公开(公告)号：US20150183268A1

公开(公告)日：2015-07-02

申请号：US14572879

申请日：2014-12-17

Applicant: MESSIER-BUGATTI-DOWTY

Inventor： Patrick BALDASSARA ,  Xavier DELAYRE ,  Martial GALLAND

IPC: B60B23/08 ,  B60B21/10

CPC classification number: B60B23/08 ,  B60B21/104 ,  B60B25/08 ,  B60B25/12 ,  B60B25/20 ,  B60B2900/113 ,  B60B2900/1214 ,  B60B2900/212 ,  B60B2900/531 ,  B60B2900/541 ,  B60Y2200/51

Abstract: Aircraft wheel rim in two parts, one of them a main part (1) comprising a hub (2), a disc (4) extending between the hub and an annular external portion (3) intended to accept a tyre and shaped to have a flange (5) at one of its ends, the other of its ends being shaped to accept a removable part (10) forming a flange (12) which removable part is attached to the annular external portion after the tyre has been fitted, the rim comprising means for preventing the removable flange from rotating relative to the rim comprising at least one link (20) having ends the centres of which define an axis which extends in a plane perpendicular to an axis of rotation of the rim while at the same time extending obliquely to make an angle (β) with respect to a radial direction, one of the ends being coupled to the main part and the other of its ends being coupled to the removable part.

Abstract translation: 飞机轮缘分成两部分，其中之一是包括轮毂（2）的主要部分（1），在所述轮毂和环形外部部分（3）之间延伸的盘（4），所述环形外部部分（3）旨在接纳轮胎并成形为具有 凸缘（5）在其一端，其另一端被成形为接受形成凸缘（12）的可移除部分（10），该可拆卸部分在轮胎安装后附接到环形外部，轮缘 包括用于防止可移除凸缘相对于轮辋旋转的装置，包括至少一个连杆（20），所述至少一个连杆（20）的中心的中心限定了在垂直于轮辋旋转轴线的平面中延伸的轴线，同时延伸 倾斜地相对于径向方向形成一个角度（端部），其中一个端部联接到主要部分，另一个端部联接到可移除部分。