DUAL-CHANNEL DEICING SYSTEM FOR A ROTARY WING AIRCRAFT
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Sep 4, 2013
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Apr 6, 2005
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Abstract
A dual primary deicing system for a rotary-wing aircraft, according to an exemplary aspect of the present disclosure includes, among other things, an electrothermal heating element system; and a controller in communication with said electrothermal heating element, said controller communicating a heating cycle to said electrothermal heating element system, said heating cycle defining a first electric pulse train associated with a main rotor blade assembly.
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