A wheel assembly is provided that includes a structure defining a wheel portion configured to receive a portion of a tire. The wheel assembly further includes a structure of the wheel portion defining an air channel from a face of the wheel portion 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
20.06.2024
Patent
Elektronische Ressource
Englisch
IPC: | B60C VEHICLE TYRES , Fahrzeugreifen |
CORROSION PROTECTION FOR AIRCRAFT WHEEL PNEUMATIC PORTS
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