| 摘要 |
The invention relates to an aircraft undercarriage (1), the undercarriage (1) comprising a rocker lever (2) having a first end zone (2a) for fastening to at least one point of the structure of the aircraft and a second end zone (2b) connected via a swivel (3) to twin wheels (4) comprising a wheel axle (9) connecting together two landing wheels (R1, R2), said swivel (3) presenting a first portion (3b) that is fastened to said second end zone (2b) of the rocker lever (2) and a second portion (3c) presenting freedom to swivel relative to the first portion (3b) about a swivel axis (A1, A2) of said swivel (3), said second portion (3c) being connected to said wheel axle (9) of the twin wheels (4). In addition, the connection between the second portion (3c) of said swivel (3) and said wheel axle (9) presents a hinge (6). |
