| 摘要 |
The mini-helicopter has a load carrier (12), a rotor (14) and a bearing structure (16) connecting the rotor to the load carrier. It includes a damping device (20) to damp vibrations emanating from the rotor. This damping device is at a height between that of the center of gravity and that of the rotor. The damping device may have active and passive damping elements (24.1, 24.2). |
