| 摘要 |
The present invention relates to retaining movable components on board an aircraft. In order to be able to transmit higher forces when retaining movable components, a retaining system (10) is provided, which comprises a support structure (12) with a first retaining area (14) and a second retaining area (16), and a movable component (18), a retaining device (20) and a locking device (22). The movable component is movably attached to the first retaining area with the retaining device, and the movable component can be locked on the second retaining area with the locking device. The locking device comprises at least one movable locking element (24) and at least one locking receptacle (26). The at least one movable locking element can be moved between an open setting (SOFF) and a locked setting (SVER), wherein the at least one movable locking element engages with the locking receptacle in the locked setting, so that the movable component is temporarily immovably retained, and allows the movable component to move in the open setting. The at least one movable locking element is situated on the second retaining area, and the at least one locking receptacle is situated on the movable component. |
