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Empty Converging nozzle based extra air flow propulsion system(E-CAP) for multirotor UAV’s

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Empty Converging nozzle based extra air flow propulsion system(E-CAP) for multirotor UAV’s

ORDINARY APPLICATION

Published

date

Filed on 5 May 2022

Patent Information

Application ID202241026158
Date of Application05/05/2022

Documents

NameDate
202241026158-COMPLETE SPECIFICATION [05-05-2022(online)].pdf05/05/2022
202241026158-DRAWINGS [05-05-2022(online)].pdf05/05/2022
202241026158-FIGURE OF ABSTRACT [05-05-2022(online)].jpg05/05/2022
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