Deicer assembly utilizing shaped memory metals

Aeronautics and astronautics – Aircraft structure – Ice prevention

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244134E, B64D 1500

Patent

active

055583040

ABSTRACT:
An apparatus for deicing an outer shell includes an element comprised of shaped memory metal which undergoes a transformation from a weaker low temperature form (Martensite) to a stronger, high temperature form (Austenite) when the element is heated through its transformation temperature. The change in shape is utilized to deflect the outer shell to thereby shed ice accumulated thereon.

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