FIELD: transport.
SUBSTANCE: invention relates to space and aircraft engineering. Proposed wing comprises element arranged inside it to take up heat emitted by wing skin heated inner surface and divert it to wing sections less heated. Aforesaid element is made from electrically conducting material. It is arranged inside wing and connected via self-contained onboard power supply with wing skin.
EFFECT: higher structural reliability.
5 cl, 1 dwg
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