FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to an anti-icing device for one of the elements of a turbojet engine gondola. The device contains an electro-thermal anti-icing device connected to a power source (3) and thus forming a group (1) of electro-thermal anti-icing devices. The group of electro-thermal anti-icing devices includes one or more subgroups of electro-thermal anti-icing devices each one of which includes in its turn one or more electro-thermal anti-icing devices of a group where separate subgroups of electro-thermal anti-icing devices have different values of ohmic resistance.
EFFECT: simplified design and lower weight of gondola.
14 cl, 5 dwg
