A deicing assembly(18) includes a pneumatic deicing apparatus (24) configured for attachment to a leading edge of an aircraft surface (12), the pneumatic deicing assembly having a plurality of inflatable chambers (30), and a carbon allotrope heater (26) having at least one sheet of a carbon allotrope material.
COMBINED ELECTRO-THERMAL AND PNEUMATIC BOOT DEICING SYSTEM
KOMBINIERTES ELEKTROTHERMISCHES UND PNEUMATISCHES GUMMIMATTEN-ENTEISUNGSSYSTEM
SYSTÈME DE DÉGIVRAGE DE CHAUSSURE PNEUMATIQUE ET ÉLECTROTHERMIQUE COMBINÉ
2022-01-26
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
COMBINED ELECTRO-THERMAL AND PNEUMATIC BOOT DEICING SYSTEM
Europäisches Patentamt | 2018
|Pneumatic boot for helicopter rotor deicing
NTRS | 1981
|Deicing System, Pneumatic Boot, Aircraft, General Specification For
SAE Technical Papers | 1997
Deicing System, Pneumatic Boot, Aircraft, General Specification for
SAE Technical Papers | 2001