An aircraft wheel rim includes a main portion and a removable portion. The main portion includes a hub and a disk extending between the hub and an annular outer portion that receives a tire and is shaped to form a rim one of its sides of the annular outer portion. A second side of the annular outer portion is shaped to receive the removable portion, which forms a second flange on the second side of the annular outer portion after a tire has been put into place. The rim further includes a blocking device that limits rotation of the removable portion relative to the main portion. The blocking element include at least one key having a head engaged in a matching receptacle in the removable portion and a root engaging a steel peg that is shrink fitted in the main portion.
ROUE D'AERONEF A TALON AMOVIBLE
AN AIRCRAFT WHEEL WITH A REMOVABLE RIM FLANGE
LUFTFAHRZEUGRAD MIT ABNEHMBAREM WULST
2019-09-11
Patent
Electronic Resource
French
IPC: | B60B VEHICLE WHEELS , Räder für Fahrzeuge |