A series of convertible aircraft with a core with an airframe defining a first axis is described; a first, a second, a third, a fourth, a fifth and a sixth rotor which are rotatable about respective first, second, third, fourth, fifth and sixth axis, and operable independently of each other so as to generate respectively a first, a second, a third, a fourth, a fifth and a sixth thrust value independent of each other; the core comprises first and second portions of respective half-wings and aerodynamic surfaces and each module comprises third and fourth portions of respective half-wings and aerodynamic surfaces.
SERIES OF CONVERTIBLE AIRCRAFT CAPABLE OF HOVERING AND METHOD FOR CONFIGURING A CONVERTIBLE AIRCRAFT CAPABLE OF HOVERING
2024-08-15
Patent
Electronic Resource
English
IPC: | B64U |
European Patent Office | 2023
|European Patent Office | 2022
|European Patent Office | 2022
|European Patent Office | 2023
|European Patent Office | 2023
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