Compressible nose dynamic de-icer

Aeronautics and astronautics – Aircraft structure – Ice prevention

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B64D 1518

Patent

active

053141458

ABSTRACT:
A de-icer comprises a compressible member immediately subjacent an outer skin overlying an apex of a leading edge. The compressible member facilitates deflection of the outer skin overlying the compressible member toward the substructure when the skin deflection means deflects the outer skin.

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WO81/00993 Blaser et al, Apr. 1981.

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