Aircraft wheel rim with removable flange

An aircraft wheel rim having an axis of rotation that defines a radial direction extending therefrom and comprising:

• a main part (1) and an auxiliary removable part (10),
• said main part comprising a hub (2), a disc (4) extending between the hub and an annular external portion (3) intended to accept a tyre, said annular external portion being shaped to have a first flange (5) at a first end thereof and a second flange (12) at a second end thereof, said second end being shaped to accept said auxiliary removable part (10), said removable part being attached to the annular external portion after the tyre has been fitted, and
• rotation-prevention link-based structure for preventing the removable flange from rotating relative to the rim,
• wherein the rotation-prevention link-based structure comprises at least one longitudinally-shaped link (20) having a first distal end coupled to the main part and a second distal end coupled to the auxiliary removable part, the first and second distal ends of the link having centres which define a longitudinal axis which extends in a plane perpendicular to the axis of rotation of the rim while at the same time extending obliquely to make an angle (β) with respect to the radial direction.