公开(公告)号：US10752351B2

公开(公告)日：2020-08-25

申请号：US15816319

申请日：2017-11-17

Applicant: DETROIT AIRCRAFT CORPORATION

Inventor： Jon Rimanelli ,  Lai Yizhang

IPC: B64C29/00 ,  B64D47/08 ,  B64D9/00 ,  B64C25/34 ,  B64C39/02 ,  B64C37/00 ,  B64C25/40

Abstract: An unmanned air vehicle is provided. The unmanned air vehicle includes a frame having a center portion connecting two substantially parallel transversely spaced apart ele-wings. The ele-wings may store batteries and rotate along a forward axis to provide lift during a transition from vertical flight to linear flight. The landing gear may be connected to the ele-wings and configured to change pitch of the ele-wing to ensure stable flight during flight mode transition. A plurality of propellers, each having propeller drive motors, are attached to the frame and able to rotate from parallel position, relative to the center portion, for vertical flight to a perpendicular position, relative to the center portion, for linear flight. The propeller drives rotate on its axis and may be configured to propel the vehicle in a ground and flight mode.