| 摘要 |
The invention relates to a seat (1) for an aircraft comprising a squab (2), a backrest (3), a leg rest (4), a support structure (5) for the squab (2) and the backrest (3), and a fixed rear separation shell (13). The support structure (5) or the squab (2) moveable in translation in a direction substantially perpendicular to the backrest (3) in the vertical position. The seat (1) is situated in a space lying between a fixed front separation shell (12) and a fixed rear separation shell (13). The movements of each of the components (2, 3, 4) of the seat are independent of each other and the fixed separation shells (12, 13).
|
