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
05.07.2018
Patent
Elektronische Ressource
Englisch
COMBINED ELECTRO-THERMAL AND PNEUMATIC BOOT DEICING SYSTEM
Europäisches Patentamt | 2022
|Pneumatic boot for helicopter rotor deicing
NTRS | 1981
|