An apparatus including a thrust vectoring system including a centrifugal fan and a nozzle configured to output an exhaust from the centrifugal fan, wherein the thrust vectoring system is configured to controllably orient at least one of, the centrifugal fan or the nozzle, to vector a thrust generated by the exhaust.
Centrifugal fans for vertical take-off and landing (VTOL) aircraft propulsion
2022-05-17
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
CENTRIFUGAL FANS FOR VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT PROPULSION
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