Hybrid deicer

Aeronautics and astronautics – Aircraft structure – Ice prevention

Patent

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Details

244134D, B64D15/12

Patent

active

059043229

ABSTRACT:
A deicer comprises a skin heating means immediately subjacent an outer skin overlying an apex of a leading edge, and a skin deflection means immediately subjacent the outer skin chordwise aft of the apex. The skin heating means prevents the formation of ice over the apex and the skin deflection means deflects the outer skin to expulse ice formed chordwise aft of the apex.

REFERENCES:
patent: 5314145 (1994-05-01), Rauckhorst, III
patent: 5356096 (1994-10-01), Rauckhorst, III et al.
patent: 5547150 (1996-08-01), Adams et al.
patent: 5609314 (1997-03-01), Rauckhorst, III et al.
patent: 5657952 (1997-08-01), Goldberg

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