| 摘要 |
<p>The present invention provides a rotating fuselage design providing comfort for passengers and pilot. According to an embodiment, a rotating fuselage design providing comfort for passengers wherein the rotating fuselage comprising a rotating fuselage, an internal sun and planet gear arrangement for rotation, a roller axis, a rotational axis, a partition wall between cockpit and other compartments, a partition wall between fuselage and tail and a tail and wherein said internal gear arrangement enables to remain in stationary condition during a sharp turn. Rotating fuselage is a cylindrical fuselage which has smaller diameter compared to an outer fuselage and inner fuselage remains stationary in horizontal direction without experiencing any turbulence or instability. Further, a sensor in the internal gear arrangement controls the rotation and to stabilize the fuselage after rotation. Furthermore, rollers are present in the middle of said rotating fuselage provides support and rolling motion between an inner fuselage and an outer fuselage.</p> |
