ANTI-ICING AND DEICING SYSTEM FOR AIRCRAFT ENGINE POD WITH RESISTIVE MAT

摘要

The invention concerns a deicing and anti-icing system for an aircraft engine pod, comprising an air intake (2) provided with a lip (3) followed by an air intake tubular part (4), equipped with a first sound attenuating panel (5), comprising deicing means (6, 6a, 6b, 6c, 6d) consisting of at least one array of resistive heating elements embedded in an insulating material, the deicing means being in the form of a mat incorporating the resistive element in the thickness of the air intake lip.