An ice detection system (122) comprising a first group of sensors (148) and a second group of sensors (170). The first group of sensors (148) is located in a first group of locations on an aircraft (100). The first group of sensors (148) in the first group of locations is configured to detect a first type of icing condition for the aircraft (100). The second group of sensors (170) is located in a second group of locations on the aircraft (100). The second group of sensors (170) in the second group of locations is configured to detect a second type of icing condition for the aircraft (100).
Supercooled large drop icing condition detection system
2016-05-26
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |