ICING CONTROL SYSTEM

Disclosed herein is a method for determining if icing has occurred on a surface of an aircraft, the method comprising: heating a surface of an air craft, after the heating has stopped, measuring the temperature of the surface as it cools, and determining if icing has occurred on the surface in depen...

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Bibliographische Detailangaben
Hauptverfasser:	BORUP, Kasper T, SØRENSEN, Kim L, JOHANSEN, Tor A
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:	Disclosed herein is a method for determining if icing has occurred on a surface of an aircraft, the method comprising: heating a surface of an air craft, after the heating has stopped, measuring the temperature of the surface as it cools, and determining if icing has occurred on the surface in dependence on the measured temperature. Advantageously, embodiments provide improved techniques for the detection of icing and the prevention, or mitigation, of icing when it has formed. Embodiments are particularly advantageous when implemented on small UAVs in civilian applications for which autonomous and energy efficient operation is particularly important.