A heater mat assembly for a blade using an electrical current is provided including a first heating element region configured to generate a first amount of heat using the electrical current and disposed at a first region of the heater mat assembly. A second heating element region extends form the first heating element region and is configured to generate a second amount of heat using the electrical current. The second amount of heat is different than the first amount of heat.
HEATING DESIGN FOR ROTORCRAFT BLADE DE-ICING AND ANTI-ICING
2018-03-29
Patent
Electronic Resource
English
HEATING DESIGN FOR ROTORCRAFT BLADE DE-ICING AND ANTI-ICING
European Patent Office | 2016
|Emerald Group Publishing | 2008
Rotorcraft Icing - Progress and Potential
NTIS | 1986
Rotorcraft Icing Technology - An Update
NTIS | 1983
|NASA's rotorcraft icing research program
NTRS | 1988
|