The invention provides a fixed wing aircraft electric heating ice prevention/control method comprising the following steps: dividing each slat in the leading edge into a plurality of heating zones along a spanwise direction; arranging a plurality of heating elements from the outer side to the inner side of the slat in each heating zone; controlling the plurality of heating zones to heat in cycle in sequence; controlling the heating elements in the heating zones to work in a work sequence so as to realize heating in a staggering manner, thus uniformly heating each heating zone. The control method can prevent and control ice formation, can effectively reduce system power consumption, thus improving aircraft fuel economic property.
Fixed wing aircraft electric heating ice prevention/control method
2016-02-17
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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