FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft and aerospace engineering and can be used for heat protection of aircraft front edge. Proposed method comprises applying heatproof coat onto said surface that represents a layer of composite material containing decomposing filler. In abrupt increase of heat load, aircraft front edge is vibrated in longitudinal direction with respect to ram high-temperature flow. To this end, said front edge is equipped with vibrator.
EFFECT: reliable heat protection.
3 cl, 3 dwg
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