| 摘要 |
A folding table arrangement 200, forming part of an aircraft seat module 100, comprises a support member 231 rotatably mounted to a base structure 224, a table element 260 translatably mounted to the support member and a locking mechanism comprising first and second locking members 232, 242. The first locking member is connected to the support member to rotate with the support member between non-aligned and aligned configurations with respect to the second locking member. The first or second locking member is translatably mounted with respect to the other locking member between a first engagement position and a second engagement position wherein, when the first locking member is in the aligned configuration the first or second locking member can translate into the second engagement position. The invention also provides methods of deploying and stowing a table arrangement 200. |
