Deicer for aircraft

Details Deicer for aircraft Deicer for aircraft

1989-08-28

1991-12-24

Carone, Michael J.

Aeronautics and astronautics

Aircraft structure

Ice prevention

244134A, B64D 1516

Patent

active

050744976

ABSTRACT:
A deicer pad for use on the airfoil of an aircraft wherein the pad has an elastomeric flexible covering with metallic spaced strips embedded therein in side by side relationship. An electromagnetic field pulse generator is mounted within the airfoil adjacent to the strips for imparting successive pulses to the strip for movement thereof to effect de-icing.

REFERENCES:
patent: 2440240 (1948-04-01), Antonson
patent: 2690890 (1954-10-01), Weeks et al.
patent: 2757273 (1956-07-01), Taylor
patent: 2992317 (1961-07-01), Hoffman
patent: 3549964 (1970-12-01), Levin et al.
patent: 4690353 (1987-09-01), Haslim et al.
patent: 4875644 (1989-10-01), Adams et al.
patent: 4894569 (1990-01-01), Lardiere, Jr. et al.

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