Aeronautics and astronautics – Aircraft structure – Ice prevention
Patent
1986-11-19
1988-08-02
Barefoot, Galen
Aeronautics and astronautics
Aircraft structure
Ice prevention
244 53B, 60 39093, B64D 1512
Patent
active
047609788
ABSTRACT:
A plurality of electrically conductive wires is connected between two terminals and cross over each other at crossover points. Wire segments connect adjacent crossover points. All such adjacent connected crossover points have different potentials when a voltage is connected between the terminals. This forms a screen which protects an engine from damage caused by foreign objects carried into the engine intake. When a power source is connected to the terminals, the screen is heated to prevent the accretion of ice.
REFERENCES:
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patent: 2129046 (1938-09-01), Clay
patent: 2507018 (1950-05-01), Jewett et al.
patent: 3022412 (1962-02-01), Waters
patent: 3204084 (1965-08-01), Spencer, Jr. et al.
patent: 3798417 (1974-03-01), Bittner
patent: 4250703 (1981-02-01), Norris et al.
Cox, II John L.
Schuyler Martin
Barefoot Galen
Cox & Company, Inc.
Jay Mark H.
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