| 摘要 |
The subject matter of the invention is a remote-controllable, disk-shaped aircraft platform, comprising a platform housing and at least one transport housing, the platform housing having a plurality of motor-driven, horizontally aligned rotors, each rotor being connected via a support arm to a support structure holding the support arms of the rotors, the support structure being centrally arranged in the platform housing, the support structure accommodating at least one transport housing in a vibrationally isolated manner. |
