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1. (WO2018060808) AIRCRAFT EQUIPPED WITH A STRUCTURALLY INTEGRATED DE-ICING SYSTEM

Pub. No.:    WO/2018/060808    International Application No.:    PCT/IB2017/055651
Publication Date: Fri Apr 06 01:59:59 CEST 2018 International Filing Date: Wed Sep 20 01:59:59 CEST 2017
IPC: B64D 15/04
Applicants: POLITECNICO DI TORINO
Inventors: MAGGIORE, Paolo
FERRO, Carlo Giovanni
VARETTI, Sara
VITTI, Fabio
Title: AIRCRAFT EQUIPPED WITH A STRUCTURALLY INTEGRATED DE-ICING SYSTEM
Abstract:
An aircraft (A) comprising at least a component part (1, 2, 3, 4, 5, 6, 7, 8) provided with thermal de-icing means (S) suitable to eliminate and/or prevent the formation of ice on said component part, said de-icing means (S) are directly integrated in the structure of said part (1, 2, 3, 4, 5, 6, 7, 8).