Centrifugal fans for vertical take-off and landing (VTOL) aircraft propulsion
Abstract:
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.
Information query
Patent Agency Ranking
0/0