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.
DUAL-CHANNEL DEICING SYSTEM FOR A ROTARY WING AIRCRAFT
DOPPELKANALENTEISUNGSSYSTEM FÜR DREHFLÜGELFLUGZEUG
SYSTEME DE DEGIVRAGE A DOUBLE PASSAGE POUR AERONEF A VOILURE TOURNANTE
2017-03-08
Patent
Electronic Resource
English