to the device (21), a controller (41) which controls the line (31), and an optimizer (50) which conveys operation-optimizing instructions (51) to the controller (41). An ice detector (60) provides an input (70) to the optimizer (50) and this ice-condition input (70) is used to generate the operation-optimizing instructions (51).
Aircraft ice protection system with operation optimization based on ice-detection input
Eisschutzsystem für Flugzeug mit optimierter Funktion basierend auf Eiserfassungseingabe
Système de protection contre la glace pour aéronef avec optimisation d'operation sur la base d'une entrée de détection de glace
2016-08-03
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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