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HYBRID HEATER FOR AIRCRAFT WING ICE PROTECTION
HYBRID HEATER FOR AIRCRAFT WING ICE PROTECTION
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机译:飞机机翼防冰混合加热器
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摘要
A hybrid heater system for aircraft wing ice protection is provided. The hybrid heater system includes a voltage source, a carbon nano-tube (CNT) heater, a first positive temperature coefficient (PTC) heater disposed in parallel with the CNT heater to form a parallel formation and a second PTC heater disposed in series between the voltage source and the parallel formation.
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