Electrical heater de-icer

Details Electrical heater de-icer Electrical heater de-icer

1993-04-06

1994-10-04

Huppert, Michael S.

Aeronautics and astronautics

Aircraft structure

Ice prevention

244134R, B64D 1500

Patent

active

053519183

ABSTRACT:
A de-icer for a structural member of an aircraft is provided. The de-icer includes first and second heaters having first and second electrically conductive strips, respectively. The first and second conductive strips are configured to form first and second marginal portions, respectively. The first and second heaters are positioned relative to each other such that the marginal portions are overlapped.

REFERENCES:
patent: 2745942 (1956-05-01), Cohen
patent: 2762897 (1956-09-01), Vrooman et al.
patent: 2992317 (1961-07-01), Hoffman
patent: 3022412 (1962-02-01), Waters
patent: 3204084 (1965-08-01), Spencer et al.
patent: 3336557 (1967-08-01), Lund et al.
patent: 4329682 (1982-05-01), Baker
patent: 4788417 (1988-11-01), Graflind
patent: 4861649 (1989-08-01), Browne
Thermal Aspects of De-Icer Design, J. R. Stallabrass, May 23, 1972.
Numerical Simulation of Two-Dimensional Heat Transfer in Composite Bodies with Application To De-icing of Aircraft Components David Fu-Kuo Chao, Nov. 19, 1983.

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