Skin for a deicer

Aeronautics and astronautics – Aircraft structure – Ice prevention

Patent

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Details

B64D 1500

Patent

active

055538142

ABSTRACT:
An aircraft deicing assembly 101 for attachment to an airfoil 99 includes a deflection shell 101 disposed over a deflection means 102. The deflection shell is comprised of a primary layer 116 comprised of a high strength fabric reinforced with a phenolic resin and a backing layer 115 comprised of a high strength fabric reinforced with an epoxy resin. The thickness of the backing layer is varied as a function of curvature of the airfoil and spanwise length of the airfoil.

REFERENCES:
patent: 4687691 (1987-08-01), Kay
patent: 4836474 (1989-06-01), Briscoe et al.
patent: 5098037 (1992-03-01), Leffel et al.
patent: 5129598 (1992-07-01), Adams et al.
patent: 5248116 (1993-09-01), Rauckhorst

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