Aircraft propulsion and torque mitigation technologies for aircraft are described. In embodiments, the disclosed technologies enable the provision of rotational torque for rotating the rotor blades of a vertical lift aircraft, while mitigating or even eliminating the need for counter torque methods and apparatuses such as tail rotors and counter rotating blades.
AIRCRAFT PROPULSION AND TORQUE MITIGATION TECHNOLOGIES
2021-02-11
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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