FIELD: aircraft engineering.
SUBSTANCE: proposed system (A) is designed to deice aircraft wing (20). Air (S2) bled from aircraft main engine (3) and air (ST) fed from air intake (31) in structure (28) and heated by aircraft heat source (26) is forced in hot air chamber (32) inside wing (2) for de-icing purposes.
EFFECT: higher de-icing efficiency.
11 cl, 9 dwg
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RU2381962C1 |
