| 摘要 |
<p>The invention relates to an aircraft fuselage comprising a front part with a cockpit, a central part and a rear part. The central part of the fuselage includes a first zone which is located at the front part and which increases in width to a maximum width towards the rear of the aircraft, a second zone that decreases in width, and a third zone which has an essentially constant width and which is located behind the second zone, width being measured along the pitch axis. The central portion having a height that is substantially constant throughout the first, second, and third zones.</p> |
