A method and apparatus for an ice detection system (806). The ice detection system (806) comprises a first sensor (400) located on a leading edge (412) of a vertical stabilizer (120) on an aircraft (100), a second sensor (402) located on a first side (414) of the vertical stabilizer (120), and a third sensor (404) located on a second side (416) of the vertical stabilizer (120). The first sensor (400) is configured to detect a first type of icing condition (860) for the aircraft (100). The second sensor (402) is configured to detect a second type of icing condition (860) for the aircraft (100). The third sensor (404) is configured to detect the second type of icing condition (860) for the aircraft (100).
Supercooled large drop icing condition detection system
Supergekühltes Großtropfen-Eis-Erkennungssystem
Système de détection d'état de givrage de goutte d'eau de grande taille en surfusion
2019-02-20
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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