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DUAL-CHANNEL DEICING SYSTEM FOR A ROTARY WING AIRCRAFT

  • US 20140076882A1
  • Filed: 09/04/2013
  • Published: 03/20/2014
  • Est. Priority Date: 04/06/2005
  • Status: Abandoned Application
First Claim
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1. A dual primary deicing system for a rotary-wing aircraft comprising:

  • 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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