Supercooled large drop icing condition detection system

Supercooled large drop icing condition detection system

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 thi...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Meis, Charles Steven, Bosetti, Cris Kevin
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung: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).