| 摘要 |
<p>An aircraft and a fuselage for an aircraft are provided. The fuselage comprises front and rear tapered double curvature skin portions (1, 2) and a central single curvature skin portion (3). Cabin doors (4, 5, 6, 7) are set into double curvature tapered portions (1, 2) of the fuselage in single curvature skin areas (19, 20, 27, 28). The single curvature skin areas are either extensions (19, 20) of the single curvature central portion (3) of the fuselage or comprise 'patches' (27, 28) of single curvature skin immediately each surrounding each door in the double curvature tapered portions (1, 2) of the fuselage.</p> |
