Metal clad electro-expulsive deicer with segmented elements

Aeronautics and astronautics – Aircraft structure – Ice prevention

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244134R, B64D 1500

Patent

active

055844502

ABSTRACT:
An electro-expulsive deicing system 114 for attachment to an airfoil 110 is comprised of a plurality of electro-expulsive elements 120 separated by a dielectric filler regions 122 all of which are disposed between a top dielectric layer 124 and a bottom dielectric layer 128. A contiguous top skin layer 116 covers the entire deicing apparatus 114.

REFERENCES:
patent: 4678144 (1987-07-01), Goehner et al.
patent: 4690353 (1987-09-01), Haslim et al.
patent: 4875644 (1989-10-01), Adams et al.
patent: 5098037 (1992-03-01), Leffel et al.
patent: 5143325 (1992-09-01), Zieve et al.

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