An aircraft which has a supporting structure which has at least one fuselage, a wing structure and at least one drive apparatus. The drive apparatus has at least one propeller and a drive motor. The aircraft has at least one energy store for providing energy for operation of the drive apparatus. The at least one drive apparatus and the at least one energy store are mechanically connected to the supporting structure and/or the wing structure of the aircraft by a securing device.
ULTRALIGHT AIRCRAFT
2016-08-18
Patent
Electronic Resource
English
TIBKAT | 1982
|Structural Design Considerations for Ultralight Aircraft
SAE Technical Papers | 1986
|An ultralight freewing aircraft design study
AIAA | 1992
|