| 摘要 |
An aircraft fuselage interior comprises a side wall (10) that extends in a direction along the length of the fuselage and includes an upper section that slopes inwardly. In one embodiment, the side wall comprises a multiplicity of visible elongate features, such as sloping lines (34, 36), arranged along the length of the side wall (10). Each elongate feature extends from a lower portion to an upper portion and slopes relative to a notional line (24) defined by the intersection of the interior surface of the side wall (10) and a plane whose normal axis is parallel to the length of the fuselage. When viewed by a seated passenger, the sloping elongate features may cause the side wall (10) to appear to have a degree of inward sloping less than the actual degree of inward sloping. The fuselage interior may therefore appear larger than it is. |
