Anti-icing and deicing system for aircraft engine pod with...

Details Anti-icing and deicing system for aircraft engine pod with... Anti-icing and deicing system for aircraft engine pod with...

B - Operations, Transporting

64

D

B64D 15/12 (2006.01) F02C 7/047 (2006.01)

Patent

CA 2611656

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.

L'objet de l'invention est un système de dégivrage et d'anti-givrage de nacelle de moteur d'aéronef, comportant une entrée d'air (2) pourvue d'une lèvre (3) suivie d'une pièce tubulaire (4) d'entrée d'air, munie d'un premier panneau (5) d'atténuation acoustique, qui comporte des moyens de dégivrage (6, 6a, 6b, 6c, 6d) constitué par au moins un réseau d'éléments résistifs chauffants noyés dans un matériau isolant, les moyens de dégivrage étant sous forme d'un tapis incorporant les éléments résistifs dans l'épaisseur de ia lèvre d'entrée d'air.

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