Title:
HYBRID HEATER SYSTEM
Document Type and Number:
Japanese Patent JP2020040655
Kind Code:
A
Abstract:
To provide a hybrid heater system for aircraft wing ice protection.SOLUTION: A 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.SELECTED DRAWING: Figure 1
Inventors:
ROBIN JACOB
GURU PRASAD MAHAPATRA
GURU PRASAD MAHAPATRA
Application Number:
JP2019165814A
Publication Date:
March 19, 2020
Filing Date:
September 12, 2019
Export Citation:
Assignee:
GOODRICH CORP
International Classes:
B64D15/12; H05B3/14
Attorney, Agent or Firm:
Hiromichi Kobayashi
Tomioka Kiyoshi
Tomioka Kiyoshi