Skin for a deicer

Details Skin for a deicer Skin for a deicer

1996-08-06

1998-12-08

Ellis, Christopher P.

Aeronautics and astronautics

Aircraft structure

Ice prevention

244134R, B64D 1500

Patent

active

058458786

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: 2421621 (1947-06-01), Hunter et al.
patent: 2506501 (1950-05-01), Harper
patent: 4516745 (1985-05-01), Ely et al.
patent: 5449133 (1995-09-01), Ely et al.
patent: 5547150 (1996-08-01), Adams et al.

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