COMPONENT OF A NACELLE HAVING IMPROVED FROST PROTECTION

摘要

The invention concerns a component (2) of an aircraft nacelle formed from at least one composite structure (23) and one heating element (30) and comprising frost protection means, characterised in that the composite structure (23) has a matrix reinforced by at least a material of which the heat conductivity at ambient temperature is greater than or equal to 800 W•m-1•K-1, so as to provide transverse heat conductivity within the nacelle element (1).