公开(公告)号：WO2019150206A1

公开(公告)日：2019-08-08

申请号：PCT/IB2019/050296

申请日：2019-01-15

Applicant: IDEAFORGE TECHNOLOGY PVT. LTD.

Inventor： SINGH, Rahul ,  BHAT, Ashish ,  KHETMALI, Vishal ,  MALI, Gulab

IPC: B64C27/08 ,  B64C29/00 ,  B64C39/02

Abstract: A fixed-wing VTOL hybrid UAV is disclosed comprising: a central frame 104; a pair of quick lockable fixed-wings 102 comprising right wing 102-2 and left wing 102-1 that lock with each other over the central frame; and four electrically operated rotors108 in downward facing configuration attached to fixed-wings with help of rotor-blade arms 110. Arms 110 are pivotally fixed to wings 102 so that arms 110 are movable between a working position in which arms110 are oriented parallel to central frame 104, and a storage position in which arms110 are aligned with wings 102. Central frame 104 is a thin rod and works as fuselage. Drivers and control modules are fitted in wings 102. UAV includes rudders attached to arms at 45 degrees for manoeuvring UAV for yaw and a secondary roll response. UAV includes two landing gears 106 attached to each end of central frame.