A deicing assembly includes a pneumatic deicing apparatus configured for attachment to a leading edge of an aircraft surface, the pneumatic deicing assembly having a plurality of inflatable chambers, and a carbon allotrope heater having at least one sheet of a carbon allotrope material.
COMBINED ELECTRO-THERMAL AND PNEUMATIC BOOT DEICING SYSTEM
2018-07-05
Patent
Electronic Resource
English
COMBINED ELECTRO-THERMAL AND PNEUMATIC BOOT DEICING SYSTEM
European Patent Office | 2022
|Pneumatic boot for helicopter rotor deicing
NTRS | 1981
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