SISTEMA PER CONTRASTARE LA FORMAZIONE DI GHIACCIO SU UNA SUPERFICIE OPERATIVAMENTE ESPOSTA ALL'ARIA DI UN AEROMOBILE.

摘要

A system (10, 110, 210) for preventing icing on an aircraft surface comprises a plasma actuator (12) which is to be applied onto an aircraft surface (28) operationally exposed to air and which is arranged for generating at least one plasma discharge (D) for inducing a flow (F) of ionized hot-air particles towards said surface (28).