A wheel assembly is provided that includes a structure defining a wheel portion (202) configured to receive a portion of a tire. The wheel assembly further includes a structure of the wheel portion (202) defining an air channel from a face of the wheel portion (202) to an area that receives the portion of the tire, an end of the air channel proximate to the face being configured to receive a valve, where the structure is further configured to receive a corrosion mitigation device within the air channel.
CORROSION PROTECTION FOR AIRCRAFT WHEEL PNEUMATIC PORTS
KORROSIONSSCHUTZ FÜR PNEUMATISCHE FLUGZEUGRADANSCHLÜSSE
PROTECTION CONTRE LA CORROSION POUR ORIFICES PNEUMATIQUES DE ROUES D'AÉRONEF
19.06.2024
Patent
Elektronische Ressource
Englisch
CORROSION PROTECTION FOR AIRCRAFT WHEEL PNEUMATIC PORTS
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