The present disclosure relates to a hybrid multi-rotor assembly for an aerial vehicle that comprises at least two internal combustion (IC) engines 102 configured with a primary set of propellers 104, said at least two IC engines 102 installed on a vertical axis at centre of body frame 112 of the aerial vehicle, and ...

An aerial vehicle powered by a hybrid power source and capable of taking-off and landing vertically is disclosed. The aerial vehicle 100 comprises a fuselage 102, a wing frame 104 coupled with the fuselage 102, a plurality of jet engines 106 and a plurality of electric ducted fans (EDF) 108 coupled at pre-determined...