An aircraft flight surface deicing system includes an electromagnetic field generator and a deicing boot configured for attachment to an aircraft flight surface. The boot includes: one or more inflation regions including a first inflation region; one or more magnetic fluid reservoirs in fluid communication with the first inflation region, the one or more fluid reservoirs including a first fluid reservoir; a magnetic fluid contained in a combination of the first inflation regions and the one or more magnetic fluid reservoirs. In a first state, the magnetic fluid is contained in the first fluid reservoir and, in a deicing state, the electromagnetic field generator generates one or more fields that cause the magnetic fluid to exit the first fluid reservoir and travels along a length of the inflation region.
DEICING BOOT UTILIZING ELECTROMAGNETISM AND MAGNETIC FOR BOOT INFLATION
BOUDIN DE DEGIVRAGE QUI UTILISE UNE COMPOSITION ELECTROMAGNETIQUE ET MAGNETIQUE POUR LE GONFLAGE
03.02.2020
Patent
Elektronische Ressource
Englisch
Deicing boot utilizing electromagnetism and magnetic for boot inflation
Europäisches Patentamt | 2022
|DEICING BOOT UTILIZING ELECTROMAGNETISM AND MAGNETIC FOR BOOT INFLATION
Europäisches Patentamt | 2020
|DEICING BOOT UTILIZING ELECTROMAGNETISM AND MAGNETICS FOR BOOT INFLATION
Europäisches Patentamt | 2022
|Pneumatic boot for helicopter rotor deicing
NTRS | 1981
|Deicing System, Pneumatic Boot, Aircraft, General Specification for
SAE Technical Papers | 2001