The aircraft thrust control system comprises a central power unit and peripheral power units. The central power unit comprises upper and lower propellers arranged one above the other and adapted to rotate in opposite directions, while propellers of the peripheral power units are located outside the aerodynamic operating range of the central power unit propellers.
AIRCRAFT THRUST CONTROL SYSTEM
29.06.2023
Patent
Elektronische Ressource
Englisch
NTRS | 1988
|NTRS | 1988
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