It is disclosed a distributed electric propulsion fixed-wing aircraft comprising a plurality of propulsive units, wherein propulsive units are arranged symmetrically with respect to the longitudinal plane, wherein of propulsive units comprises first propulsive units at a first side of the longitudinal plane and second propulsive units at a second side of the longitudinal plane, wherein the distributed propulsion aircraft further comprises a control unit configured to provide a yawing moment so that a sideslip angle is generated, so that the distributed electric propulsion aircraft flies as a fixed-wing aircraft equipped with a single propeller.
Distributed Electric Propulsion Aircraft Simulating a Single Propeller Aircraft
Trainelli, L.;Riboldi, C. E. D.;
2021-01-01
Abstract
It is disclosed a distributed electric propulsion fixed-wing aircraft comprising a plurality of propulsive units, wherein propulsive units are arranged symmetrically with respect to the longitudinal plane, wherein of propulsive units comprises first propulsive units at a first side of the longitudinal plane and second propulsive units at a second side of the longitudinal plane, wherein the distributed propulsion aircraft further comprises a control unit configured to provide a yawing moment so that a sideslip angle is generated, so that the distributed electric propulsion aircraft flies as a fixed-wing aircraft equipped with a single propeller.| File | Dimensione | Formato | |
|---|---|---|---|
|
WO2021224490A1_Original_document_20220616100010.pdf
accesso aperto
Descrizione: Testo della Domanda di Brevetto
:
Publisher’s version
Dimensione
7.17 MB
Formato
Adobe PDF
|
7.17 MB | Adobe PDF | Visualizza/Apri |
I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
