De-icing device, in particular for an aircraft nacelle

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 15/12 (2006.01) H05B 3/26 (2006.01)

Patent

CA 2752998

The invention relates to a de-icing device (1) in particular for an aircraft nacelle comprising at least two electric bands (5) each made from at least one main conductor (7) oriented substantially along the length of said band (5), characterised in that said bands (5) comprising rectilinear elements (13) and bent elements (17), and in that said bands (5) comprising spirals (15) formed by the association of several bent elements (17), and in that the contiguous bands (5) are embedded together at least in pairs.

Dispositif (1 ) de dégivrage notamment pour nacelle d'aéronef comprenant au moins deux rubans (5) électriques réalisés chacun à partir d'au moins un conducteur principal (7) orienté sensiblement suivant la longueur dudit ruban (5), caractérisé en ce que lesdits rubans (5) présentent des éléments rectilignes (13) et des éléments coudés (17), en ce que lesdits rubans (5) présentent des spirales (15) formés par l'association de plusieurs desdits éléments coudés (17), et en ce que les rubans (5) contigus sont imbriqués au moins deux à deux.

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