CONVERTIPLANE AND ASSOCIATED FOLDING METHOD
CONVERTIPLANE AND ASSOCIATED FOLDING METHOD
- Neue Suche nach: BIANCO MENGOTTI RICCARDO
- Neue Suche nach: PIZZAGALLI MATTEO
- Neue Suche nach: CASSINELLI CARLO
- Neue Suche nach: BRUGHERA PAOLO
- Neue Suche nach: SAMPUGNARO LUCA
- Neue Suche nach: BIANCO MENGOTTI RICCARDO
- Neue Suche nach: PIZZAGALLI MATTEO
- Neue Suche nach: CASSINELLI CARLO
- Neue Suche nach: BRUGHERA PAOLO
- Neue Suche nach: SAMPUGNARO LUCA
A method is described for the folding of a convertiplane with a fuselage having a first axis , a pair of wings and a pair of rotors arranged on respective mutually opposite sides of the respective wings; each rotor comprises a mast rotatable about a second axis and a plurality of blades; each wing comprises a first portion fixed with respect to the fuselage; a second tip portion opposite to the first portion; and a third intermediate portion, which is interposed between the associated first portion and second tip portion; the mast of each rotor is integrally tiltable with the second axis and associated second tip portion about a third axis transversal to the second axis and the fuselage so as to set said convertiplane between a helicopter configuration and an aeroplane configuration; the method comprises the steps i) of arranging the convertiplane in the helicopter configuration and ii) rotating a pair of assemblies of respective wings with respect to the fuselage and the associated first portion about respective fifth axes , so as to arrange the convertiplane in a stowage configuration. A convertiplane is also disclosed.
Dokumentinformationen
CONVERTIPLANE AND ASSOCIATED FOLDING METHOD
2023-01-19
Patent
Elektronische Ressource
Englisch
| IPC: | B64C AEROPLANES , Flugzeuge |