METHOD OF AIRCRAFT FRONT EDGE HEAT PROTECTION

摘要

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