| 摘要 |
The remote controllable, disk-shaped aircraft platform (1) has a platform housing which has multiple motor-driven, horizontally aligned rotors (5), where each rotor stands in connection with a support structure (20) by a support arm (11). The support structure receives the support arms of the rotors. The support structure is arranged centrally in the platform housing. A transport housing is received from the motor-driven rotors by the support structure in a vibration-decoupled manner. |
