| 摘要 |
The invention relates to a locking mechanism for a folding wing tip (12). The locking mechanism has a locked configuration, in which a first part (20) is received in a second part (30) such that the first part (20) may not be withdrawn from the second part (30) along the longitudinal axis of the locking mechanism, and an unlocked configuration, in which the first part (20) is received in the second part (30) such that the first part (20) may be withdrawn from the second part (30) along the longitudinal axis of the locking mechanism, wherein the locking mechanism is moved between the locked configuration and the unlocked configuration by rotation of at least one of the first part (20) or second part (30) around the longitudinal axis of the locking mechanism. |
